TWI652430B - Twelve axes mechanism for spherical coordinates orientating - Google Patents
Twelve axes mechanism for spherical coordinates orientating Download PDFInfo
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Abstract
本發明可直接輸出力或力矩的十二軸球座標轉向機構,技術相關於機械人運動或載台操控,可應用於機械人的肩關結或髖關結,亦可應於多軸複合加工中心機或多次元檢測量床,以達球座標三自由度轉向致動量。 The invention can directly output the force or torque of the twelve-axis ball coordinate steering mechanism, and the technology is related to the robot movement or the stage control, and can be applied to the shoulder joint or the hip joint of the robot, and can also be applied to the multi-axis composite processing. The central machine or the multi-element detection bed can achieve the three-degree-of-freedom steering amount of the ball coordinate.
Description
本發明可直接輸出力或力矩的十二軸球座標轉向機構,技術相關於機械人運動或載台操控,可應用於機械人的肩關結或髖關結,亦可應於多軸複合加工中心機或多次元檢測量床,以達球座標三自由度轉向致動量。 The invention can directly output the force or torque of the twelve-axis ball coordinate steering mechanism, and the technology is related to the robot movement or the stage control, and can be applied to the shoulder joint or the hip joint of the robot, and can also be applied to the multi-axis composite processing. The central machine or the multi-element detection bed can achieve the three-degree-of-freedom steering amount of the ball coordinate.
十二軸球座標轉向機構乃架構於本發明人之二前案(US20120083347A1及US20150082934A1/EP2863102A1/CN104511904A),將二前案設計之二組內框四面體結構與外框四面體結構,取消其中一組外框結構或內框結構之原四面體幾何定義,更新為二端框結構,再將餘留之外框或內框結構更名為基框結構,但仍保留原四面體幾何定義。四組之內軌與外軌弧桿組之十二軸仍如前案軸接定義,本發明新更名之環轉弧桿組。前案(US20150082934A1/EP2863102A1/CN104511904A)新增之至少一組終端弧桿組,本發明更新為至多二組承載弧桿組。前案(US20120083347A1)所探討的各種奇異現象與其因應的幾何限 制,本發明仍延續引用。 The twelve-axis ball coordinate steering mechanism is constructed in the second inventor of the present invention (US20120083347A1 and US20150082934A1/EP2863102A1/CN104511904A), and the two sets of inner frame tetrahedral structure and outer frame tetrahedral structure of the second pre-case design are cancelled. The original tetrahedral geometry definition of the outer frame structure or the inner frame structure is updated to the two-end frame structure, and the remaining outer frame or inner frame structure is renamed to the base frame structure, but the original tetrahedral geometric definition is retained. The twelve axes of the four sets of inner rail and outer rail arcs are still defined as in the previous case, and the newly renamed ring-turning rod set of the present invention. In the previous case (US20150082934A1/EP2863102A1/CN104511904A), at least one set of terminal arc bar sets is added, and the present invention is updated to at most two sets of bearing arc bar sets. The various singularities discussed in the previous case (US20120083347A1) and the geometric limitations of their response, the present invention continues to be cited.
本發明一種十二軸球座標轉向機構,包含:為一組基框組合件,基框組合件包含一基框結構0c及四基框轉動元件0a,該基框結構0c由數個弧框組成,該基框結構0c上具有四端角,可定義一基框幾何四面體,且該四面體的四角心線共交於基框結構的中心,該基框結構0c固裝該四基框轉動元件0a,該四基框轉動元件0a輸出軸線,標示為單位向量 U i ,其中 i=1 ~ 4 。界定該四基框轉動元件0a的輸出軸線分別與該基框幾何四面體的四角心線重合,並向心交會於基框幾何四面體中心,基框結構0c固裝四基框轉動元件0a之任二輸出軸線間夾角,幾何標示為 ∧ ij =ArcCos(U i ˙U j ) ,其中 i≠j 。基框轉動元件0a可為扭力輸出器(例如馬達或油壓旋轉缸)、角度檢知器(例如光學編碼器)或軸承中的任意一個。基框結構幾何定義如圖1A、圖2A、圖3A及圖4A。 A twelve-axis ball coordinate steering mechanism of the present invention comprises: a set of base frame assemblies, the base frame assembly comprising a base frame structure 0c and a four-base frame rotating element 0a, the base frame structure 0c being composed of a plurality of arc frames The base frame structure 0c has a four-terminal angle, and a base frame geometric tetrahedron can be defined, and the four-corner core line of the tetrahedron is co-located to the center of the base frame structure, and the base frame structure 0c fixes the four-base frame rotation. Element 0a, the output axis of the four-base frame rotating element 0a, denoted as a unit vector U i , where i = 1 ~ 4 . The output axis defining the four-base frame rotating element 0a coincides with the four-corner line of the base frame geometric tetrahedron, and intersects the center of the base frame geometric tetrahedron, and the base frame structure 0c fixes the four-base frame rotating element 0a. The angle between any two output axes is geometrically labeled ∧ ij =ArcCos(U i ̇ U j ) , where i≠j . The base frame rotating member 0a may be any one of a torque output device (such as a motor or a hydraulic rotary cylinder), an angle detector (such as an optical encoder), or a bearing. The geometry of the base frame structure is defined in Figures 1A, 2A, 3A and 4A.
根據本發明人之前案(US20120083347A1)揭露,基框結構0c的幾何定義若為正四面體,因其單一對稱的特性較易於參數設計與運算模擬。如此則基框結構0c的各角心線間的六夾角皆相等約109.5°,即: ∧ 12 =∧ 13 =∧ 14 =∧ 23 =∧ 24 =∧ 34 ≒109.5 °。但需注意正四面體最易發生奇異現象。為避免奇異,故基框結構0c的幾何定義不必為正四面體。基框結構0c軸接可概分為四種構型,即:構型一如圖1B、構型二如圖2B、構型三如圖3B及構型 四如圖4B。基框結構0c可設計為閉環式或開環式。閉環式設計可強化剛性避免振動或變形如圖1B,開環式設計可減免運轉時可能的干涉如圖4B。 According to the inventor's previous case (US20120083347A1), the geometric definition of the base frame structure 0c is a regular tetrahedron, and its single symmetrical characteristic is easier to parameter design and operation simulation. Thus, the six angles between the corner lines of the base frame structure 0c are equal to about 109.5°, that is, ∧ 12 = ∧ 13 = ∧ 14 = ∧ 23 = ∧ 24 = ∧ 34 ≒ 109.5 ° . However, it should be noted that the regular tetrahedron is most prone to singularity. To avoid singularities, the geometric definition of the base frame structure 0c need not be a regular tetrahedron. The base frame structure 0c can be roughly divided into four configurations, that is, the configuration 1 as shown in FIG. 1B, the configuration 2 as shown in FIG. 2B, the configuration 3 as shown in FIG. 3B, and the configuration 4 as shown in FIG. 4B. The base frame structure 0c can be designed as a closed loop or an open loop. The closed-loop design enhances rigidity to avoid vibration or deformation. Figure 1B. The open-loop design eliminates possible interference during operation, as shown in Figure 4B.
二組端框組,每組端框組包含一端框結構4c及二端框轉動元件4a,該端框結構4c上具有二端角,該端框結構固裝該二端框轉動元件4a。界定該二端框轉動元件4a的輸出軸線分別與該端框幾何的二角心線重合,並向心交會於基框幾何四面體中心,以使該端框組環軌同心繞轉。第一組端框結構上二端框轉動元件0a之輸出軸線,標示為單位向量 V 1 及 V 2 ,該二端框轉動元件0a之輸出軸線間夾角,幾何標示為 λ 12 =ArcCos(V 1 ˙V 2 ) 。第二組端框結構上二端框轉動元件0a之輸出軸線,標示為單位向量 V 3 及 V 4 ,該二端框轉動元件0a之輸出軸線間夾角,幾何標示為 λ 34 =ArcCos(V 3 ˙V 4 ) 。每組端框組之端框轉動元件的輸出軸線間夾角皆大於90度且小於150度,即: 90°<λ 12 <150° 及 90°<λ 34 <150° 。端框轉動元件4a可為扭力輸出器(例如馬達或油壓旋轉缸)、角度檢知器(例如光學編碼器)或軸承中的任意一個。端框結構幾何定義如圖5A、圖6A、圖7A及圖8A。 Two sets of end frames, each set of end frames comprising an end frame structure 4c and a two end frame rotating element 4a having a double end angle, the end frame structure fixing the two end frame rotating elements 4a. The output axes defining the two end frame rotating elements 4a respectively coincide with the two-corner lines of the end frame geometry, and intersect centripetally at the center of the base frame geometric tetrahedron so that the end frame group ring tracks are concentrically rotated. The output axes of the two end frame rotating elements 0a of the first set of end frame structures are indicated as unit vectors V 1 and V 2 , and the angle between the output axes of the rotating elements 0a of the two end frames is geometrically labeled as λ 12 =ArcCos (V 1 ̇ V 2 ) . The output axes of the two end frame rotating elements 0a of the second group end frame structure are indicated as unit vectors V 3 and V 4 , and the angle between the output axes of the rotating elements 0a of the two end frames is geometrically marked as λ 34 =ArcCos (V 3 ̇ V 4 ) . The angle between the output axes of the end frame rotating elements of each group of end frames is greater than 90 degrees and less than 150 degrees, namely: 90° < λ 12 < 150 ° and 90 ° < λ 34 < 150 ° . The end frame rotating member 4a may be any one of a torque output device (such as a motor or a hydraulic rotary cylinder), an angle detector (such as an optical encoder), or a bearing. The geometry of the end frame structure is defined in Figures 5A, 6A, 7A and 8A.
四組環轉弧桿組,每組環轉弧桿組包括一基接弧桿1c、一端接弧桿2c及一中接轉動元件2a。該基接弧桿1c之連桿端與該端接弧桿2c之連桿端以該中接轉動元件2a軸接,該中接轉動元件2a標示為單位向量 W i ,其中 i=1 ~ 4 。該基接弧桿1c的基框端與一基框轉動元件1a(前已向量標示為 U i ,其中 i=1 ~ 4 )軸接。該端 接弧桿的端框端與一端框轉動元件4a(前已向量標示為 V i ,其中 i=1 ~ 4 )軸結。中接轉動元件2a輸出軸線,常態指向該基框幾何四面體中心,以使該環轉弧桿組環軌同心繞轉於該基框組合件與該二組端框組之間。中接轉動元件2a可為扭力輸出器(例如馬達或油壓旋轉缸)、角度檢知器(例如光學編碼器)或軸承中的任意一個。 The four sets of ring-turning arc bar sets each of which includes a base connecting rod 1c, an end connecting rod 2c and a middle connecting rotating element 2a. The connecting rod end of the base connecting rod 1c and the connecting end of the connecting rod 2c are axially connected by the intermediate rotating element 2a, and the intermediate rotating element 2a is denoted as a unit vector W i , wherein i=1 ~ 4 . The base frame end of the base connecting rod 1c is pivotally coupled to a base frame rotating element 1a (the front vector is labeled U i , where i = 1 to 4 ). The end frame end of the terminating arc bar is pivoted with the end frame rotating element 4a (the front vector is labeled V i , where i=1 ~ 4 ). The intermediate rotating element 2a outputs an axis, and the normal direction points to the center of the base frame geometric tetrahedron, so that the ring rotating rod set ring track is concentrically rotated between the base frame assembly and the two sets of end frame groups. The intermediate rotating member 2a may be any one of a torque output device (for example, a motor or a hydraulic rotary cylinder), an angle detector (for example, an optical encoder), or a bearing.
基接弧桿1c弧長定義為基框轉動元件0a與中接轉動元件2a的夾角,幾何標示為 α i =ArcCos(U i ˙W i ) 。端接弧桿2c弧長定義為端框轉動元件4a與中接轉動元件2a的夾角,幾何標示為 β i =ArcCos(V i ˙W i ) 。任二基框轉動元件0a輸出軸線夾角小於或等於相對應之二基接弧桿1c弧長之和,即: ∧ ij α i +α j ,其中 i≠j 。任一端框之二端框轉動元件4a輸出軸線間夾角小於或等於相對應之二端接弧桿2c弧長之和,即: λ 12 β 1 +β 2 或 λ 34 β 3 +β 4 。 The base arc bar 1c arc length is defined as the angle between the base frame rotating element 0a and the intermediate connecting rotating element 2a, and is geometrically labeled as α i =ArcCos(U i ̇ W i ) . The arc length of the terminating arc bar 2c is defined as the angle between the end frame rotating element 4a and the intermediate rotating element 2a, and is geometrically labeled β i =ArcCos(V i ̇ W i ) . The output shaft angle of any two base frame rotating elements 0a is less than or equal to the sum of the arc lengths of the corresponding two base arcing rods 1c, namely: ∧ ij α i +α j , where i≠j . The angle between the output axes of the two end frame rotating elements 4a of any end frame is less than or equal to the sum of the arc lengths of the corresponding two end connecting rods 2c, namely: λ 12 β 1 +β 2 or λ 34 β 3 +β 4 .
四組環轉弧桿組分別與基框結構0c及端框結構4c軸接,共十二軸分別以基框轉動元件0a(如前標示為單位向量 U i ,其中 i=1 ~ 4 )、中接轉動元件2a(如前標示為單位向量 W i ,其中 i=1 ~ 4 )及端框轉動元件4a(如前標示為單位向量 V i ,其中 i=1 ~ 4 )軸接。二組端框組之端框結構4c,使其遠向於端接弧桿之酬載端側設置一酬載座4s,以裝設酬載物。其中酬載座4s可是力臂伸縮的舉升機構,如氣壓缸、油壓缸或電動螺旋桿,可應用於機械人的肩關結或髖關結,以達球座標三自由度轉向致動量。 The four sets of ring-turning rod groups are respectively connected with the base frame structure 0c and the end frame structure 4c, and the twelve axes respectively rotate the component 0a with the base frame (as previously indicated as the unit vector U i , where i=1 ~ 4 ), The middle rotating element 2a (as previously indicated as unit vector W i , where i = 1 ~ 4 ) and the end frame rotating element 4a (as previously indicated as unit vector V i , where i = 1 ~ 4 ) are axially coupled. The end frame structure 4c of the two end frame groups is arranged such that a payload carrier 4s is disposed on the side of the payload end of the terminating arc bar to install the payload. The 4s can be a lifting mechanism for the telescopic arm, such as a pneumatic cylinder, a hydraulic cylinder or an electric auger, which can be applied to the shoulder joint or hip joint of the robot to achieve the three-degree-of-freedom steering actuation amount of the ball coordinate. .
為回避奇異現象,根據本發明人之前案(US20150082934A1/EP2863102A1/CN104511904A)揭露:各基接弧桿1c之半徑可大於或小於各端接弧桿2c之半徑,且各基接弧桿1c之半徑與各端接弧桿2c之半徑亦不必相等。故十二軸軸接可分為四構型,即:構型一如圖5B、構型二如圖6B、構型三如圖7B及構型四如圖8B。 In order to avoid the singularity phenomenon, according to the present inventor's previous case (US20150082934A1/EP2863102A1/CN104511904A), the radius of each base connecting rod 1c can be larger or smaller than the radius of each end connecting rod 2c, and the radius of each base connecting rod 1c The radius of each of the end arcs 2c is not necessarily equal. Therefore, the twelve-axis shaft connection can be divided into four configurations, that is, the configuration is as shown in FIG. 5B, the configuration is as shown in FIG. 6B, the configuration is as shown in FIG. 7B, and the configuration is as shown in FIG. 8B.
至多二組承載弧桿組,每組承載弧桿組包含一承載弧桿3c及一承載轉動元件3a。該承載弧桿3c之基框端與一基接弧桿1c之基框端共軸套裝一基框轉動元件0a,以使該承載弧桿3c可環軌同心繞轉。該承載轉動元件3a搭接於該承載弧桿3c之遠向基框結構0c端側,並共軸套裝於該基框轉動元件0a,該承載轉動元件3a可適時驅動該承載弧桿3c迴避基框結構0c與任一基接弧桿1c可能干涉。承載弧桿之承載端輸出軸線,標示為單位向量 N i ,其中 i=1 ~ 2 。承載弧桿3c弧長定義為基框轉動元件0a與承載弧桿之承載端輸出軸線的夾角,幾何標示為 δ i =ArcCos(U i ˙N i ) ,其中 i=1 ~ 2 。該承載弧桿3c的弧長小於或等於90度,即: δ i 90° ,其中 i=1 ~ 2 。承載轉動元件3a可為扭力輸出器(例如馬達或油壓旋轉缸)、角度檢知器(例如光學編碼器)或軸承中的任意一個。至多二組承載弧桿組之幾何定義如圖9A及圖10A。 Up to two sets of load-bearing arc rod sets, each set of load-bearing arc-rod sets comprises a load-bearing arc bar 3c and a load-bearing rotating element 3a. The base frame end of the carrying arch 3c and the base frame end of a base connecting rod 1c are coaxially provided with a base frame rotating element 0a, so that the carrying arch 3c can be concentrically rotated around the track. The bearing rotating member 3a is overlapped on the end side of the distal base frame structure 0c of the supporting arch 3c, and is coaxially fitted to the base frame rotating member 0a. The carrying rotating member 3a can drive the carrying arch 3c to avoid the base. The frame structure 0c may interfere with any of the base connecting rods 1c. The bearing end of the carrier rod arc output axis, labeled unit vector N i, where i = 1 ~ 2. The arc length of the arc carrier rod 3c is defined as a rotation angle of the base frame carrying the output end of the axis of the carrier member 0a arc strokes, geometric denoted δ i = ArcCos (U i ˙ N i), where i = 1 ~ 2. The arc length of the load bearing rod 3c is less than or equal to 90 degrees, namely: δ i 90° , where i=1 ~ 2 . The load bearing rotary member 3a may be any one of a torque output device (for example, a motor or a hydraulic rotary cylinder), an angle detector (for example, an optical encoder), or a bearing. The geometric definition of at most two sets of load bearing arc sets is shown in Figures 9A and 10A.
至多二組承載弧桿組之承載弧桿3c,使其遠向於基框結構之承載端側設置承載座3s,以裝設承載物。其中承載座3s可是固持裝置,例如工具機的夾持模組,可應於多軸複合加工中 心機或多次元檢測量床,以達球座標三自由度轉向致動量,至多二組承載弧桿組與基框結構0c之軸接方式如圖9B及圖10B。 Up to two sets of load-bearing arc rods 3c carrying the arc-rod group, such that the bearing end 3s is disposed far away from the bearing end side of the base frame structure to install the carrier. The carrier 3s can be a holding device, for example, a clamping module of the machine tool, which can be applied to a multi-axis composite machining center machine or a multi-element detection measuring bed, to achieve a three-degree-of-freedom steering amount of the ball coordinate, and at most two groups of bearing rods. The manner in which the group is coupled to the base frame structure 0c is as shown in Figs. 9B and 10B.
參考本發明人之二前案(US20120083347A1及US20150082934A1/EP2863102A1/CN104511904A),本發明十二軸球座標轉向機構的實施例,可為十二軸軸接構型一搭配承載弧桿軸接構型一所構組球座標轉向機構,立體視圖如圖11A、正視圖如圖11B及側視圖如圖11C,可為十二軸軸接構型二搭配承載弧桿軸接構型二所構組球座標轉向機構,立體視圖如圖12A、正視圖如圖12B及側視圖如圖12C,可為十二軸軸接構型三搭配承載弧桿軸接構型一所構組球座標轉向機構,立體視圖如圖13A、正視圖如圖13B及側視圖如圖13C,可為十二軸軸接構型四搭配承載弧桿軸接構型二所構組球座標轉向機構,立體視圖如圖14A、正視圖如圖14B及側視圖如圖14C。 Referring to the second inventors of the present invention (US20120083347A1 and US20150082934A1/EP2863102A1/CN104511904A), the embodiment of the twelve-axis ball coordinate steering mechanism of the present invention can be a twelve-axis shaft-connecting configuration and a matching bearing-arc shaft coupling configuration. The spherical coordinate steering mechanism of the assembled group, the stereoscopic view is as shown in FIG. 11A, the front view is as shown in FIG. 11B and the side view is shown in FIG. 11C, and the twelve-axis axial configuration can be used to match the bearing shaft of the arc-shaft. Steering mechanism, the stereoscopic view is as shown in Fig. 12A, the front view is as shown in Fig. 12B and the side view is shown in Fig. 12C, which can be a twelve-axis shaft-constructed three-matching bearing-arc shaft-aligning configuration, a constituting ball-coordinate steering mechanism, and a stereoscopic view 13A, a front view of FIG. 13B, and a side view of FIG. 13C, which may be a twelve-axis shaft-constructed four-position bearing-arc shaft-arranged configuration, and a two-frame ball coordinate steering mechanism, and the perspective view is as shown in FIG. 14A. Figure 14B and side view are shown in Figure 14C.
0a‧‧‧基框轉動元件 0a‧‧‧Base frame rotating element
0c‧‧‧基框結構 0c‧‧‧Base frame structure
1c‧‧‧基接弧桿 1c‧‧‧Based arc
2a‧‧‧中接轉動元件 2a‧‧‧Chinese rotating element
2c‧‧‧端接弧桿 2c‧‧‧Terminal arc
3a‧‧‧承載轉動元件 3a‧‧‧ Carrying rotating elements
3c‧‧‧承載弧桿 3c‧‧‧bearing arc
3s‧‧‧承載座 3s‧‧‧ bearing seat
4a‧‧‧端框轉動元件 4a‧‧‧End frame rotating element
4c‧‧‧端框結構 4c‧‧‧End frame structure
4s‧‧‧酬載座 4s‧‧‧
圖1為基框結構軸接構型一的幾何定義圖與立體視圖 Figure 1 is a geometrical definition and perspective view of the pivotal configuration of the base frame structure
圖2為基框結構軸接構型二的幾何定義圖與立體視圖 Figure 2 is a geometrical definition and perspective view of the pivotal configuration of the base frame structure
圖3為基框結構軸接構型三的幾何定義圖與立體視圖 Figure 3 is a geometrical definition and perspective view of the pivotal configuration of the base frame structure
圖4為基框結構軸接構型四的幾何定義圖與立體視圖 Figure 4 is a geometrical definition and perspective view of the four-frame structure of the framing structure
圖5為十二軸機構之軸接構型一的幾何定義圖與立體視圖 Figure 5 is a geometrical definition and perspective view of the axial configuration of the twelve-axis mechanism
圖6為十二軸機構之軸接構型二的幾何定義圖與立體視圖 Figure 6 is a geometrical definition and perspective view of the axial configuration of the twelve-axis mechanism
圖7為十二軸機構之軸接構型三的幾何定義圖與立體視圖 Figure 7 is a geometrical definition and perspective view of the axial configuration of the twelve-axis mechanism.
圖8為十二軸機構之軸接構型四的幾何定義圖與立體視圖 Figure 8 is a geometrical and stereoscopic view of the axial configuration of the twelve-axis mechanism.
圖9為承載弧桿軸接構型一的幾何定義圖與立體視圖 Figure 9 is a geometrical definition and a perspective view of the bearing shaft of the bearing shaft
圖10為承載弧桿軸接構型二的幾何定義圖與立體視圖 Figure 10 is a geometric definition and a perspective view of the bearing arrangement of the bearing shaft
圖11為十二軸軸接構型一搭配承載弧桿軸接構型一所構組球座標轉向機構之立體視圖、正視圖與側視圖 Figure 11 is a perspective view, front view and side view of a twelve-axis shaft-connected configuration with a coupled-arc shaft steering configuration
圖12為十二軸軸接構型二搭配承載弧桿軸接構型二所構組球座標轉向機構之立體視圖、正視圖與側視圖 Figure 12 is a perspective view, front view and side view of a two-frame ball coordinate steering mechanism with a twelve-axis shaft-connected configuration and a two-armed axle-axis configuration.
圖13為十二軸軸接構型三搭配承載弧桿軸接構型一所構組球座標轉向機構之立體視圖、正視圖與側視圖 Figure 13 is a perspective view, front view and side view of a twelve-axis shaft-constructed three-matched bearing-arc axle configuration
圖14為十二軸軸接構型四搭配承載弧桿軸接構型二所構組球座標轉向機構之立體視圖、正視圖與側視圖 Figure 14 is a perspective view, front view and side view of a two-frame ball-coordinate steering mechanism of a twelve-axis shaft-conducting four-matched bearing shaft-axis configuration.
Claims (4)
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| TW105143085A TWI652430B (en) | 2016-12-23 | 2016-12-23 | Twelve axes mechanism for spherical coordinates orientating |
| CN201710025223.7A CN107030682B (en) | 2016-01-15 | 2017-01-13 | Twelve-axis spherical coordinate motion mechanism |
| JP2017005465A JP6912205B2 (en) | 2016-01-15 | 2017-01-16 | 12-axis spherical coordinate control device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| TW105143085A TWI652430B (en) | 2016-12-23 | 2016-12-23 | Twelve axes mechanism for spherical coordinates orientating |
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| Publication Number | Publication Date |
|---|---|
| TW201823624A TW201823624A (en) | 2018-07-01 |
| TWI652430B true TWI652430B (en) | 2019-03-01 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| TW105143085A TWI652430B (en) | 2016-01-15 | 2016-12-23 | Twelve axes mechanism for spherical coordinates orientating |
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| TW (1) | TWI652430B (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3979090A (en) | 1975-03-17 | 1976-09-07 | Sperry Rand Corporation | Velocity damped erection system for stable gyroscopic attitude and heading reference apparatus |
| US4270393A (en) | 1979-03-12 | 1981-06-02 | Martin Marietta Corporation | Isolation system |
| US6687645B2 (en) | 2001-06-28 | 2004-02-03 | Northrop Grumman Corporation | Motion and trajectory data generator for a multi-gimbaled rotating platform |
| TW201215443A (en) | 2010-10-04 | 2012-04-16 | Wen-Der Trui | A space disorientation mechanism by two tetrahedrons and eight arc-links |
| CN103470925A (en) | 2013-09-04 | 2013-12-25 | 中国科学院深圳先进技术研究院 | Automatic-control spatial rotating device |
-
2016
- 2016-12-23 TW TW105143085A patent/TWI652430B/en active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3979090A (en) | 1975-03-17 | 1976-09-07 | Sperry Rand Corporation | Velocity damped erection system for stable gyroscopic attitude and heading reference apparatus |
| US4270393A (en) | 1979-03-12 | 1981-06-02 | Martin Marietta Corporation | Isolation system |
| US6687645B2 (en) | 2001-06-28 | 2004-02-03 | Northrop Grumman Corporation | Motion and trajectory data generator for a multi-gimbaled rotating platform |
| EP1271100B1 (en) | 2001-06-28 | 2006-04-05 | Northrop Grumman Corporation | Motion and trajectory data generator for a multi-gimbaled rotating platform |
| TW201215443A (en) | 2010-10-04 | 2012-04-16 | Wen-Der Trui | A space disorientation mechanism by two tetrahedrons and eight arc-links |
| CN103470925A (en) | 2013-09-04 | 2013-12-25 | 中国科学院深圳先进技术研究院 | Automatic-control spatial rotating device |
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| Publication number | Publication date |
|---|---|
| TW201823624A (en) | 2018-07-01 |
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