TW201812362A - Plano-convex lens, fiber matrix module and light receiving module - Google Patents
Plano-convex lens, fiber matrix module and light receiving module Download PDFInfo
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- TW201812362A TW201812362A TW106129113A TW106129113A TW201812362A TW 201812362 A TW201812362 A TW 201812362A TW 106129113 A TW106129113 A TW 106129113A TW 106129113 A TW106129113 A TW 106129113A TW 201812362 A TW201812362 A TW 201812362A
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Classifications
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- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B13/00—Optical objectives specially designed for the purposes specified below
- G02B13/18—Optical objectives specially designed for the purposes specified below with lenses having one or more non-spherical faces, e.g. for reducing geometrical aberration
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- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B17/00—Systems with reflecting surfaces, with or without refracting elements
- G02B17/08—Catadioptric systems
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
- G02B6/24—Coupling light guides
- G02B6/26—Optical coupling means
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
- G02B6/24—Coupling light guides
- G02B6/26—Optical coupling means
- G02B6/28—Optical coupling means having data bus means, i.e. plural waveguides interconnected and providing an inherently bidirectional system by mixing and splitting signals
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
- G02B6/24—Coupling light guides
- G02B6/26—Optical coupling means
- G02B6/32—Optical coupling means having lens focusing means positioned between opposed fibre ends
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- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10F—INORGANIC SEMICONDUCTOR DEVICES SENSITIVE TO INFRARED RADIATION, LIGHT, ELECTROMAGNETIC RADIATION OF SHORTER WAVELENGTH OR CORPUSCULAR RADIATION
- H10F77/00—Constructional details of devices covered by this subclass
- H10F77/40—Optical elements or arrangements
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Optical Couplings Of Light Guides (AREA)
Abstract
Description
本發明係關於一種具有非球面之平凸透鏡及具備此之光纖矩陣模組及受光模組。The present invention relates to a plano-convex lens having an aspheric surface, and an optical fiber matrix module and a light receiving module having the same.
提出有一種WDM(Wavelength Division Multiplexing:波長分割多工)傳輸用之受光模組(例如參照專利文獻1)。專利文獻1之受光模組係利用透鏡矩陣對自光纖矩陣出射之光束進行準直,且為了監視傳輸路徑中之光,而利用分束器將光束之一部分分支,並利用設置於後段之PD(Photo Detector,光偵測器)接收光。 專利文獻1之受光模組係利用分束器將經透鏡矩陣準直之光束之大部分反射至透鏡矩陣,並朝光纖矩陣返回。 [先前技術文獻] [專利文獻] [專利文獻1]日本專利特開2009-093131號公報 [專利文獻2]日本專利特開平3-131803號公報A light receiving module for WDM (Wavelength Division Multiplexing) transmission is proposed (for example, refer to Patent Document 1). The light-receiving module of Patent Document 1 uses a lens matrix to collimate a light beam emitted from the fiber matrix, and in order to monitor the light in the transmission path, a beam splitter is used to branch a part of the light beam, and a PD ( Photo Detector). The light receiving module of Patent Document 1 uses a beam splitter to reflect most of the light beam collimated by the lens matrix to the lens matrix, and returns to the fiber matrix. [Prior Art Literature] [Patent Literature] [Patent Literature 1] Japanese Patent Laid-Open No. 2009-093131 [Patent Literature 2] Japanese Patent Laid-Open No. 3-131803
[發明所欲解決之問題] 若經小型化且經透鏡矩陣準直之光束相對於透鏡直徑相對變粗,則透鏡之像差之影響變得顯著,而有局部分支為監視用後之應再次返回至光纖之光難以與光纖耦合之問題。因此,本發明之目的在於,於反射型之透鏡-光纖耦合系統中,使局部分支為監視用後之應再次返回至光纖之光與光纖效率良好地耦合。 [解決問題之技術手段] 具體而言,本發明之平凸透鏡係具備平坦面及凸面者,且 上述凸面具有第1非球面及第2非球面,該等第1非球面及第2非球面係使自端面配置於第1位置及第2位置之2條光纖之上述端面出射之光為平行光,且 於自上述第1非球面入射之平行光由形成於上述平坦面之反射面反射之情形時,上述第2非球面將該平行光聚光於上述第2位置。 具體而言,本發明之平凸透鏡係具備平坦面及凸面者,且 上述凸面具有第1非球面及第2非球面,該等第1非球面及第2非球面係使自端面配置於第1位置及第2位置之2條光纖之上述端面入射至上述平坦面之光為平行光,且以聚光於配置於與上述第1位置及上述第2位置相距預設之特定距離之反射面之一點的方式出射,且 於自上述第1非球面出射之平行光於上述一點反射之情形時,上述第2非球面將該平行光聚光於上述第2位置。 於本發明之平凸透鏡中亦可為,上述第1非球面具有第1凸面,該第1凸面係於通過上述第1位置且垂直於上述反射面之直線與上述凸面之交點、與上述凸面之中心之間具有頂點,且上述第2非球面具有第2凸面,該第2凸面係於通過上述第2位置且垂直於上述反射面之直線與上述凸面之交點、與上述凸面之中心之間具有頂點。 於該情形時,上述凸面較佳為於上述第1凸面與上述第2凸面之間,進而具備緩和上述第1凸面及上述第2凸面之邊界之形狀變化的鞍部。 於本發明之平凸透鏡中,亦可於上述反射面設置有反射部,該反射部使自上述第1非球面入射之平行光之一部分透過,且將上述平行光之一部分朝上述第2非球面反射。 具體而言,本發明之光纖矩陣模組具備: 第1透鏡矩陣,其具有本發明之複數個平凸透鏡,且上述平凸透鏡之中心軸於預設之特定平面內並排排列;及 光纖矩陣,其相對於各個上述平凸透鏡具有2條光纖,且各光纖之端面配置於各個上述平凸透鏡之上述第1位置或上述第2位置。 於本發明之光纖矩陣模組中,亦可進而具備GRIN透鏡矩陣,該GRIN透鏡矩陣具有複數個GRIN透鏡,供自上述反射面透過之各個上述平行光入射至不同之上述GRIN透鏡之一端,且將自上述GRIN透鏡之另一端出射之各光聚光於依上述GRIN透鏡之每一者所規定之點。 於本發明之光纖矩陣模組中,亦可具備: 本發明之光纖矩陣模組; 光零件,其具有將自上述反射面透過之平行光透過之複數個貫通孔,供自上述反射面透過之各個上述平行光入射至不同之上述貫通孔之一端,且將通過上述貫通孔後之平行光自各貫通孔之另一端出射;及 第2透鏡矩陣,其將自上述複數個貫通孔之上述另一端出射之各光聚光於依上述貫通孔之每一者所規定之點。 具體而言,本發明之受光模組具備本發明之光纖矩陣模組、及受光元件矩陣。 [發明之效果] 根據本發明,於反射型透鏡-光纖耦合系統中,可使局部分支為監視用後之應再次返回至光纖之光與光纖效率良好地耦合。[Problems to be Solved by the Invention] If the light beam that is miniaturized and collimated by the lens matrix is relatively thicker than the diameter of the lens, the effect of the lens aberration becomes significant, and it should be returned again after a partial branch is used for monitoring It is difficult to couple the light to the optical fiber with the optical fiber. Therefore, an object of the present invention is to efficiently couple the light which should be returned to the optical fiber again after the local branch is used for monitoring in the reflective lens-fiber coupling system. [Technical means to solve the problem] Specifically, the plano-convex lens of the present invention includes a flat surface and a convex surface, and the convex surface has a first aspheric surface and a second aspherical surface, and the first aspheric surface and the second aspherical surface system A case where the light emitted from the above-mentioned end faces of the two optical fibers whose end faces are arranged at the first position and the second position is parallel light, and the parallel light incident from the first aspheric surface is reflected by a reflecting surface formed on the flat surface At this time, the second aspheric surface condenses the parallel light at the second position. Specifically, the plano-convex lens of the present invention includes a flat surface and a convex surface, and the convex surface has a first aspherical surface and a second aspherical surface, and the first aspheric surface and the second aspherical surface are arranged from the end surface to the first The light incident from the above-mentioned end faces of the two optical fibers at the second and second positions to the flat surface is parallel light, and is focused on a reflecting surface disposed at a predetermined distance from the first position and the second position at a predetermined distance. When the parallel light emitted from the first aspheric surface is reflected at the one point, the second aspheric surface condenses the parallel light at the second position. In the plano-convex lens of the present invention, the first aspheric surface may have a first convex surface, and the first convex surface is at an intersection between the straight line passing through the first position and perpendicular to the reflective surface, and the convex surface, and the convex surface. There is a vertex between the centers, and the second aspheric surface has a second convex surface, and the second convex surface is between an intersection of a straight line passing through the second position and perpendicular to the reflective surface and the convex surface, and between the center of the convex surface vertex. In this case, it is preferable that the convex surface is provided between the first convex surface and the second convex surface, and further includes a saddle portion for reducing a change in shape of a boundary between the first convex surface and the second convex surface. In the plano-convex lens of the present invention, a reflecting portion may be provided on the reflecting surface, and the reflecting portion transmits a part of the parallel light incident from the first aspheric surface, and a part of the parallel light is directed toward the second aspheric surface. reflection. Specifically, the fiber matrix module of the present invention includes: a first lens matrix having a plurality of plano-convex lenses of the present invention, and the center axes of the plano-convex lenses are arranged side by side in a predetermined specific plane; and a fiber matrix, There are two optical fibers with respect to each of the plano-convex lenses, and an end face of each optical fiber is disposed at the first position or the second position of each of the plano-convex lenses. The optical fiber matrix module of the present invention may further include a GRIN lens matrix, the GRIN lens matrix having a plurality of GRIN lenses for each of the parallel light transmitted through the reflecting surface to enter one end of different GRIN lenses, and Each light emitted from the other end of the GRIN lens is condensed at a point specified by each of the GRIN lenses. The optical fiber matrix module of the present invention may also include: the optical fiber matrix module of the present invention; an optical component having a plurality of through holes for transmitting parallel light transmitted through the reflective surface for transmission from the reflective surface; Each of the parallel light is incident on one end of a different through-hole, and the parallel light that passes through the through-hole is emitted from the other end of each through-hole; and a second lens matrix, which will pass from the other end of the plurality of through-holes Each emitted light is condensed at a point prescribed by each of the above-mentioned through holes. Specifically, the light receiving module of the present invention includes the optical fiber matrix module of the present invention and a light receiving element matrix. [Effects of the Invention] According to the present invention, in a reflective lens-fiber coupling system, light that should be returned to the optical fiber after being partially branched for monitoring can be efficiently coupled with the optical fiber.
以下,一面參照圖式,一面對本發明之實施形態詳細地進行說明。再者,本發明並不限定於以下所示之實施形態。該等實施例僅為例示,本發明可以基於業者之知識實施各種變更、改良所得之形態實施。再者,本說明書及圖式中符號相同之構成要素表示彼此相同者。 (第1實施形態) 於圖1中表示本實施形態之光學系統。於本實施形態中,於平凸透鏡之凸面23側配置有光纖11A及11B,於平凸透鏡之平坦面21側配置有部分反射部4。光纖11A及11B之端面分別配置於第1位置P1及第2位置P2。光纖11A及11B之長度方向於特定平面PC 內與平凸透鏡之中心軸AC 平行配置。 本實施形態之平凸透鏡於凸面23具有第1非球面A1及第2非球面A2。自光纖11A之端面P1出射之光自第1非球面A1入射至平凸透鏡。第1非球面A1使自光纖11A之端面P1出射之光為平行光。利用第1非球面A1成為平行光之光透過平凸透鏡,並由配置於平坦面21之部分反射部4將一部分朝向第2非球面A2反射。第2非球面A2將經部分反射部4反射之平行光聚光至第2位置P2。藉此,經部分反射部4反射之平行光入射至光纖11B。 本實施形態之平凸透鏡由於第2非球面A2將經部分反射部4反射之平行光聚光至第2位置P2,故而可使將監視光局部分支(以下表現為經抽頭)後之光與光纖11B效率良好地耦合。 (第2實施形態) 於圖2中表示本實施形態之光纖矩陣模組之構成例。本實施形態之光纖矩陣模組具備:第1實施形態之複數個凸面23-1~23-4排列而成之透鏡矩陣2、及第1實施形態之複數個光纖11A及11B排列而成之光纖矩陣1。光纖矩陣1及透鏡矩陣2係表示將第1實施形態之4個光纖-透鏡光學系統並排配置於特定平面PC 上之例。透鏡矩陣2作為第1透鏡矩陣發揮功能。 透鏡矩陣2具有第1實施形態之複數個平凸透鏡。透鏡矩陣2所具備之各平凸透鏡具備第1實施形態之光纖-透鏡光學系統作為基本單位。各平凸透鏡之中心軸即光軸AC 並排排列於特定平面PC 內。光纖矩陣1相對於各凸面23-1~23-4具有2條光纖11A及11B。 一面參照圖3一面對圖1及圖2之光學系統進行說明。以下方向係仿照圖中之正交xyz座標軸而進行說明。於圖之左側,配置有於xz平面內與z軸平行地於x軸方向上以等間隔df 將光纖排列而成的光纖矩陣1。該光纖矩陣1係以平行於x軸且相對於y軸呈特定角度之平面為端面,例如藉由TEMPAX玻璃等之殼體保持而構成。 具有平行於z軸之光軸AC 之凸面23將垂直於光軸AC 即z軸之面設為共通平面,且於x軸方向上以光纖矩陣1之兩倍之間隔2df 矩陣化。透鏡矩陣2之凸側朝向光纖矩陣1隔著下述之特定距離之空氣層3而配置。透鏡矩陣2之厚度如圖中所示,以凸面23與對向之相反側之平坦面21之距離和凹側焦距fc 一致之方式設定。 光纖矩陣1與透鏡矩陣2之相對位置以如下方式設定:於x軸方向上,平凸透鏡之光軸AC 與光纖矩陣1之鄰接光纖彼此之中心線(於該圖中係第1光纖11A與第2光纖11B之中心線)一致,於y方向上,由透鏡光軸AC 之矩陣形成之平面與由光纖矩陣之中心線形成之平面一致,以及於z方向上,光纖矩陣1之端面與透鏡矩陣2之凸面頂點之距離與平凸透鏡之凸側焦距fv 一致。 亦可於透鏡矩陣2之平坦面21側表面施加具有使特定波長之光以所期望之比率反射/透過之功能的部分透過膜41。 於透鏡矩陣2之兩端,設置有將透鏡矩陣與光纖矩陣1之間隔保持為特定值之間隔件22。間隔件22可預先與形成相當於透鏡之凹部同時地於模具形成相當於間隔件之凹部,然後與形成透鏡同時地以模塑法形成,或者亦可為夾入特定厚度之板之形態。 且說,於此種構成中,以光線近似研究自第1光纖11A之端面出射之光之路徑。由於第1光纖11A之端面位於凸側焦點面上,故以第1光纖11A之端面為點光源而自此處出射並入射至透鏡矩陣2之對應之透鏡的光朝光軸AC 側折射,並成為與光軸AC 呈某角度之平行光線而於透鏡中行進。其中,自光纖11A及11B之端與光軸AC 即z軸平行地出射之光線即平行光之中心光線於入射至平凸透鏡後通過凹側焦點。如上所述,平凸透鏡之厚度恰好設定為凹側焦距fc ,且該部位成為平坦面,並於該部位施加有部分透過膜41,因此,該平行光之特定強度部分透過部分透過膜41並以相對於光軸AC 為之角度直進,但其餘之強度部分由部分透過膜41反射,並於相對於光軸AC 對稱之x方向位置再次到達至平凸透鏡表面。已到達至透鏡表面之反射光為通過凹側焦點之平行光,沿著與自第1光纖11A出射並入射至平凸透鏡之光路相對於光軸AC 對稱的路徑,最後聚光至位於相對於光軸AC 與第1光纖11A對稱之位置之第2光纖11B的端面P2。 此處,若將平凸透鏡之厚度設為較凹側焦距fc 薄,則反射平行光相較透鏡厚度為fc 時到達光軸AC 側之表面,於此處平行光未被收束而於第2光纖11B之端面進一步擴散。另一方面,於透鏡厚度厚於fc 之情形時,反射光進一步到達透鏡外側表面,故平行光被過度收束,結果於第2光纖11B之端面擴散。於任一情形時,反射光線之光軸均與第2光纖11B之光軸偏移。較佳為光纖11A及11B之端面與透鏡矩陣2間之距離設定為凸側焦距fv ,同時透鏡矩陣2之平坦面21為凹側焦點面。 再者,於部分透過膜41透過之光線如圖3所示,若鄰接介質之折射率與空氣層3之折射率nv 相同,則以角度ψ出射。又,雖未圖示,但若鄰接介質之折射率與透鏡矩陣2之折射率相同,則以角度出射。 且說,於欲以此種反射光學系統於光纖11A及11B之間實現低損耗之耦合的情形時,對凸面23所要求之表面形狀一般稱為非球面。非球面形狀根據光學系統之設定形態而各自不同,根據圖4說明本實施形態之非球面形狀之求出方法。於圖4中,為了便於說明,而記述為光自第2光纖11B出射,但由於光學系統相對於光軸對稱,故而此並不有損真實性。 如圖所示,設定包含光軸AC 之xz平面,並將透鏡曲面設為以z軸為對稱軸之旋轉曲面,將該xz剖面之形狀設為Z(x)。此處設為對象之光學系統成為如下模型:自於xz面內之第2象限中與z軸平行地置於與x軸相距凸側焦距fv 之地點的第2光纖11B朝上方以θ之角度出射之光線在與假定曲線Z(x)之交點折射,並以圖3中所說明之反射角度於透鏡中行進。根據折射部位之斯奈爾定律,下式成立,即, (數式1)。 此處,nv 、nc 、θv 、θc 分別係空氣層3之折射率、平凸透鏡之折射率、向透鏡表面之入射角、自透鏡表面之出射角。若將光線入射位置之曲線Z(x)之切線與x軸所成之角度設為θt ,則根據圖4中之角度關係,容易知曉有下式之關係,即, (數式2)。 根據式(1)與式(2)而下式成立。 (數式3)此處,由於角度θt 係曲線Z(x)之切線角度,故而下式成立。 [數式4]又,來自光纖11B之出射光線與光軸AC 所成之角θ之正切滿足下式,即, (數式5)。 藉由將式(4)之θt 與式(5)之θ代入式(3),可獲得與Z(x)相關之微分方程式。根據式(3)~式(5)、及由下式表示之原點(0,0)之邊界條件求出曲線,但成為複雜之非線性微分方程式而無法解析性地求解,而以近似計算求出。此時,由於有可解析性地求解之情形,故而預先基於此而確定函數形式。 [數式6]可解析性地求解之情形係於圖4中第2光纖11B之x方向位置與透鏡光軸AC 一致之情形(df /2=0)。此時,圖4中之反射角度成為零,Z(x)係解析性地求出而成為式(7)之雙曲線。 [數式7]此處,Ch 係曲率,且為下式,即, (數式8), Kh 係圓錐常數,且為下式,即, (數式9)。 於如本實施形態般光纖11A及11B自光軸AC 偏移之情形時,假定以式(7)為基本式並附加基於以下所示之多項式之近似項所得者。 [數式10]此處,n係2以上之整數,A3 、A4 、…A2n - 1 、A2n 係非球面係數。於式(10)中確定對應於目標精度之次數後,代入式(3)、式(4)、式(5)進行殘差計算,根據阻尼最小平方法求出成為整體解之曲率Ch 、圓錐常數Kh 、及非球面係數A2n - 1 、A2n 之組合即可。若指定式(10)中之係數值,則可於模具加工其表面形狀。可以式(3)~式(5)確定該應指定之係數。 即便不進行此種計算,亦可驗證其可能性。首先,於圖5左欄表示圖3及圖4所示之各參數之名稱及其記號。於圖3及圖4中,自於凸側焦點面具有端面之第1光纖11A出射並通過空氣層3入射至凸面23的光線成為與光軸AC 呈之角度之平行光。因此,對於該等光線中入射至透鏡光軸AC 與透鏡表面之交點(即透鏡之凸面23之頂點)之光線,由於透鏡表面切平面恰好垂直於與光軸AC 平行之z軸,故於光線之透鏡中心入射角ψ、出射角與折射率nv 、nc 之間,斯奈爾定律成立,即, (數式11)。 又,由於光纖矩陣1以間隔df 矩陣化且透鏡矩陣2以其兩倍之2df 矩陣化,故若給出光纖間隔df 與透鏡中心入射角ψ、及出射角度之值,則凸側、凹側各側之焦距fv 、fc 由以下之式(12)、式(13)確定。 (數式12)(數式13)於上述式(11)~式(13)中未加入近似操作而係嚴格之式,滿足該關係之以光軸AC 為對稱軸之旋轉曲面成為以旋轉雙曲面為基本之高次曲面。根據式(12)與式(13)而確定平凸透鏡之凸凹之兩個焦距fv 、fc ,即,確定光纖11A及11B與平凸透鏡之距離及透鏡厚度。 其次,對此種光學系統之限制因素進行敍述。來自第1光纖11A之出射光依據光纖之NA(Numerical Aperture,數值孔徑)擴散,但根據圖3可明確,其光束直徑BD必須使得於距離fv 處不觸及至鄰接透鏡,故下述條件必須成立,即, (數式14)。 關於凸面23之表面形狀亦有限制事項。具備凸面23之透鏡矩陣2係藉由使用模具之模塑法製作,但此時,凹面形狀研削加工之曲率半徑有限制,通常設為150 μm以上。透鏡表面形狀成為非球面,其曲率半徑於作為光軸AC 之透鏡中心最小,且隨著遠離光軸AC 而逐漸增大。因此,係於製作模塑模具時成為問題之最小曲率半徑,但由於其於透鏡中心最小,故而若對此以球面近似進行估算,則成為以下之式(15)。 [數式15]此處,為了明確起見,附記凸側焦距fv 與凹側焦距fc 於球面近似時由以下之式給出。 [數式16][數式17]且說,嘗試向該等式(11)~式(15)代入實際可能之值而計算圖3中之透鏡中心入射角ψ以下之值所得者係圖5之估算例。光纖間隔df 選擇經常使用之值即250 μm及127 μm,透鏡折射率選擇耐候性較高之硼矽酸系模塑透鏡用玻璃之折射率1.501。其次,係反射角,本實施形態考慮對以由光纖11A與第2光纖11B構成之光纖對為主光路且將部分透過膜41設為使90%以上反射而使幾%透過之所謂抽頭膜的光抽頭模組之應用,而設定於部分透過光不產生極化相依性之角度5度。 於光纖間隔df 為250 μm與127 μm之情形時,凸側焦距fv 分別成為947.3 μm與481.2 μm。此時,自光纖11A出射之光於透鏡表面之光束直徑BD分別成為小於光纖間隔df 之227.4 μm、115.5 μm,因此,該光不會觸及至鄰接透鏡。此處,作為光纖11A及11B之NA,選擇1.3/1.55 μm波段中標準之眾數徑9.0/10.0 μm之單模光纖之值即0.12。又,由於透鏡矩陣2之凸面23表面之光軸AC 上之球面近似曲率半徑係474.6 μm、241.1 μm,故充分超過模具之機械加工極限即150 μm,而可進行模塑透鏡之模具加工。 雖為部分透過膜41,但此通常係由以二氧化矽為低折射率膜材料且以二氧化鈦或五氧化鉭為高折射率膜材料之交替多層積層膜形成。作為此時之基板,由於透鏡矩陣2之與凸面23對向之平坦面21為相同之氧化物系材料,故成為良好之基板。總之,可知能夠實現圖1、圖2及圖3之構成。 (第3實施形態) 於圖6中表示本實施形態之光學系統之立體圖。本實施形態之平凸透鏡2係於第1實施形態及第2實施形態中,第1非球面A1及第2非球面A2成為凸面的雙峰型之雙峰透鏡。於第3實施形態及第4實施形態中,將第1非球面A1稱為第一凸面A1,將第2非球面A2稱為第二凸面A2。 本實施形態之平凸透鏡2係於具備平行於圖中xyz正交座標軸之邊之長方形狀之由透鏡材質構成之平坦基板上,具有包含三個曲面之凸面23。第一個係由以平行於z軸之直線R1為中心線且以與R1之交點為峰P6之旋轉曲面構成的第一凸面A1。第二個係由以平行於z軸之直線R2為中心線且以與R2之交點為峰P8之旋轉曲面構成的第二凸面A2。第二凸面A2係將第一凸面A1於x方向上平行移動峰間隔dp 所得之形狀。於圖中以R2表示第二凸面A2之旋轉中心線。該等發揮透鏡作用之兩個凸面A1、A2係透鏡直徑設定為較峰間隔dp 大,且以彼此相互重疊之方式配置。重疊部分如圖所示被削去,並於該部位以連接A1、A2兩凸面之形式設置第三個曲面即寬度ws 之鞍部A3。根據圖中之以虛線表示之等高線可知,鞍部A3亦成為自周圍平面突出且平滑地連接2個凸面A1、A2之形態。作為整體,平凸透鏡2通過由凸面A1、A2形成之兩個峰之中點,且以平行於z軸之直線Ac為透鏡中心線。以下將通過凸面A1及A2之峰且平行於x軸之直線稱為峰線Bc。 具有平行於z軸之光軸之直線狀之第一光纖11A相對於雙峰透鏡係以其光軸於與凸面A1之中心線R1相距特定距離之外側與峰線Bc相交之方式配置,來自第一光纖11A之出射光偏移入射至相對於第一透鏡凸面之峰P6更外側之交點P4。交點P4係通過第1位置P1且垂直於平坦面21之直線與凸面23之交點。入射之光之特定量強度部分以下述之機制反射,並自相對於第二透鏡凸面之峰P8更外側之交點P7聚光、入射至與第一光纖11A相對於透鏡中心線Ac對稱配置之第二光纖11B。交點P7係通過第2位置P2且垂直於平坦面21之直線與凸面23之交點。 雙峰透鏡可利用使用模具之玻璃模塑法製作。於圖7中表示模具製作步驟中之自z軸方向觀察模具所得之等高線圖。首先,如圖7所示,於模具面形成對應於第一、第二凸面A1、A2之凹面。若於邊界存在棱線,則有妨礙模塑作業中之物質移動之可能性。因此,如圖8所示,以未到達來自光纖之出射光強度分佈圖案於xy面之投影部分Pd之方式對邊界進行切削,而緩和邊界處之形狀變化。藉此,成為如圖6所示之具備鞍部A3之形狀。 其次,為了更易於理解地說明本實施形態之光學系統,而利用以包含旋轉中心線R1、R2之平面剖切所得之剖視圖即圖9進行說明。於本實施形態中,於平凸透鏡2之凸面23側配置有光纖11A及11B,於平凸透鏡2之平坦面21側配置有部分反射部4。光纖11A及11B之端面分別配置於第1位置P1及第2位置P2。光纖11A及11B之長度方向於特定平面PC 內與雙峰透鏡之中心軸AC 平行配置。以下,將該實施形態稱為類型I。 本實施形態之平凸透鏡2於凸面23具有2處凸面。第一凸面A1係以與平凸透鏡之中心軸Ac平行且包含於由光纖11A及11B形成之平面Pc之直線R1為旋轉中心的旋轉曲面,第二凸面A2亦同樣係以與平凸透鏡之中心軸Ac平行且包含於由光纖11A及11B形成之平面Pc之直線R2為旋轉中心的旋轉曲面,旋轉中心線R1、R2相對於中心軸Ac對稱,且相對於2條光纖中心線朝內側偏移特定距離。 (第4實施形態) 於圖10中表示本實施形態之光纖矩陣模組之構成例。本實施形態之光纖矩陣模組係於實施形態2之光纖矩陣模組中,對凸面23-1~23-4應用第3實施形態之平凸透鏡2。 一面參照圖11,一面對圖9及圖10中之光學系統進行說明。於圖之左側,配置有於xz平面內與z軸平行地於x軸方向上以週期間隔df 將光纖排列而成的光纖矩陣1。該光纖矩陣1係以平行於x軸且相對於y軸呈特定角度之平面為端面,例如藉由TEMPAX玻璃等之殼體保持而構成。 第一凸面A1係以包含於由光纖矩陣形成之面Pc且平行於z軸之直線R1為中心之旋轉曲面,且發揮透鏡作用。而且,相對於光纖11A之光軸,朝內側(中心軸Ac側)偏移特定距離。第二凸面A2形成為相對於透鏡中心軸Ac隔著寬度ws 之鞍部與第一凸面A1對稱之形狀。第一與第二凸面A1與A2各自之旋轉中心線R1與R2之間隔dp (以下稱為峰間隔dp )設定為小於光纖間隔df 之距離。 透鏡矩陣2之凸側朝向光纖矩陣1隔著厚度與凸側焦距fv 相等之空氣層3而配置。透鏡矩陣2之厚度如圖中所示成為雙峰凸面23與對向之相反側之平坦面21之距離,但設定為厚於凹側焦距fc 之透鏡厚度t1 。 光纖矩陣1與透鏡矩陣2之相對位置以如下方式設定,即,於x軸方向上,雙峰透鏡之中心軸AC 與光纖矩陣1之鄰接光纖彼此之中心線(於該圖中係第1光纖11A與第2光纖11B之中心線)一致,於y方向上,由透鏡中心軸AC 之矩陣形成之平面與由光纖矩陣之中心線形成之平面一致,及於z方向上,如上所述,光纖矩陣1之端面與透鏡矩陣2之凸面頂點之距離與雙峰透鏡之凸側焦距fv 一致。 於如此之構成中,以光線近似而探討自第1光纖11A之端面出射之光之路徑。由於第1光纖11A之端面位於凸側焦點面上,且如上所述雙峰凸面中之第一凸面A1之中心線R1相對於光纖中心線於x方向上偏移,故以第1光纖11A之端面為點光源而自其處出射並入射至透鏡矩陣2之第一凸面A1之光朝中心軸AC 側折射,成為與中心軸AC 呈特定角度之平行光線而於透鏡中行進。其中,自光纖11A之端與中心軸AC 即z軸平行地出射之光線即中心光線於入射至平凸透鏡後通過凹側焦點。若如上述般設定為平凸透鏡之厚度t1 厚於凹側焦距fc ,而且平坦面21位於上述中心光線與透鏡中心軸Ac 相交之點,且於該平坦面21施加有部分透過膜41,則該平行光之特定強度部分透過部分透過膜41並以相對於中心軸AC 為ψ之角度直進,但其餘之強度部分由部分透過膜41反射,於相對於中心軸AC 對稱之x方向位置到達第二凸面A2。到達第二凸面A2之反射光為通過凹側焦點之平行光,沿著與自第1光纖11A出射並入射至雙峰透鏡之光路相對於中心軸AC 對稱之路徑,最後聚光至位於相對於中心軸AC 與第1光纖11A對稱之位置之第2光纖11B的端面P2。 其次,使用數式將上述說明公式化。於圖11中,自於凸側焦點面具有端面之第1光纖11A出射並通過空氣層3而入射至凸面23之第一凸面A1之光線,成為與透鏡中心軸AC 呈之角度之平行光。對於該等光線中入射至第一凸面A1之峰(中心對稱線R1與第一凸面之交點)之光線,由於入射點之透鏡表面切平面垂直於中心軸AC ,故而於光線之峰中心入射角ψ、出射角及折射率nv 、nc 之間,斯奈爾定律成立。 (數式31)此處,nv 、nc 分別係空氣折射率、及透鏡折射率。 又,由於光纖矩陣1以週期間隔df 矩陣化,且透鏡矩陣2以其兩倍之週期2df 矩陣化,故凸側、凹側各側之焦距fv 、fc 基於光纖間隔df 、第一凸面A1與第二凸面A2之峰間隔dp 、透鏡中心入射角ψ、及出射角度之值而由以下之式(32)、式(33)確定。 (數式32)(數式33)又,關於透鏡厚度t1 亦同樣地,下式成立,即, (數式34)。 進而,凸面A1及A2之峰處之曲率半徑即峰曲率半徑Rp 由下式給出,即, (數式35)。 構成雙峰之第一、第二凸面A1、A2均滿足上述式(31)~式(35)即可,但滿足該等關係且以平行於透鏡中心軸AC 之軸為對稱軸之旋轉曲面成為以旋轉雙曲面為基本之高次曲面,一般稱為非球面。若給出光纖間隔df 、透鏡之峰間隔dp 、透鏡折射率nc 、空氣折射率nv 、及反射角,則基於式(32)與式(33)而確定雙峰透鏡之凸凹之兩個焦距fv 、fc ,即,確定光纖11A及11B與雙峰透鏡之距離、及基於式(34)而確定透鏡厚度t1 。又,根據式(35)可知成為作為透鏡製作步驟之模塑步驟中使用之模具之形狀標準之峰曲率半徑。 其次,對用以使此種光學系統成立之條件進行敍述。為了實現第一光纖11A與第二光纖11B之間之低損耗耦合,而必須極力地抑制於透鏡面之遮光。來自第1光纖11A之出射光依據光纖之NA擴散,但該擴散經常表現為以光纖端為光束腰位置之高斯光束之傳輸。自光纖端出射並到達透鏡面之高斯光束之功率分佈於光束中心至光束半徑ω之1.73倍之範圍內成為總功率之99.75%。 因此,若將至此為止之範圍設為到達透鏡表面即凸面23之光束之光束直徑BD,則其係由下式給出。 [數式36]此處,ω0 、λ分別係光纖11A之眾數半徑、及光之波長。 其次,基於透鏡之構成,根據圖12研究於透鏡表面之光束直徑BD所要求之條件。於本實施形態之雙峰透鏡中,若擴大峰間隔dp ,則如圖12(a)所示,2個透鏡凸面之重疊消除而成為2個個別凸面狀態。即,鞍部曲面A3與透鏡周圍平面成為同一面。將此稱為2片狀態,並以此與雙峰狀態之比較進行研究。 首先,根據圖12(a),對2片系統進行研究。於2片系統中,為了實現無遮光、低損耗之光纖-光纖耦合,而平行於z軸之光纖中心線與靠近該中心線側之透鏡外緣之x軸方向距離DE 必須大於透鏡表面之光纖出射光之光束直徑BD之一半,因此,以下必須成立。 (數式37)即 (數式38)此處,BD表示透鏡表面之光纖出射光之光束直徑,dp 表示凸面A1與凸面A2之峰間隔,df 表示光纖之間隔,ws 表示鞍部A3之寬度。此係2片條件。以下,將2dp -df -ws 稱為2片條件指數。若與式(38)所示之條件相反而透鏡上光束直徑BD大於2片條件指數,則為了構成無遮光之光學系統,而必須採用雙峰構成。 另一方面,於圖12(b)所示之雙峰系統中,無遮光之條件係於圖12(b)中,光纖中心線與x軸方向透鏡外緣兩端間之距離DC 、DE 均必須大於光束直徑BD之一半,因此,下式必須成立,即, (數式39)。 該條件如下所述成為包含式(38)之條件之更寬泛之條件。 此處,預先敍述有亦可不必為雙峰形狀之情形。於圖12之2例中,於透鏡表面之光束區域均跨及透鏡峰之兩側,但亦考慮如圖13(a)所示,光束區域僅分佈於透鏡峰外側之情形。該情形相當於在透鏡表面之光束直徑BD充分小而滿足式(38)及式(39)之條件且亦滿足下式的情形。 (數式40)於此種情形時,透鏡形狀無須為雙峰,而可為如圖13(b)、或圖14之等高線圖中所示之梯形狀,又,此時,模具加工亦較容易,且其耐久性亦較高。 進而還有另一個條件。其係於製作模具時與峰曲率半徑Rp 相關者。 (數式41)其理由如下。本實施形態中作為對象之平凸透鏡係藉由模塑法製作。該方法係於形成於模具之凹狀之孔壓製原料玻璃而將凹形狀轉印為玻璃之凸形狀的方法,透鏡曲面之曲率半徑依存於製作模具之工具機可實現之孔之曲率半徑,且將其設為150 μm以上。即,意味著無法形成此以下之較小之曲率半徑之深度。 其次,將上述內容表示於圖15、圖16所示之曲線圖中而對可構成類型I之光學系統之條件進行敍述。 首先,對計算時採用之數值進行說明。 光纖間隔df :作為光纖矩陣1中經常採用之光纖週期間隔,於圖15中使用配合通用250 μm間距帶狀光纖之250 μm,於圖16中使用設為上下嵌套件而矩陣化之127 μm。 波長λ:設為光通信波段之代表值即1.55 μm。 眾數半徑ω0 :設為單模光纖之波長1.55 μm下之代表值即5.2 μm。 透鏡折射率nc :用於透鏡之光學玻璃之折射率分佈於低折射率側之冕牌玻璃之1.4至高折射率側之火石玻璃之2.0。因此,此處考慮透鏡折射率nc 為1.4至2.0。 空氣折射率nv :由於透鏡外側通常為空氣,故設為1.0。 鞍部A3之寬度ws 與鄰接間隔dn :於利用玻璃模塑法製作透鏡之情形時,於模具挖出透鏡形狀之孔,於經驗上,鄰接之孔之間需要10~20 μm左右之平坦部。其理由在於:若寬度窄於此,則於鄰接之孔之間產生寬度較窄之尖銳之凸部,導致於模塑壓製步驟之高溫高壓下(1 MPa、450℃以上)變形,而有損作為模具之耐久性。因此,此處,將鞍部A3之寬度ws 、鄰接間隔dn 均設為17 μm。 反射角:設想對部分透過膜41使用光學厚度為λ/4且將低折射率透明材料與高折射率透明材料交替積層而成之介質多層膜。於構造上,傾斜地入射至該多層膜,因此,成為問題的是已透過之抽頭光之極化相依性。於使用SiO2 (折射率1.44)作為低折射率材料且使用Ta2 O5 (折射率2.12)作為高折射率材料之情形時,在理論計算上,為了將C+L波段(波長1530~1625 nm)中透過之抽頭光之極化相依性設為0.05 dB以下,而必須將反射角設為4度以下。因此,此處,亦考慮實際製作時之折射率或膜厚之變動所引起之影響而將反射角設為2度。 圖15係對於類型I之構成中光纖間隔df 為250 μm之情形,針對每一峰間隔dp 對透鏡折射率nc 與峰曲率半徑Rp 之關係進行繪圖所得的曲線圖。根據式(31)~(35),對各峰間隔而言,隨著透鏡折射率增加而光線折射能力增加,因而峰曲率半徑增大。關於峰間隔,隨著增大而光線接近峰中心,因此,為了保持相同之折射能力,而曲率半徑減小。 於該曲線圖中,應用雙峰條件、2片條件及模具加工條件者係曲線圖中之3條虛線。2片條件由式(38)規定,本發明之雙峰條件由式(39)規定,模具加工條件由式(41)規定。較根據2片條件獲得之值更下方係可構成無遮光之2片形態之光學系統之nc -Rp 區域。較根據雙峰條件獲得之值更下方係可構成無遮光之雙峰形態之光學系統之nc -Rp 區域。較根據模具加工條件獲得之值更上方成為可構成之nc -Rp 區域。可知根據雙峰條件及模具加工條件獲得之區域較根據2片條件及模具加工條件獲得之區域更廣,而設計自由度放寬至2倍以上。尤其,於雙峰條件下,可構成曲率半徑更大之條件之光學系統,此意味著模具加工之難度較低。 圖16係對於類型I之構成中光纖間隔df 為較圖15窄之127 μm之情形,針對每一峰間隔dp 對透鏡折射率nc 與峰曲率半徑Rp 之關係進行繪圖所得的曲線圖。與圖15同樣地,對各峰間隔而言,隨著透鏡折射率增加而光線折射能力增加,因而峰曲率半徑增大。關於峰間隔,隨著增大而光線接近峰中心,因此,為了保持相同之折射能力,而曲率半徑減小。 於該曲線圖中,與圖15同樣地,應用雙峰條件、2片條件及模具加工條件者係曲線圖中之3條虛線。一看便知,可實現雙峰形態之區域與2片形態相比絕對更廣。若與光纖間隔df =250 μm之情形相比,則隨著光纖間隔df 變窄而可實現之nc -Rp 區域亦變窄,可實現雙峰形態之區域成為由雙峰條件與模具加工條件之虛線包圍之三角形區域,於透鏡折射率nc 為1.44以下時無法構成。然而,於可靠性較高之硼矽酸玻璃之代表即BK7之折射率為1.501時,雖然峰間隔dp 之寬度較窄且為91.7~95.6 μm,但可構成光學系統,可知雙峰形態可應對小型化。 另一方面,至於2片條件,僅可於nc 為1.81以上而且峰間隔亦為105至107 μm之極其有限之區域實現。該高折射率區域為就可靠性之方面而言黃變之產生等成為問題之區域,不得不說實用上之應用性較低,可認為於df =127 μm時無法應用2片形態。 (第5實施形態) 於圖17中表示本實施形態之光學系統。於本實施形態中,於平凸透鏡之平坦面21側配置有光纖11A及11B,於平凸透鏡之凸面23側配置有部分反射部4。光纖11A及11B之端面分別配置於第1位置P1及第2位置P2。光纖11A及11B之長度方向於特定平面PC 內與平凸透鏡之中心軸AC 平行配置。 本實施形態之平凸透鏡於凸面23具有第1非球面A1及第2非球面A2。自光纖11A之端面出射之光自平坦面21入射至平凸透鏡。入射至平凸透鏡之光透過平凸透鏡,並自第1非球面A1出射至空氣層3中。此時,第1非球面A1使出射至空氣層3中之光為平行光。 於第1非球面A1成為平行光之光通過空氣層3中,並於部分透過膜41之反射面之一點P3使一部分朝向第2非球面A2反射。經部分反射部4反射之平行光自第2非球面A2入射至平凸透鏡。第2非球面A2將經部分反射部4反射之平行光聚光至第2位置P2。藉此,經部分反射部4反射之平行光入射至光纖11B。 本實施形態之平凸透鏡由於第2非球面A2將經部分反射部4反射之平行光聚光至第2位置P2,故而可使對監視光進行抽頭後之光與光纖11B效率良好地耦合。 (第6實施形態) 於圖18中表示本實施形態之光纖矩陣模組之構成例。本實施形態之光纖矩陣模組具備:第5實施形態之複數個凸面23-1~23-4排列而成之透鏡矩陣2、及第5實施形態之複數個光纖11A及11B排列而成之光纖矩陣1。光纖矩陣1及透鏡矩陣2係表示將第5實施形態之4個光纖-透鏡光學系統並排配置於特定平面PC 上之例。透鏡矩陣2作為第1透鏡矩陣發揮功能。 透鏡矩陣2具有第5實施形態之複數個平凸透鏡。透鏡矩陣2所具備之各平凸透鏡具備第5實施形態之光纖-透鏡光學系統作為基本單位。各平凸透鏡之中心軸即光軸AC 並排排列於特定平面PC 內。光纖矩陣1相對於各凸面23-1~23-4具有2條光纖11A及11B。 於透鏡矩陣2之兩端,設置有將透鏡矩陣與部分透過部4之間隔保持為特定值之間隔件22。間隔件22可預先與形成相當於透鏡之凹部同時地於模具形成相當於間隔件之凹部,然後與形成透鏡同時地以模塑法形成,或者亦可為夾入特定厚度之板之形態。 一面參照圖19,一面對圖17及圖18之光學系統進行說明。以下方向係仿照圖中之正交xyz座標軸而進行說明。於圖之左端,配置有於xz平面內與z軸平行地於x軸方向上以等間隔df 排列而成的光纖矩陣1。該光纖矩陣1係以平行於x軸且相對於y軸呈特定角度之平面為端面,例如藉由TEMPAX玻璃等之殼體保持而構成。 且說,於圖19中,與第1及第2實施形態之光學系統不同,於光纖1之端面,直接貼附有透鏡矩陣2之平坦面21側,且光纖矩陣1之2倍週期之凸面23側朝向平坦面21之相反側。光纖矩陣1與透鏡矩陣2之相對位置以如下方式設定,即,於x軸方向上,平凸透鏡之光軸AC 與光纖矩陣1之鄰接光纖彼此之中心線(於該圖中係第1光纖11A與第2光纖11B之中心線)一致,於y方向上,由透鏡光軸AC 之矩陣形成之平面與由光纖矩陣1之中心線形成之平面一致,及於z方向上,光纖矩陣1之端面與透鏡矩陣2之凸面頂點之距離與平凸透鏡之凹側焦距fc 一致。於圖19之右側,隔著特定間隔之空氣層3,垂直於與光軸AC 平行之z軸地設置有具有使特定波長之光以所期望之比率反射/透過之功能的部分透過膜41。於第1及第2實施形態中,部分透過膜41直接安裝於透鏡矩陣2之平坦側,但於本實施形態中,個別地安裝於與透鏡矩陣2相同折射率之玻璃基板42。 且說,於此種構成中,以光線近似研究自第1光纖11A之端面P1出射之光之路徑。由於第1光纖11A之端面P1位於凹側焦點面上,故以第1光纖11A之端面P1為點光源而自此處出射並自透鏡矩陣2之對應之凸面23出射之光線朝光軸AC 側折射,而成為與光軸AC 呈某角度之平行光線而於空氣層3中行進。其中,自光纖端P1與光軸AC 平行地出射之光線即出射光之中心光線於到達部分透過膜41時,通過對應於第1非球面A1之凸側焦點。空氣層3之厚度恰好設定為凸側焦距fv ,且該部位成為平坦面,並於該部位施加有部分透過膜41,因此,該平行光之特定強度部分透過部分透過膜41並以相對於光軸AC 為之角度直進,但其餘之強度部分由部分透過膜41反射,並於相對於光軸AC 對稱之x方向位置再次到達透鏡矩陣2之表面。已到達透鏡矩陣2之表面之反射光為通過凸側焦點之平行光,沿著與自第1光纖11A出射並自透鏡矩陣2之表面入射之光路相對於光軸AC 對稱之路徑,最後聚光至位於相對於光軸AC 與第1光纖11A對稱之位置之第2光纖11B的端面。 此處,若將空氣層3之厚度設為較凸側焦距fv 薄,則反射平行光相較空氣層3之厚度為fv 時到達光軸AC 側之表面,於此處平行光未被收束而於第2光纖11B之端面進一步擴散。另一方面,於空氣層3之厚度厚於fv 之情形時,反射光進一步到達透鏡外側表面,而平行光被過度收束,結果於第2光纖11B之端面擴散。於任一情形時,反射光線之光軸均與第2光纖11B之光軸偏移。因此,於本實施形態中重要的點是:將第1、第2光纖11A及11B之端面與平凸透鏡之凸頂點之距離設定為凹側焦距fc ,同時平凸透鏡與部分透過膜41之間隔為凸側焦距fv 。 再者,由部分透過膜41透過之光線如圖19所示,若使部分透過膜41附著之基板之折射率與透鏡矩陣2之折射率nc 相同,則雖未於圖中表示,但以角度ψ出射。又,若使部分透過膜41附著之玻璃基板42為平行基板,則最終出射至空氣層3時以角度出射。 且說,於欲以此種反射光學系統於光纖11A及11B間實現低損耗之耦合之情形時,凸面23所要求之表面形狀一般稱為非球面。非球面形狀根據光學系統之設定形態而各自不同,根據圖20說明本實施形態中之非球面形狀之求出方法。於圖20中,為了便於說明,而記述為光自第2光纖11B出射,但由於光學系統相對於光軸AC 對稱,故而此並非有損合理性者。 如圖所示,設定包含光軸AC 之xz平面,並將透鏡曲面設為以z軸為對稱軸之旋轉曲面,將該xz剖面之形狀設為Z(x)。此處設為對象之光學系統成為如下模型:自於xz面內之第3象限中與z軸平行地置於與x軸相距凹側焦距fc 之地點的第2光纖11B朝上方以θ之角度出射之光線在與假定曲線Z(x)之交點折射,並以圖20中所說明之反射角度於空氣層3中行進。 根據折射部位之斯奈爾定律而上述之式(1)成立。若將光線入射位置之曲線Z(x)之切線與x軸所成之角度設為θt ,則根據圖20中之角度關係,容易知曉有下式之關係,即, (數式18)。 根據式(1)與式(18)而下式成立。 (數式19)此處,由於角度θt 係曲線Z(x)之切線角度,故而上述式(4)成立。又,來自光纖11B之出射光線與光軸AC 所成之角θ之正切滿足下式,即, (數式20)。 藉由將式(4)之θt 與式(20)之θ代入式(19),而獲得與Z(x)相關之微分方程式。根據式(4)、式(19)~式(20)與下式之原點(0,0)之邊界條件求出曲線,即, (數式21), 但成為複雜之非線性微分方程式而無法解析性地求解,而以近似計算求出。此時,由於有可解析性地求解之情形,故而預先基於此而確定函數形式。 可解析性地求解之情形係光纖11A及11B與透鏡光軸AC 一致之情形。於光纖11A及11B與透鏡光軸AC 一致之情形時,圖20之反射角度f 成為零,Z(x)係解析性地求出而成為式(22)之橢圓。 [數式22]此處,Ce 係曲率,且為下式,即, (數式23), Ke 係圓錐常數,且為下式,即, (數式24)。 於如本實施形態般光纖11B自光軸AC 偏移之情形時,假定以式(22)為基本式並附加基於以下所示之多項式之近似項所得者。 [數式25]此處,n係2以上之整數,B3 、B4 、…B2n - 1 、B2n 係非球面係數。於式(25)中確定對應於目標精度之次數後,代入式(4)、式(19)、式(20)進行殘差計算,根據阻尼最小平方法求出成為整體解之曲率Ce 、圓錐常數Kh 、及非球面係數B2n - 1 、B2n 之組合即可。若指定式(25)中之係數值,則可於模具加工其表面形狀。可以式(4)、式(19)~式(20)確定該應指定之係數。 即便不進行此種計算,亦可驗證其可能性。首先,於圖21左欄表示圖19及圖20所示之各參數之名稱及其記號。該等與第1實施形態相關之圖5同樣,但較大之不同之處在於:透鏡矩陣2相對於光纖矩陣1之朝向反轉,隨之,反射角與透鏡中心入射角ψ之大小關係亦反轉。 於圖19及圖20中,自具有直接接著於凹側焦點面之端面之第1光纖11A出射並通過平凸透鏡自透鏡表面出射之光線成為與光軸AC 呈之角度之平行光。因此,對於該等光線中入射至透鏡光軸AC 與透鏡表面之交點之光線,由於透鏡表面切平面恰好垂直於與光軸AC 平行之z軸,故而於光線之透鏡中心入射角ψ、出射角與折射率nv 、nc 之間,斯奈爾定律成立,即, (數式26)。 又,由於光纖矩陣1以間隔df 矩陣化,且透鏡矩陣2以其兩倍之2df 矩陣化,故而若給出光纖間隔df 與透鏡中心入射角ψ、及出射角度之值,則凸側、凹側各側之焦距fv 、fc 由以下之式(27)、式(28)確定。 (數式27)(數式28)於上述式(26)~式(28)中未加入近似操作而係嚴格之式,滿足該關係之以光軸AC 為對稱軸之旋轉曲面成為以旋轉橢圓面為基本之高次曲面。根據式(27)與式(28)而確定平凸透鏡之凸凹之2個焦距fv 、fc ,即,確定光纖11A及11B與平凸透鏡之距離及平凸透鏡之厚度。 關於此種光學系統之限制因素,與上述第2實施形態同樣。嘗試向該等式(26)~式(28)代入實際可能之值,亦使用上述之式(14)、式(15)而計算圖19及圖20中之透鏡中心入射角ψ以下之值所得者係圖21之估算例。光纖間隔df 選擇250 μm與127 μm,透鏡折射率選擇耐候性較高之硼矽酸系模塑透鏡用玻璃之折射率1.501。其次,係反射角,本實施形態考慮對以由光纖11A與光纖11B構成之光纖對為主光路且將部分透過膜41設為使90%以上反射而使幾%透過之所謂抽頭膜的光抽頭模組之應用,而設定於部分透過光不產生極化相依性之角度。 於光纖間隔df 為250 μm與127 μm之情形時,凸側焦距fv 成為889.4 μm與451.8 μm。此時,自光纖11A出射之光於透鏡表面之光束直徑BD分別成為小於光纖間隔df 之214.6 μm、109.0 μm,因此,該光不會觸及至鄰接透鏡。又,由於透鏡表面之光軸AC 上之球面近似曲率半徑係445.6 μm與226.4 μm,故而充分超過模具之機械加工極限即150 μm,而可進行模塑透鏡之模具加工。總之,可知亦可實現圖17、圖18及圖19所示之構成。 此處,對圖5及圖21所示之於透鏡矩陣2表面之光纖入射出射光之光束直徑BD之限制、及用於模具加工之曲率半徑條件進行敍述。可利用模具模塑成形之氧化物玻璃之折射率以波長1.55 μm時之值計達到nc =1.426~2.068。根據式(1)~式(15)、式(26)~(28)可確認到,於(例如,住田光學玻璃:玻璃目錄資料Ver.9.01)圖5及圖21所列舉之光纖間隔df 、空氣折射率nv 、及反射角之值下,於上述透鏡折射率nc 之範圍內始終滿足該等條件。 (第7實施形態) 於圖22中表示本實施形態之光學系統。本實施形態之平凸透鏡2係於第5實施形態及第6實施形態中,第1非球面A1及第2非球面A2成為凸面的雙峰型之雙峰透鏡。於第7實施形態及第8實施形態中,將第1非球面A1稱為第一凸面A1,將第2非球面A2稱為第二凸面A2。本實施形態之凸面23之形狀及製造步驟與第3實施形態及第4實施形態相同。 (第8實施形態) 於圖23中表示本實施形態之光纖矩陣模組之構成例。本實施形態之光纖矩陣模組係於實施形態6之光纖矩陣模組中對凸面23-1~23-4應用第7實施形態之平凸透鏡2。 一面參照圖24,一面對圖22及圖23之光學系統進行說明。以下方向係仿照圖中之正交xyz座標軸而進行說明。於圖之左端,配置有於xz平面內與z軸平行地於x軸方向上以週期間隔df 將光纖排列而成的光纖矩陣1。該光纖矩陣1係以平行於x軸且相對於y軸呈特定角度之平面為端面,例如藉由TEMPAX玻璃等之殼體保持而構成。 且說,於圖24中,與第3及第4實施形態之光學系統不同,於光纖矩陣1之端面,直接貼附有雙峰透鏡矩陣2之平坦面21側,且光纖矩陣1之2倍週期之雙峰凸面23側朝向平坦面21之相反側。雙峰凸面23具有平行於z軸之透鏡中心軸AC ,且以垂直於z軸之面為共通平面,於x軸方向上以光纖矩陣1之兩倍之週期間隔2df ,且與鄰接之透鏡隔開鄰接間隔dn 而矩陣化。 雙峰凸面23由第一凸面A1與第二凸面A2構成。第一凸面A1係以包含於由光纖矩陣形成之面Pc且平行於z軸之直線R1為中心之旋轉曲面,且發揮透鏡作用。而且,相對於第一光纖11A之光軸,向內側(中心軸Ac側)偏移特定距離。第二凸面A2形成為相對於透鏡中心軸Ac隔著寬度ws之鞍部與第一凸面A1對稱之形狀。第一與第二凸面A1與A2之旋轉中心線R1與R2之間隔即峰間隔dp 設定為較光纖間隔df 小特定長度之距離。 雙峰透鏡矩陣2之凸側隔著空氣層3配置有具有垂直於z軸之部分透過膜41之部分透過部4。空氣層3之厚度如圖中所示,設定為雙峰凸面23與對向之部分透過膜41之距離厚於凸側焦距fv 之反射層厚度tr 。 光纖矩陣1與雙峰透鏡矩陣2之相對位置以如下方式設定,即,於x軸方向上,雙峰透鏡之中心軸AC 與光纖矩陣1之鄰接光纖彼此之中心線(於該圖中係第1光纖11A與第2光纖11B之中心線)一致,於y方向上,由透鏡中心軸AC 之矩陣形成之平面與由光纖矩陣1之中心線形成之平面一致,及於z方向上,光纖矩陣1之端面與雙峰透鏡矩陣2之凸面頂點之距離與平凸透鏡之凹側焦距fc 一致。於圖24之右側,隔著特定間隔之空氣層3,垂直於與中心軸AC 平行之z軸地設置有具有使特定波長之光以所期望之比率反射/透過之功能的部分透過膜41。於第3及第4實施形態中,部分透過膜41直接安裝於透鏡矩陣2之平坦側,但於本實施形態中,個別地安裝於與透鏡矩陣2相同折射率之玻璃基板42。 且說,於此種構成中,以光線近似研究自第1光纖11A之端面出射之光之路徑。由於第1光纖11A之端面位於凹側焦點面上,且如上所述雙峰凸面中之第一凸面A1之中心線R1相對於光纖中心線於x方向上偏移,故以第1光纖11A之端面P1為點光源而自其處出射並入射至透鏡矩陣2之第一凸面A1的光朝中心軸AC 側折射,成為與中心軸AC 呈特定角度之平行光線而於空氣層3中行進。其中,自光纖11A及11B之端與中心軸AC 即z軸平行地出射之光線即出射光之中心光線於自雙峰透鏡出射後通過凸側焦點。如上所述,由於設定為空氣層即反射層之厚度tr 厚於凸側焦距fv ,而且部分透過膜41位於上述中心光線與透鏡中心軸Ac 相交之點,因此,該平行光之特定強度部分透過部分透過膜41並以相對於中心軸AC 為ψ之角度直進,但其餘之強度部分由部分透過膜41反射,於相對於中心軸AC 對稱之x方向位置到達第二凸面A2。已到達第二凸面A2之反射光為通過凸側焦點之平行光,沿著與自第1光纖11A出射並入射至第一凸面A1之光路相對於中心軸AC 對稱之路徑,最後聚光至位於相對於中心軸AC 與第1光纖11A對稱之位置之第2光纖11B的端面P2。 此處,若將空氣層3之厚度設為較反射層厚度tr 薄,則反射平行光於第二凸面A2,相較於空氣層3之厚度為tr 時到達光軸AC 側之表面,於其處平行光收束不足而於第2光纖11B之端面進一步擴散。另一方面,於空氣層3之厚度厚於tr 之情形時,反射光進一步到達透鏡外側表面,而平行光被過度收束,結果於第2光纖11B之端面擴散。無論為何者之情形,反射光線之光軸均與第2光纖11B之光軸偏移。因此,於本實施形態中之重點在於:第1、第2光纖11A及11B之端面與雙峰透鏡之凸頂點之距離設定為凹側焦距fc ,並且雙峰透鏡與部分透過膜41之間隔為特定之反射層厚度tr 。 再者,由部分透過膜41透過之光線如圖24所示,若使部分透過膜41附著之基板之折射率與透鏡矩陣2之折射率nc 相同,則雖未於圖中表示,但以角度ψ出射。又,若使部分透過膜41附著之玻璃基板42為平行基板,則最終出射至空氣層3時以角度出射。 其次,使用數式將上述說明公式化。於圖24中,自於凹側焦點面具有端面之第1光纖11A出射並通過透鏡矩陣2而入射至雙峰透鏡凸面23之第一凸面A1的光線成為與透鏡中心軸AC 呈之角度之平行光。對於該等光線中入射至第一凸面A1之峰(中心對稱線R1與第一凸面之交點)之光線,由於入射點之透鏡表面切平面垂直於中心軸AC ,故而於光線之峰中心入射角ψ、出射角及折射率nv 、nc 之間,斯奈爾定律成立,即, (數式42)。 又,由於光纖矩陣1以間隔df 矩陣化,且透鏡矩陣2以其兩倍之2df 矩陣化,故而凹側、凸側各側之焦距fc 、fv 根據光纖間隔df 、第一凸面A1與第二凸面A2之峰間隔dp 、透鏡中心入射角ψ、及出射角度之值而由以下之式(43)、式(44)確定。 (數式43)(數式44)又,關於反射層厚度tr 亦同樣,下式成立,即, (數式45)。 構成雙峰之第一、第二凸面A1、A2均滿足上述式(42)~式(45)即可,但滿足該等關係且以平行於透鏡中心軸AC 之軸為對稱軸之旋轉曲面成為以旋轉橢圓面為基本之高次曲面,一般稱為非球面。若給出光纖間隔df 、透鏡峰間隔dp 、透鏡折射率nc 、空氣折射率nv 、及反射角,則根據式(43)與式(44)而確定雙峰透鏡之凹凸之兩個焦距fc 、fv ,確定透鏡之厚度fc 、及根據式(45)而確定空氣層3之厚度tr 。 其次,對用以使此種光學系統成立之條件進行敍述。為了實現第一光纖11A與第二光纖11B之間之低損耗耦合,而必須極力地抑制於透鏡面之遮光。來自第1光纖11A之出射光依據光纖之NA擴散,但該擴散經常表現為以光纖端為光束腰位置之高斯光束之傳輸。自光纖端出射並到達透鏡面之高斯光束之功率分佈於光束中心至光束半徑ω之1.73倍之範圍內成為總功率之99.75%。因此,若將至此為止之範圍設為到達透鏡表面23之光束之光束直徑BD,則其係由下式給出,即,。 此處,ω0 、λ分別係光纖11A之眾數半徑、及光之波長。 其次,係關於類型II之透鏡表面之光束直徑BD所要求之條件,此係與關於上述之類型I同樣之研究成立,與式(38)及式(39)之條件完全相同。然而,峰曲率半徑Rp 所要求之條件替換為下式,即, (數式47)。 根據上述內容,關於類型II之構成,與類型I同樣地,將峰間隔dp 與光束直徑BD、峰曲率半徑Rp (根據式(47))、及2片條件指數之關係曲線圖化所得者係圖25與圖26。於計算時採用之值與第3及第4實施形態中所說明之類型I相同。 圖25係對於類型II之構成中光纖間隔df 為250 μm之情形,針對每一峰間隔dp 對透鏡折射率nc 與峰曲率半徑Rp 之關係進行繪圖所得的曲線圖。根據式(42)~式(44)、式(46)~式(47),對各峰間隔而言,隨著透鏡折射率增加而光線折射能力增加,因而峰曲率半徑增大。關於峰間隔,隨著增大而光線接近峰中心,因此,為了保持相同之折射能力,而曲率半徑減小。 於該曲線圖中,應用雙峰條件、2片條件及模具加工條件者係曲線圖中之3條虛線。2片條件由式(38)規定,雙峰條件由式(39)規定,模具加工條件由式(47)規定。較根據雙峰條件獲得之值更下方係可構成無遮光之雙峰形態之光學系統之nc -Rp 區域。較根據2片條件獲得之值更下方係可構成無遮光之2片形態之光學系統之nc -Rp 區域。較根據模具加工條件獲得之值更上方成為可構成之nc -Rp 區域。可知根據雙峰條件及模具加工條件獲得之區域較根據2片條件及模具加工條件獲得之區域廣,而設計自由度放寬至2倍左右。尤其,於雙峰條件下,可構成曲率半徑更大之條件之光學系統,此意味著模具加工之難度較低。 圖26係對於類型II之構成中光纖間隔df 為較圖25窄之127 μm之情形,針對每一峰間隔dp 對透鏡折射率nc 與峰曲率半徑Rp 之關係進行繪圖所得的曲線圖。根據式(42)~式(44)、式(46)~式(47),與圖25同樣地,對各峰間隔而言,隨著透鏡折射率增加而光線折射能力增加,因而峰曲率半徑增大。關於峰間隔,隨著增大而光線接近峰中心,因此,為了保持相同之折射能力,而曲率半徑減小。 於該曲線圖中,與圖25同樣地,應用式(38)~式(39)、式(47)之條件者係曲線圖中之3條虛線。一看便知,可實現雙峰形態之區域與2片形態相比絕對更廣。若與光纖間隔df =250 μm之情形相比,則隨著光纖間隔df 變窄而可實現之nc -Rp 區域亦變窄,可實現雙峰形態之區域成為由雙峰條件與模具加工條件之虛線包圍之三角形區域,於透鏡折射率nc為1.44以下時無法構成。然而,於可靠性較高之硼矽酸玻璃之代表性玻璃材料即BK7之折射率為1.501時,雖然峰間隔dp 之寬度較窄且為103.5~106.1 μm,但可構成光學系統,可知雙峰形態可應對小型化。 另一方面,於2片條件下,僅可於nc 為1.64以上而且峰間隔亦為111至116 μm之有限之區域實現。該高折射率區域亦包含就可靠性之方面而言黃變之產生等成為問題之區域,不得不說於實用上應用性相當低,可認為於df =127 μm時,僅可極其有限地應用2片形態。 以上,若比較2片與雙峰構成,則可敍述以下內容。 於考慮2個主要參數即透鏡折射率nc 與峰曲率半徑Rp 之情形時,雙峰構成係nc -Rp 區域大至2片構成之2~3倍左右,而設計自由度較高。 雙峰構成亦可應對更窄之光纖間隔df ,而適於小型化。 雙峰構成由於峰曲率半徑Rp 可選擇較大之值,而可增大透鏡直徑,故而亦可較高地保持光纖間耦合效率。 雙峰構成由於製作模具時之孔之曲率半徑較大,故而更易於製作。 就類型I與II之差異而言,於光纖間隔df 為250 μm之情形時,2片條件係兩種類型大致相等,於峰間隔dp 之區域為14.2~14.3 μm。另一方面,就雙峰條件而言,可知類型I係峰間隔dp 之允許寬度擴大1.5倍左右而容易製作透鏡。尤其,於光纖間隔df 為127 μm之情形時,類型I之dp 允許寬度為3.9 μm,相對於此,類型II之允許寬度僅為2.6 μm。該允許寬度之1 μm以上之差於製作模具方面顯得非常大,類型I相當容易製作。 (第9實施形態) 於圖27中表示本實施形態之光纖矩陣模組之一例。圖27所示之光纖矩陣模組具備圖2所示之光纖矩陣模組、遮光板7、及透鏡矩陣9。遮光板7作為光零件發揮功能,透鏡矩陣9作為第2透鏡矩陣發揮功能。本實施形態之光纖矩陣模組亦可為圖10所示之第4實施形態之光纖矩陣模組。 遮光板7具有複數個貫通孔71。自部分透過膜41之反射面透過之各平行光入射至不同之貫通孔71之一端。然後,將通過貫通孔71後之平行光自各貫通孔71之另一端出射。透鏡矩陣9將自複數個貫通孔71之另一端出射之各光聚光至針對每一貫通孔71所規定之點。於該點設置光功能元件即可。 於圖28中表示本實施形態之受光模組之一例。圖28所示之受光模組具備圖27所示之光纖矩陣模組、及受光元件矩陣8。受光元件矩陣8所具備之各受光元件81接收經透鏡矩陣9聚光之各光。圖28所示之受光模組可用作4矩陣光抽頭監視模組。 本實施形態之應用區域係例如波長1.55 μm波段光通信系統。該模組自圖之左側起具備光纖矩陣1、透鏡矩陣2、具備部分透過膜41之部分反射部4、遮光板7、透鏡矩陣9、及受光元件矩陣8。對於以光纖間隔df 為首之各參數,作為一例,若採用圖5所示之值則可在現實中實現。 首先,對模組之動作、功能進行說明。自光纖11A入射至透鏡矩陣2之光線中95%由部分透過膜41以反射角(5度)反射並入射至第2光纖11B,入射光強度之5%被抽頭並返回至主線。5%強度之抽頭光係後段成為空氣層,而以出射角ψ(7.5度)出射,但於部分透過膜41之後段,為了防止因於空間傳輸之抽頭光彼此之混合所致之串擾降低,而設置開設有貫通孔71之遮光板7。遮光板7成為外形與透鏡矩陣2匹配之尺寸,且於其中央部配合抽頭光路而開設有該光束直徑之貫通孔71。於遮光板7之後段,與透鏡矩陣2反向地設置有與透鏡矩陣2相同者即透鏡矩陣9。透鏡矩陣9使於空間傳輸並擴散之抽頭光束聚光至受光元件81之受光面。 以下對上述各構成要素進行敍述。 光纖矩陣1:光纖矩陣1使用250 μm間隔8矩陣之波長1.3/1.55 μm單模帶狀光纖作為光纖構件。使其排列於TEMPAX玻璃且1 mm厚之60度V溝槽板並蓋上1 mm厚之上蓋,利用UV(Ultraviolet:紫外線)接著劑固定,並進行端面研磨而製作連接用光纖矩陣1。矩陣間隔與所使用之帶狀光纖相同為250 μm。光纖光軸於圖28中為z方向,與其他元件之連接端面係平行於x軸,且為了使因端面反射所引起之返回光減少,而設定為與y軸方向傾斜8度。再者,核心端面相對於光纖光軸之角度並不限定於8度。傾斜8度之端面表面施加有針對波長1.55 μm之AR(Anti-Reflection:防反射)塗層。全寬為4 mm。 透鏡矩陣2:由波長1.55 μm時折射率為1.501之硼矽酸系玻璃構成,且於厚度13690 m(z方向)之平板狀玻璃上表面,於4000×2000 μm(x×y)之中央部以矩陣間隔500 μm形成有具有第1非球面A1及第2非球面A2之凸面23。於鄰接之凸面23之間設置有1 μm之平坦部,自平坦部(透鏡保持面)算起之凸量即凹陷量為例如69 μm。 於透鏡矩陣2之x方向兩端部,設置有於透鏡模塑加工時一體成形之間隔件22。間隔件22係梯形凸部,其表面成為配合光纖矩陣1之傾斜8度之端面之角度,其面積例如單側為該1×1.5 mm(x×y)。間隔件22之高度較佳為以於例如透鏡光軸位置(Ac)成為特定之凸側焦距fv (此處係947.3 μm)之方式設定。 此處,一面參照圖33,一面對間隔件22之角度進行說明。於將光纖11之核心端面之法線Ln 相對於光纖11之光軸亦即z軸之角度設為θ1 ,將自光纖11之核心端面出射至空氣層3之光之中心光相對於核心端面法線Ln 之角度設為θ2 之情形時,根據斯奈爾定律,角度θ1 與角度θ2 滿足以下關係。 (數式51)此處,nf 係光纖11之傳輸光之透過折射率。因此,於nf 為1.445、空氣層3之折射率nc 為1且角度θ1 設定為8度之情形時,角度θ2 成為11.6度。光纖與透鏡系統間之光耦合成為最高效率之情形係來自光纖11之出射光與透鏡面垂直之情形。於該情形時,如圖33中所明確般,間隔件22之透鏡側平坦面22B與光纖矩陣側之傾斜端面22A之角度、即間隔件22之傾斜角度亦與θ2 相等而成為11.6度。換個角度來看,間隔件22之角度θ2 成為除了光纖11之端面之角度θ1 (8度)以外,還加上空氣層3中之自光纖光軸(z軸)之折射角度(3.6度)所得之角度。 於透鏡矩陣2之平坦面21附著有將入射角設定為5度之透過膜41。其反射/透過之比例較佳為95%/5%,作為其材質,例如可例示利用離子束輔助蒸鍍法形成之SiO2 -TiO2 多層膜。 遮光板7:遮光板7由外形4000×2000×1000 μm之方形之紅外線吸收玻璃構成。於其中央部,如圖27及圖28所示,配合抽頭光之光路,與xz面平行地開設有與z軸方向呈透鏡中心入射角ψ即7.5度之角度的30 μm見方之貫通孔71。x方向矩陣間距與透鏡矩陣2相同為500 μm。於抽頭光之光束直徑為圖5所示之227.4 μm之情形時,不與遮光板7之貫通孔71之壁接觸地傳輸,但因前段之透鏡矩陣2或部分透過膜41之反射透過而產生之由構造不規整所致之漫反射成分被該遮光板7阻止,而防止到達受光元件矩陣8成為串擾。 透鏡矩陣9:此處,透鏡矩陣9使用與透鏡矩陣2相同者。通常,受光元件81之受光面與封裝表面相距1 mm左右,因此,於透鏡矩陣9與受光元件矩陣8之間插入焦距調整樹脂91而相較透鏡矩陣2長焦點化,而於受光元件矩陣8中之受光元件81之受光面內聚光。透鏡矩陣9之朝向與透鏡矩陣2相反係為了以焦距調整樹脂91填滿透鏡矩陣9與受光元件矩陣8之間。透鏡矩陣9較佳為僅對平坦面21側施加AR塗層。 受光元件矩陣8:受光元件81係例如受光直徑80 μm、500 μm間距4矩陣之InGaAs光電二極體矩陣。將二極體矩陣密封,且自封裝表面至受光元件81之受光部為止之距離為該1 mm。根據圖28所示之側視圖可知,受光元件矩陣8自z軸方向即光軸傾斜地連接於透鏡矩陣9。 如圖27及圖28之側視圖所示,自光纖矩陣1至受光元件矩陣8為止連接界面全部保持傾斜,因此,成為防止反射返回光之構造。 組裝步驟:步驟具有3個步驟。 第1步驟係光纖矩陣1與透鏡矩陣2之連接。此係以與如下通常之光纖波導連接相同之步驟連接:於光纖波導連接裝置,自光纖矩陣1之兩端即光纖11A-1及光纖11A-4入射調芯光,一面監視來自光纖11B-1、光纖11B-4之光一面進行2軸調芯固定。連接部位係間隔件22與光纖矩陣1間。 第2步驟係遮光板7、透鏡矩陣9、及受光元件矩陣8之連接。該等之連接係於顯微鏡下依序設置受光元件矩陣8、透鏡矩陣9、遮光板7,以可自遮光板7之貫通孔看見受光元件81之受光面之方式,利用目視對準法調芯,並利用接著劑固定。 第3步驟係使調芯光入射至光纖11A-1、與光纖11A-4,一面監視受光元件矩陣8之輸出一面將附光纖矩陣1之透鏡矩陣2與附受光元件矩陣8及透鏡矩陣9的遮光板7連接固定。 特性:所製作之4 ch抽頭監視模組之於波長1.55 μm之特性係插入損耗為0.4~0.5 dB、反射衰減量為46 dB以上、受光感度為50~60 mA/W。鄰接串擾亦為45 dB以上。 於圖34中表示本實施形態之光纖矩陣模組之另一形態。圖34所示之光纖矩陣模組於光纖矩陣1之端面貼附有AR板101,又,具備GRIN(Graded Index:梯度折射率)透鏡矩陣109而代替圖27所示之遮光板7及透鏡矩陣9。光纖矩陣模組亦可為圖10所示之第4實施形態之光纖矩陣模組。 AR板101係使AR膜附著於折射率與光纖之等效折射率大致相等之透明薄板之單側而成者。於難以於光纖矩陣1之端面直接形成AR膜之情形時,於光纖矩陣1之端面,以AR板101之未形成AR膜之面為接著面利用折射率與兩者大致相等之透明接著劑貼附而使用,而獲得與直接之AR塗層同等之效果。 於圖35中表示本實施形態之受光模組之另一形態。圖35所示之受光模組具備圖34所示之光纖矩陣模組、與受光元件矩陣8。受光元件矩陣8所具備之各受光元件81接收經GRIN透鏡矩陣109聚光之各光。 GRIN透鏡矩陣109具有作為GRIN透鏡發揮功能之複數個GI(Graded Index)光纖174。GRIN透鏡矩陣109成為外形與透鏡矩陣2匹配之尺寸,且於其中央部配合抽頭光路配置有GI光纖174。GI光纖174較佳為藉由以2塊V溝槽板夾持而固定。自部分透過膜41透過之各平行光入射至不同之GI光纖174之一端。然後,將自GI光纖174之另一端出射之各光聚光至針對每一GI光纖174所規定之點P9-1~P9-4。於該點配置有受光元件81之受光面。 (第10實施形態) 於圖29中表示本實施形態之光纖矩陣模組之一例。圖29所示之光纖矩陣模組具備圖18所示之光纖矩陣模組、遮光板7、及透鏡矩陣9。遮光板7作為光零件發揮功能,透鏡矩陣9作為第2透鏡矩陣發揮功能。本實施形態之光纖矩陣模組亦可為圖23所示之第8實施形態之光纖矩陣模組。 遮光板7具有複數個貫通孔71。自部分透過膜41之反射面透過之各平行光入射至不同之貫通孔71之一端。然後,將通過貫通孔71後之平行光自各貫通孔71之另一端出射。透鏡矩陣9將自複數個貫通孔71之另一端出射之各光聚光至針對每一貫通孔71所規定之點。於該點配置有受光元件81之受光面。 於圖30中表示本實施形態之受光模組之一例。圖30所示之受光模組具備圖29所示之光纖矩陣模組、與受光元件矩陣8。受光元件矩陣8所具備之各受光元件81接收經透鏡矩陣9聚光之各光。圖30所示之受光模組可用作4矩陣光抽頭監視模組。 應用區域係波長1.55 μm波段光通信系統。該模組自圖之左側起具備光纖矩陣1、透鏡矩陣2、部分透過膜41及玻璃基板42、遮光板7、透鏡9、及受光元件矩陣8。對於以光纖間隔df 為首之各參數,作為一例,若採用圖21所示之值則可在現實中實現。 首先,對模組之動作、功能進行說明。自光纖11A不經由空氣層而直接自平坦面21側入射至透鏡矩陣2並自透鏡表面23出射的光線中95%由部分透過膜41以反射角f (8度)反射後再次返回至透鏡矩陣2並入射至光纖11B,入射光強度之5%被抽頭並返回至主線。5%強度之抽頭光係後段經過平行於部分透過膜41之玻璃基板42而成為空氣層,而以出射角(8.0度)出射,但於玻璃基板42之後段,為了防止因於空間傳輸之抽頭光彼此混合所致之串擾降低,而設置開設有貫通孔71之遮光板7。遮光板7成為外形與透鏡矩陣2匹配之尺寸,且於其中央部配合抽頭光路而開設有該光束直徑之貫通孔71。於遮光板7之後段,與透鏡矩陣2同向地設置有與透鏡矩陣2相同者即透鏡矩陣9。透鏡矩陣9使於空間傳輸並擴散之抽頭光束聚光至受光元件81之受光面。 以下針對上述各構成要素對與第9實施形態不重複之內容進行敍述。 光纖矩陣1:與第9實施形態不同,不對傾斜8度之端面表面施加AR塗層。再者,與第9實施形態同樣,核心端面相對於光纖光軸之角度不限定於8度。 透鏡矩陣2:由波長1.55 μm時折射率為1.501之硼矽酸系玻璃構成,且於平行於xy面之透鏡保持面上之中央部,以矩陣間隔500 μm朝向z軸之正方向形成有具有第1非球面A1及第2非球面A2之凸面23。於鄰接之凸面23之間設置有1 μm之平坦部,自平坦部(透鏡保持面)算起之凸量即凹陷量為例如75 μm。 於透鏡矩陣2之x方向兩端部,設置有於透鏡模塑加工時一體成形之間隔件22。間隔件22係梯形凸部,梯形凸部之表面與透鏡保持面平行,且其面積係單側為該1×1.5 mm(x×y)。間隔件22之高度以於透鏡光軸位置(Ac)成為特定之凸側焦距fv (此處係889.4 μm)之方式設定。 透鏡矩陣2之平坦面21與光纖矩陣1之端面平行且相對於y軸傾斜,且以該傾斜平坦面21與透鏡凸面23之透鏡光軸(Ac)上距離成為凹側焦距fc =1342 μm的方式設定。 部分透過膜41及玻璃基板42:於本構成中,部分透過膜41附著於與透鏡矩陣2分開之透明玻璃基板42但具備同一折射率nc 者。於兩面平行之玻璃基板42上附著有將入射角設定為8度之部分透過膜41。其反射/透過比例較佳為95%/5%,作為其材質,例如可例示利用離子束輔助蒸鍍法形成之SiO2 -TiO2 多層膜。 遮光板7:遮光板7由外形4000×2000×1000 μm之方形之紅外線吸收玻璃構成。於其中央部,如圖29及圖30所示,配合抽頭光之光路,與xz面平行地開設有與z軸方向呈透鏡中心入射角f 即8度之角度的300 μm見方之貫通孔。x方向矩陣間距與透鏡矩陣2相同為500 μm。於抽頭光之光束直徑為圖21所示之214.6 μm之情形時,不與遮光板7之貫通孔71之壁接觸地傳輸,但因前段之透鏡矩陣2或部分透過膜41之反射透過而產生之由構造不規整所致之漫反射成分被該遮光板7阻止,而防止到達受光元件矩陣8成為串擾。 如圖29及圖30之側視圖所示,自光纖矩陣1至受光元件矩陣8為止連接界面全部保持傾斜,因此,成為防止反射返回光之構造。 組裝步驟:與上述第9實施形態之不同之處在於:於第1步驟中,首先連接透鏡矩陣2與部分透過膜41。此步驟由於部分透過膜41為普通之平板,故不需要調芯作業,而可僅以對模作業連接。其他與上述第9實施形態相同。 特性:所製作之4 ch抽頭監視模組之於波長1.55 μm之特性係插入損耗為0.4~0.5 dB、反射衰減量為46 dB以上、受光感度為50~60 mA/W。鄰接串擾亦為45 dB以上。與第3實施形態相同。 (第11實施形態) 於上述實施形態中係一維排列之矩陣,但亦可為二維矩陣。於該情形時,圖2或圖18所示之光纖矩陣模組於y方向上並排排列。 此時,最成問題的是光纖矩陣,但光纖矩陣1可根據專利文獻2而實現。於圖31中表示光纖矩陣1之自z方向觀察之連接面。圖31所示之光纖矩陣1具備施加有光纖矩陣用之60度之V溝槽14之V溝槽板13-2~13-5。於V溝槽板13-2~13-5,於V溝槽14之矩陣之兩側,設置有上下對位用V溝槽15-1、15-2。而且,於該V溝槽板13-2~13-5之背面亦於與正面側相同之x方向位置形成有對位溝槽15-3、15-4。對位用光纖12使用與圖示之光纖11A、11B相同者即可。 於該情形時,若將V溝槽14之開口寬度設為W14 且對位溝槽15之開口寬度設為W15 ,則該等設定為下式即可,即, (數式29)(數式30)。 若如此,則於對位用光纖12恰好嵌合於對位溝槽15時,藉由上板而以上板按壓波導用光纖11。此處,R係光纖之半徑,d係V溝槽板13-2~13-5與上板之距離。於本實施例中,由於將d設為20 μm,故而設為W14 =193 μm、w15 =61 μm。 對位溝槽15-1、15-2、15-3、15-4於V溝槽板之正面及背面x方向位置必須一致,正面及背面之對位係事先於切片機或切割機等溝槽加工裝置中,調整溝槽形成位置觀察鏡筒之上下對焦軸相對於加工面之垂直度即可。如此一來,以TEMPAX玻璃製作之8×4光纖矩陣之x方向間距為250 μm,y方向間距為1 mm。藉此,可製作x方向500 μm間距、y方向1 mm間距之4×4矩陣之光纖矩陣模組及受光模組。 此處,光纖矩陣1較佳為如圖32之側視圖所示,僅對光纖核心附近之部分實施傾斜加工。其原因在於,若跨及矩陣之端面整面設為傾斜,則尤其難以實現透鏡矩陣2以下後段之所有零件之二維矩陣化。加工可使用雙頭切割機。此係縱列具備2台切割機者,係可於1次步驟中使用不同之2種刀片連續加工之裝置。 亦進行光纖矩陣1以外之透鏡矩陣2、9或遮光板7、及受光元件矩陣8之2D(two dimensional,二維)矩陣化,且均為x方向500 μm間距、y方向1 mm間距之4×4矩陣。於圖32中表示所製作之4×4抽頭監視模組之側視圖。外觀上,俯視圖與圖28完全相同,於側視圖中,成為如於y方向上堆積般之形態。 再者,本實施形態不限於圖2或圖18所示之光纖矩陣模組,亦可應用於上述所有實施形態之光纖矩陣模組。又,於上述所有實施形態中,對照進行第1非球面A1及第2非球面A2之光學設計,但本發明不限定於此。例如,第1非球面A1及第2非球面A2之形狀亦可不同,第1及第2凸面之峰位置亦可不同。 又,於至此為止之說明中,為了方便起見而設為透鏡光軸Ac與由光纖光軸形成之平面Pc平行。然而,於光纖端面為了防止反射而如本發明之說明圖般傾斜設定之情形時,較理想為於光纖矩陣1與透鏡矩陣2之間進行繞與x軸平行之軸之歪斜調整。 (本發明之效果) 如上所述,若設為於平凸透鏡之平坦面側直接連接前後段之元件之構造,則可構成小型之光模組。又,藉由如本發明中所敍述般將透鏡表面非球面化,而可充分使用透鏡孔徑,即便為經積體化之小口徑透鏡,亦可實現高效率之光耦合。進而,由於為平凸構造,故而不需要如兩凸透鏡般之正面及背面兩面對位之類之作業,亦有以單面模塑步驟容易地矩陣化所得者能夠量產之優點。根據該等內容,可明確大有助於光通信用器件之經濟化。 [產業上之可利用性] 本發明可應用於資訊通信產業。Hereinafter, embodiments of the present invention will be described in detail with reference to the drawings. The present invention is not limited to the embodiments described below. These examples are merely examples, and the present invention can be implemented in the form of various changes and improvements based on the knowledge of the practitioner. It should be noted that constituent elements having the same reference numerals in this specification and the drawings indicate those that are the same as each other. (First Embodiment) Fig. 1 shows an optical system according to this embodiment. In this embodiment, optical fibers 11A and 11B are arranged on the convex surface 23 side of the plano-convex lens, and a partially reflecting portion 4 is arranged on the flat surface 21 side of the plano-convex lens. The end faces of the optical fibers 11A and 11B are arranged at a first position P1 and a second position P2, respectively. The length direction of the optical fibers 11A and 11B is on a specific plane PC Center axis A of internal and plano-convex lensesC Parallel configuration. The plano-convex lens of this embodiment has a first aspherical surface A1 and a second aspherical surface A2 on the convex surface 23. The light emitted from the end surface P1 of the optical fiber 11A is incident on the plano-convex lens from the first aspherical surface A1. The first aspherical surface A1 makes the light emitted from the end surface P1 of the optical fiber 11A parallel light. The light that becomes parallel light by the first aspheric surface A1 passes through the plano-convex lens, and a part of the reflecting portion 4 disposed on the flat surface 21 reflects a portion toward the second aspheric surface A2. The second aspherical surface A2 condenses the parallel light reflected by the partial reflection portion 4 to the second position P2. Thereby, the parallel light reflected by the partial reflection portion 4 is incident on the optical fiber 11B. In the plano-convex lens of this embodiment, since the second aspherical surface A2 condenses the parallel light reflected by the partial reflection portion 4 to the second position P2, it is possible to branch the monitoring light locally (hereinafter referred to as a tap) and the optical fiber 11B is well coupled. (Second Embodiment) FIG. 2 shows a configuration example of an optical fiber matrix module according to this embodiment. The optical fiber matrix module of this embodiment includes: a lens matrix 2 in which a plurality of convex surfaces 23-1 to 23-4 are arrayed in the first embodiment; and an optical fiber in which a plurality of optical fibers 11A and 11B are aligned in the first embodiment. Matrix 1. The optical fiber matrix 1 and the lens matrix 2 indicate that the four optical fiber-lens optical systems of the first embodiment are arranged side by side on a specific plane PC The example above. The lens matrix 2 functions as a first lens matrix. The lens matrix 2 includes a plurality of plano-convex lenses according to the first embodiment. Each of the plano-convex lenses included in the lens matrix 2 includes the optical fiber-lens optical system of the first embodiment as a basic unit. Optical axis A is the central axis of each plano-convex lensC Arranged side by side on a specific plane PC Inside. The optical fiber matrix 1 has two optical fibers 11A and 11B for each of the convex surfaces 23-1 to 23-4. The optical system of FIGS. 1 and 2 will be described with reference to FIG. 3. The following directions are described following the orthogonal xyz coordinate axes in the figure. On the left side of the figure, it is arranged in the xz plane in parallel with the z axis in the x axis direction at equal intervals df An optical fiber matrix 1 in which optical fibers are arranged. The optical fiber matrix 1 has a plane that is parallel to the x-axis and has a specific angle with respect to the y-axis as an end surface, and is configured, for example, by being held by a casing such as TEMPAX glass. Has an optical axis A parallel to the z-axisC Convex surface 23 will be perpendicular to the optical axis AC That is, the plane of the z-axis is set as a common plane, and is spaced 2d in the x-axis direction at twice the interval of the fiber matrix 1.f Matrix. The convex side of the lens matrix 2 is disposed toward the optical fiber matrix 1 with an air layer 3 at a specific distance described below. As shown in the figure, the thickness of the lens matrix 2 is the distance between the convex surface 23 and the flat surface 21 on the opposite side and the concave focal length f.c Set in a consistent manner. The relative position of the fiber matrix 1 and the lens matrix 2 is set as follows: in the x-axis direction, the optical axis A of the plano-convex lensC The center lines of the adjacent fibers of the optical fiber matrix 1 (the center lines of the first optical fiber 11A and the second optical fiber 11B in the figure) are the same, and in the y direction, the optical axis A of the lensC The plane formed by the matrix is consistent with the plane formed by the centerline of the fiber matrix, and in the z direction, the distance between the end face of the fiber matrix 1 and the convex vertex of the lens matrix 2 and the convex side focal length f of the plano-convex lensv Consistent. A partial transmission film 41 having a function of reflecting / transmitting light of a specific wavelength at a desired ratio may be applied to the side surface of the flat surface 21 of the lens matrix 2. Spacers 22 are provided at both ends of the lens matrix 2 to maintain the distance between the lens matrix and the optical fiber matrix 1 at a specific value. The spacer 22 may be formed in advance with a concave portion corresponding to the lens in a mold simultaneously with forming the concave portion corresponding to the lens, and then formed by a molding method simultaneously with forming the lens, or may be in the form of sandwiching a plate of a specific thickness. In addition, in this configuration, the path of light emitted from the end face of the first optical fiber 11A is approximately studied with light rays. Since the end face of the first optical fiber 11A is located on the convex side focal plane, the light emitted from the end face of the first optical fiber 11A as a point light source and incident on the corresponding lens of the lens matrix 2 is directed toward the optical axis A.C Side refraction and becomes with the optical axis AC At an angleThe parallel rays of light travel through the lens. Among them, the ends of the optical fibers 11A and 11B and the optical axis AC That is, the light rays emitted in parallel with the z-axis, that is, the central light rays of the parallel light, enter the plano-convex lens and pass through the focal point on the concave side. As mentioned above, the thickness of the plano-convex lens is set exactly to the concave focal length fc And the part becomes a flat surface, and a part of the transmissive film 41 is applied to the part. Therefore, a part of the specific intensity of the parallel light is transmitted through the part of the transmissive film 41 and relative to the optical axis AC forThe angle is straight, but the remaining intensity is partially reflected by the partially transmitting film 41 and is relative to the optical axis A.C The symmetrical x-direction position reaches the plano-convex lens surface again. The reflected light that has reached the surface of the lens is parallel light that passes through the focal point on the concave side, along the optical path that exits from the first optical fiber 11A and enters the plano-convex lens with respect to the optical axis AC Symmetric path, finally focused to a position relative to the optical axis AC An end face P2 of the second optical fiber 11B at a position symmetrical to the first optical fiber 11A. Here, if the thickness of the plano-convex lens is set to the focal length f of the concave side,c Thin, the reflected parallel light is f compared to the lens thicknessc Optical axis AC The side surface is here where the parallel light is not bundled and further diffuses on the end face of the second optical fiber 11B. On the other hand, the lens thickness is thicker than fc In this case, the reflected light further reaches the outer surface of the lens, so the parallel light is excessively collected, and as a result, it diffuses on the end face of the second optical fiber 11B. In either case, the optical axis of the reflected light is offset from the optical axis of the second optical fiber 11B. The distance between the end faces of the optical fibers 11A and 11B and the lens matrix 2 is preferably set to the convex side focal length fv Meanwhile, the flat surface 21 of the lens matrix 2 is a concave focal surface. In addition, the light transmitted through the part of the transmissive film 41 is shown in FIG. 3.v If it is the same, it shoots out at an angle ψ. Although not shown, if the refractive index of the adjacent medium is the same as the refractive index of the lens matrix 2,Shoot out. In addition, when a low-loss coupling is desired between the optical fibers 11A and 11B with such a reflection optical system, the surface shape required for the convex surface 23 is generally called an aspheric surface. The aspheric shape differs depending on the setting form of the optical system, and the method for obtaining the aspheric shape in this embodiment will be described with reference to FIG. 4. In FIG. 4, for convenience of description, light is described as being emitted from the second optical fiber 11B. However, since the optical system is symmetrical with respect to the optical axis, the authenticity is not impaired. As shown in the figure, the setting includes the optical axis AC The xz plane, and the lens curved surface as the rotation curved surface with the z axis as the axis of symmetry, and the shape of the xz section as Z (x). The optical system set here is a model in which the second quadrant in the xz plane is placed parallel to the z-axis and placed on the convex side focal distance f from the x-axis.v The light emitted from the second optical fiber 11B at an upward position at an angle of θ is refracted at an intersection with the hypothetical curve Z (x), and reflected at the reflection angle illustrated in FIG. 3Travel in the lens. According to Snell's law of the refracting position, the following equation holds, that is, (Equation 1). Here, nv , Nc , Θv , Θc The refractive index of the air layer 3, the refractive index of the plano-convex lens, the incident angle to the lens surface, and the exit angle from the lens surface, respectively. If the angle formed by the tangent to the curve Z (x) of the light incident position and the x-axis is set to θt , According to the angular relationship in FIG. 4, it is easy to know that there is a relationship of the following formula, that is, (Equation 2). The following formula is established based on the formulas (1) and (2). (Equation 3)Here, because the angle θt The tangent angle of the curve Z (x), so the following formula holds. [Equation 4]In addition, the outgoing light from the optical fiber 11B and the optical axis AC The tangent of the formed angle θ satisfies the following formula, that is, (Equation 5). By changing θ of equation (4)t Substituting θ with Equation (5) into Equation (3), a differential equation related to Z (x) can be obtained. The curve is obtained according to the boundary conditions of equations (3) to (5) and the origin (0, 0) expressed by the following equation, but it becomes a complex nonlinear differential equation that cannot be solved analytically, and is approximately calculated Find it out. At this time, since it may be solved analytically, the function form is determined based on this in advance. [Equation 6]The situation that can be solved analytically is the position of the x-direction of the second optical fiber 11B and the optical axis A of the lens in FIG. 4C Consistent situation (df / 2 = 0). At this time, the reflection angle in FIG. 4It becomes zero, Z (x) is calculated | required analytically, and it becomes a hyperbola of Formula (7). [Equation 7]Here, Ch Is a curvature, and is the following formula, that is, (Equation 8), Kh Is a conic constant, and is the following formula, that is, (Equation 9). As in this embodiment, the optical fibers 11A and 11B are from the optical axis A.C In the case of a shift, it is assumed that Equation (7) is used as the basic equation and an approximate term based on the polynomial shown below is added. [Equation 10]Here, n is an integer of 2 or more, A3 , A4 , ... A2n - 1 , A2n Aspheric coefficient. After determining the number of times corresponding to the target accuracy in equation (10), substitute equations (3), (4), and (5) to calculate the residual error, and find the curvature C that is the global solution according to the damping least square method.h Cone constant Kh , And aspheric coefficient A2n - 1 , A2n Combination. If the coefficient value in formula (10) is specified, the surface shape can be processed in the mold. The coefficients to be specified can be determined by equations (3) to (5). Even without such calculations, the possibility can be verified. First, the names and symbols of the parameters shown in FIGS. 3 and 4 are shown in the left column of FIG. 5. In FIGS. 3 and 4, the light emitted from the first optical fiber 11A having the end surface on the convex side focal surface and entering the convex surface 23 through the air layer 3 becomes the optical axis AC PresentAngle of parallel light. Therefore, for these rays to enter the lens optical axis AC The light rays at the intersection with the lens surface (that is, the apex of the convex surface 23 of the lens), because the tangent plane of the lens surface is exactly perpendicular to the optical axis AC The parallel z-axis, so the incident angle ψ and the exit angle of the lens center of the lightWith refractive index nv , Nc In the meantime, Snell's law holds, that is, (Equation 11). Since the fiber matrix 1f Matrixed and lens matrix 2 is 2d twicef Matrixization, so if the fiber spacing d is givenf Incident angle ψ and exit angle from lens centerValue, the focal length f on each of the convex and concave sidesv , Fc It is determined by the following formulas (12) and (13). (Equation 12)(Equation 13)In the above formulas (11) to (13), no approximate operation is added and the formula is strict, and the optical axis A that satisfies this relationship isC The rotation surface that is the axis of symmetry becomes a higher-order surface based on the rotation hyperbola. Determine the two focal lengths f of the convexo-concave of the plano-convex lens according to equations (12) and (13)v , Fc That is, the distance between the optical fibers 11A and 11B and the plano-convex lens and the lens thickness are determined. Second, the limiting factors of this optical system are described. The emitted light from the first optical fiber 11A is diffused according to NA (Numerical Aperture) of the optical fiber, but it is clear from FIG. 3 that the beam diameter BD must be such that the distance fv The adjacent lens is not touched everywhere, so the following condition must be satisfied, that is, (Equation 14). There are also restrictions on the surface shape of the convex surface 23. The lens matrix 2 having the convex surface 23 is produced by a molding method using a mold, but at this time, the curvature radius of the concave shape grinding process is limited, and is generally set to 150 μm or more. The shape of the lens surface is aspheric, and its radius of curvature is as the optical axis AC The lens center is the smallest and moves away from the optical axis AC And gradually increased. Therefore, it is the minimum radius of curvature that is a problem when manufacturing a mold, but since it is the smallest at the center of the lens, if it is estimated by a spherical approximation, it becomes the following formula (15). [Equation 15]Here, for clarity, the convex side focal length f is added.v With concave focal length fc The spherical approximation is given by the following formula. [Equation 16][Equation 17]In addition, an attempt is made to substitute equations (11) to (15) into actual possible values and calculate a value below the lens central incident angle ψ in FIG. 3 as an example of the estimation in FIG. 5. Fiber spacing df Choose the commonly used values of 250 μm and 127 μm. The refractive index of the lens is 1.501. The refractive index of the glass with high weather resistance is 1.501. Second, the reflection angleIn the present embodiment, an optical tap module with a so-called tap film having an optical fiber pair consisting of the optical fiber 11A and the second optical fiber 11B as the main optical path and a part of the transmissive film 41 reflecting 90% or more and transmitting a few% is considered The application is set to an angle of 5 degrees that does not produce polarization dependence on partially transmitted light. At fiber spacing df For 250 μm and 127 μm, the convex focal length fv They are 947.3 μm and 481.2 μm, respectively. At this time, the diameter BD of the light beams emitted from the optical fiber 11A on the lens surface becomes smaller than the fiber interval d, respectively.f 227.4 μm, 115.5 μm, so this light does not touch the adjacent lens. Here, as the NA of the optical fibers 11A and 11B, a standard single-mode optical fiber having a mode diameter of 9.0 / 10.0 μm in the 1.3 / 1.55 μm band is selected as 0.12. In addition, since the optical axis A of the surface of the convex surface 23 of the lens matrix 2C The approximate radii of curvature of the upper spheres are 474.6 μm and 241.1 μm, so they fully exceed the mechanical processing limit of the mold, which is 150 μm, and can be used for mold lens processing. Although it is a partially transmissive film 41, it is usually formed by alternating multilayer laminated films using silicon dioxide as a low refractive index film material and titanium dioxide or tantalum pentoxide as a high refractive index film material. As the substrate at this time, the lens matrix 2 is a good substrate because the flat surface 21 facing the convex surface 23 is the same oxide-based material. In short, it can be seen that the configurations of FIGS. 1, 2, and 3 can be realized. (Third Embodiment) Fig. 6 is a perspective view of an optical system according to this embodiment. The plano-convex lens 2 of this embodiment is a bi-modal bi-modal lens in which the first aspherical surface A1 and the second aspherical surface A2 are convex in the first embodiment and the second embodiment. In the third embodiment and the fourth embodiment, the first aspherical surface A1 is referred to as a first convex surface A1, and the second aspherical surface A2 is referred to as a second convex surface A2. The plano-convex lens 2 of this embodiment is a flat substrate made of lens material having a rectangular shape parallel to the axis of the xyz orthogonal coordinate in the figure, and has a convex surface 23 including three curved surfaces. The first is a first convex surface A1 composed of a curved surface having a straight line R1 parallel to the z-axis as a center line and an intersection point with R1 as a peak P6. The second is a second convex surface A2 which is formed by a curved surface having a straight line R2 parallel to the z-axis as a center line and an intersection point with R2 as a peak P8. The second convex surface A2 moves the first convex surface A1 in parallel in the x direction by a peak interval d.p The resulting shape. In the figure, the rotation center line of the second convex surface A2 is represented by R2. The diameters of the two convex surfaces A1 and A2 series lenses that function as a lens are set to a peak interval dp Large and arranged so as to overlap each other. The overlapping part is cut out as shown in the figure, and a third surface, that is, the width w is connected to the convex surface of A1 and A2 at this part.s Saddle A3. According to the contour line indicated by the dotted line in the figure, it can be seen that the saddle portion A3 also protrudes from the surrounding plane and smoothly connects the two convex surfaces A1 and A2. As a whole, the plano-convex lens 2 passes through the midpoint of two peaks formed by the convex surfaces A1 and A2, and uses a straight line Ac parallel to the z-axis as the lens centerline. Hereinafter, a straight line passing through the peaks of the convex surfaces A1 and A2 and parallel to the x-axis is referred to as a peak line Bc. The linear first optical fiber 11A having an optical axis parallel to the z-axis is disposed with respect to the bimodal lens such that its optical axis intersects the peak line Bc outside the specified distance from the center line R1 of the convex surface A1, and is from The light emitted from an optical fiber 11A is shifted and incident at the intersection point P4 which is further outside than the peak P6 of the convex surface of the first lens. The intersection point P4 is an intersection point between the straight line passing through the first position P1 and perpendicular to the flat surface 21 and the convex surface 23. A specific amount of intensity of the incident light is reflected by the following mechanism, and is condensed from the intersection point P7, which is more outward than the peak P8 of the convex surface of the second lens, and is incident on the first optical fiber 11A symmetrically disposed with respect to the lens centerline Ac. Two optical fibers 11B. The intersection point P7 is an intersection point of the straight line passing through the second position P2 and perpendicular to the flat surface 21 and the convex surface 23. A bimodal lens can be produced by a glass molding method using a mold. FIG. 7 shows a contour map obtained when the mold is viewed from the z-axis direction in the mold manufacturing step. First, as shown in FIG. 7, concave surfaces corresponding to the first and second convex surfaces A1 and A2 are formed on the mold surface. If there is a ridgeline at the boundary, there is a possibility that the movement of substances during the molding operation may be hindered. Therefore, as shown in FIG. 8, the boundary is cut in such a way that it does not reach the projection light intensity distribution pattern from the optical fiber on the projection portion Pd on the xy plane, and the shape change at the boundary is eased. Thereby, it becomes the shape provided with the saddle part A3 as shown in FIG. Next, in order to more easily explain the optical system of this embodiment, FIG. 9 is used as a cross-sectional view obtained by cutting the plane including the rotation center lines R1 and R2. In this embodiment, optical fibers 11A and 11B are arranged on the convex surface 23 side of the plano-convex lens 2, and a partially reflecting portion 4 is arranged on the flat surface 21 side of the plano-convex lens 2. The end faces of the optical fibers 11A and 11B are arranged at a first position P1 and a second position P2, respectively. The length direction of the optical fibers 11A and 11B is on a specific plane PC Center axis A of inner and bimodal lensesC Parallel configuration. Hereinafter, this embodiment is referred to as type I. The plano-convex lens 2 of this embodiment has two convex surfaces on the convex surface 23. The first convex surface A1 is a rotating curved surface that is parallel to the center axis Ac of the plano-convex lens and is included in the straight line R1 of the plane Pc formed by the optical fibers 11A and 11B. The second convex surface A2 is also similar to the center axis of the plano-convex lens. Ac is a rotation curved surface parallel to the straight line R2 included in the plane Pc formed by the optical fibers 11A and 11B. The rotation center lines R1 and R2 are symmetrical with respect to the central axis Ac, and are offset inward relative to the two fiber centerlines. distance. (Fourth Embodiment) Fig. 10 shows a configuration example of an optical fiber matrix module according to this embodiment. The optical fiber matrix module of the present embodiment is the optical fiber matrix module of the second embodiment, and the plano-convex lens 2 of the third embodiment is applied to the convex surfaces 23-1 to 23-4. The optical system in FIGS. 9 and 10 will be described with reference to FIG. 11. On the left side of the figure, a periodic interval d is arranged in the xz plane parallel to the z axis in the x axis direction.f An optical fiber matrix 1 in which optical fibers are arranged. The optical fiber matrix 1 has a plane that is parallel to the x-axis and has a specific angle with respect to the y-axis as an end surface, and is configured, for example, by being held by a casing such as TEMPAX glass. The first convex surface A1 is a curved surface that is centered on a line R1 that is included in a surface Pc formed by the fiber matrix and is parallel to the z-axis, and functions as a lens. Further, the optical axis of the optical fiber 11A is shifted toward the inside (on the center axis Ac side) by a certain distance. The second convex surface A2 is formed with a width w with respect to the lens central axis Ac.s The saddle is symmetrical to the first convex surface A1. The interval d between the centerlines of rotation R1 and R2 of the first and second convex surfaces A1 and A2, respectivelyp (Hereinafter referred to as peak interval dp ) Set to less than the fiber spacing df Distance. The convex side of the lens matrix 2 faces the optical fiber matrix 1 through the thickness and the convex side focal length fv Equivalent air layer 3 is arranged. As shown in the figure, the thickness of the lens matrix 2 is the distance between the bimodal convex surface 23 and the flat surface 21 on the opposite side, but it is set to be thicker than the concave focal length f.c Lens thickness t1 . The relative position of the fiber matrix 1 and the lens matrix 2 is set in such a manner that, in the x-axis direction, the center axis A of the bimodal lensC The center lines of the adjacent fibers of the optical fiber matrix 1 (the center lines of the first optical fiber 11A and the second optical fiber 11B in the figure) are the same, and in the y direction, the central axis A of the lensC The plane formed by the matrix is consistent with the plane formed by the centerline of the fiber matrix, and in the z direction, as described above, the distance between the end face of the fiber matrix 1 and the convex vertex of the lens matrix 2 and the convex side focal length f of the bimodal lensv Consistent. In such a configuration, the path of light emitted from the end face of the first optical fiber 11A is examined by approximating the light. Since the end face of the first optical fiber 11A is located on the convex side focal plane, and the centerline R1 of the first convex surface A1 in the bimodal convex surface is shifted in the x direction relative to the fiber centerline as described above, The end face is a point light source, and the light that exits from it and enters the first convex surface A1 of the lens matrix 2 is directed toward the central axis AC Side refraction, with the central axis AC At a specific angleThe parallel rays of light travel through the lens. Among them, the end of the optical fiber 11A and the central axis AC That is, the light rays emitted in parallel with the z-axis, that is, the central light rays, enter the plano-convex lens and pass through the focal point of the concave side. If set to the thickness t of the plano-convex lens as described above1 Thicker than the concave focal length fc And the flat surface 21 is located at the above-mentioned central ray and the lens central axis Ac At the point of intersection, and a part of the transmissive film 41 is applied to the flat surface 21, a part of the specific intensity of the parallel light is partially transmitted through the film 41 and relative to the central axis AC Straight forward at an angle of ψ, but the rest of the intensity is reflected by the partially transmitting film 41, relative to the central axis AC The symmetrical x-direction position reaches the second convex surface A2. The reflected light that reaches the second convex surface A2 is parallel light that passes through the focal point of the concave side, and is along the optical path that exits from the first optical fiber 11A and enters the bimodal lens with respect to the central axis A.C Symmetric path, finally focused to A relative to the central axis AC An end face P2 of the second optical fiber 11B at a position symmetrical to the first optical fiber 11A. Next, the above description is formulated using a formula. In FIG. 11, the light emitted from the first optical fiber 11A having the end surface on the convex side focal surface and entering the first convex surface A1 of the convex surface 23 through the air layer 3 becomes the center axis A of the lens.C PresentAngle of parallel light. Among these rays, the rays incident on the peak of the first convex surface A1 (the intersection point of the central symmetry line R1 and the first convex surface), because the tangent plane of the lens surface of the incident point is perpendicular to the central axis AC , So the incident angle ψ and the exit angle at the center of the peak of the lightAnd refractive index nv , Nc In between, Snell's law holds. (Equation 31)Here, nv , Nc Respectively the refractive index of the air and the refractive index of the lens. In addition, since the fiber matrix 1 is spaced at periodic intervals df Matrix, and the lens matrix 2 is 2d with a period twicef Matrix, so focal length f on each side of convex side and concave sidev , Fc Based on fiber spacing df Peak interval d between the first convex surface A1 and the second convex surface A2p , Lens center incident angle ψ, and exit angleThe value is determined by the following equations (32) and (33). (Equation 32)(Equation 33)About lens thickness t1 Similarly, the following equation holds, (Equation 34). Furthermore, the radius of curvature at the peaks of the convex surfaces A1 and A2 is the peak radius of curvature Rp Is given by: (Equation 35). The first and second convex surfaces A1 and A2 constituting the double peak may satisfy the above-mentioned formulas (31) to (35), but satisfy these relationships and be parallel to the lens central axis A.C The rotating surface whose axis is the axis of symmetry becomes a higher-order surface based on a rotating hyperbola, which is generally called an aspheric surface. If fiber spacing d is givenf Peak interval of lens dp Lens refractive index nc Refractive index nv , And reflection angle, The two focal lengths f of the convexo-concave of the bimodal lens are determined based on equations (32) and (33)v , Fc That is, the distance between the optical fibers 11A and 11B and the bimodal lens is determined, and the lens thickness t is determined based on equation (34).1 . In addition, it is known from the formula (35) that the peak radius of curvature is a standard for the shape of the mold used in the molding step of the lens production step. Next, the conditions for establishing such an optical system will be described. In order to achieve the low-loss coupling between the first optical fiber 11A and the second optical fiber 11B, it is necessary to suppress the shading of the lens surface as much as possible. The outgoing light from the first optical fiber 11A is diffused according to the NA of the optical fiber, but the diffusion often manifests as the transmission of a Gaussian beam with the fiber end as the waist position of the beam. The power of the Gaussian beam exiting from the fiber end and reaching the lens surface is distributed from the center of the beam to 1.73 times the beam radius ω to become 99.75% of the total power. Therefore, if the range up to this point is the beam diameter BD of the light beam reaching the lens surface, that is, the convex surface 23, it is given by the following formula. [Equation 36]Here, ω0 And λ are the mode radius of the optical fiber 11A and the wavelength of light, respectively. Next, based on the configuration of the lens, the conditions required for the beam diameter BD on the lens surface were studied in accordance with FIG. 12. In the bimodal lens of this embodiment, if the peak interval d is increased,p Then, as shown in FIG. 12 (a), the overlap of the convex surfaces of the two lenses is eliminated, and the two convex surfaces are in a state. That is, the saddle curved surface A3 becomes the same plane as the plane around the lens. This is referred to as a two-plate state, and a comparison between this and a bimodal state is performed. First, a two-chip system will be studied based on FIG. 12 (a). In a two-chip system, in order to achieve a light-shielding, low-loss fiber-to-fiber coupling, the distance x in the x-axis direction between the centerline of the fiber parallel to the z-axis and the outer edge of the lens near the centerline sideE Must be larger than half of the beam diameter BD of the light emitted from the optical fiber on the lens surface, so the following must be true. (Equation 37)I.e. (Equation 38)Here, BD represents the beam diameter of the light emitted from the optical fiber on the lens surface, and dp Represents the peak interval between convex A1 and convex A2, df Represents the distance between optical fibers, ws Indicates the width of the saddle A3. This is a 2 piece condition. Following, will 2dp -Df -Ws Called the 2-chip condition index. If the conditions shown in formula (38) are opposite and the beam diameter BD on the lens is greater than two conditions index, in order to form an optical system without light blocking, a bimodal configuration must be used. On the other hand, in the two-peak system shown in Fig. 12 (b), the condition of no shading is shown in Fig. 12 (b). The distance D between the center line of the fiber and the two ends of the outer edge of the lens in the x-axis direction is D.C , DE Both must be larger than one and a half of the beam diameter BD, so the following equation must hold, that is, (Equation 39). This condition becomes a broader condition including the condition of formula (38) as described below. Here, a case where the bimodal shape is unnecessary may be described in advance. In the example of FIG. 12, the beam area on the lens surface is across both sides of the lens peak, but also consider the case where the beam area is only distributed outside the lens peak as shown in FIG. 13 (a). This case corresponds to a case where the beam diameter BD on the lens surface is sufficiently small to satisfy the conditions of Expressions (38) and (39) and also satisfy the following expression. (Equation 40)In this case, the shape of the lens does not need to be doublet, but may be a ladder shape as shown in the contour map of FIG. 13 (b) or FIG. Sex is also higher. Then there is another condition. It is related to the peak curvature radius R when making the moldp relevant person. (Equation 41)The reason is as follows. The target plano-convex lens in this embodiment is produced by a molding method. The method is a method in which a concave hole formed in a mold is pressed on a raw glass to transfer the concave shape into a convex shape of the glass. The curvature radius of the curved surface of the lens depends on the curvature radius of the hole that can be achieved by a machine tool for making the mold. It is set to 150 μm or more. That is, it means that a depth with a smaller radius of curvature below this cannot be formed. Next, the above-mentioned contents are shown in the graphs shown in FIG. 15 and FIG. 16 to describe the conditions under which the type I optical system can be constructed. First, the numerical values used in the calculation will be explained. Fiber spacing df : As the fiber periodic interval often used in fiber matrix 1, 250 μm with a general 250 μm pitch ribbon fiber is used in FIG. 15, and 127 μm, which is matrixed as an upper and lower nest, is used in FIG. 16. Wavelength λ: 1.55 μm, which is the representative value of the optical communication band. Mode radius ω0 : Set to 5.2 μm as the representative value of single-mode fiber at a wavelength of 1.55 μm. Lens refractive index nc : The refractive index distribution of the optical glass used for the lens is 1.4 from the crown glass on the low refractive index side to 2.0 on the flint glass on the high refractive index side. Therefore, consider the lens refractive index n herec It is 1.4 to 2.0. Air refractive index nv : Since the outside of the lens is usually air, it is set to 1.0. Saddle A3 width ws Distance from adjacencyn : When the lens is manufactured by the glass molding method, a lens-shaped hole is excavated from the mold. In experience, a flat portion of about 10 to 20 μm is required between adjacent holes. The reason is that if the width is narrower than this, sharp protrusions with a narrow width will be generated between adjacent holes, which will cause deformation at the high temperature and high pressure (1 MPa, 450 ° C or higher) in the molding step, which will cause damage. As the durability of the mold. Therefore, here, the width w of the saddle A3s Adjacency interval dn Both are set to 17 μm. Reflection angle: It is assumed that a dielectric multilayer film having an optical thickness of λ / 4 and a low-refractive-index transparent material and a high-refractive-index transparent material is alternately laminated for a part of the transmissive film 41. Structurally, the multilayer film is incident obliquely. Therefore, what is problematic is the polarization dependence of the transmitted tap light. For the use of SiO2 (Refractive index 1.44) as a low refractive index material and using Ta2 O5 (Refractive index 2.12) In the case of a high refractive index material, theoretically, in order to set the polarization dependence of the tap light transmitted in the C + L band (wavelength 1530 to 1625 nm) to 0.05 dB or less, the reflection must be set. angleSet it to 4 degrees or less. Therefore, here, the reflection angle is also considered in consideration of the influence caused by changes in the refractive index or film thickness during actual production.Set to 2 degrees. Figure 15 shows the fiber spacing d in the type I configuration.f In the case of 250 μm, for each peak interval dp Refractive index nc With peak curvature radius Rp The relationship is obtained by plotting the graph. According to equations (31) to (35), for each peak interval, as the refractive index of the lens increases, the refractive power of the light increases, so the peak curvature radius increases. Regarding the peak interval, as the light increases toward the center of the peak, the radius of curvature is reduced in order to maintain the same refractive power. In this graph, the three-dotted line in the graph is applied to the two-peak condition, the two-piece condition, and the mold processing condition. The two-piece condition is specified by the formula (38), the bimodal condition of the present invention is specified by the formula (39), and the mold processing conditions are specified by the formula (41). Below the value obtained based on the two-piece condition, n is an optical system that can form a two-piece optical system without shading.c -Rp region. Below the value obtained based on the bimodal condition is the n of the optical system that can form a bimodal morphology without shadingc -Rp region. Higher than the value obtained according to the processing conditions of the mold, it becomes a formable n.c -Rp region. It can be seen that the area obtained according to the two-peak condition and the mold processing conditions is wider than the area obtained according to the two-piece conditions and the mold processing conditions, and the design freedom is relaxed to more than twice. In particular, under bimodal conditions, an optical system with a larger radius of curvature can be constructed, which means that the difficulty of mold processing is lower. Figure 16 shows the fiber spacing d in the type I configuration.f In the case of 127 μm narrower than that in FIG. 15, for each peak interval dp Refractive index nc With peak curvature radius Rp The relationship is obtained by plotting the graph. As in FIG. 15, for each peak interval, as the refractive index of the lens increases, the refractive power of the light increases, so that the peak curvature radius increases. Regarding the peak interval, as the light increases toward the center of the peak, the radius of curvature is reduced in order to maintain the same refractive power. In this graph, similar to FIG. 15, the three dotted lines in the graph are those in which the two-peak condition, the two-piece condition, and the mold processing condition are applied. It can be seen at a glance that the area where the bimodal morphology can be achieved is definitely wider than the two-chip morphology. If distance from fiber df = 250 μm, as the fiber spacing df Narrow and achievable nc -Rp The area is also narrowed. The area where the bimodal shape can be realized becomes a triangular area surrounded by the dotted line of the bimodal condition and the mold processing condition.c It cannot be configured when it is 1.44 or less. However, when the refractive index of BK7, which is the representative of borosilicate glass with higher reliability, is 1.501, although the peak interval dp It has a narrow width of 91.7 to 95.6 μm, but it can constitute an optical system, and it can be seen that the bimodal shape can cope with miniaturization. On the other hand, as for the two-chip condition, only nc It is realized in an extremely limited area of 1.81 or more and a peak interval of 105 to 107 μm. This high-refractive-index region is a region that causes problems such as the occurrence of yellowing in terms of reliability. It has to be said that the practical applicability is low, and it can be considered as df At 127 μm, a two-piece configuration cannot be applied. (Fifth Embodiment) Fig. 17 shows an optical system according to this embodiment. In this embodiment, the optical fibers 11A and 11B are arranged on the flat surface 21 side of the plano-convex lens, and the partially reflecting portion 4 is arranged on the convex surface 23 side of the plano-convex lens. The end faces of the optical fibers 11A and 11B are arranged at a first position P1 and a second position P2, respectively. The length direction of the optical fibers 11A and 11B is on a specific plane PC Center axis A of internal and plano-convex lensesC Parallel configuration. The plano-convex lens of this embodiment has a first aspherical surface A1 and a second aspherical surface A2 on the convex surface 23. The light emitted from the end surface of the optical fiber 11A enters the plano-convex lens from the flat surface 21. The light incident on the plano-convex lens passes through the plano-convex lens and exits from the first aspheric surface A1 into the air layer 3. At this time, the first aspherical surface A1 makes the light emitted into the air layer 3 be parallel light. The light that becomes parallel light on the first aspherical surface A1 passes through the air layer 3 and is partially reflected toward the second aspheric surface A2 at one point P3 of the reflecting surface that partially transmits the film 41. The parallel light reflected by the partial reflection portion 4 enters the plano-convex lens from the second aspherical surface A2. The second aspherical surface A2 condenses the parallel light reflected by the partial reflection portion 4 to the second position P2. Thereby, the parallel light reflected by the partial reflection portion 4 is incident on the optical fiber 11B. In the plano-convex lens of this embodiment, the second aspherical surface A2 condenses the parallel light reflected by the partial reflection portion 4 to the second position P2, so that the light after tapping the monitoring light can be efficiently coupled with the optical fiber 11B. (Sixth Embodiment) FIG. 18 shows a configuration example of an optical fiber matrix module according to this embodiment. The optical fiber matrix module of this embodiment includes: a lens matrix 2 in which a plurality of convex surfaces 23-1 to 23-4 are arranged in a fifth embodiment; and an optical fiber in which a plurality of optical fibers 11A and 11B are arranged in a fifth embodiment. Matrix 1. The optical fiber matrix 1 and the lens matrix 2 indicate that the four optical fiber-lens optical systems of the fifth embodiment are arranged side by side on a specific plane PC The example above. The lens matrix 2 functions as a first lens matrix. The lens matrix 2 includes a plurality of plano-convex lenses according to the fifth embodiment. Each of the plano-convex lenses included in the lens matrix 2 includes a fiber-lens optical system according to the fifth embodiment as a basic unit. Optical axis A is the central axis of each plano-convex lensC Arranged side by side on a specific plane PC Inside. The optical fiber matrix 1 has two optical fibers 11A and 11B for each of the convex surfaces 23-1 to 23-4. Spacers 22 are provided at both ends of the lens matrix 2 to maintain the distance between the lens matrix and the partial transmission portion 4 at a specific value. The spacer 22 may be formed in advance with a concave portion corresponding to the lens in a mold simultaneously with forming the concave portion corresponding to the lens, and then formed by a molding method simultaneously with forming the lens, or may be in the form of sandwiching a plate of a specific thickness. The optical system of FIGS. 17 and 18 will be described with reference to FIG. 19. The following directions are described following the orthogonal xyz coordinate axes in the figure. At the left end of the figure, it is arranged in the xz plane parallel to the z axis in the x axis direction at equal intervals df Arrayed fiber matrix 1. The optical fiber matrix 1 has a plane that is parallel to the x-axis and has a specific angle with respect to the y-axis as an end surface, and is configured, for example, by being held by a casing such as TEMPAX glass. Furthermore, in FIG. 19, unlike the optical systems of the first and second embodiments, the flat surface 21 side of the lens matrix 2 is directly attached to the end face of the optical fiber 1, and the convex surface 23 of the fiber matrix 1 has a double period. The side faces the opposite side of the flat surface 21. The relative position of the fiber matrix 1 and the lens matrix 2 is set in such a manner that, in the x-axis direction, the optical axis A of the plano-convex lensC The center lines of the adjacent fibers of the optical fiber matrix 1 (the center lines of the first optical fiber 11A and the second optical fiber 11B in the figure) are the same, and in the y direction, the optical axis A of the lensC The plane formed by the matrix is consistent with the plane formed by the center line of the fiber matrix 1, and in the z direction, the distance between the end face of the fiber matrix 1 and the convex vertex of the lens matrix 2 and the focal length f of the concave side of the plano-convex lensc Consistent. On the right side of FIG. 19, the air layer 3 with a certain interval is perpendicular to the optical axis AC A partial transmission film 41 having a function of reflecting / transmitting light of a specific wavelength at a desired ratio is provided in parallel with the z-axis. In the first and second embodiments, a part of the transmissive film 41 is directly mounted on the flat side of the lens matrix 2, but in this embodiment, it is individually mounted on a glass substrate 42 having the same refractive index as the lens matrix 2. In addition, in this configuration, the path of light emitted from the end face P1 of the first optical fiber 11A is approximately studied with light rays. Since the end face P1 of the first optical fiber 11A is located on the concave focal plane, the light emitted from the end face P1 of the first optical fiber 11A from there and emitted from the corresponding convex surface 23 of the lens matrix 2 is directed toward the optical axis A.C Side refraction while becoming with the optical axis AC At an angleThe parallel rays of light travel in the air layer 3. Among them, from the fiber end P1 and the optical axis AC When the light rays emitted in parallel, that is, the central light rays of the emitted light reach the partially transmitted film 41, they pass through the focal point of the convex side corresponding to the first aspherical surface A1. The thickness of the air layer 3 is set exactly to the convex focal length fv And the part becomes a flat surface, and a part of the transmissive film 41 is applied to the part. Therefore, a part of the specific intensity of the parallel light is transmitted through the part of the transmissive film 41 and relative to the optical axis AC forThe angle is straight, but the remaining intensity is partially reflected by the partially transmitting film 41 and is relative to the optical axis A.C The symmetrical x-direction position reaches the surface of the lens matrix 2 again. The reflected light that has reached the surface of the lens matrix 2 is parallel light that passes through the focal point of the convex side, and is along the optical path that exits from the first optical fiber 11A and is incident from the surface of the lens matrix 2 with respect to the optical axis A.C Symmetric path, finally focused to a position relative to the optical axis AC An end face of the second optical fiber 11B at a position symmetrical to the first optical fiber 11A. Here, if the thickness of the air layer 3 is set to the convex side focal length fv Thin, the thickness of reflected parallel light is f compared to air layer 3v Optical axis AC The side surface is here where the parallel light is not bundled and further diffuses on the end face of the second optical fiber 11B. On the other hand, the thickness of the air layer 3 is thicker than fv In this case, the reflected light further reaches the outer surface of the lens, and the parallel light is excessively collected, and as a result, it diffuses on the end surface of the second optical fiber 11B. In either case, the optical axis of the reflected light is offset from the optical axis of the second optical fiber 11B. Therefore, an important point in this embodiment is that the distance between the end faces of the first and second optical fibers 11A and 11B and the convex apex of the plano-convex lens is set to the concave focal length f.c The distance between the plano-convex lens and the partially transmitting film 41 is the convex side focal length fv . In addition, as shown in FIG. 19, the light transmitted by the partially transmitting film 41 is shown in FIG. 19. If the refractive index n of the substrate to which the partially transmitting film 41 is attached and the refractive index n of the lens matrix 2 are made,c The same, although not shown in the figure, it is emitted at an angle ψ. In addition, if the glass substrate 42 to which a part of the transmissive film 41 is attached is a parallel substrate, when it is finally emitted to the air layer 3 at an angleShoot out. In addition, when a low-loss coupling is desired between the optical fibers 11A and 11B with such a reflection optical system, the surface shape required by the convex surface 23 is generally called an aspheric surface. The aspheric shape is different depending on the setting form of the optical system, and the method for obtaining the aspheric shape in this embodiment will be described with reference to FIG. 20. In FIG. 20, for convenience of description, it is described that light is emitted from the second optical fiber 11B, but the optical system is relative to the optical axis A.C Symmetry, so this is not a compromise on rationality. As shown in the figure, the setting includes the optical axis AC The xz plane, and the lens curved surface as the rotation curved surface with the z axis as the axis of symmetry, and the shape of the xz section as Z (x). The optical system set here is a model in which the third quadrant in the xz plane is placed parallel to the z-axis and placed on the concave side focal distance f from the x-axis.c The light emitted from the second optical fiber 11B at an upward position at an angle of θ is refracted at the intersection with the hypothetical curve Z (x), and reflected at the reflection angle illustrated in FIG. 20Travel in the air layer 3. The above formula (1) holds based on Snell's law of the refracting portion. If the angle formed by the tangent to the curve Z (x) of the light incident position and the x-axis is set to θt , According to the angular relationship in FIG. 20, it is easy to know that there is a relationship of the following formula, that is, (Equation 18). From the formulas (1) and (18), the following formula holds. (Equation 19)Here, because the angle θt Since the tangent angle of the curve Z (x), the above formula (4) holds. In addition, the outgoing light from the optical fiber 11B and the optical axis AC The tangent of the formed angle θ satisfies the following formula, that is, (Equation 20). By changing θ of equation (4)t Θ of equation (20) is substituted into equation (19) to obtain a differential equation related to Z (x). Calculate the curve according to the boundary conditions of formula (4), formula (19) to formula (20), and the origin (0,0) of the following formula, that is, (numerical formula 21)However, it becomes a complex nonlinear differential equation that cannot be solved analytically, and is obtained by approximate calculation. At this time, since it may be solved analytically, the function form is determined based on this in advance. Cases that can be solved analytically are the optical fibers 11A and 11B and the lens optical axis AC Consistent situation. On the optical fibers 11A and 11B and the lens optical axis AC In the same situation, the reflection angle of Figure 20f When it becomes zero, Z (x) is obtained analytically and becomes an ellipse of Formula (22). [Equation 22]Here, Ce Is a curvature, and is the following formula, that is, (Equation 23), Ke Is a conic constant, and is the following formula, that is, (Equation 24). As in this embodiment, the optical fiber 11B is from the optical axis AC In the case of a shift, it is assumed that Equation (22) is used as the basic equation and an approximation term based on the polynomial shown below is added. [Equation 25]Here, n is an integer of 2 or more, and B3 , B4 , ... B2n - 1 , B2n Aspheric coefficient. After determining the number of times corresponding to the target accuracy in equation (25), substitute equations (4), (19), and (20) to calculate the residual error, and find the curvature C that is the global solution according to the damping least square method.e Cone constant Kh , And aspheric coefficient B2n - 1 , B2n Combination. If the coefficient value in formula (25) is specified, the surface shape can be processed in the mold. The coefficient to be specified can be determined by equations (4), (19) to (20). Even without such calculations, the possibility can be verified. First, the names and symbols of the parameters shown in FIGS. 19 and 20 are shown in the left column of FIG. 21. These are the same as FIG. 5 related to the first embodiment, but the major difference is that the orientation of the lens matrix 2 with respect to the fiber matrix 1 is reversed, and the reflection angleThe magnitude relationship with the lens center incident angle ψ is also reversed. In FIG. 19 and FIG. 20, the light emitted from the first optical fiber 11A having an end surface directly adjoining the concave focal surface and emitted from the lens surface through a plano-convex lens becomes the optical axis A.C PresentAngle of parallel light. Therefore, for these rays to enter the lens optical axis AC The light at the intersection with the lens surface, because the tangent plane of the lens surface is exactly perpendicular to the optical axis AC The parallel z-axis, so the incident angle ψ and the exit angle of the lens center of the lightWith refractive index nv , Nc In the meantime, Snell's law holds, that is, (Equation 26). Since the fiber matrix 1f Matrix, and lens matrix 2 is 2d twicef Matrixization, so if the fiber spacing d is givenf Incident angle ψ and exit angle from lens centerValue, the focal length f on each of the convex and concave sidesv , Fc It is determined by the following formulas (27) and (28). (Equation 27)(Equation 28)In the above formulas (26) to (28), no approximate operation is added and the formula is strict, and the optical axis A that satisfies this relationship isC The surface of rotation that is the axis of symmetry becomes a higher-order surface based on a rotating ellipse. Determine the two focal lengths f of the convexo-concave of the plano-convex lens according to equations (27) and (28)v , Fc That is, the distance between the optical fibers 11A and 11B and the plano-convex lens and the thickness of the plano-convex lens are determined. The limiting factors of such an optical system are the same as those of the second embodiment. Trying to substitute these equations (26) to (28) into actual possible values, and also using the above equations (14) and (15) to calculate the values below the lens center incident angle ψ in Figs. 19 and 20 This is the estimation example of FIG. 21. Fiber spacing df Choose 250 μm and 127 μm, and the refractive index of the lens is 1.501. The refractive index of the glass with high weather resistance is 1.501. Second, the reflection angleThis embodiment considers the application of an optical tap module using a fiber pair consisting of optical fiber 11A and optical fiber 11B as the main optical path, and a part of the transmissive film 41 being a so-called tap film that reflects more than 90% and transmits a few%. It is set at an angle at which part of the transmitted light does not produce polarization dependence. At fiber spacing df For 250 μm and 127 μm, the convex focal length fv It is 889.4 μm and 451.8 μm. At this time, the diameter BD of the light beams emitted from the optical fiber 11A on the lens surface becomes smaller than the fiber interval d, respectively.f 214.6 μm, 109.0 μm, so this light does not touch the adjacent lens. Also, because the optical axis A of the lens surfaceC The approximate radii of curvature of the upper spheres are 445.6 μm and 226.4 μm, so they sufficiently exceed the mechanical processing limit of the mold, that is, 150 μm, and can be used for mold lens processing. In short, it can be seen that the structures shown in Figs. 17, 18, and 19 can also be realized. Here, the limitation of the beam diameter BD of the incident light emitted from the optical fiber on the surface of the lens matrix 2 shown in FIG. 5 and FIG. 21 and the conditions of the radius of curvature used for mold processing will be described. The refractive index of oxide glass that can be molded by a mold reaches n at a value of 1.55 μmc = 1.426 to 2.068. From Equations (1) to (15) and Equations (26) to (28), it can be confirmed that (for example, Sumita Optical Glass: Glass Catalogue Ver.9.01), the fiber spacing d listed in Figs. 5 and 21f Refractive index nv , And reflection angleRefractive index nc These conditions are always met within the scope. (Seventh embodiment) Fig. 22 shows an optical system according to this embodiment. The plano-convex lens 2 of this embodiment is a bi-modal bi-modal lens of which the first aspherical surface A1 and the second aspherical surface A2 are convex in the fifth and sixth embodiments. In the seventh embodiment and the eighth embodiment, the first aspherical surface A1 is referred to as a first convex surface A1, and the second aspheric surface A2 is referred to as a second convex surface A2. The shape and manufacturing steps of the convex surface 23 of this embodiment are the same as those of the third embodiment and the fourth embodiment. (Eighth Embodiment) Fig. 23 shows a configuration example of an optical fiber matrix module according to this embodiment. The optical fiber matrix module of this embodiment is a plano-convex lens 2 of the seventh embodiment applied to the convex surfaces 23-1 to 23-4 of the optical fiber matrix module of the sixth embodiment. The optical system of FIGS. 22 and 23 will be described with reference to FIG. 24. The following directions are described following the orthogonal xyz coordinate axes in the figure. At the left end of the figure, a period interval d is arranged in the xz plane parallel to the z axis in the x axis direction.f An optical fiber matrix 1 in which optical fibers are arranged. The optical fiber matrix 1 has a plane that is parallel to the x-axis and has a specific angle with respect to the y-axis as an end surface, and is configured, for example, by being held by a casing such as TEMPAX glass. Furthermore, in FIG. 24, unlike the optical systems of the third and fourth embodiments, the flat surface 21 side of the bimodal lens matrix 2 is directly attached to the end face of the optical fiber matrix 1, and the double period of the optical fiber matrix 1 The bimodal convex surface 23 side faces the opposite side of the flat surface 21. The bimodal convex surface 23 has a lens central axis A parallel to the z-axisC , And the plane perpendicular to the z-axis is the common plane, and the period of the fiber-optic matrix 2 is 2d in the x-axis direction, and the interval is 2df And separated from adjacent lenses by an adjacent interval dn And matrix. The bimodal convex surface 23 is composed of a first convex surface A1 and a second convex surface A2. The first convex surface A1 is a curved surface that is centered on a line R1 that is included in a surface Pc formed by the fiber matrix and is parallel to the z-axis, and functions as a lens. The optical axis of the first optical fiber 11A is shifted inward (on the center axis Ac side) by a specific distance. The second convex surface A2 is formed in a shape symmetrical to the first convex surface A1 with the saddle portion of the width ws with respect to the lens central axis Ac. The interval between the rotation centerlines R1 and R2 of the first and second convex surfaces A1 and A2 is the peak interval d.p Set to df A small specific length of distance. The convex side of the bimodal lens matrix 2 is provided with a partially transmitting portion 4 having a partially transmitting film 41 perpendicular to the z-axis with the air layer 3 interposed therebetween. As shown in the figure, the thickness of the air layer 3 is set so that the distance between the bi-convex convex surface 23 and the opposite part of the transmissive film 41 is thicker than the convex side focal length f.v Reflective layer thickness tr . The relative position of the fiber matrix 1 and the bimodal lens matrix 2 is set in such a manner that, in the x-axis direction, the central axis A of the bimodal lensC The center lines of the adjacent fibers of the optical fiber matrix 1 (the center lines of the first optical fiber 11A and the second optical fiber 11B in the figure) are the same, and in the y direction, the central axis A of the lensC The plane formed by the matrix is consistent with the plane formed by the center line of the fiber matrix 1, and in the z direction, the distance between the end face of the fiber matrix 1 and the convex vertex of the bimodal lens matrix 2 and the focal length f of the concave side of the plano-convex lensc Consistent. On the right side of FIG. 24, the air layer 3 with a certain interval is perpendicular to the center axis AC A partial transmission film 41 having a function of reflecting / transmitting light of a specific wavelength at a desired ratio is provided in parallel with the z-axis. In the third and fourth embodiments, a part of the transmissive film 41 is directly mounted on the flat side of the lens matrix 2, but in this embodiment, it is individually mounted on a glass substrate 42 having the same refractive index as the lens matrix 2. In addition, in this configuration, the path of light emitted from the end face of the first optical fiber 11A is approximately studied with light rays. Since the end face of the first optical fiber 11A is located on the concave focal plane, and the centerline R1 of the first convex surface A1 in the bimodal convex surface is shifted in the x direction relative to the fiber centerline as described above, The end surface P1 is a point light source, and the light emitted from the end surface P1 and incident on the first convex surface A1 of the lens matrix 2 is directed toward the central axis A.C Side refraction, with the central axis AC At a specific angleThe parallel rays of light travel in the air layer 3. Among them, the ends of the optical fibers 11A and 11B and the central axis AC That is, the light rays emitted in parallel with the z-axis, that is, the central rays of the emitted light, pass through the convex focal point after being emitted from the bimodal lens. As described above, since the thickness tr Thicker than the focal length fv And part of the transmissive film 41 is located at the above-mentioned central light and the lens central axis Ac The point of intersection, therefore, a part of the specific intensity of the parallel light is partially transmitted through the film 41 and is relative to the central axis AC Straight forward at an angle of ψ, but the rest of the intensity is reflected by the partially transmitting film 41, relative to the central axis AC The symmetrical x-direction position reaches the second convex surface A2. The reflected light that has reached the second convex surface A2 is parallel light that passes through the focal point of the convex side, and is along the optical path that exits from the first optical fiber 11A and enters the first convex surface A1 with respect to the central axis A.C Symmetric path, finally focused to A relative to the central axis AC An end face P2 of the second optical fiber 11B at a position symmetrical to the first optical fiber 11A. Here, if the thickness of the air layer 3 is set to be thicker than the thickness t of the reflective layerr Thin, the parallel light is reflected on the second convex surface A2, compared to the thickness of the air layer 3 is tr Optical axis AC On the side surface, the parallel light beam is insufficiently condensed there and further diffuses on the end surface of the second optical fiber 11B. On the other hand, the thickness of the air layer 3 is thicker than tr In this case, the reflected light further reaches the outer surface of the lens, and the parallel light is excessively collected, and as a result, it diffuses on the end surface of the second optical fiber 11B. In any case, the optical axis of the reflected light is offset from the optical axis of the second optical fiber 11B. Therefore, the important point in this embodiment is that the distance between the end faces of the first and second optical fibers 11A and 11B and the convex apex of the bimodal lens is set to the concave focal length f.c And the distance between the bimodal lens and the partially transmitting film 41 is a specific reflection layer thickness tr . In addition, as shown in FIG. 24, the light transmitted by the partially transmitting film 41 is shown in FIG. 24. If the refractive index of the substrate to which the partially transmitting film 41 is attached and the refractive index n of the lens matrix 2c The same, although not shown in the figure, it is emitted at an angle ψ. In addition, if the glass substrate 42 to which a part of the transmissive film 41 is attached is a parallel substrate, when it is finally emitted to the air layer 3 at an angleShoot out. Next, the above description is formulated using a formula. In FIG. 24, the light rays emitted from the first optical fiber 11A having the end surface on the concave focal surface and entering the first convex surface A1 of the bimodal lens convex surface 23 through the lens matrix 2 become the lens central axis A.C PresentAngle of parallel light. Among these rays, the rays incident on the peak of the first convex surface A1 (the intersection point of the central symmetry line R1 and the first convex surface), because the tangent plane of the lens surface of the incident point is perpendicular to the central axis AC , So the incident angle ψ and the exit angle at the center of the peak of the lightAnd refractive index nv , Nc In between, Snell's law holds, that is, (Equation 42). Since the fiber matrix 1f Matrix, and lens matrix 2 is 2d twicef Matrix, so the focal length f on each side of the concave and convex sidesc , Fv Based on fiber spacing df Peak interval d between the first convex surface A1 and the second convex surface A2p , Lens center incident angle ψ, and exit angleThe value is determined by the following equations (43) and (44). (Equation 43)(Equation 44)The thickness t of the reflective layerr Similarly, the following formula holds: (Equation 45). The first and second convex surfaces A1 and A2 constituting the double peaks may all satisfy the above formulas (42) to (45), but satisfy these relationships and be parallel to the lens central axis A.C The curved surface whose axis is the axis of symmetry becomes a higher-order curved surface based on a rotating ellipse, and is generally called an aspheric surface. If fiber spacing d is givenf Lens peak interval dp Lens refractive index nc Refractive index nv , And reflection angle, The two focal lengths f of the asperity of the bimodal lens are determined according to equations (43) and (44).c , Fv To determine the thickness f of the lensc And the thickness t of the air layer 3 is determined according to formula (45)r . Next, the conditions for establishing such an optical system will be described. In order to achieve the low-loss coupling between the first optical fiber 11A and the second optical fiber 11B, it is necessary to suppress the shading of the lens surface as much as possible. The outgoing light from the first optical fiber 11A is diffused according to the NA of the optical fiber, but the diffusion often manifests as the transmission of a Gaussian beam with the fiber end as the waist position of the beam. The power of the Gaussian beam exiting from the fiber end and reaching the lens surface is distributed from the center of the beam to 1.73 times the beam radius ω to become 99.75% of the total power. Therefore, if the range so far is set to the beam diameter BD of the light beam reaching the lens surface 23, it is given by the following formula, that is,. Here, ω0 And λ are the mode radius of the optical fiber 11A and the wavelength of light, respectively. Secondly, the conditions required for the beam diameter BD of the lens surface of type II are the same as those for the type I described above, and the conditions are the same as those of formulas (38) and (39). However, the peak curvature radius Rp The required condition is replaced by the following formula, that is, (Equation 47). Based on the above, regarding the configuration of type II, the peak interval d is the same as that of type I.p With beam diameter BD, peak curvature radius Rp (According to equation (47)) and the graph of the relationship between the two condition indexes are shown in Figs. 25 and 26. The value used in the calculation is the same as the type I described in the third and fourth embodiments. Figure 25 shows the fiber spacing d in the type II configuration.f In the case of 250 μm, for each peak interval dp Refractive index nc With peak curvature radius Rp The relationship is obtained by plotting the graph. According to equations (42) to (44) and equations (46) to (47), for each peak interval, as the refractive index of the lens increases, the refractive power of the light increases, so the peak curvature radius increases. Regarding the peak interval, as the light increases toward the center of the peak, the radius of curvature is reduced in order to maintain the same refractive power. In this graph, the three-dotted line in the graph is applied to the two-peak condition, the two-piece condition, and the mold processing condition. The two-piece condition is specified by formula (38), the bimodal condition is specified by formula (39), and the mold processing conditions are specified by formula (47). Below the value obtained based on the bimodal condition is the n of the optical system that can form a bimodal morphology without shadingc -Rp region. Below the value obtained based on the two-piece condition, n is an optical system that can form a two-piece optical system without shading.c -Rp region. Higher than the value obtained according to the processing conditions of the mold, it becomes a formable n.c -Rp region. It can be seen that the area obtained according to the two-peak condition and the mold processing conditions is wider than the area obtained according to the two-chip conditions and the mold processing conditions, and the design freedom is relaxed to about 2 times. In particular, under bimodal conditions, an optical system with a larger radius of curvature can be constructed, which means that the difficulty of mold processing is lower. Figure 26 shows the fiber spacing d in the type II configuration.f For the case of 127 μm narrower than that in FIG. 25, the interval d for each peak isp Refractive index nc With peak curvature radius Rp The relationship is obtained by plotting the graph. From equations (42) to (44) and equations (46) to (47), as in FIG. 25, for each peak interval, as the refractive index of the lens increases, the refractive power of the light increases, so the peak radius of curvature Increase. Regarding the peak interval, as the light increases toward the center of the peak, the radius of curvature is reduced in order to maintain the same refractive power. In this graph, as in FIG. 25, the conditions of Expressions (38) to (39) and (47) are applied as three dotted lines in the graph. It can be seen at a glance that the area where the bimodal morphology can be achieved is definitely wider than the two-chip morphology. If distance from fiber df = 250 μm, as the fiber spacing df Narrow and achievable nc -Rp The area is also narrowed, and the area where the bimodal shape can be realized becomes a triangular area surrounded by a dotted line of the bimodal condition and the mold processing condition, and cannot be constituted when the lens refractive index nc is 1.44 or less. However, when the refractive index of BK7, which is a representative glass material of borosilicate glass with higher reliability, is 1.501, although the peak interval dp It has a narrow width of 103.5 to 106.1 μm, but it can constitute an optical system, and it can be seen that the bimodal shape can cope with miniaturization. On the other hand, under two-chip conditions,c A limited area of 1.64 or more and a peak interval of 111 to 116 μm is also achieved. This high-refractive-index region also includes regions that cause problems such as the occurrence of yellowing in terms of reliability. It has to be said that the practical applicability is quite low, and it can be considered as df At 127 μm, only two-piece morphology can be used to a very limited extent. In the above, if two pieces are compared with the bimodal structure, the following can be described. In consideration of 2 main parameters, the lens refractive index nc With peak curvature radius Rp In this case, the bimodal composition system nc -Rp The area is about two to three times that of the two-piece structure, and the design freedom is high. Double-peak configuration can also cope with narrower fiber spacing df And suitable for miniaturization. Bimodal composition due to peak curvature radius Rp A larger value can be selected to increase the lens diameter, so the coupling efficiency between fibers can also be maintained higher. The bimodal structure is easier to make because the radius of curvature of the hole when making the mold is larger. For the differences between Types I and II, at the fiber spacing df In the case of 250 μm, the two conditions are approximately equal to each other.p The area is 14.2 to 14.3 μm. On the other hand, in terms of bimodal conditions, it can be seen that the peak interval d of the type I system isp It allows the width to be expanded by about 1.5 times, making it easy to make lenses. Especially at fiber spacing df In the case of 127 μm, type dp The allowable width is 3.9 μm. In contrast, the allowable width of Type II is only 2.6 μm. The difference of 1 μm or more of the allowable width is very large in terms of mold making, and Type I is relatively easy to make. (Ninth Embodiment) Fig. 27 shows an example of an optical fiber matrix module according to this embodiment. The fiber matrix module shown in FIG. 27 includes the fiber matrix module shown in FIG. 2, a light shielding plate 7, and a lens matrix 9. The light shielding plate 7 functions as an optical component, and the lens matrix 9 functions as a second lens matrix. The fiber matrix module of this embodiment may also be a fiber matrix module of the fourth embodiment shown in FIG. 10. The light shielding plate 7 has a plurality of through holes 71. Each parallel light transmitted through the reflecting surface of the partially transmitting film 41 is incident on one end of a different through hole 71. Then, the parallel light that has passed through the through-holes 71 is emitted from the other end of each through-hole 71. The lens matrix 9 condenses each light emitted from the other end of the plurality of through holes 71 to a point defined for each of the through holes 71. Just set the optical function element at this point. An example of the light receiving module of this embodiment is shown in FIG. 28. The light receiving module shown in FIG. 28 includes the optical fiber matrix module shown in FIG. 27 and a light receiving element matrix 8. Each light-receiving element 81 provided in the light-receiving element matrix 8 receives each light condensed by the lens matrix 9. The light receiving module shown in FIG. 28 can be used as a 4-matrix light tap monitoring module. The application area of this embodiment is, for example, an optical communication system with a wavelength of 1.55 μm. The module includes a fiber matrix 1, a lens matrix 2, a partially reflecting portion 4 having a partially transmitting film 41, a light shielding plate 7, a lens matrix 9, and a light receiving element matrix 8 from the left side of the figure. For fiber spacing df Each of the parameters, as an example, can be realized in reality if the values shown in FIG. 5 are used. First, the operation and function of the module will be described. 95% of the light incident from the optical fiber 11A to the lens matrix 2 is partially transmitted through the film 41 at a reflection angle(5 degrees) is reflected and incident on the second optical fiber 11B, and 5% of the incident light intensity is tapped and returned to the main line. The 5% -intensity tapped light system becomes the air layer at the rear and emits at an exit angle ψ (7.5 degrees). However, in the rear section of the partially transmitted film 41, in order to prevent the reduction of crosstalk caused by the mixing of tap lights in space transmission, A light shielding plate 7 provided with a through hole 71 is provided. The light shielding plate 7 has a size matching the external shape of the lens matrix 2, and a through hole 71 having a beam diameter is provided at a central portion of the light shielding plate 7 in cooperation with the tap optical path. A lens matrix 9, which is the same as the lens matrix 2, is provided in the rear stage of the light shielding plate 7 opposite to the lens matrix 2. The lens matrix 9 condenses the tap beam transmitted and diffused in space to the light receiving surface of the light receiving element 81. Each of these constituent elements will be described below. Fiber Matrix 1: Fiber Matrix 1 uses 250 μm spaced 8 matrix wavelength 1.3 / 1.55 μm single-mode ribbon fibers as fiber components. They were arranged on a TEMPAX glass, 60-degree V-groove plate with a thickness of 1 mm, covered with a 1 mm-thick top cover, fixed with a UV (Ultraviolet) adhesive, and polished at the end surface to produce a fiber matrix 1 for connection. The matrix spacing is the same as the ribbon fiber used is 250 μm. The optical axis of the optical fiber is the z-direction in FIG. 28, and the end faces connected to other components are parallel to the x-axis, and in order to reduce the return light caused by the end-face reflection, it is set to be inclined 8 degrees from the y-axis direction. Moreover, the angle of the core end surface with respect to the optical axis of the fiber is not limited to 8 degrees. An AR (Anti-Reflection) coating with a wavelength of 1.55 μm is applied to the end surface inclined at 8 degrees. Full width is 4 mm. Lens matrix 2: It is composed of borosilicate glass with a refractive index of 1.501 at a wavelength of 1.55 μm, and is on the upper surface of a flat glass with a thickness of 13,690 m (z direction), at the center of 4000 × 2000 μm (x × y) A convex surface 23 having a first aspherical surface A1 and a second aspherical surface A2 is formed at a matrix interval of 500 μm. A flat portion having a thickness of 1 μm is provided between the adjacent convex surfaces 23, and the amount of depression, that is, the amount of depression from the flat portion (lens holding surface) is, for example, 69 μm. Spacers 22 are integrally formed at both ends in the x direction of the lens matrix 2 during the lens molding process. The spacer 22 is a trapezoidal convex portion, the surface of which is an angle that matches the inclined end face of the optical fiber matrix 1 by 8 degrees, and its area is, for example, 1 × 1.5 mm (x × y) on one side. The height of the spacer 22 is preferably such that, for example, the lens optical axis position (Ac) becomes a specific convex-side focal length f.v (Here is 947.3 μm). Here, the angle of the spacer 22 will be described with reference to FIG. 33. Normal line L at the core end face of the optical fiber 11n The angle with respect to the optical axis of the optical fiber 11, that is, the z-axis is set to θ1 , The center light of the light emitted from the core end face of the optical fiber 11 to the air layer 3 is relative to the core end face normal Ln The angle is set to θ2 In the case, according to Snell's law, the angle θ1 With angle θ2 The following relationships are satisfied. (Equation 51)Here, nf Refractive index of transmitted light of the optical fiber 11. Therefore, in nf Is 1.445, the refractive index n of the air layer 3c Is 1 and the angle θ1 When set to 8 degrees, the angle θ2 It was 11.6 degrees. The case where the optical coupling between the optical fiber and the lens system becomes the highest efficiency is the case where the outgoing light from the optical fiber 11 is perpendicular to the lens surface. In this case, as is clear from FIG. 33, the angle between the lens-side flat surface 22B of the spacer 22 and the inclined end surface 22A of the fiber matrix side, that is, the inclination angle of the spacer 22 also θ2 Equal to 11.6 degrees. From another perspective, the angle θ of the spacer 222 Becomes the angle θ other than the end face of the optical fiber 111 In addition to (8 degrees), an angle obtained from the refraction angle (3.6 degrees) of the optical fiber optical axis (z-axis) in the air layer 3 is added. An incident angle is attached to the flat surface 21 of the lens matrix 2The transmission film 41 is set to 5 degrees. The reflection / transmission ratio is preferably 95% / 5%. As the material, for example, SiO formed by ion beam assisted evaporation can be exemplified.2 -TiO2 Multilayer film. Light-shielding plate 7: The light-shielding plate 7 is composed of a rectangular infrared-absorbing glass having a shape of 4000 × 2000 × 1000 μm. In the central part, as shown in FIG. 27 and FIG. 28, a 30 μm square through hole 71 is formed in parallel with the xz plane in parallel with the xz plane to form an angle of incidence ψ of the lens center, i.e., 7.5 degrees with the z-axis direction. . The x-direction matrix pitch is 500 μm, which is the same as the lens matrix 2. When the beam diameter of the tap light is 227.4 μm as shown in FIG. 5, it is transmitted without being in contact with the wall of the through hole 71 of the light shielding plate 7, but is generated by the reflection and transmission of the lens matrix 2 or a part of the transmission film 41 in the previous stage. The diffuse reflection component caused by the irregular structure is prevented by the light shielding plate 7 and prevents the light receiving element matrix 8 from reaching the crosstalk. Lens matrix 9: Here, the lens matrix 9 is the same as the lens matrix 2. Generally, the light receiving surface of the light receiving element 81 is about 1 mm away from the package surface. Therefore, a focal length adjustment resin 91 is inserted between the lens matrix 9 and the light receiving element matrix 8 to make it longer focal length than the lens matrix 2 and the light receiving element matrix 8 The light-receiving surface of the middle light-receiving element 81 condenses light. The orientation of the lens matrix 9 is opposite to that of the lens matrix 2 in order to fill the space between the lens matrix 9 and the light receiving element matrix 8 with the focus adjustment resin 91. The lens matrix 9 is preferably applied with an AR coating only on the flat surface 21 side. Light receiving element matrix 8: The light receiving element 81 is, for example, an InGaAs photodiode matrix having a light receiving diameter of 80 μm and a 500 μm pitch 4 matrix. The diode matrix is sealed, and the distance from the package surface to the light receiving portion of the light receiving element 81 is 1 mm. As can be seen from the side view shown in FIG. 28, the light receiving element matrix 8 is connected to the lens matrix 9 obliquely from the z-axis direction, that is, the optical axis. As shown in the side views of FIG. 27 and FIG. 28, since the connection interface from the fiber matrix 1 to the light receiving element matrix 8 remains inclined, it has a structure that prevents reflected return light. Assembly steps: The steps have 3 steps. The first step is the connection of the fiber matrix 1 and the lens matrix 2. This is connected by the same steps as the usual fiber waveguide connection: In the fiber waveguide connection device, the aligning light is incident from the two ends of the fiber matrix 1, namely, the optical fiber 11A-1 and the optical fiber 11A-4, while monitoring from the optical fiber 11B-1 2. The light side of the optical fiber 11B-4 is fixed by 2-axis alignment. The connection portion is between the spacer 22 and the optical fiber matrix 1. The second step is the connection of the light shielding plate 7, the lens matrix 9, and the light receiving element matrix 8. These connections are sequentially arranged under the microscope with a light-receiving element matrix 8, a lens matrix 9, and a light-shielding plate 7, so that the light-receiving surface of the light-receiving element 81 can be seen through the through-hole of the light-shielding plate 7, and the core is aligned by visual alignment. And fixed with adhesive. The third step is to make the alignment light incident on the optical fibers 11A-1 and 11A-4, while monitoring the output of the light receiving element matrix 8 while attaching the lens matrix 2 with the optical fiber matrix 1 and the light receiving element matrix 8 and the lens matrix 9 The light shielding plate 7 is connected and fixed. Characteristics: The characteristics of the manufactured 4 ch tap monitoring module at a wavelength of 1.55 μm are an insertion loss of 0.4 to 0.5 dB, a reflection attenuation of 46 dB or more, and a light receiving sensitivity of 50 to 60 mA / W. Adjacent crosstalk is also above 45 dB. FIG. 34 shows another form of the optical fiber matrix module of this embodiment. The fiber matrix module shown in FIG. 34 has an AR plate 101 attached to the end face of the fiber matrix 1, and includes a GRIN (Graded Index) lens matrix 109 instead of the light shielding plate 7 and the lens matrix shown in FIG. 27. 9. The fiber matrix module may also be the fiber matrix module of the fourth embodiment shown in FIG. 10. The AR plate 101 is formed by attaching an AR film to one side of a transparent thin plate having a refractive index approximately equal to the equivalent refractive index of an optical fiber. When it is difficult to directly form an AR film on the end face of the optical fiber matrix 1, use the transparent adhesive patch with the refractive index substantially equal to the AR film 101 on the end face of the optical fiber matrix 1 without the AR film 101 Use it side-by-side for the same effect as a direct AR coating. FIG. 35 shows another aspect of the light receiving module according to this embodiment. The light receiving module shown in FIG. 35 includes the fiber matrix module shown in FIG. 34 and a light receiving element matrix 8. Each light-receiving element 81 provided in the light-receiving element matrix 8 receives each light condensed by the GRIN lens matrix 109. The GRIN lens matrix 109 includes a plurality of GI (Graded Index) optical fibers 174 functioning as GRIN lenses. The GRIN lens matrix 109 has a size matching that of the lens matrix 2 and a GI optical fiber 174 is arranged at the central portion to match the tap optical path. The GI optical fiber 174 is preferably fixed by being clamped by two V-groove plates. Each parallel light transmitted through the partial transmission film 41 is incident on one end of a different GI optical fiber 174. Then, each light emitted from the other end of the GI optical fiber 174 is focused to the points P9-1 to P9-4 specified for each GI optical fiber 174. A light-receiving surface of the light-receiving element 81 is arranged at this point. (Tenth embodiment) Fig. 29 shows an example of an optical fiber matrix module according to this embodiment. The optical fiber matrix module shown in FIG. 29 includes the optical fiber matrix module shown in FIG. 18, a light shielding plate 7, and a lens matrix 9. The light shielding plate 7 functions as an optical component, and the lens matrix 9 functions as a second lens matrix. The fiber matrix module of this embodiment may also be the fiber matrix module of the eighth embodiment shown in FIG. 23. The light shielding plate 7 has a plurality of through holes 71. Each parallel light transmitted through the reflecting surface of the partially transmitting film 41 is incident on one end of a different through hole 71. Then, the parallel light that has passed through the through-holes 71 is emitted from the other end of each through-hole 71. The lens matrix 9 condenses each light emitted from the other end of the plurality of through holes 71 to a point defined for each of the through holes 71. A light-receiving surface of the light-receiving element 81 is arranged at this point. An example of a light receiving module according to this embodiment is shown in FIG. 30. The light receiving module shown in FIG. 30 includes the fiber matrix module shown in FIG. 29 and a light receiving element matrix 8. Each light-receiving element 81 provided in the light-receiving element matrix 8 receives each light condensed by the lens matrix 9. The light receiving module shown in FIG. 30 can be used as a 4-matrix light tap monitoring module. The application area is an optical communication system with a wavelength of 1.55 μm. The module includes an optical fiber matrix 1, a lens matrix 2, a partial transmission film 41 and a glass substrate 42, a light shielding plate 7, a lens 9, and a light receiving element matrix 8 from the left side of the figure. For fiber spacing df Each of the parameters, as an example, can be realized in reality if the values shown in FIG. 21 are adopted. First, the operation and function of the module will be described. 95% of the light that is incident from the optical fiber 11A to the lens matrix 2 from the flat surface 21 side without passing through the air layer and exits from the lens surface 23 is partially transmitted through the film 41 at a reflection anglef (8 degrees) After reflection, it returns to the lens matrix 2 again and is incident on the optical fiber 11B. 5% of the incident light intensity is tapped and returned to the main line. The rear section of the 5% intensity tap light system passes through the glass substrate 42 parallel to the partially transmitting film 41 to become an air layer, and the exit angle is(8.0 degrees), but at the rear stage of the glass substrate 42, in order to prevent crosstalk caused by the mixing of tap light transmitted in space, the light shielding plate 7 provided with a through hole 71 is provided. The light shielding plate 7 has a size matching the external shape of the lens matrix 2, and a through hole 71 having a beam diameter is provided at a central portion of the light shielding plate 7 in cooperation with the tap optical path. A lens matrix 9, which is the same as the lens matrix 2, is provided in the same direction as the lens matrix 2 at the rear stage of the light shielding plate 7. The lens matrix 9 condenses the tap beam transmitted and diffused in space to the light receiving surface of the light receiving element 81. The following description will be made with respect to each of the above-mentioned components without overlapping with the ninth embodiment. Optical fiber matrix 1: Unlike the ninth embodiment, an AR coating is not applied to an end surface inclined by 8 degrees. In addition, as in the ninth embodiment, the angle of the core end surface with respect to the optical axis of the optical fiber is not limited to 8 degrees. Lens matrix 2: It is composed of borosilicate glass with a refractive index of 1.501 at a wavelength of 1.55 μm, and is formed at a matrix interval of 500 μm in the positive direction of the z-axis at the center of the lens holding surface parallel to the xy plane The convex surface 23 of the first aspherical surface A1 and the second aspherical surface A2. A flat portion having a thickness of 1 μm is provided between the adjacent convex surfaces 23, and a convex amount, ie, a depression amount, from the flat portion (lens holding surface) is, for example, 75 μm. Spacers 22 are integrally formed at both ends in the x direction of the lens matrix 2 during the lens molding process. The spacer 22 is a trapezoidal convex portion, the surface of the trapezoidal convex portion is parallel to the lens holding surface, and the area thereof is 1 × 1.5 mm (x × y) on one side. The height of the spacer 22 is such that the lens optical axis position (Ac) becomes a specific convex side focal length fv (Here is 889.4 μm). The flat surface 21 of the lens matrix 2 is parallel to the end face of the optical fiber matrix 1 and is inclined with respect to the y-axis, and the distance between the inclined flat surface 21 and the lens optical axis (Ac) of the lens convex surface 23 becomes the concave focal length fc = 1342 μm. Partially transmissive film 41 and glass substrate 42: In this configuration, partly transmissive film 41 is attached to transparent glass substrate 42 separated from lens matrix 2 but has the same refractive index nc By. An incident angle is attached to a glass substrate 42 whose two surfaces are parallel.The partial transmission film 41 is set to 8 degrees. The reflection / transmission ratio is preferably 95% / 5%. As a material, for example, SiO formed by an ion beam assisted evaporation method can be exemplified.2 -TiO2 Multilayer film. Light-shielding plate 7: The light-shielding plate 7 is composed of a rectangular infrared-absorbing glass having a shape of 4000 × 2000 × 1000 μm. At the central part, as shown in FIGS. 29 and 30, in accordance with the optical path of the tap light, a lens center incident angle with the z-axis direction is provided in parallel with the xz plane.f That is, a 300 μm square through hole with an angle of 8 degrees. The x-direction matrix pitch is 500 μm, which is the same as the lens matrix 2. When the beam diameter of the tap light is 214.6 μm as shown in FIG. 21, the light is transmitted without being in contact with the wall of the through hole 71 of the light shielding plate 7, but is generated by the reflection and transmission of the lens matrix 2 or the partial transmission film 41 in the previous stage. The diffuse reflection component caused by the irregular structure is prevented by the light shielding plate 7 and prevents the light receiving element matrix 8 from reaching the crosstalk. As shown in the side views of FIGS. 29 and 30, the connection interface from the fiber matrix 1 to the light-receiving element matrix 8 all remains inclined, so it has a structure that prevents reflected return light. Assembly step: The difference from the ninth embodiment is that in the first step, the lens matrix 2 and a part of the transmissive film 41 are connected first. In this step, since a part of the transmissive film 41 is an ordinary flat plate, the alignment operation is not required, and the connection can be performed only by the mold alignment operation. The rest is the same as the ninth embodiment. Characteristics: The characteristics of the manufactured 4 ch tap monitoring module at a wavelength of 1.55 μm are an insertion loss of 0.4 to 0.5 dB, a reflection attenuation of 46 dB or more, and a light receiving sensitivity of 50 to 60 mA / W. Adjacent crosstalk is also above 45 dB. This is the same as the third embodiment. (Eleventh embodiment) In the above embodiment, the matrix is a one-dimensional array, but it may be a two-dimensional matrix. In this case, the fiber matrix modules shown in FIG. 2 or FIG. 18 are arranged side by side in the y direction. At this time, the fiber matrix is the most problematic, but the fiber matrix 1 can be realized according to Patent Document 2. FIG. 31 shows a connection surface of the optical fiber matrix 1 as viewed from the z direction. The optical fiber matrix 1 shown in FIG. 31 includes V-groove plates 13-2 to 13-5 to which a 60-degree V-groove 14 for the optical fiber matrix is applied. On the V-groove plates 13-2 to 13-5, on both sides of the matrix of the V-groove 14, V-grooves 15-1 and 15-2 for vertical alignment are provided. Furthermore, alignment grooves 15-3 and 15-4 are formed on the back surface of the V-groove plates 13-2 to 13-5 at the same x-direction positions as the front side. The alignment optical fiber 12 may be the same as the optical fibers 11A and 11B shown in the figure. In this case, if the opening width of the V-groove 14 is set to W14 And the opening width of the alignment trench 15 is set to W15 , Then these settings can be set as follows, that is, (Equation 29)(Equation 30). In this case, when the alignment optical fiber 12 fits into the alignment groove 15, the waveguide optical fiber 11 is pressed by the upper plate and the upper plate. Here, R is the radius of the optical fiber, and d is the distance between the V-groove plate 13-2 to 13-5 and the upper plate. In this embodiment, since d is set to 20 μm, it is set to W14 = 193 μm, w15 = 61 μm. The alignment grooves 15-1, 15-2, 15-3, and 15-4 must be in the same position on the front and back of the V-groove plate in the x direction. The front and back alignments must be in advance in the grooves such as a slicer or cutter. In the groove processing device, it is sufficient to adjust the groove formation position to observe the verticality of the upper and lower focusing axes of the lens barrel with respect to the processing surface. As a result, the 8 × 4 fiber matrix made of TEMPAX glass has a pitch of 250 μm in the x direction and a pitch of 1 mm in the y direction. With this, a 4 × 4 matrix fiber matrix module and a light receiving module with a 500 μm pitch in the x direction and a 1 mm pitch in the y direction can be manufactured. Here, as shown in the side view of FIG. 32, the optical fiber matrix 1 is preferably subjected to an inclination process only to a portion near the optical fiber core. The reason is that if the entire surface of the end surface of the matrix is set to be inclined, it is particularly difficult to realize a two-dimensional matrix of all parts below the lens matrix 2. Processing can use a double-headed cutting machine. This series is equipped with two cutting machines, and it is a device that can continuously process two different types of blades in one step. 2D (two dimensional) matrix of lens matrix 2, 9 or light-shielding plate 7 other than fiber matrix 1 and light receiving element matrix 8 are also used, and they are 4 times of 500 μm pitch in x direction and 1 mm pitch in y direction. × 4 matrix. A side view of the manufactured 4 × 4 tap monitoring module is shown in FIG. 32. In appearance, the top view is exactly the same as that in FIG. 28, and in the side view, it is in the form of being stacked in the y direction. Moreover, this embodiment is not limited to the fiber matrix module shown in FIG. 2 or FIG. 18, and can also be applied to the fiber matrix modules of all the above embodiments. In addition, in all the embodiments described above, the optical design of the first aspherical surface A1 and the second aspherical surface A2 was performed in comparison, but the present invention is not limited to this. For example, the shapes of the first aspherical surface A1 and the second aspherical surface A2 may be different, and the peak positions of the first and second convex surfaces may also be different. In the description so far, it is assumed that the optical axis of the lens Ac is parallel to the plane Pc formed by the optical axis of the optical fiber for convenience. However, in the case where the end face of the optical fiber is tilted as shown in the explanatory diagram of the present invention in order to prevent reflection, it is desirable to perform skew adjustment between the optical fiber matrix 1 and the lens matrix 2 about an axis parallel to the x-axis. (Effects of the Invention) As described above, if the structure of directly connecting the front and rear elements on the flat surface side of the plano-convex lens is provided, a compact optical module can be constructed. In addition, by making the lens surface aspherical as described in the present invention, the lens aperture can be fully used, and even if it is an integrated small-aperture lens, high-efficiency optical coupling can be achieved. Furthermore, since it has a plano-convex structure, it does not require operations such as front-side and back-side facing like a two-convex lens, and also has the advantage that it can be mass-produced by easily matrixing it with a single-sided molding step. According to these contents, it is clear that it contributes greatly to the economicalization of optical communication devices. [Industrial availability] The present invention can be applied to the information and communication industry.
1‧‧‧光纖矩陣1‧‧‧ Fiber Matrix
2‧‧‧透鏡矩陣2‧‧‧ lens matrix
3‧‧‧空氣層3‧‧‧air layer
4‧‧‧部分反射部4‧‧‧partial reflection
7‧‧‧遮光板7‧‧‧shield
8‧‧‧受光元件矩陣8‧‧‧ light receiving element matrix
9‧‧‧透鏡矩陣9‧‧‧ lens matrix
11‧‧‧光纖11‧‧‧ Optical Fiber
11A‧‧‧光纖11A‧‧‧Optical fiber
11A-1‧‧‧光纖11A-1‧‧‧Optical fiber
11A-2‧‧‧光纖11A-2‧‧‧Optical fiber
11A-3‧‧‧光纖11A-3‧‧‧Optical fiber
11A-4‧‧‧光纖11A-4‧‧‧Optical fiber
11A-11‧‧‧光纖11A-11‧‧‧ Fiber
11A-12‧‧‧光纖11A-12‧‧‧Optical fiber
11A-13‧‧‧光纖11A-13‧‧‧ Fiber
11A-14‧‧‧光纖11A-14‧‧‧ Fiber
11A-21‧‧‧光纖11A-21‧‧‧ Fiber
11A-31‧‧‧光纖11A-31‧‧‧Optical fiber
11A-41‧‧‧光纖11A-41‧‧‧Optical fiber
11B‧‧‧光纖11B‧‧‧ Fiber
11B-1‧‧‧光纖11B-1‧‧‧optical fiber
11B-2‧‧‧光纖11B-2‧‧‧Optical fiber
11B-3‧‧‧光纖11B-3‧‧‧ Fiber
11B-4‧‧‧光纖11B-4‧‧‧ Fiber
11B-11‧‧‧光纖11B-11‧‧‧ Fiber
11B-12‧‧‧光纖11B-12‧‧‧Optical fiber
11B-13‧‧‧光纖11B-13‧‧‧Optical fiber
11B-14‧‧‧光纖11B-14‧‧‧ Fiber
11B-21‧‧‧光纖11B-21‧‧‧optical fiber
11B-31‧‧‧光纖11B-31‧‧‧Optical fiber
11B-41‧‧‧光纖11B-41‧‧‧Optical fiber
12-1‧‧‧對位用光纖12-1‧‧‧ Optic Fiber
12-2‧‧‧對位用光纖12-2‧‧‧Alignment fiber
13-1、13-2、13-3、13-4、13-5‧‧‧V溝槽板13-1, 13-2, 13-3, 13-4, 13-5‧‧‧V groove plate
14‧‧‧V溝槽14‧‧‧V groove
15-1、15-2、15-3、15-4‧‧‧對位溝槽15-1, 15-2, 15-3, 15-4
21‧‧‧平坦面21‧‧‧ flat surface
22‧‧‧間隔件22‧‧‧ spacer
22A‧‧‧傾斜端面22A‧‧‧inclined face
22B‧‧‧透鏡側平坦面22B‧‧‧ lens side flat surface
23‧‧‧凸面23‧‧‧ convex
23-1~23-4‧‧‧凸面23-1 ~ 23-4‧‧‧ convex
41‧‧‧部分透過膜41‧‧‧ partially transmissive membrane
42‧‧‧玻璃基板42‧‧‧ glass substrate
71‧‧‧貫通孔71‧‧‧through hole
81‧‧‧受光元件81‧‧‧ light receiving element
91‧‧‧焦距調整樹脂91‧‧‧focus adjustment resin
101‧‧‧AR塗層板101‧‧‧AR coated board
109‧‧‧GRIN透鏡矩陣109‧‧‧GRIN lens matrix
174‧‧‧GI光纖174‧‧‧GI fiber
A1‧‧‧第1非球面A1‧‧‧1st aspherical surface
A2‧‧‧第2非球面A2‧‧‧2nd aspherical surface
A3‧‧‧鞍部A3‧‧‧ Saddle
AC‧‧‧透鏡光軸(透鏡中心軸)A C ‧‧‧ lens optical axis (lens central axis)
Bc‧‧‧峰線Bc‧‧‧Peak Line
BD‧‧‧光束直徑BD‧‧‧Beam Diameter
DC‧‧‧光纖中心線與x軸方向之透鏡外 緣兩端間之距離D C ‧‧‧The distance between the center line of the optical fiber and the two ends of the lens outer edge in the x-axis direction
DE‧‧‧光纖中心線與x軸方向之透鏡外 緣兩端間之距離D E ‧‧‧ The distance between the center line of the fiber and the two ends of the lens' outer edge in the x-axis direction
d‧‧‧V溝槽板與上板之距離d‧‧‧V distance between groove plate and upper plate
df‧‧‧光纖間隔d f ‧‧‧ fiber spacing
2df‧‧‧間隔2d f ‧‧‧ interval
dn‧‧‧鄰接間隔d n ‧‧‧adjacent interval
dp‧‧‧峰間隔d p ‧‧‧ peak interval
fc‧‧‧凹側焦距f c ‧‧‧ concave side focal length
fv‧‧‧凸側焦距f v ‧‧‧ convex side focal length
Ln‧‧‧法線L n ‧‧‧ normal
nc‧‧‧透鏡折射率n c ‧‧‧ lens refractive index
nv‧‧‧空氣折射率n v ‧‧‧ air refractive index
P1‧‧‧第1位置P1‧‧‧1st position
P2‧‧‧第2位置P2‧‧‧ 2nd position
P3‧‧‧反射面之一點P3‧‧‧A point on the reflective surface
P4‧‧‧交點P4‧‧‧ intersection
P6‧‧‧峰P6‧‧‧peak
P7‧‧‧交點P7‧‧‧Intersection
P8‧‧‧峰P8‧‧‧Peak
P9-1~P9-4‧‧‧點P9-1 ~ P9-4‧‧‧‧points
PC‧‧‧特定平面P C ‧‧‧ specific plane
Pd‧‧‧投影部分Pd‧‧‧ projection
R1‧‧‧直線R1‧‧‧Straight
R2‧‧‧直線R2‧‧‧Straight
t1‧‧‧透鏡厚度t 1 ‧‧‧ lens thickness
tr‧‧‧反射層厚度t r ‧‧‧thickness of reflective layer
W14‧‧‧V溝槽之開口寬度W 14 ‧‧‧V Groove opening width
W15‧‧‧對位溝槽之開口寬度W 15 ‧‧‧ Opening width of registration groove
ws‧‧‧寬度w s ‧‧‧ width
x‧‧‧方向x‧‧‧ direction
y‧‧‧方向y‧‧‧direction
z‧‧‧方向z‧‧‧ direction
Z(x)‧‧‧曲線Z (x) ‧‧‧curve
‧‧‧光纖反射角 ‧‧‧Fiber reflection angle
ψ‧‧‧光纖入射角ψ‧‧‧Fiber Incident Angle
θ‧‧‧角度θ‧‧‧ angle
θ1‧‧‧光纖相對法線之角度θ 1 ‧‧‧ Angle of fiber with respect to normal
θ2‧‧‧自光纖之中心端面出射至空氣層 之光之中心光相對於法線之角度θ 2 ‧‧‧ the angle of the center light of the light emitted from the center end face of the optical fiber to the air layer with respect to the normal
θc‧‧‧自透鏡表面之出射角θ c ‧‧‧ exit angle from lens surface
θt‧‧‧切線角度θ t ‧‧‧tangent angle
θv‧‧‧向透鏡表面之入射角θ v ‧‧‧ incident angle to lens surface
圖1表示第1實施形態之平凸透鏡之一例。 圖2表示第2實施形態之光纖矩陣模組之構成例。 圖3係關於第1及第2實施形態之光學系統之說明圖。 圖4係關於第1及第2實施形態之非球面形狀之說明圖。 圖5表示第1及第2實施形態中之參數之一例。 圖6表示第3實施形態之平凸透鏡之立體圖。 圖7表示第3實施形態之平凸透鏡之模具之第1例。 圖8表示第3實施形態之平凸透鏡之模具之第2例。 圖9表示第3實施形態之平凸透鏡之一例。 圖10表示第4實施形態之光纖矩陣模組之構成例。 圖11係關於第3及第4實施形態之光學系統之說明圖。 圖12(a)、(b)係關於第3及第4實施形態之於透鏡表面之光束直徑BD之第1說明圖。 圖13(a)、(b)係關於第3及第4實施形態之於透鏡表面之光束直徑BD之第2說明圖。 圖14係第3及第4實施形態之平凸透鏡之另一形態。 圖15係第3及第4實施形態之曲率半徑之第1計算例。 圖16係第3及第4實施形態之曲率半徑之第2計算例。 圖17表示第5實施形態之平凸透鏡之一例。 圖18表示第6實施形態之光纖矩陣模組之構成例。 圖19係關於第5及第6實施形態之光學系統之說明圖。 圖20係關於第5及第6實施形態之非球面形狀之說明圖。 圖21表示第5及第6實施形態中之參數之一例。 圖22表示第7實施形態之平凸透鏡之一例。 圖23表示第8實施形態之光纖矩陣模組之構成例。 圖24係關於第7及第8實施形態之光學系統之說明圖。 圖25係第7及第8實施形態之曲率半徑之第1計算例。 圖26係第7及第8實施形態之曲率半徑之第2計算例。 圖27表示第9實施形態之光纖矩陣模組之一例。 圖28表示第9實施形態之受光模組之一例。 圖29表示第10實施形態之光纖矩陣模組之一例。 圖30表示第10實施形態之受光模組之一例。 圖31表示第11實施形態之光纖矩陣之自z方向觀察之連接面之一例。 圖32表示第11實施形態之受光模組之自x方向觀察之構成之一例。 圖33表示第9實施形態之光纖矩陣與透鏡矩陣之放大圖之一例。 圖34表示第9實施形態之光纖矩陣模組之另一例。 圖35表示第9實施形態之受光模組之另一例。FIG. 1 shows an example of a plano-convex lens according to the first embodiment. FIG. 2 shows a configuration example of the optical fiber matrix module according to the second embodiment. FIG. 3 is an explanatory diagram of the optical system according to the first and second embodiments. FIG. 4 is an explanatory view of aspherical shapes of the first and second embodiments. Fig. 5 shows an example of parameters in the first and second embodiments. Fig. 6 is a perspective view of a plano-convex lens according to a third embodiment. Fig. 7 shows a first example of a mold for a plano-convex lens according to a third embodiment. Fig. 8 shows a second example of a mold for a plano-convex lens according to a third embodiment. FIG. 9 shows an example of a plano-convex lens according to the third embodiment. FIG. 10 shows a configuration example of an optical fiber matrix module according to the fourth embodiment. FIG. 11 is an explanatory diagram of optical systems according to the third and fourth embodiments. 12 (a) and 12 (b) are first explanatory diagrams of the beam diameter BD on the lens surface in the third and fourth embodiments. 13 (a) and 13 (b) are second explanatory diagrams of the beam diameter BD on the lens surface in the third and fourth embodiments. Fig. 14 shows another embodiment of the plano-convex lens according to the third and fourth embodiments. FIG. 15 is a first calculation example of the radius of curvature of the third and fourth embodiments. FIG. 16 is a second calculation example of the curvature radius of the third and fourth embodiments. FIG. 17 shows an example of a plano-convex lens according to the fifth embodiment. FIG. 18 shows a configuration example of an optical fiber matrix module according to the sixth embodiment. FIG. 19 is an explanatory diagram of the optical systems according to the fifth and sixth embodiments. FIG. 20 is an explanatory view of aspherical shapes of the fifth and sixth embodiments. Fig. 21 shows an example of parameters in the fifth and sixth embodiments. FIG. 22 shows an example of a plano-convex lens according to the seventh embodiment. FIG. 23 shows a configuration example of an optical fiber matrix module according to the eighth embodiment. FIG. 24 is an explanatory diagram of the optical systems of the seventh and eighth embodiments. FIG. 25 is a first calculation example of the radius of curvature of the seventh and eighth embodiments. Fig. 26 is a second example of calculation of the radius of curvature of the seventh and eighth embodiments. Fig. 27 shows an example of a fiber matrix module according to a ninth embodiment. Fig. 28 shows an example of a light receiving module according to the ninth embodiment. FIG. 29 shows an example of an optical fiber matrix module according to the tenth embodiment. Fig. 30 shows an example of a light receiving module according to the tenth embodiment. FIG. 31 shows an example of a connection surface of the optical fiber matrix according to the eleventh embodiment as viewed from the z direction. FIG. 32 shows an example of the configuration of the light receiving module according to the eleventh embodiment when viewed from the x direction. FIG. 33 shows an example of an enlarged view of the optical fiber matrix and the lens matrix in the ninth embodiment. FIG. 34 shows another example of the optical fiber matrix module according to the ninth embodiment. FIG. 35 shows another example of the light receiving module according to the ninth embodiment.
Claims (12)
Applications Claiming Priority (6)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2016166447 | 2016-08-29 | ||
| JP??2016-166447 | 2016-08-29 | ||
| JP??2017-035484 | 2017-02-27 | ||
| JP2017035484 | 2017-02-27 | ||
| PCT/JP2017/026395 WO2018042936A1 (en) | 2016-08-29 | 2017-07-21 | Plano-convex lens, fiber array module, and light reception module |
| ??PCT/JP2017/026395 | 2017-07-21 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| TW201812362A true TW201812362A (en) | 2018-04-01 |
| TWI658295B TWI658295B (en) | 2019-05-01 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| TW106129113A TWI658295B (en) | 2016-08-29 | 2017-08-28 | Plano-convex lens, fiber matrix module and light receiving module |
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| TW (1) | TWI658295B (en) |
| WO (1) | WO2018042936A1 (en) |
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| TW202119072A (en) * | 2019-10-31 | 2021-05-16 | 佑勝光電股份有限公司 | An optical transceiver module and an optical cable module |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH11317836A (en) * | 1998-02-02 | 1999-11-16 | Sharp Corp | Optical waveguide type reduction optical image sensor |
| JP2003084168A (en) * | 2001-09-14 | 2003-03-19 | Asahi Glass Co Ltd | Multilayer lens and optical fiber collimator |
| US20060165351A1 (en) * | 2002-06-14 | 2006-07-27 | Nippon Sheet Glass Co., Ltd. | Optical device unit, optical device and microlens array |
| US7068883B2 (en) * | 2002-10-01 | 2006-06-27 | Eastman Kodak Company | Symmetric, bi-aspheric lens for use in optical fiber collimator assemblies |
| JP2009093131A (en) * | 2007-10-11 | 2009-04-30 | Global Fiber Optics:Kk | Array type tap photodiode module and its manufacturing method |
| KR101076603B1 (en) * | 2008-07-16 | 2011-10-26 | 옵티시스 주식회사 | Optical communication module for optical wavelength division multipexing |
| JP2011028140A (en) * | 2009-07-29 | 2011-02-10 | Alps Electric Co Ltd | Lens |
| TW201250318A (en) * | 2011-06-08 | 2012-12-16 | Hon Hai Prec Ind Co Ltd | Optical fiber communication apparatus |
-
2017
- 2017-07-21 WO PCT/JP2017/026395 patent/WO2018042936A1/en not_active Ceased
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| WO2018042936A1 (en) | 2018-03-08 |
| TWI658295B (en) | 2019-05-01 |
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