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TW201037840A - Polyester film for solar cell, backsheet of solar cell using the same and solar cell - Google Patents

Polyester film for solar cell, backsheet of solar cell using the same and solar cell Download PDF

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Publication number
TW201037840A
TW201037840A TW099108818A TW99108818A TW201037840A TW 201037840 A TW201037840 A TW 201037840A TW 099108818 A TW099108818 A TW 099108818A TW 99108818 A TW99108818 A TW 99108818A TW 201037840 A TW201037840 A TW 201037840A
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film
solar cell
polyester film
solar
polyester
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TW099108818A
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Chinese (zh)
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TWI467776B (en
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Masato Ushijima
Kenta Morishita
Shigeru Aoyama
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Toray Industries
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    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/18Manufacture of films or sheets
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/06Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/06Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B27/08Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/36Layered products comprising a layer of synthetic resin comprising polyesters
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G63/00Macromolecular compounds obtained by reactions forming a carboxylic ester link in the main chain of the macromolecule
    • C08G63/02Polyesters derived from hydroxycarboxylic acids or from polycarboxylic acids and polyhydroxy compounds
    • C08G63/12Polyesters derived from hydroxycarboxylic acids or from polycarboxylic acids and polyhydroxy compounds derived from polycarboxylic acids and polyhydroxy compounds
    • C08G63/16Dicarboxylic acids and dihydroxy compounds
    • C08G63/18Dicarboxylic acids and dihydroxy compounds the acids or hydroxy compounds containing carbocyclic rings
    • C08G63/181Acids containing aromatic rings
    • C08G63/183Terephthalic acids
    • HELECTRICITY
    • H10SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
    • H10FINORGANIC SEMICONDUCTOR DEVICES SENSITIVE TO INFRARED RADIATION, LIGHT, ELECTROMAGNETIC RADIATION OF SHORTER WAVELENGTH OR CORPUSCULAR RADIATION
    • H10F19/00Integrated devices, or assemblies of multiple devices, comprising at least one photovoltaic cell covered by group H10F10/00, e.g. photovoltaic modules
    • H10F19/80Encapsulations or containers for integrated devices, or assemblies of multiple devices, having photovoltaic cells
    • HELECTRICITY
    • H10SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
    • H10FINORGANIC SEMICONDUCTOR DEVICES SENSITIVE TO INFRARED RADIATION, LIGHT, ELECTROMAGNETIC RADIATION OF SHORTER WAVELENGTH OR CORPUSCULAR RADIATION
    • H10F19/00Integrated devices, or assemblies of multiple devices, comprising at least one photovoltaic cell covered by group H10F10/00, e.g. photovoltaic modules
    • H10F19/80Encapsulations or containers for integrated devices, or assemblies of multiple devices, having photovoltaic cells
    • H10F19/85Protective back sheets
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/30Properties of the layers or laminate having particular thermal properties
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/30Properties of the layers or laminate having particular thermal properties
    • B32B2307/306Resistant to heat
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/30Properties of the layers or laminate having particular thermal properties
    • B32B2307/308Heat stability
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/40Properties of the layers or laminate having particular optical properties
    • B32B2307/416Reflective
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/70Other properties
    • B32B2307/714Inert, i.e. inert to chemical degradation, corrosion
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2457/00Electrical equipment
    • B32B2457/12Photovoltaic modules
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J2367/00Characterised by the use of polyesters obtained by reactions forming a carboxylic ester link in the main chain; Derivatives of such polymers
    • C08J2367/02Polyesters derived from dicarboxylic acids and dihydroxy compounds
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/50Photovoltaic [PV] energy
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/50Photovoltaic [PV] energy
    • Y02E10/52PV systems with concentrators

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Health & Medical Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Medicinal Chemistry (AREA)
  • Polymers & Plastics (AREA)
  • Organic Chemistry (AREA)
  • Materials Engineering (AREA)
  • Manufacture Of Macromolecular Shaped Articles (AREA)
  • Photovoltaic Devices (AREA)
  • Compositions Of Macromolecular Compounds (AREA)

Abstract

The present invention provides a polyester film for solar cell having excellent heat resistance and hydrolysis resistance, and a solar cell using the same has high durability. The present invention provides a polyester film for solar cell, wherein the concentration of carboxyl end group is less than 13eq/ton and the temperature of endothermic peak value of less than 220 DEG C is measured by a differential scanning calorimeter (DSC).

Description

201037840 六、發明說明: 【發明所屬之技術領域】 本發明係關於一種耐熱性與耐水解性優良的太陽電池 用聚酯膜、使用它之太陽電池背板及使用它之太陽電池》 【先前技術】 近年來,作爲半永久性且無公害之次世代能源之乾淨 能源的太陽能發電受到囑目,而太陽電池正急速地普及 中。作爲太陽電池背板之膜係已知可使用例如聚乙烯系樹 〇 脂和聚酯系樹脂薄片,及使用氟系薄膜(參照專利文獻1 〜3)。太陽電池多半設置於屋外,在這種情況下十分要求 對於自然環境的耐久性(耐候性、耐熱性、耐UV (紫外線) 性)。 先前技術文獻 專利文獻 專利文獻1 :日本專利特開平第11-26 1 08 5號公報。 專利文獻2:日本專利特開平第11-186575號公報。 Ο 專利文獻3 :日本專利特開第2006-270025號公報。 【發明內容】 但是,即便是專利文獻1〜3記載的膜,耐熱性與耐水 解性仍不足,防礙太陽電池在屋外之長期使用。 因此,本發明爲解決這些問題,欲提供一種同時具耐 熱性及耐水解性的太陽電池用聚酯膜、使用它之太陽電池 背板及太陽電池。 換言之,本發明係羧基末端基濃度爲l3eq/t〇n以下, 201037840 且根據示差掃描量熱法(DSC)所求得之微小吸熱峰値溫 度Tmeta ( °C )爲220°C以下的太陽電池用聚酯膜、使用它 之太陽電池背板及太陽電池。 根據本發明’可提供一種同時具耐熱性及耐水解性的 太陽電池用聚酯膜、使用它之太陽電池背板及太陽電池。 又’藉由使用它,太陽電池背板能能達成比習知更佳的耐 久性提升和薄型化等,故可讓太陽電池的耐久性提升、薄 型化等。 【實施方式】 本發明的膜必需爲聚酯膜。較佳,本發明的聚酯膜中, 相對於聚酯類之酯類成分,係由乙烯成分90mol%以上者所 調製而成,具有耐熱性和機械特性的特點,但作爲其它共 聚合成分可使用各種二羧酸或其酯類形成性誘導體與二醇 共聚者。可共聚合的二羧酸成分能列舉如:間苯二甲酸、 苯二甲酸、1,4-萘二甲酸、1,5-萘二甲酸、2,6·萘二甲酸、 4,4’-二苯基二羧酸、4,4’-二苯醚二羧酸、4,4’-二苯颯二羧 酸等。又,能共聚合的脂環族二羧酸成分可列舉如:1,4-環己烷二羧酸等。又,二醇成分可列舉如:乙二醇、1,2-丙二醇、新戊二醇、1,3-丁二醇、1,4-丁二醇、1,5-戊二醇、 1,6-己二醇、1,2-環己烷二甲醇、1,3-環己烷二甲醇、1,4-環己烷二甲醇、二甘醇、三甘醇、聚伸烷基二醇、2,2-雙 (4’β-羥乙氧基苯基)丙烷等之脂肪族、脂環族、芳香族 二醇等。這些成分可以僅使用一種,亦可兩種以上倂用。 所使用之聚酯熔點較佳爲耐熱性較佳的250°C以上者,而 201037840 3 00t以下者則對於生產性較佳。只要是在此範圍內,亦可 共聚合、混合其他成分。又,在該聚酯中,亦可添加各種 習知的添加劑,例如抗氧化劑、抗靜電劑、結晶成核劑、 無機粒子、有機粒子等。特別是,無機粒子或有機粒子可 有效地賦予膜表面易滑性,以提升膜的使用性。 聚酯可根據過去習知之聚酯製造方法進行製造。換言 之,可使用二烷基酯作爲酸成分,在其與二醇成分進行酯 交換反應後,在減壓環境下針對其反應生成物進行加熱, 〇 除去剩餘的二醇成分並且進行聚縮合的方式製成。又,也 可使用二羧酸作爲酸成分,並根據過去習知之直接聚合法 來製造。可使用鈦化合物、鋰化合物、鈣化合物、鎂化合 物、銻化合物、鍺化合物等作爲反應觸媒。如此獲得之聚 酯,由於採用固相聚合,因此更加可提升其聚合度,且可 降低羧基末端基濃度。該固相聚合係可在200〜25 0°c的乾 燥機中,且在ltorr以下的減壓環境下或氮氣氣流下所進行 者。 ® 在本發明中,爲了滿足耐水解性,聚酯膜的固有黏度 較佳在0.6〜1 .2dl/g的範圍內。更佳在0.65〜0.8dl/g的範 圍內,最佳在0.7〜0.8dl/g的範圍內。爲了提升耐水解性, 雖然較佳可提升固有黏度,但是當固有黏度超過1.2dl/g 時,必須延長聚酯樹脂製造時的固相聚合時間而使得成本 明顯增高,並非較佳選擇。另外在小於0.6 dl/g的情況中, 因較低的聚合度而明顯地降低耐熱性、耐水解性,並非較 佳選擇。可調整聚酯樹脂製造時的聚合條件以使得固有黏 201037840 度維持於前述較佳的範圍內。 在本發明中,爲了提升耐水解性’聚酯膜的羧基末端 基濃度必須在13eq (當量)/ton以下的範圍內。較佳在 1 2eq/ton以下,更佳在8eq/ton以下,最佳在5eq/ton以下。 雖然下限並無特別限制,但理論上下限爲Oeq/ton ° 爲使得羧基末端基濃度在前述的較佳範圍內’關於作 爲原料的聚酯樹脂,較佳係使用羧基末端基濃度較小的聚 酯樹脂。可藉由加長聚酯樹脂製造時的固相聚合時間來達 〇 到減少聚酯樹脂中羧基末端基濃度之目的。 又,爲使得羧基末端基濃度在前述的較佳範圍內,在 一較佳實施例中亦可使用封端劑。封端劑可列舉如:碳化 二亞胺化合物、噚唑啉化合物、環氧化合物、碳酸鹽化合 物等等。在製膜時與聚酯樹脂一同進行添加的效果較高。 較佳可使用碳化二亞胺化合物化合物,相對於聚酯膜整 體,使得其含有量爲0.3〜5重量%者爲佳。當然亦可同時 運用固相聚合及封端劑。 Θ 本發明之膜爲滿足足夠的耐水解性,根據示差掃描量 熱法(DSC)所求得之微小吸熱峰値溫度Tmeta ( °C )必須 在220 °C以下的範圍。較佳在205 °C以下、更佳在195 °C以 下。雖然下限並無特別限制,但是未滿1 50°C時熱收縮率 將顯著地提高,因此較佳在150°C以上。更佳在160°C以上。 可藉由改變製膜時的熱處理溫度以使得微小吸熱峰値 溫度在前述的較佳範圍內。雖然會因爲製膜時的膜厚與製 膜速度而有所不同,但熱處理溫度以22(TC以下者爲佳, 201037840 而本發明之膜的製膜方法及熱處理步驟細節如後述。 由於太陽電池的製造步驟多半爲熱接觸步驟,當太陽 電池用聚酯膜的熱收縮率過大時,在太陽電池的製造步驟 中,太陽電池用聚酯膜或太陽電池背板會產生收縮,有可 能導致太陽電池單元整體因此扭曲而產生裂縫。有鑑於 此’較佳本發明之膜的熱收縮率較小。具體而言,膜的長 邊方向(MD)及其橫向(TD)(有時稱作寬度方向)於 150 °C、30分鐘之熱收縮率較佳皆爲〇.6 %以下。更佳爲0.4% ^ 以下,更佳爲0.2%以下。又,熱收縮率較佳可爲—0.5%以 上。 再者,本發明中爲了提升耐水解性而較佳應降低熱處 理溫度,其結果可能會提高熱收縮率。因此,爲使得熱收 縮率達前述的較佳範圍內,較佳可採用後述(1)或(2) 其中一種方法(當然,亦可同時倂用(1)和(2)方法)^ 方法(1):在熱處理步驟中,針對膜進行熱處理的同 時,分別讓膜之MD方向和TD方向收縮0·5〜10%的方法》 〇 方法(2):針對完成製膜的膜採用其它設備(例如爐 等)以離線方式進行加熱處理的方法。在本方法中,加熱 溫度較佳爲150〜220 °C,而加熱時間較佳在10〜60秒之 間。 本發明之膜的平面配向係數爲0.130以上者爲佳。較 佳爲0.165以上、更佳爲0.168以上、又更佳爲0.170以上、 最佳爲0· 1 74以上。係可讓耐水解性更加提高。本發明所 稱之平面配向係數係使用阿貝折射計並根據下述公式(A^ 201037840 所求得。[Technical Field] The present invention relates to a polyester film for a solar cell excellent in heat resistance and hydrolysis resistance, a solar cell backsheet using the same, and a solar cell using the same. In recent years, solar power generation, which is a clean energy source of semi-permanent and pollution-free next-generation energy, has attracted attention, and solar cells are rapidly gaining popularity. As the film system of the solar battery back sheet, for example, a polyethylene-based resin and a polyester-based resin sheet, and a fluorine-based film can be used (see Patent Documents 1 to 3). Most of the solar cells are installed outside the house, and in this case, durability (weather resistance, heat resistance, and UV (UV) resistance) to the natural environment is highly demanded. PRIOR ART DOCUMENT Patent Document Patent Document 1: Japanese Patent Laid-Open No. Hei 11-26 1 08 5A. Patent Document 2: Japanese Laid-Open Patent Publication No. Hei 11-186575.专利 Patent Document 3: Japanese Patent Laid-Open No. 2006-270025. SUMMARY OF THE INVENTION However, even in the films described in Patent Documents 1 to 3, heat resistance and hydrolysis resistance are insufficient, which hinders long-term use of solar cells outside the house. Accordingly, the present invention has been made to solve such problems, and it is desired to provide a polyester film for a solar cell which has both heat resistance and hydrolysis resistance, a solar battery back sheet and a solar battery using the same. In other words, the present invention is a solar cell having a carboxyl end group concentration of 13 eq/t 〇 n or less, 201037840 and having a small endothermic peak temperature Tmeta ( ° C ) of 220 ° C or less according to differential scanning calorimetry (DSC). Use a polyester film, a solar cell backsheet using it, and a solar cell. According to the present invention, a polyester film for a solar cell having both heat resistance and hydrolysis resistance, a solar battery back sheet using the same, and a solar battery can be provided. Further, by using this, the solar cell backsheet can achieve better durability and thinner than conventional ones, so that the durability and thickness of the solar cell can be improved. [Embodiment] The film of the present invention must be a polyester film. Preferably, the polyester film of the present invention is prepared from an ester component of a polyester component in an amount of 90 mol% or more of an ethylene component, and has heat resistance and mechanical properties, but may be used as another copolymerization component. A copolymer of a dicarboxylic acid or an ester-forming form inducer and a diol is used. The copolymerizable dicarboxylic acid component can be exemplified by isophthalic acid, phthalic acid, 1,4-naphthalene dicarboxylic acid, 1,5-naphthalene dicarboxylic acid, 2,6 naphthalene dicarboxylic acid, 4,4'- Diphenyldicarboxylic acid, 4,4'-diphenyl ether dicarboxylic acid, 4,4'-diphenylindole dicarboxylic acid, and the like. Further, examples of the alicyclic dicarboxylic acid component which can be copolymerized include 1,4-cyclohexanedicarboxylic acid. Further, examples of the diol component include ethylene glycol, 1,2-propylene glycol, neopentyl glycol, 1,3-butylene glycol, 1,4-butanediol, 1,5-pentanediol, and 1, 6-hexanediol, 1,2-cyclohexanedimethanol, 1,3-cyclohexanedimethanol, 1,4-cyclohexanedimethanol, diethylene glycol, triethylene glycol, polyalkylene glycol An aliphatic, alicyclic or aromatic diol such as 2,2-bis(4'β-hydroxyethoxyphenyl)propane. These components may be used alone or in combination of two or more. The melting point of the polyester to be used is preferably 250 ° C or more in which heat resistance is preferable, and the productivity is preferably in the case of 201037840 3 00 t or less. As long as it is within this range, other components may be copolymerized and mixed. Further, various additives such as an antioxidant, an antistatic agent, a crystal nucleating agent, inorganic particles, organic particles and the like may be added to the polyester. In particular, inorganic particles or organic particles can effectively impart smoothness to the surface of the film to improve the usability of the film. The polyester can be produced according to a conventional polyester production method. In other words, a dialkyl ester can be used as the acid component, and after the transesterification reaction with the diol component, the reaction product is heated under reduced pressure, and the remaining diol component is removed and polycondensed. production. Further, a dicarboxylic acid can also be used as an acid component, and it can be produced by a conventional direct polymerization method. As the reaction catalyst, a titanium compound, a lithium compound, a calcium compound, a magnesium compound, a ruthenium compound, a ruthenium compound or the like can be used. The polyester thus obtained, by solid phase polymerization, can further increase the degree of polymerization and lower the concentration of the carboxyl end group. The solid phase polymerization can be carried out in a dryer of 200 to 250 ° C under a reduced pressure atmosphere of ltorr or under a nitrogen gas stream. In the present invention, in order to satisfy the hydrolysis resistance, the inherent viscosity of the polyester film is preferably in the range of 0.6 to 1.2 dl/g. More preferably, it is in the range of 0.65 to 0.8 dl/g, and most preferably in the range of 0.7 to 0.8 dl/g. In order to improve the hydrolysis resistance, although it is preferable to increase the intrinsic viscosity, when the intrinsic viscosity exceeds 1.2 dl/g, it is necessary to lengthen the solid phase polymerization time in the production of the polyester resin, so that the cost is remarkably increased, which is not preferable. Further, in the case of less than 0.6 dl/g, heat resistance and hydrolysis resistance are remarkably lowered due to a low degree of polymerization, which is not a preferable choice. The polymerization conditions at the time of production of the polyester resin can be adjusted so that the intrinsic viscosity of 201037840 is maintained within the above preferred range. In the present invention, in order to enhance the hydrolysis resistance, the carboxyl group end group concentration of the polyester film must be in the range of 13 eq (equivalent) / ton or less. It is preferably 1 2 eq/ton or less, more preferably 8 eq/ton or less, and most preferably 5 eq/ton or less. Although the lower limit is not particularly limited, the theoretical lower limit is Oeq/ton ° such that the carboxyl terminal group concentration is within the above preferred range. With regard to the polyester resin as a raw material, it is preferred to use a polycondensation having a small carboxyl terminal group concentration. Ester resin. The purpose of reducing the concentration of the carboxyl end group in the polyester resin can be achieved by lengthening the solid phase polymerization time in the production of the polyester resin. Further, in order to make the carboxyl terminal group concentration within the above preferred range, a terminal blocking agent can also be used in a preferred embodiment. The blocking agent may, for example, be a carbodiimide compound, an oxazoline compound, an epoxy compound, a carbonate compound or the like. The effect of adding together with the polyester resin at the time of film formation is high. It is preferred to use a carbodiimide compound compound, and it is preferably contained in an amount of from 0.3 to 5% by weight based on the total amount of the polyester film. Of course, solid phase polymerization and blocking agents can also be used at the same time. Θ The film of the present invention satisfies sufficient hydrolysis resistance, and the micro endothermic peak temperature Tmeta (°C) obtained by differential scanning calorimetry (DSC) must be in the range of 220 ° C or less. It is preferably 205 ° C or lower, more preferably 195 ° C or lower. Although the lower limit is not particularly limited, the heat shrinkage rate is remarkably improved when the temperature is less than 150 ° C, and therefore it is preferably 150 ° C or more. More preferably at 160 ° C or above. The temperature of the heat treatment at the time of film formation can be changed so that the temperature of the minute endothermic peak 在 is within the above preferred range. Although the film thickness at the time of film formation differs from the film forming speed, the heat treatment temperature is preferably 22 (TC or less, 201037840), and the film forming method and heat treatment step of the film of the present invention will be described later. Most of the manufacturing steps are thermal contact steps. When the heat shrinkage rate of the polyester film for solar cells is too large, in the manufacturing process of the solar cell, the polyester film or the solar cell back sheet of the solar cell may shrink, possibly causing the sun. The entire battery unit is thus twisted to cause cracks. In view of the above, the film of the present invention preferably has a small heat shrinkage rate. Specifically, the long side direction (MD) of the film and its transverse direction (TD) (sometimes referred to as width) The heat shrinkage rate at 150 ° C for 30 minutes is preferably 〇 6 % or less, more preferably 0.4% ^ or less, more preferably 0.2% or less. Further, the heat shrinkage rate is preferably -0.5%. Further, in the present invention, in order to improve hydrolysis resistance, it is preferred to lower the heat treatment temperature, and as a result, the heat shrinkage ratio may be increased. Therefore, in order to achieve a heat shrinkage ratio within the above preferred range, it is preferred to use the latter. (1) or (2) One of the methods (of course, the methods (1) and (2) can also be used at the same time). Method (1): In the heat treatment step, while the film is heat-treated, the MD direction and the TD direction of the film are respectively contracted by 0. 5 to 10% of the method 〇 Method (2): A method of performing heat treatment on an off-line basis using a film (for example, a furnace, etc.) for the film to be formed into a film. In the method, the heating temperature is preferably 150 to 220 °. C, and the heating time is preferably between 10 and 60 seconds. The film of the present invention preferably has a plane alignment coefficient of 0.130 or more, preferably 0.165 or more, more preferably 0.168 or more, still more preferably 0.170 or more, and most Preferably, it is 0. 1 74 or more, and the hydrolysis resistance is further improved. The plane alignment coefficient referred to in the present invention is obtained by using an Abbe refractometer according to the following formula (A^201037840).

(A) 平面配向係數=(nMD + nTD ) /2-nZD 前述公式(A)中,nMD代表膜之長邊方向(MD)的 折射率、nTD代表膜之橫向(TD )的折射率、nZD代表膜 之厚度方向的折射率。 藉由提升製膜時的延伸倍率可達成使得膜之平面配向 係數維持前述之數値範圍內。較佳可將膜之長邊方向(MD) 及膜之橫向(TD)的延伸倍率皆調整至2.5〜6.0倍,而爲 了使得膜之平面配向係數達0.165以上,MD及TD方向的 延伸倍率各自調整至3.0〜5.0倍者較佳。再者,膜之平面 配向係數的上限雖無特別限制,但是如爲了提升平面配向 係數而繼續增加延伸倍率時,會使得製膜安定性惡化,因 此從生產性之觀點來看,較佳爲0.200以下,更佳爲0.185 以下。 關於本發明之膜,根據示差掃描量熱法(DSC )所求 得之微小吸熱峰値溫度Tmeta (°C)與膜之平面配向係數 B2較佳滿足以下公式(B)。 (B) B2^ 0.0 0 0 8 6 X Tmeta-0.0 0 2 8 6 ° 滿足公式(B )時,可提升耐水解性(於125 °C、濕度 100%的條件下放置72小時之後的平均伸度保持率等)。 本發明較佳可在膜中添加抑制水解之降解化合物。較 佳含有特別磷化合物。因此,本發明較佳以螢光X光測量 時聚酯膜中的磷原子量爲200ppm以上。更佳爲300ppm以 上’更佳爲400ppm以上。磷化合物較佳可使用磷酸、亞磷 201037840 酸、膦酸、該些的甲酯、乙酯、苯基、半酯以及其它誘導 體所組成之群組中所選出之一種以上的磷化合物。較佳本 發明特別可爲磷酸、亞磷酸、膦酸的甲酯、乙酯、苯基。 又,磷化合物的含有方法較佳可在製造聚酯原料基片的同 時添加磷化合物。 作爲太陽電池背板使用時,以較不易因太陽光產生劣 化影響者爲佳。因此,可在膜中添加UV (紫外線)吸收劑 及反射UV特性之物質。又,在一較佳實施例中至少於一 側膜表面,波長400〜7 OOnm的平均反射率爲80%以上。更 佳爲85%以上,最佳爲90%以上。藉由使得波長400〜700nm 的平均反射率達80%以上,於太陽光直接照射之情況下利 用本發明之膜之太陽電池的亦不容易造成膜之劣化。 使得波長400〜700nm之平均反射率達80%以上的方 法係可讓膜中含有無機粒子之方法、抑或藉由加入聚酯與 非相溶樹脂而在聚酯膜中產生空隙之方法。適合前者所使 用的無機粒子例如有:濕式及乾二氧化矽、膠態二氧化矽、 碳酸鈣、鋁矽酸鹽、磷酸鈣、氧化鋁、碳酸鎂、碳酸鋅、 鈦氧化物、氧化鋅(鋅白)、氧化銻、氧化鈽、氧化锆、氧 化錫、氧化鑭、氧化鎂、碳酸鋇、碳酸鋅、碳酸鉛(鉛白)、 硫酸鋇、硫酸鈣、硫酸鉛、硫化鋅、雲母、雲母鈦、滑石、 黏土、高嶺土、氟化鋰及氟化鈣等,但是較佳特別可爲二 鈦氧化物、硫酸鋇。相對於聚酯膜整體,無機粒子的含有 量以5〜5 5重量%爲佳,較佳爲5〜3 5重量%。若含有量少 於前述範圍時,會形成反射率劣化的膜,相反地若含有量 201037840 多於前述範圍時,膜在進行延伸時容易產生破裂,會降低 生產性。在重視生產性的情況下,本發明之膜較佳具有2 層以上的聚酯層。在具有2層以上聚酯層的情況下,於其 中任一層聚酯層中,前述無機粒子以5〜5 5重量%爲佳(相 對於該聚酯層)。更佳以含有5〜35重量%爲佳。雖然另一 層聚酯層的無機粒子含有量並無特別限制,但是含有量越 小,可更提升生產性。 又,作爲在後者方法中所使用之聚酯的非相溶樹脂, Ο 較佳使用:聚乙烯、聚丙烯、聚丁烯、聚戊烯等之聚烯烴 樹脂、聚苯乙烯樹脂、聚丙烯樹脂、聚碳酸酯樹脂、聚丙 烯腈樹脂、聚苯硫醚樹脂及氟系樹脂。該些非相溶樹脂可 爲均聚物或共聚物,亦可爲並用2種以上的非相溶樹脂。 其中較佳爲表面張力小的聚丙烯及聚戊烯等聚烯烴樹脂, 最佳爲聚戊烯。該聚戊烯與聚酯之間的表面張力差相對於 地較大,且熔點高,其特徵爲每單位添加量所能產生之形 成空洞的效果較佳,是特別合適的非相溶樹脂。含有非相 ^ 溶樹脂的情況中,相對於聚酯膜整體,該份量以〇·5〜20 重量%爲佳,較佳在0.5〜10重量%的範圍內。含有量較前 述範圍更少的情況中,會形成反射率劣化的膜,相反地含 有量較前述範圍更多的情況中,由於降低了膜整體的密 度,因此膜在進行延伸時容易產生破裂,會降低生產性。 本發明爲了更加提升耐水解性,較佳至少具有2層以 上的聚酯層。最佳,係層積有耐水解性特別優良之層以及 波長400〜7OOnm平均反射率在80%以上之層,前述結構從 -10- 201037840 特性和成本方面來看是有利的° 本發明之太陽電池用聚酯膜於125 °C、濕度100%的條 件下,放置4 8小時之後的平均伸度保持率達5 0%以上者爲 佳。較佳爲55%以上,更佳爲60%以上,最佳在65%以上, 特佳在70%以上。平均伸度保持率未滿50 %時,將降低長 期使用時的機械強度,其結果是,使用具有以其作爲背板 的太陽電池時,若施加任何來自外部的衝撃於太陽電池上 (例如,太陽電池被落石等擊中之情況等),有可能會讓背 〇 板斷裂等,並非較佳選擇。於本發明之太陽電池用聚酯膜 中,藉由讓平均伸度保持率達50%以上,可提高長期使用 時之背板機械強度的耐久性。 本發明之太陽電池用聚酯膜於125 °C、濕度100%的條 件下,放置72小時之後的平均伸度保持率較佳在1 〇%以 上。前述於125°C、濕度1〇〇%的條件下,放置72小時之 後的平均伸度保持率實驗係較放置48小時之後的平均伸 度保持率實驗更爲嚴峻的促進試驗。因此,太陽電池用途 0 等特別要求長時間之耐久性的用途之情況,可使用72小時 之後的平均伸度保持率作爲評價指標。72小時之後的平均 伸度保持率較佳在20%以上,更佳在30%以上,最佳在40% 以上,特佳在50%以上。 當72小時之後的平均伸度保持率小於1 〇%時,作爲太 陽電池用薄膜時,將明顯降低長期使用時內部的機械強 度。因此,若施加任何來自外部的衝擊於太陽電池上(例 如,太陽電池被落石擊中等情況),有可能會讓背板斷裂 -11- 201037840 等,並非較佳選擇。 又,包含有1片以上的本發明太陽電池用聚酯膜之太 陽電池背板,於125°C、濕度100%的條件下,放置48小 時之後的平均伸度保持率較佳在50%以上。依前述方法所 求得之平均伸度保持率5 5%以上者爲佳,較佳在60%以上, 更佳在65%以上,最佳在70%以上。 爲使得平均伸度保持率維持於前述較佳範圍內,本發 明之太陽電池用聚酯膜的厚度相對於背板整體厚度的比例 ^ 較佳在5〜100%之間。換言之,爲了更加提升平均伸度保 持率,較佳本發明之太陽電池用聚酯膜的厚度應更爲加厚。 以下記載本發明之聚酯膜的具體製造方法(一實施 例)。 首先,依需要將聚對苯二甲酸乙二醇酯(PET)樹脂置 於氮氣環境或真空環境中進行乾燥。接著,將乾燥之聚酯 樹脂供給單螺桿或雙螺桿擠出機後進行熔融擠出,而藉由 T型模具在冷卻筒上排出成薄片狀,以獲得未延伸薄片。 Ο 其次,針對該未延伸膜沿長邊方向進行延伸之後’再 沿寬度方向進行延伸,或者於沿寬度方向進行延伸之後, 再沿長邊方向進行延伸(逐次雙軸延伸方法)’亦或者可大 約同時地延伸膜之長邊方向與寬度方向(同時雙軸延伸方 法)來進行延伸。 延伸之後,再進行膜之熱處理。熱處理可藉由拉幅機、 加熱爐中或於加熱輥上等過去習知之任意方法來進行。該 熱處理雖然一般係在聚酯之熔點以下的溫度進行’本發明 -12- 201037840 爲使得Tmeta ( °C )在220°C以下,故熱處理溫度在22〇t 以下者爲佳。較佳在2 1 0 °C以下,更佳在2 0 0 °C以下,最佳 在1 90°C以下。熱處理溫度的下限雖無特別限制,但是在 未滿150°C時熱收縮率將明顯提升,因此較佳在150°C以 上,更佳在1 6 0 °C以上。 其次,亦可將膜朝長邊方向及/或寬度方向進行鬆驰的 同時進行熱處理。接著,將經前述熱處理的膜捲曲成形, 便可獲得本發明之膜。 ^ 又,亦可進行多次熱處理步驟,但此一情況中,最高 溫之熱處理步驟的熱處理溫度在22(TC以下者爲佳。較佳 在2 10°C以下,更佳在200°C以下,最佳在190°C以下》 〔特性的評價方法〕 (1 )固有黏度 將膜溶解至鄰氯苯酚中,於25 °C測量出溶液黏度,並 根據以下公式得到固有黏度。(A) Plane alignment coefficient = (nMD + nTD ) / 2-nZD In the above formula (A), nMD represents the refractive index of the long side direction (MD) of the film, nTD represents the transverse direction (TD) of the film, nZD Represents the refractive index in the thickness direction of the film. By increasing the stretching ratio at the time of film formation, it is achieved that the plane alignment coefficient of the film is maintained within the aforementioned range. Preferably, the longitudinal direction (MD) of the film and the transverse direction (TD) of the film are adjusted to 2.5 to 6.0 times, and in order to make the plane alignment coefficient of the film reach 0.165 or more, the MD and TD directions are respectively extended. It is preferred to adjust to 3.0 to 5.0 times. Further, although the upper limit of the plane alignment coefficient of the film is not particularly limited, if the stretching ratio is continuously increased in order to increase the plane alignment coefficient, the film stability is deteriorated, so from the viewpoint of productivity, it is preferably 0.200. Hereinafter, it is more preferably 0.185 or less. With respect to the film of the present invention, the micro endothermic peak temperature Tmeta (°C) obtained by differential scanning calorimetry (DSC) and the plane alignment coefficient B2 of the film preferably satisfy the following formula (B). (B) B2^ 0.0 0 0 8 6 X Tmeta-0.0 0 2 8 6 ° When formula (B) is satisfied, hydrolysis resistance can be improved (average elongation after 72 hours at 125 ° C and 100% humidity) Degree retention rate, etc.). In the present invention, it is preferred to add a degradation compound which inhibits hydrolysis to the film. It is preferred to contain a special phosphorus compound. Therefore, in the present invention, the amount of phosphorus atoms in the polyester film is preferably 200 ppm or more as measured by fluorescent X-ray. More preferably, it is 300 ppm or more and more preferably 400 ppm or more. As the phosphorus compound, preferably one or more phosphorus compounds selected from the group consisting of phosphoric acid, phosphorous acid, acid, phosphonic acid, methyl ester, ethyl ester, phenyl group, half ester, and other inducers may be used. Preferably, the invention may specifically be a methyl ester, an ethyl ester or a phenyl group of phosphoric acid, phosphorous acid or phosphonic acid. Further, the method of containing the phosphorus compound is preferably carried out by adding a phosphorus compound while producing a polyester raw material substrate. When used as a solar cell backsheet, it is preferable to be less susceptible to deterioration by sunlight. Therefore, a UV (ultraviolet) absorber and a substance that reflects UV characteristics can be added to the film. Further, in a preferred embodiment, the average reflectance of the wavelength of 400 to 700 nm is 80% or more on at least one of the film surfaces. More preferably, it is 85% or more, and the best is more than 90%. By making the average reflectance of the wavelength of 400 to 700 nm 80% or more, the solar cell using the film of the present invention in the case of direct sunlight irradiation is less likely to cause deterioration of the film. The method of making the average reflectance of the wavelength of 400 to 700 nm by 80% or more is a method of allowing the film to contain inorganic particles, or a method of generating a void in the polyester film by adding a polyester and a non-compatible resin. Suitable inorganic particles for the former are: wet and dry cerium oxide, colloidal cerium oxide, calcium carbonate, aluminosilicate, calcium phosphate, aluminum oxide, magnesium carbonate, zinc carbonate, titanium oxide, zinc oxide. (zinc white), cerium oxide, cerium oxide, zirconium oxide, tin oxide, antimony oxide, magnesium oxide, barium carbonate, zinc carbonate, lead carbonate (lead white), barium sulfate, calcium sulfate, lead sulfate, zinc sulfide, mica, Mica titanium, talc, clay, kaolin, lithium fluoride, calcium fluoride, and the like, but preferably, particularly, titanium oxide or barium sulfate. The content of the inorganic particles is preferably 5 to 55% by weight, preferably 5 to 5% by weight, based on the entire polyester film. When the content is less than the above range, a film having a deteriorated reflectance is formed. Conversely, when the content of 201037840 is more than the above range, the film is likely to be broken when it is stretched, and productivity is lowered. In the case where productivity is important, the film of the present invention preferably has two or more layers of polyester. In the case of having two or more polyester layers, in any of the polyester layers, the inorganic particles are preferably 5 to 5% by weight (relative to the polyester layer). More preferably, it is contained in an amount of 5 to 35% by weight. Although the inorganic particle content of the other polyester layer is not particularly limited, the smaller the content, the more the productivity can be improved. Further, as the non-compatible resin of the polyester used in the latter method, Ο is preferably used: a polyolefin resin such as polyethylene, polypropylene, polybutene or polypentene, a polystyrene resin, or a polypropylene resin. , polycarbonate resin, polyacrylonitrile resin, polyphenylene sulfide resin and fluorine resin. These non-compatible resins may be a homopolymer or a copolymer, or two or more kinds of incompatible resins may be used in combination. Among them, a polyolefin resin such as polypropylene having a small surface tension and polypentene is preferable, and polypentene is preferable. The difference in surface tension between the polypentene and the polyester is relatively large and has a high melting point, and is characterized in that the effect of forming voids per unit addition amount is preferable, and is a particularly suitable non-compatible resin. In the case of containing a non-phase-soluble resin, the amount is preferably from 5 to 20% by weight, preferably from 0.5 to 10% by weight, based on the total amount of the polyester film. When the content is less than the above range, a film having a deteriorated reflectance is formed. Conversely, when the content is more than the above range, since the density of the entire film is lowered, the film is liable to be broken when it is stretched. Will reduce productivity. In order to further improve the hydrolysis resistance, the present invention preferably has at least two or more polyester layers. Preferably, the layer is laminated with a layer excellent in hydrolysis resistance and a layer having a wavelength of 400 to 700 nm and an average reflectance of 80% or more, and the foregoing structure is advantageous from the viewpoint of characteristics and cost of -10-201037840. It is preferable that the polyester film for a battery has an average elongation retention ratio of 50% or more after being left for 48 hours at 125 ° C and a humidity of 100%. It is preferably 55% or more, more preferably 60% or more, most preferably 65% or more, and particularly preferably 70% or more. When the average elongation retention ratio is less than 50%, the mechanical strength in long-term use is lowered, and as a result, when a solar cell having the same as the backing plate is used, if any externally applied surface is applied to the solar cell (for example, When the solar cell is hit by a falling stone or the like, it may cause the backing plate to break, etc., which is not a preferable choice. In the polyester film for a solar cell of the present invention, by maintaining the average elongation retention ratio of 50% or more, the durability of the mechanical strength of the back sheet during long-term use can be improved. The polyester film for a solar cell of the present invention preferably has an average elongation retention ratio of at most 1% by weight after being left for 72 hours at 125 ° C and a humidity of 100%. The above average elongation retention test after 72 hours of storage at 125 ° C and a humidity of 1% was more severe than the average elongation retention test after 48 hours of the test. Therefore, in the case of applications such as solar cell use 0 that require long-term durability, the average elongation retention rate after 72 hours can be used as an evaluation index. The average elongation retention after 72 hours is preferably 20% or more, more preferably 30% or more, most preferably 40% or more, and particularly preferably 50% or more. When the average elongation retention rate after 72 hours is less than 1%, the film strength for the solar cell will significantly reduce the internal mechanical strength during long-term use. Therefore, if any external impact is applied to the solar cell (for example, if the solar cell is hit by a falling stone), the back plate may be broken -11-201037840, etc., which is not a preferred choice. Moreover, the solar cell back sheet containing one or more polyester films for solar cells of the present invention preferably has an average elongation retention ratio of 50% or more after being left for 48 hours at 125 ° C and a humidity of 100%. . The average elongation retention ratio obtained by the above method is preferably 55% or more, preferably 60% or more, more preferably 65% or more, and most preferably 70% or more. In order to maintain the average elongation retention ratio within the above preferred range, the ratio of the thickness of the polyester film for a solar cell of the present invention to the overall thickness of the back sheet is preferably between 5 and 100%. In other words, in order to further increase the average elongation retention ratio, it is preferred that the thickness of the polyester film for a solar cell of the present invention should be more thick. Hereinafter, a specific production method (one embodiment) of the polyester film of the present invention will be described. First, the polyethylene terephthalate (PET) resin is dried in a nitrogen atmosphere or a vacuum atmosphere as needed. Next, the dried polyester resin is supplied to a single-screw or twin-screw extruder, melt-extruded, and discharged into a sheet shape on a cooling cylinder by a T-die to obtain an unstretched sheet. Ο Next, after the unstretched film is extended in the longitudinal direction, it is extended in the width direction, or after extending in the width direction, and then extended in the longitudinal direction (sequential biaxial stretching method) The extension is performed by extending the longitudinal direction and the width direction of the film at the same time (simultaneous biaxial stretching method). After the extension, heat treatment of the film is performed. The heat treatment can be carried out by any conventional method known in the art such as a tenter, a heating furnace or a heating roll. Although the heat treatment is generally carried out at a temperature lower than the melting point of the polyester, the present invention -12-201037840 is such that Tmeta (°C) is at most 220 ° C, so that the heat treatment temperature is preferably 22 〇t or less. It is preferably at most 2 1 ° C, more preferably below 200 ° C, and most preferably below 1 90 ° C. The lower limit of the heat treatment temperature is not particularly limited, but the heat shrinkage rate is remarkably improved at less than 150 ° C, so it is preferably at least 150 ° C, more preferably at least 160 ° C. Next, the film may be heat-treated while being relaxed in the longitudinal direction and/or the width direction. Next, the film of the present invention can be obtained by crimping the film subjected to the above heat treatment. ^ Further, a plurality of heat treatment steps may be performed, but in this case, the heat treatment temperature of the highest temperature heat treatment step is preferably 22 (TC or less, preferably 2 10 ° C or lower, more preferably 200 ° C or lower). (Optimum below 190 °C) [Evaluation method of characteristics] (1) Intrinsic viscosity The film was dissolved in o-chlorophenol, and the viscosity of the solution was measured at 25 ° C, and the intrinsic viscosity was obtained according to the following formula.

nsp/C=〔r(〕+Κ〔η〕2 · C 〇 此處,nsp=(溶液黏度/溶劑黏度)-1,C係100ml 溶劑中含有的溶解聚合物重量(本次測量爲lg/10 〇ml),K 係Huggins常數(0.3 43 )。又,溶液黏度及溶劑黏度係使 用奧斯特華德(Ostwald)黏度計測量出來的。 (2) 羧基末端基濃度 將〇.5g的膜溶解至〇-甲酚中,使用氫氧化鉀進行電位 差滴定的方式來測量,以求得羧基末端基濃度。 (3) 根據示差掃描量熱法(DSC )來求得微小吸熱峰 -13- 201037840 値溫度τ m e t a ( °c ) 微小吸熱峰値溫度Tmeta(°C )係依據JISK7122-1987 (參照JIS手冊1999年版)使用精工電子工業(公司) (Seiko Instruments ) 製造之示差掃描量熱法設備 「DSC-RDC220自動控制設備」’且分析資料時係使用碟片 (Sessions Disc)「SSC/5200」所測量得出。在坦渦中抨量 5mg的膜,以20°C/分的升溫速度從25°C升溫至300。(:並且 測量。以所獲得之示差掃描量熱法圖表中結晶溶解峰値前 的微小吸熱峰値溫度作爲Tmeta ( °c )。若是難以觀察微小 吸熱峰値時,則在資料分析部將峰値附近放大,進而讀取 峰値。 雖然JIS中沒有記載微小吸熱圖表的讀取方法,不過 可根據以下方法來進行。首先,畫出135 °c與155 °c値的直 線,以求得與圖表曲線之吸熱側的面積。同樣地求出140 °C 與 160°C、145°C 與 165°C、150°C 與 17(TC、155°C 與 175°C、 160°C 與 180°C、165°C 與 185°C、170°C 與 190°C、175°C 與 ❹ 195°C、180°C 與 200°C、185°C 與 205°C、190°C 與 210°C、 195°C 與 215°C、200°C 與 220°C、205 °C 與 225°C、210°C 與 230°C、215°C 與 235 °C、220°C 與 240°C 等 17 處的面積。微 小峰値的吸熱量通常爲〇·2〜5.0J/g,因此僅取0.2J/g以 上、5. (U/g以下的資料作爲有效數據。在總計18個面積數 據中,以有效數據中面積最大之數據資料的溫度領域中的 吸熱峰値之峰値溫度作爲Tmeta ( °C )。在無有效數據的情 況下,則沒有Tmeta ( °C )。圖表範例如第1圖所示。 -14- 201037840 (4) 熱收縮率 依據JIS-C23 1 8 ( 2007 ),將寬度10mm、標記間隙約 100mm的樣本於溫度150°C、負載0.5g進行30分鐘熱處 理。使用TECHNO NEEDS COMPANY LTD.製造之熱收縮率 測量器(AMM- 1號機)並針對該熱處理前後的標記間隙進 行測量,且根據下列公式計算出熱收縮率。 熱收縮率(%) ={(L0-L) /L0} χΙΟΟ L0 :加熱處理前的標記間隙 ^ L :加熱處理後的標記間隙 (5) 平面配向係數 使用愛宕(ATAGO )公司製造之ABBE阿貝式折射計 type 4T,以鈉氣燈作爲光源進行薄膜折射率的測量。Nsp/C=[r(]+Κ[η]2 · C 〇 where nsp=(solution viscosity/solvent viscosity)-1, C system 100ml Solvent polymer weight contained in the solvent (this measurement is lg/ 10 〇ml), K system Huggins constant (0.3 43). Also, the solution viscosity and solvent viscosity were measured using an Ostwald viscometer. (2) The carboxyl end group concentration will be 〇.5g of film. It is dissolved in hydrazine-cresol and measured by potentiometric titration using potassium hydroxide to determine the concentration of the carboxyl end group. (3) The micro endothermic peak is obtained by differential scanning calorimetry (DSC)-13- 201037840値temperature τ meta ( °c ) The micro endothermic peak temperature Tmeta (°C ) is based on JIS K7122-1987 (refer to the JIS Handbook 1999 edition) using the differential scanning calorimetry equipment manufactured by Seiko Instruments. The DSC-RDC220 automatically controls the device'' and analyzes the data using the Discs Discs "SSC/5200". The 5mg film is measured in a vortex at a temperature increase rate of 20 °C / min from 25 °C is raised to 300. (: and measured. With the differential scanning calorimetry obtained In the table, the micro endothermic peak temperature before the peak of the crystal dissolution is Tmeta (°c). If it is difficult to observe the micro endothermic peak, the data analysis unit enlarges the peak and the peak, and then reads the peak. The method of reading the micro endothermic chart is described, but it can be performed by the following method. First, draw a straight line of 135 °c and 155 °c値 to obtain the area on the heat absorbing side of the graph curve. C with 160 ° C, 145 ° C and 165 ° C, 150 ° C and 17 (TC, 155 ° C and 175 ° C, 160 ° C and 180 ° C, 165 ° C and 185 ° C, 170 ° C with 190°C, 175°C and ❹195°C, 180°C and 200°C, 185°C and 205°C, 190°C and 210°C, 195°C and 215°C, 200°C and 220 The area of 17 °C, such as °C, 205 °C and 225 °C, 210 °C and 230 °C, 215 °C and 235 °C, 220 °C and 240 °C. The heat absorption of the tiny peaks is usually 〇· 2 to 5.0 J/g, so only 0.2 J/g or more and 5. (U/g or less) is used as valid data. Among the total of 18 area data, the temperature data area of the largest area of the effective data is in the temperature field. Endothermic The peak temperature as Zhi Zhi Tmeta (° C). In the absence of valid data, there is no Tmeta ( °C ). The chart is shown in Figure 1. -14- 201037840 (4) Heat shrinkage rate According to JIS-C23 1 8 (2007), a sample having a width of 10 mm and a mark gap of about 100 mm was heat-treated at a temperature of 150 ° C and a load of 0.5 g for 30 minutes. The heat shrinkage rate measuring device (AMM-1 No. 1) manufactured by TECHNO NEEDS COMPANY LTD. was used and the mark gap before and after the heat treatment was measured, and the heat shrinkage rate was calculated according to the following formula. Heat shrinkage rate (%) = {(L0-L) / L0} χΙΟΟ L0 : Marking gap before heat treatment ^ L : Marking gap after heat treatment (5) Plane alignment coefficient using ABBE manufactured by ATAGO The shell type refractometer type 4T uses a sodium gas lamp as a light source to measure the refractive index of the film.

(A ) 平面配向係數=(nMD + nTD ) /2-nZD 前述公式(A)中,nMD代表膜之長邊方向(MD)的 折射率、nTD代表膜之橫向(TD )的折射率、nZD代表膜 之厚度方向的折射率。 〇 (6) 以螢光X光測定法來量測磷原子含有量 根據螢光X光法(Rigaku公司製造之ZSXIOOe)測量 磷原子的含有量。 (7) 波長400〜700nm的平均反射率 在分光光度計(島津製作所UV245 0 )中安裝積分球附 屬設備(島津製作所製造之ISR2200 ),以硫酸鋇作爲標準 板,以100%標準板之相對反射率作爲量測値。在波長400 〜700nm中,測量波長每0.5nm的相對反射率,並以該些 -15- 201037840 相對反射率的平均値作爲平均反射率。 (8 )於125 °C、濕度100%的條件下放置48小時之後 的伸度保持率 斷裂伸度的測量係依據AS TM-D 8 8 2-97 (參照1 999年 版ASTM年度標準索引手冊(ANNUAL BOOK OF ASTM STANDARDS)),將樣x本切成lcmx20cm的大小,於夾具 間距爲5cm、拉伸速度爲3 00mm/min時,測量拉伸時的斷 裂伸度(初始)。又,針對5個樣本進行測量,以所得之該 〇 平均値作爲斷裂伸度(初始)A0。 其次,將樣本切成lcmx20cm的大小,使用ESPEC CORP. 製造之高度加速壽命試驗設備EHS-221MD,於125°C、濕 度 100%的條件下進行 48小時的處理之後,依據 ASTM-D882-97C參照1999年版ASTM年度標準索引手冊) 的處理後樣本斷裂伸度,於夾具間距圍5cm、拉伸速度爲 3 0 0mm/min時,測量拉伸時的斷裂伸度(處理後)。又,針 對5個樣本進行測量,以所得之該平均値作爲斷裂伸度(處 理後)A 1。 使用求得之斷裂伸度A0及A1,依據以下公式(1)計 算出伸度保持率。 伸度保持率(% ) =A1/A〇x 100 ( 1 ) 又,依據以下公式(2)計算出平均伸度保持率。 平均伸度保持率(%) = (MD方向伸度保持率+ TD方 向伸度保持率)/2 ( 2 ) 另外,即使使用平山製作所之高加速壽命試驗設備 -16- 201037840 (HAST設備)PC-30 4R8D進行測量,會獲得與使用ESPEC CORP.之高度加速壽命試驗設備EHS-221MD進行測量時相 同的數値,因此亦可使用平山製作所之高加速壽命試驗設 備(HAST設備)PC-304R8D進行測量。 (9 )於125 °C、濕度100%的條件下放置72小時之後 的伸度保持率 斷裂伸度的測量係依據ASTM-D882-97 (參照1999年 版ASTM年度標準索引手冊),將樣本切成lcmx20cm的大 ^ 小,於夾具間距爲5cm、拉伸速度爲3 00mm/min時,測量 拉伸時的斷裂伸度(初始)。又,針對5個樣本進行測量, 以所得之該平均値作爲斷裂伸度(初始)A2。 其次,將樣本切成lcmx20cm的大小,使用平山製作 所製造之高加速壽命試驗設備(HAST設備)PC-304R8D, 於125°C、濕度100%的條件下進行72小時的處理之後, 處理後之樣本斷裂伸度係依據ASTM-D 882-97 ( 1 999 ) -97 (參照1 999年版ASTM年度標準索引手冊),於夾具間距(A) Plane alignment coefficient = (nMD + nTD ) / 2-nZD In the above formula (A), nMD represents the refractive index of the long side direction (MD) of the film, nTD represents the transverse direction (TD) of the film, nZD Represents the refractive index in the thickness direction of the film. 〇 (6) Measurement of phosphorus atom content by fluorescent X-ray measurement The content of phosphorus atoms was measured by a fluorescent X-ray method (ZSXIOOe, manufactured by Rigaku Corporation). (7) The average reflectance at a wavelength of 400 to 700 nm is attached to an integrating sphere accessory (ISR2200 manufactured by Shimadzu Corporation) in a spectrophotometer (Shimadzu Corporation UV245 0), with barium sulfate as a standard plate and relative reflection at 100% standard plate. The rate is measured as a measure. In the wavelengths of 400 to 700 nm, the relative reflectance per wavelength of 0.5 nm is measured, and the average 値 of the relative reflectances of the -15-201037840 is taken as the average reflectance. (8) The elongation retention after 48 hours of standing at 125 ° C and 100% humidity is measured according to AS TM-D 8 8 2-97 (refer to the 1 999 ASTM Annual Standard Index Manual ( ANNUAL BOOK OF ASTM STANDARDS)), the sample x was cut into a size of 1 cm x 20 cm, and the elongation at break (initial) at the time of stretching was measured at a jig pitch of 5 cm and a tensile speed of 300 mm/min. Further, the measurement was performed for 5 samples, and the obtained average value of 〇 was taken as the elongation at break (initial) A0. Next, the sample was cut into a size of 1 cm x 20 cm, and subjected to a highly accelerated life test apparatus EHS-221MD manufactured by ESPEC CORP., and subjected to treatment at a temperature of 125 ° C and a humidity of 100% for 48 hours, and then referred to ASTM-D882-97C. The tensile elongation of the sample after treatment in the 1999 ASTM Annual Standard Index Manual was measured for elongation at break (after treatment) at a clamp pitch of 5 cm and a tensile speed of 300 mm/min. Further, five samples were measured for the average enthalpy obtained as the elongation at break (after treatment) A 1 . Using the obtained elongation at breaks A0 and A1, the elongation retention ratio was calculated according to the following formula (1). The elongation retention ratio (%) = A1/A 〇 x 100 ( 1 ) Further, the average elongation retention ratio is calculated according to the following formula (2). Average elongation retention rate (%) = (MD direction elongation retention rate + TD direction elongation retention rate) / 2 ( 2 ) In addition, even using the high accelerated life test equipment of Hirayama Manufacturing Co., Ltd.-16- 201037840 (HAST Equipment) PC -30 4R8D is measured in the same number as ESP-221MD, which is used in ESPEC CORP.'s highly accelerated life testing equipment. Therefore, it can also be used in the high-acceleration life testing equipment (HAST equipment) PC-304R8D of Hirayama Works. measuring. (9) Measurement of elongation at break after standing for 72 hours at 125 ° C and humidity of 100% The measurement of elongation at break is based on ASTM-D882-97 (refer to the 1999 ASTM Annual Standard Index Manual). The lcmx20cm is large and small, and the elongation at break (initial) at the time of stretching is measured at a jig pitch of 5 cm and a tensile speed of 300 mm/min. Further, measurements were made for 5 samples, and the obtained average enthalpy was taken as the elongation at break (initial) A2. Next, the sample was cut into a size of 1 cm x 20 cm, and the sample was processed using a high accelerated life test apparatus (HAST equipment) PC-304R8D manufactured by Hirayama Seisakusho Co., Ltd. under the conditions of 125 ° C and a humidity of 100% for 72 hours. The elongation at break is based on ASTM-D 882-97 (1 999 ) -97 (refer to the 1 999 edition of the ASTM Annual Standard Index Manual).

Q 爲5cm、拉伸速度爲3 00mm/min時,測量拉伸時的斷裂伸 度(處理後)。又’針對5個樣本進行測量,以所得之該平 均値作爲斷裂伸度(處理後)A3。 使用求得之斷裂伸度A2及A3,依據以下公式(3 )計 算出伸度保持率。 伸度保持率(%) =Α3/Α2χ100 (3) 又,依據以下公式(4)計算出平均伸度保持率。 平均伸度保持率(%) = (MD方向伸度保持率+TD方 -17- 201037840 向伸度保持率)/2 (4) 實施例 以下,對本發明之相關實施例進行舉例說明,但本發 明並不限制於該些實施例。 實施例1 (原料 PET-1 ) 針對100重量份之對苯二甲酸二甲酯及60重量份之乙 二醇的混合物,添加0.08重量份之醋酸鈣、0.03重量份之 三氧化二銻,並依習知方法加熱升溫以進行酯交換反應。 其次,針對該酯交換反應生成物添加0.16重量份之醋酸鋰 及0.11重量份之磷酸三甲酯之後,移置聚合反應器中。接 著,在針對正在加熱升溫之反應系緩慢地進行減壓至 ImmHg減壓環境下,依習知方法於290 °C進行聚合’獲得 固有黏度〔η〕0.52的聚酯(聚對苯二甲酸乙二醇酯)。將 該聚酯切成2mmx4mmx4mm的立方體,使用旋轉式真空聚 合設備,在〇.5mmHg的減壓環境下,以23 0 °C進行20小時 的加熱處理,獲得固有黏度〔η〕〇·79的、羧基末端基濃度 1 0,5eq/ton 的聚醋。 針對前述所獲得之原料PET-1在溫度180 °C、真空度 0.5mmHg條件下進行2小時的減壓乾燥,供給至295 °C加 熱過的擠出機,以50 μιη過濾器將異物濾出後,導入至T 型模具蓋。其次,於Τ型模具蓋內,擠出成薄片狀的熔融 單層薄片,讓該熔融單層薄片在表面溫度20°C之保存筒上 以靜電印加法(pinning)進行接觸冷卻而固化,以獲得未 -18 - 201037840 延伸單層膜。接著,針對該未延伸單層薄膜以溫度8 5 °C之 加熱輥群進行預熱後,針對長邊方向(MD)使用溫度90°C 之加熱輥群以3.3倍的延伸倍率進行延伸,再以溫度25°C 之輥群進行冷卻而獲得單軸延伸膜(單軸配向膜)。以夾具 來夾持所獲得之單軸延伸膜的兩端,並引導至拉幅機內溫 度95 °C的預熱區,接著於溫度105 °C加熱區持續地針對長 邊方向之垂直方向(TD)以3.6倍的延伸倍率進行延伸。 接著繼續步驟,於拉幅機內的熱處理區以185 °C的熱處理 〇 溫度(第1熱處理溫度)進行20秒的熱處理,再者,以溫 度180 °C、3 %的鬆驰率於寬度方向(TD)進行鬆弛處理。 其次,均勻冷卻至25°C之後,捲起即可獲得厚度爲125μιη 的膜。評價結果列示於表1。該膜的耐水解性評價爲良好。 又,可依以下方法製造太陽電池背板。 首先,使用前述所獲得厚度125μπι的本發明之膜作爲 第1層。其次,作爲黏附層將90重量份之「TAKELAC:™」 O—A310C三井武田化學公司製造)及「ΑΚΕΝΑΤΕ™」Α3(三 井武田化學公司製造)塗布至第1層表面,接著於該黏附 層上,以厚度12μιη之Barrialox™「HGTS」(東麗薄膜加 工公司(TORAY)製造之氧化鋁沉積PET薄膜)之沉積層 作爲第2層並貼合至第1層之相反側。接著,在第2層上 塗布與前述黏附層相同的黏附層,並且將厚度5 0 μηι的雙 軸配向聚酯膜「Lumirr〇r™」Ε20(東麗薄膜加工公司製造) 相互貼合在該黏附層上,以製成總厚度1 87μιη的背板。該 背板之評價結果列示於表格中。該背板的耐水解性評價爲 -19- 201037840 良好。 實施例2〜4 除了表格中列示的製膜條件以外’以與實施例1相同 的方法進行製膜以獲得聚酯膜。所獲得之膜的評價結果列 示於表格中。該膜的耐水解性評價爲良好。 接著,使用所獲得之聚酯膜,以與實施例1相同的方 法製成背板。該背板的評價結果列示於表格中。該背板的 0 耐水解性評價爲良好。 實施例5 (原料 PET-2 ) 除了使用旋轉式真空聚合設備,在〇.5mmHg的減壓環 境下,於23 0 °C進行40小時的熱處理之外,且以與原料 PET-1相同之製法以獲得固有黏度〔η〕0.82、羧基末端基 濃度8.5eq/t〇n的聚酯(聚對苯二甲酸乙二醇酯)。 除了使用前述原料PET-2作爲原料之外,且以與實施 Q 例1相同之方法進行製膜以獲得聚酯膜。所獲得之膜的評 價結果列示於表格中。該膜的耐水解性評價爲良好。 接著,使用所獲得之聚酯膜,以與實施例1相同之方 法製成背板。該背板之評價結果列示於表格中。該背板的 耐水解性評價爲良好。 實施例6〜8 除了表格中列示的製膜條件以外,以與實施例5相同 的方法進行製膜以獲得聚酯膜。所獲得之膜的評價結果列 示於表格中。該膜的耐水解性評價爲良好。 -20- 201037840 接著’使用所獲得之聚酯膜’以與實施例"目同之方 法製成背板。該背板之評價結果列示於表格中。該背板的 耐水解性評價爲良好。 實施例9 (原料 PET-3) 相對於90重重份之原料pet-1’添加1〇重量份之萊 因化學(Rhein Chemie C〇rporation)製造之 stabax〇i@pi〇〇 0 (聚碳化二亞胺)而進行混合。該混合物即爲原料PET_^ 除了使用90重量份之原料pet-1與1〇重量份之原料 PET-3 (相當於1重量份之聚碳化二亞胺)進行混合以作爲 原料之外,且以與實施例1相同的方法進行製膜以獲得聚 酯膜。所獲得之膜的評價結果列示於表格中。該膜的耐水 解性評價爲良好。 接著,使用所獲得之聚酯膜,以與實施例1相同之方 法製成背板。該背板之評價結果列示於表格中。該背板的 〇 耐水解性評價爲良好。 實施例1 0〜1 2 除了表格中列示的製膜條件以外,以與實施例9相同 的方法進行製膜以獲得聚酯膜。所獲得之膜的評價結果列 示於表格中。該膜的耐水解性評價爲良好。 接著,使用所獲得之聚酯膜’以與實施例1相同之方 法製成背板。該背板之評價結果列示於表格中。該背板的 耐水解性評價爲良好。 實施例1 3〜1 4 -21- 201037840 除了表格中列示的製膜條件以外,以與實施例6相同 的方法進行製膜以獲得聚酯膜。所獲得之膜的評價結果列 示於表格中。該膜的耐水解性評價爲良好。 接著,使用所獲得之聚酯膜,以與實施例1相同之方 法製成背板。該背板之評價結果列示於表格中。該背板的 耐水解性評價爲良好。 實施例1 5 ^ (原料 PET-4 ) 〇 除了將磷酸三甲酯的添加量改爲0.13重量份,且使用 旋轉式真空聚合設備,在〇.5mmHg的減壓環境下,於230°C 進行40小時的熱處理之外,且以與原料petu相同之製法 以獲得固有黏度〔η〕0.82、羧基末端基濃度8.5eq/t〇I1的 聚酯(聚對苯二甲酸乙二醇酯)。 除了使用前述PET-4作爲原料之外,且以與實施例13 相同之方法進行製膜以獲得聚酯膜。所獲得之膜的評價結 q 果列示於表格中。該膜的耐水解性評價爲良好, 接著’使用所獲得之聚酯膜’以與實施例1相同之方 法製成背板。該背板之評價結果列示於表格中。該背板的 耐水解性評價爲良好。 實施例1 6 (原料 PET-5 ) 除了將磷酸三甲酯的添加量改爲0.25重量份,且使用 旋轉式真空聚合設備,在0.5mmHg的減壓環境下,於23〇°c 進行40小時的熱處理之外’且以與原料pEjd相同之製法 -22- 201037840 以獲得固有黏度〔η〕0.82、羧基末端基濃度8_5eq/toii的 聚酯(聚對苯二甲酸乙二醇酯)。 除了使用前述PET-5作爲原料之外,且以與實施例13 相同之方法進行製膜以獲得聚酯膜。所獲得之膜的評價結 果列示於表格中。該膜的耐水解性評價爲良好。 接著,使用所獲得之聚酯膜,以與實施例1相同之方 法製成背板。該背板之評價結果列示於表格中。該背板的 耐水解性評價爲良好。 實施例1 7 在溫度180°C、真空度0.5mmHg的條件下針對原料 PET-5進行2小時的減壓乾燥,供給至295 °C加熱過的擠出 機,以50μπι過濾器將異物濾出後,導入至T型模具蓋。 其次,於Τ型模具蓋內,擠出成薄片狀的熔融單層薄片, 讓該熔融單層薄片在表面溫度20°C之保存筒上以靜電印加 法進行接觸冷卻而固化,以獲得未延伸單層膜。接著,針 對該未延伸單層薄膜以溫度85 °C之加熱輥群進行預熱後, 針對長邊方向(MD )使用溫度90°C之加熱輥群以3.3倍的 延伸倍率進行延伸,再以溫度25 °C之輥群進行冷卻而獲得 單軸延伸膜。以夾具來夾持所獲得之單軸延伸膜的兩端, 並引導至拉幅機內溫度95 °C的預熱區,接著,於溫度1〇5 °C 加熱區持續地針對長邊方向之垂直方向(TD)以4.0倍的 延伸倍率進行延伸。接著繼續步驟,於拉幅機內的熱處理 區以205 1的熱處理溫度(第1熱處理溫度)進行20秒的 熱處理。再接著於溫度18(TC環境下,以3%的鬆弛率於寬 -23- 201037840 度方向(TD)進行鬆驰處理,又,長邊方向(MD)因拉幅 機之夾具間隔縮減而以1.5%的鬆驰率進行鬆弛。其次,均 勻冷卻至25 °C之後,捲起即可獲得聚酯膜。評價結果列示 於表格中。該膜的耐水解性評價爲良好。 接著,使用所獲得之聚酯膜,以與實施例1相同之方 法製成背板。該背板之評價結果列示於表格中。該背板的 耐水解性評價爲良好。 實施例1 8 除了長邊方向(MD)因拉幅機之夾具間隔縮減而鬆弛 率爲2.0 %之外,且以與實施例17相同之方法進行製膜以 獲得聚酯膜。所獲得之膜的評價結果列示於表格中。該膜 的耐水解性評價爲良好。 接著,使用所獲得之聚酯膜,以與實施例1相同之方 法製成背板。該背板之評價結果列示於表格中。該背板的 耐水解性評價爲良好。 實施例1 9 使用具有擠出機(a)及擠出機(b)的複合製膜設備。 依5重量份之平均粒子徑0.2 μιη鈦氧化物(表面未處理、 金紅石型)、0.15重量份之螢光增白劑「ΟΒ-1」(伊士曼柯 達公司製造(Eastman Kodak Company))以及94.85重量 份之原料PET-5的比例進行混合,於溫度180°C、真空度 〇.5mmHg的條件下進行2小時的減壓乾燥後,供給至擠出 機(Ο側,於280°C進行熔融擠出之後’以50μιη過濾器 將異物濾出後,導入至Τ型模具之複合蓋。 -24- 201037840 又,將原料PET-5於溫度180°C '真空度〇.5mmHg的 條件下進行2小時的減壓乾燥,且將其供給至29 5 °C之加 熱過的擠出機(a)側,以50μιη過濾器將異物濾出後,導 入至Τ型模具之複合蓋。 其次,於Τ型模具之複合蓋內,來自擠出機(a)之聚 合物與來自擠出機(b)之聚合物進行2層積層並匯流之 後,共同擠出薄片狀之熔融疊層薄片。不過,控制兩個擠 出機之擠出量的前述複合比例:擠出機(a)層/〔擠出機 (a)層+擠出機(b )層〕應爲12%。 其次,藉由T型模具蓋內而擠出成薄片狀的熔融疊層 薄片,在表面溫度20 °C之保存筒上以靜電印加法(pinning) 進行接觸冷卻而固化,以獲得未延伸積層膜。接著,針對 該未延伸薄膜以溫度85 t之加熱輥群進行預熱後,針對長 邊方向(MD)使用溫度9 0 °C之加熱輥群以3.5倍的延伸倍 率進行延伸,再以溫度25 °C之輥群進行冷卻而獲得單軸延 伸膜。以夾具來夾持所獲得之單軸延伸膜的兩端,並引導 至拉幅機內溫度95 °C的預熱區,接著,於溫度1〇5 °C加熱 區持續地針對長邊方向之垂直方向(TD)以4.0倍的延伸 倍率進行延伸。接著繼續步驟,於拉幅機內的熱處理區以 2〇5 °C的熱處理溫度(第1熱處理溫度)進行20秒的熱處 理。再接著於溫度180°C環境下,以3%的鬆驰率於寬度方 向(TD)進行鬆弛處理,又,長邊方向(MD)因拉幅機之 夾具間隔縮減而以1.5 %的鬆弛率進行鬆弛。 其次,均勻冷卻至25 °C之後,捲起即可獲得厚度爲 -25- 201037840 125 μπι的聚酯膜。所獲得之膜的(a)層厚度爲 層厚度爲ιιομιη。所獲得之膜的評價結果列示 該膜的耐水解性評價爲良好。 又,可依以下方法製造太陽電池背板。 首先,使用前述所獲得之2層積層膜作爲 爲黏附層,以90重量份之「TAKELACTM」—Α2 田化學公司製造)及「ΑΚΕΝΑΤΕ·™」A3 (三井 司製造)塗布至(b)層表面,以厚度12 μιη之 ^ 「HGTS」(東麗薄膜加工公司製造之氧化鋁沉獲 之沉積層作爲其上的第2層,並貼合至第1層 接著在第2層上塗布與前述黏附層相同的 且將厚度50μιη的雙軸配向聚酯膜「Lumi rror1 麗薄膜加工公司製造)相互貼合在該黏附層上 厚度187μιη的背板。評價結果列示於表1。該 解性評價爲良好。又,由於(a)層位於最表層 此耐UV性良好。 ❹ 實施例2 0 除了將平均粒子徑〇.2μιη氧化鈦(表面未 石型)改爲30重量份、將螢光增白劑「〇Β 4 達公司製造)改爲0.15重量份及將原料pETd 重量份的比例進行混合,於溫度1 8 〇 、真空 的條件下進行2小時的減壓乾燥後,供給至擠 之外’再以與實施例19相同的方法進行製膜 膜。所獲得之膜的評價結果列示於表格中。該 1 5 μιη - ( b ) 於表格中。 第1層。作 丨10 (三井武 武田化學公 Barrialox™ 【PET薄膜) 相反側。 黏附層,並 別」E20 (東 ,以製成總 背板的耐水 的位置,因 處理、金紅 j (伊士曼柯 5改爲69.85 度 0.5mmHg 出機(a)側 以獲得聚酯 膜的耐水解 -26- 201037840 性評價爲良好。 接著,使用所獲得之聚酯膜,以與實施例1相同之方 法製成背板。該背板之評價結果列示於表格中。該背板的 耐水解性評價爲良好。 實施例2 1 (原料 PET-6 ) 除了使用旋轉式真空聚合設備,在0.5mmHg的減壓環 境下,以230 r進行5小時的加熱處理之外,且以與原料 Ο PET-1相同的製法以獲得固有黏度〔η〕0.65的、羧基末端 基濃度18eq/ton的聚酯(聚對苯二甲酸乙二醇酯)。 (原料 PET-7 ) 於9 0重量份之原料PET-6添加10重量份之萊因化學 製造之Stabaxol P100 (聚碳化二亞胺)以進行混合。該混 合物即爲原料PET-7。 除了使用90重量份之原料PET-6與10重量份之原料 Q PET·7 (相當於1重量份之聚碳化二亞胺)進行混合以作爲 原料之外,以與實施例6相同的方法進行製膜以獲得聚醋 膜。所獲得之膜的評價結果列示於表格中。該膜的耐水解 性評價爲良好。 接著’使用所獲得之聚酯膜,以與實施例1相同之方 法製成背板。該背板之評價結果列示於表格中。該背板的 耐水解性評價爲良好。 實施例22 (原料 PET-8 ) -27- 201037840 除了使用旋轉式真空聚合設備,在〇.5mmHg的減壓環 境下’以2 3 0 °C進行1 〇 0小時的加熱處理之外,且以與原 料PET-1相同之製法以獲得固有黏度〔η〕2、羧基末端 基濃度8.0eq/ton的聚酯。 除了使用前述原料PET-8作爲原料之外,且以與實施 例6相同之方法進行製膜以獲得聚酯膜。所獲得之膜的評 價結果列示於表格中。該膜的耐水解性評價爲良好。 接著,使用所獲得之聚酯膜,以與實施例1相同之方 法製成背板。該背板之評價結果列示於表格中。該背板的 耐水解性評價爲良好。 實施例2 3 以與實施例6相同的方法進行以獲得厚度1 2 5 μπι的 膜。評價結果列示於表格中。 又,可依以下方法製造太陽電池背板。 使用前述所獲得之厚度125μιη的膜作爲第1層。其 次,作爲黏附層,將90重量份之「TAKELAC™」—Α310 (三井武田化學公司製造)及「ΑΚΕΝΑΤΕ™」A3 (三井武 田化學公司製造)塗布至第1層表面,以厚度12μιη之 BarrialoxTM「HGTS」(東麗薄膜加工公司製造之氧化鋁沉 積PET薄膜)之沉積層作爲該黏附層上的第2層,並貼合 至第1層之相反側,接著在第2層上塗布與前述黏附層相 同的黏附層,並且將厚度250μηι的雙軸配向聚酯膜 「Lumirr〇r™」S10 (東麗薄膜加工公司製造)相互貼合在 該黏附層上作爲第3層。接著在第3層上塗布與前述黏附 -28- 201037840 層相同的黏附層,且將厚度50 μιη的雙軸配向聚酯膜 「Lumirror™」Ε2〇 (東麗薄膜加工公司製造)相互貼合在 該黏附層上,以製成總厚度43 7 μιη的背板》該背板之評價 結果列示於表格中。該背板的耐水解性評價爲良好。 實施例24 除了使用厚度50μιη的聚酯膜之外,以與實施例6相 同的製法獲得聚酯膜。膜的評價結果列示於表格中。 又,可依以下方法製造太陽電池背板。 使用前述所獲得之厚度50μιη的膜作爲第1層。其次, 作爲黏附層,將90重量份之「TAKELAC™」一 A3 10 (三井 武田化學公司製造)及「ΑΚΕΝ ATE™」A3 (三井武田化學 公司製造)塗布至第1層,以厚度12μιη之BarrialoxTM 「HGTS」(東麗薄膜加工公司製造之氧化鋁沉積PET薄膜) 之沉積層作爲該黏附層上的第2層,並貼合至第1層之相 反側,接著在第2層上塗布與前述黏附層相同的黏附層, 並且將厚度250μηι的雙軸配向聚酯膜「1^111^(^说」810(東 麗薄膜加工公司製造)相互貼合在該黏附層上作爲第3 層。接著在第3層上塗布與前述黏附層相同的黏附層,且 將厚度188μιη的雙軸配向聚酯膜「Lumirror™」Ε20(東麗 薄膜加工公司製造)相互貼合在該黏附層上,以製成總厚 度500 μηι的背板。該背板之評價結果列示於表i。該背板 的耐水解性評價爲良好。 實施例25〜42 除了表格中列示的製膜條件以外,以與實施例5相同 -29- 201037840 的方法進行製膜以獲得聚酯膜。所獲得之膜的評價結果列 示於表格中。該膜的耐水解性評價爲良好。 接著,使用所獲得之聚酯膜,以與實施例1相同之方 法製成背板。該背板之評價結果列示於表格中。該背板的 耐水解性評價爲良好。 比較例1 (原料 PET-9 ) 將100重量份之對苯二甲酸二甲酯及60重量份之乙二 醇之混合物中,添加0.08重量份之醋酸鈣、0.03重量份之 三氧化二銻,依習知方法加熱升溫進行酯交換反應。其次, 針對該酯交換反應生成物添加0.16重量份之醋酸鋰及0.11 重量份之磷酸三甲酯之後,移置聚合反應器中。接著,在 針對正在加熱升溫之反應系緩慢地進行減壓的lmmHg減 壓環境下,依習知方法於290°C進行聚合,獲得固有黏度 〔η〕0.52的聚酯。將該聚酯切成各邊長2mmx4mmx4mm 的立方體,使用旋轉式真空聚合設備’在〇.5mmHg的減壓 環境下,以2 3 0 °C進行8小時的加熱處理,獲得固有黏度 〔η〕0.74的、羧基末端基濃度13 eq/ton的聚酯。 除了使用前述原料PET-9作爲原料之外’以與實施例 1相同的方法獲得厚度125μιη的膜。對於該膜進行評價, 即可發現耐水解性較差。 又,以與實施例1相同的方法製成厚度187 μιη的背 板。評價結果列示於表格中。對於該背板進行評價’即可 發現耐水解性較差。 -30- 201037840 比較例2 ‘ 除了表格中列示的製膜條件以外,以與比較例1相同 的方法進行製膜以獲得聚酯膜。所獲得之膜的評價結果列 示於表格中》尤其出現了耐水解性較差的結果。 又’亦以實施例1的方法製成背板,獲得厚度187 μιη 的背板。評價結果列示於表格中。尤其出現了耐水解性較 差的結果。 比較例3 除了表格中列示的製膜條件以外,以與實施例1相同 的方法進行製膜以獲得聚酯膜。所獲得之膜的評價結果列 示於表格中。尤其出現了耐水解性較差的結果。 又,亦以實施例1的方法製成背板,獲得厚度187 μιη @背板。評價結果列示於表1 »尤其出現了耐水解性較差 的結果。 比較例4 除了表格中列示的製膜條件以外,以與實施例9相同 @方法進行製膜以獲得聚酯膜。所獲得之膜的評價結果列 $於表格中。尤其出現了耐水解性較差的結果。 又,亦以實施例1的方法製成背板,獲得厚度187 μιη @背板。評價結果列示於表1。尤其出現了耐水解性較差 的結果。 比較例5 除了表格中列示的製膜條件以外,以與實施例5相同 @方法進行製膜以獲得聚酯膜。所獲得之膜的評價結果列 -31 - 201037840 1 8 7 μ m 性較差 示於表格中。尤其出現了耐水解性較差的結果》 又,亦以實施例1的方法製成背板’獲得厚 的背板。評價結果列示於表丨。尤其出現了耐水 的結果。When Q was 5 cm and the drawing speed was 300 mm/min, the elongation at break (after treatment) was measured. Further, measurements were made for 5 samples, and the average enthalpy obtained was taken as the elongation at break (after treatment) A3. Using the obtained elongation at breaks A2 and A3, the elongation retention ratio was calculated according to the following formula (3). The elongation retention ratio (%) = Α 3 / Α 2 χ 100 (3) Further, the average elongation retention ratio is calculated according to the following formula (4). Average elongation retention ratio (%) = (MD direction elongation retention rate + TD side -17 - 201037840 extension elongation retention rate) / 2 (4) EXAMPLES Hereinafter, the related embodiments of the present invention will be exemplified, but The invention is not limited to the embodiments. Example 1 (raw material PET-1) For a mixture of 100 parts by weight of dimethyl terephthalate and 60 parts by weight of ethylene glycol, 0.08 parts by weight of calcium acetate and 0.03 parts by weight of antimony trioxide were added, and The temperature is raised by a conventional method to carry out a transesterification reaction. Next, 0.16 part by weight of lithium acetate and 0.11 part by weight of trimethyl phosphate were added to the transesterification reaction product, followed by displacement in a polymerization reactor. Next, the reaction was carried out under reduced pressure to a temperature of 1 mmHg for the reaction under heating, and the polymerization was carried out at 290 ° C by a conventional method to obtain a polyester having an intrinsic viscosity [η] of 0.52 (polyethylene terephthalate). Glycol ester). The polyester was cut into a cube of 2 mm x 4 mm x 4 mm, and subjected to heat treatment at 23 ° C for 20 hours under a reduced pressure of 5 5 mmHg using a rotary vacuum polymerization apparatus to obtain an intrinsic viscosity [η] 〇 · 79. A carboxylic acid having a carboxyl end group concentration of 10,5 eq/ton. The raw material PET-1 obtained above was dried under reduced pressure at a temperature of 180 ° C and a vacuum of 0.5 mmHg for 2 hours, and supplied to a heated extruder at 295 ° C to filter out foreign matter with a 50 μm filter. After that, import it into the T-die cover. Next, in the crucible mold cover, a molten single-layer sheet is extruded into a sheet, and the molten single-layer sheet is solidified by contact cooling on a storage cylinder having a surface temperature of 20 ° C by means of pinning. Obtained a non--18 - 201037840 extended monolayer film. Next, the unstretched single-layer film was preheated by a heating roll group having a temperature of 85 ° C, and then extended by a heating roll group having a temperature of 90 ° C in the longitudinal direction (MD) at a stretching ratio of 3.3 times. The uniaxially stretched film (uniaxial alignment film) was obtained by cooling with a roll group of a temperature of 25 °C. The two ends of the obtained uniaxially stretched film are clamped by a jig and guided to a preheating zone at a tenter temperature of 95 ° C, and then the heating zone at a temperature of 105 ° C continuously for the vertical direction of the long side direction ( TD) is extended at a magnification ratio of 3.6 times. Then, the process is continued, and the heat treatment zone in the tenter is heat-treated at a heat treatment temperature of 185 ° C (first heat treatment temperature) for 20 seconds, and further, at a temperature of 180 ° C and a relaxation rate of 3% in the width direction. (TD) performs relaxation treatment. Next, after uniformly cooling to 25 ° C, it was rolled up to obtain a film having a thickness of 125 μm. The evaluation results are shown in Table 1. The hydrolysis resistance of the film was evaluated as good. Further, the solar battery back sheet can be manufactured in the following manner. First, the film of the present invention having a thickness of 125 μm as described above was used as the first layer. Next, as the adhesion layer, 90 parts by weight of "TAKELAC: TM" O-A310C manufactured by Mitsui Takeda Chemical Co., Ltd. and "ΑΚΕΝΑΤΕTM" Α3 (manufactured by Mitsui Takeda Chemical Co., Ltd.) were applied to the surface of the first layer, followed by the adhesion layer. A deposited layer of BarrialoxTM "HGTS" (aluminum-deposited PET film manufactured by Toray Film Processing Co., Ltd.) having a thickness of 12 μm was used as the second layer and bonded to the opposite side of the first layer. Next, the same adhesion layer as the above-mentioned adhesion layer was applied to the second layer, and a biaxial alignment polyester film "Lumirr〇rTM" Ε20 (manufactured by Toray Film Processing Co., Ltd.) having a thickness of 50 μm was bonded to each other. On the adhesion layer, a backing plate having a total thickness of 1 87 μm was formed. The evaluation results of the backboard are listed in the table. The hydrolysis resistance of the back sheet was evaluated as -19-201037840. Examples 2 to 4 Film formation was carried out in the same manner as in Example 1 except for the film formation conditions listed in the table to obtain a polyester film. The evaluation results of the obtained film are shown in the table. The hydrolysis resistance of the film was evaluated as good. Next, using the obtained polyester film, a back sheet was produced in the same manner as in Example 1. The evaluation results of the backboard are listed in the table. The 0 hydrolysis resistance of the back sheet was evaluated as good. Example 5 (raw material PET-2) The same method as the raw material PET-1 was carried out except that a rotary vacuum polymerization apparatus was used, which was subjected to a heat treatment at 230 ° C for 40 hours under a reduced pressure of 5 mmHg. A polyester (polyethylene terephthalate) having an intrinsic viscosity [η] of 0.82 and a carboxyl end group concentration of 8.5 eq/t〇n was obtained. A film was formed in the same manner as in the practice of Example Q except that the above-mentioned raw material PET-2 was used as a raw material to obtain a polyester film. The evaluation results of the obtained film are shown in the table. The hydrolysis resistance of the film was evaluated as good. Next, using the obtained polyester film, a back sheet was produced in the same manner as in Example 1. The evaluation results of the backboard are listed in the table. The hydrolysis resistance of the back sheet was evaluated as good. Examples 6 to 8 Film formation was carried out in the same manner as in Example 5 except for the film formation conditions listed in the table to obtain a polyester film. The evaluation results of the obtained film are shown in the table. The hydrolysis resistance of the film was evaluated as good. -20- 201037840 Then, using the obtained polyester film, a back sheet was produced in the same manner as in the example " The evaluation results of the backboard are listed in the table. The hydrolysis resistance of the back sheet was evaluated as good. Example 9 (raw material PET-3) Stabax〇i@pi〇〇0 (polycarbodiene) manufactured by Rhein Chemie C〇rporation was added in an amount of 1 part by weight relative to 90 parts by weight of the raw material pet-1'. Imine) is mixed. The mixture is a raw material PET_^, except that 90 parts by weight of the raw material pet-1 is mixed with 1 part by weight of the raw material PET-3 (corresponding to 1 part by weight of the polycarbodiimide) as a raw material, and Film formation was carried out in the same manner as in Example 1 to obtain a polyester film. The evaluation results of the obtained film are shown in the table. The water resistance of the film was evaluated as good. Next, using the obtained polyester film, a back sheet was produced in the same manner as in Example 1. The evaluation results of the backboard are listed in the table. The hydrazine hydrolysis resistance of this back sheet was evaluated as good. Example 1 0 to 1 2 Film formation was carried out in the same manner as in Example 9 except for the film formation conditions listed in the table to obtain a polyester film. The evaluation results of the obtained film are shown in the table. The hydrolysis resistance of the film was evaluated as good. Next, a back sheet was produced in the same manner as in Example 1 using the obtained polyester film'. The evaluation results of the backboard are listed in the table. The hydrolysis resistance of the back sheet was evaluated as good. Example 1 3 to 1 4 - 21 to 201037840 A film was formed in the same manner as in Example 6 except for the film forming conditions listed in the table to obtain a polyester film. The evaluation results of the obtained film are shown in the table. The hydrolysis resistance of the film was evaluated as good. Next, using the obtained polyester film, a back sheet was produced in the same manner as in Example 1. The evaluation results of the backboard are listed in the table. The hydrolysis resistance of the back sheet was evaluated as good. Example 1 5 ^ (raw material PET-4) 〇 In addition to the addition amount of trimethyl phosphate to 0.13 parts by weight, and using a rotary vacuum polymerization apparatus, it was carried out at 230 ° C under a reduced pressure of mm 5 mmHg. A polyester (polyethylene terephthalate) having an intrinsic viscosity [η] of 0.82 and a carboxyl end group concentration of 8.5 eq/t〇I1 was obtained in the same manner as the raw material petu except for the heat treatment for 40 hours. A film was formed in the same manner as in Example 13 except that the aforementioned PET-4 was used as a raw material to obtain a polyester film. The evaluation results of the obtained film are shown in the table. The hydrolysis resistance of the film was evaluated as good, and then a back sheet was produced in the same manner as in Example 1 using the obtained polyester film. The evaluation results of the backboard are listed in the table. The hydrolysis resistance of the back sheet was evaluated as good. Example 1 6 (raw material PET-5) In addition to changing the amount of trimethyl phosphate added to 0.25 parts by weight, and using a rotary vacuum polymerization apparatus, 40 hours at 23 ° C under a reduced pressure of 0.5 mmHg. In addition to the heat treatment, and in the same manner as the raw material pEjd-22-201037840, a polyester (polyethylene terephthalate) having an intrinsic viscosity [η] of 0.82 and a carboxyl end group concentration of 8 to 5 eq/toii was obtained. A film was formed in the same manner as in Example 13 except that the aforementioned PET-5 was used as a raw material to obtain a polyester film. The evaluation results of the obtained film are shown in the table. The hydrolysis resistance of the film was evaluated as good. Next, using the obtained polyester film, a back sheet was produced in the same manner as in Example 1. The evaluation results of the backboard are listed in the table. The hydrolysis resistance of the back sheet was evaluated as good. Example 1 7 The raw material PET-5 was dried under reduced pressure for 2 hours under the conditions of a temperature of 180 ° C and a vacuum of 0.5 mmHg, and supplied to a heated extruder at 295 ° C, and the foreign matter was filtered out with a 50 μm filter. After that, import it into the T-die cover. Next, in the crucible mold cover, a molten single-layer sheet is extruded into a sheet, and the molten single-layer sheet is solidified by contact printing on a storage cylinder having a surface temperature of 20 ° C to obtain unstretched Single layer film. Next, the unstretched single-layer film is preheated by a heating roll group having a temperature of 85 ° C, and then extended by a heating roll group having a temperature of 90 ° C for a longitudinal direction (MD) at a stretching ratio of 3.3 times. The roll group at a temperature of 25 ° C was cooled to obtain a uniaxially stretched film. The two ends of the obtained uniaxially stretched film are clamped by a jig and guided to a preheating zone at a tenter temperature of 95 ° C, and then, at a temperature of 1 〇 5 ° C, the heating zone is continuously oriented for the long side direction. The vertical direction (TD) is extended at a stretching ratio of 4.0 times. Then, the process was continued, and the heat treatment in the tenter was performed at a heat treatment temperature of 205 1 (first heat treatment temperature) for 20 seconds. Then, at a temperature of 18 (TC environment, the relaxation treatment is performed at a relaxation rate of 3% in the width direction of -23-201037840 degrees (TD), and the longitudinal direction (MD) is reduced by the clamp interval of the tenter. The relaxation rate of 1.5% was relaxed. Secondly, after uniformly cooling to 25 ° C, the polyester film was obtained by rolling up. The evaluation results are shown in the table. The hydrolysis resistance of the film was evaluated as good. The obtained polyester film was formed into a back sheet in the same manner as in Example 1. The evaluation results of the back sheet are shown in the table. The hydrolysis resistance of the back sheet was evaluated as good. Example 1 8 Except for the long side direction (MD) Film formation was carried out in the same manner as in Example 17 except that the tenter interval of the tenter was reduced by a relaxation rate of 2.0%. The evaluation results of the obtained film are shown in the table. The hydrolysis resistance of the film was evaluated as good. Next, using the obtained polyester film, a back sheet was produced in the same manner as in Example 1. The evaluation results of the back sheet are shown in the table. The hydrolysis resistance was evaluated as good. Example 1 9 Using an extruder (a) The composite film forming apparatus of the extruder (b) is based on 5 parts by weight of an average particle diameter of 0.2 μm of titanium oxide (surface untreated, rutile type), and 0.15 part by weight of a fluorescent whitening agent "ΟΒ-1" ( The ratio of the raw material PET-5 manufactured by Eastman Kodak Company and 94.85 parts by weight is mixed, and dried under reduced pressure for 2 hours under the conditions of a temperature of 180 ° C and a vacuum of 5 5 mmHg. To the extruder (the side of the crucible, after melt extrusion at 280 ° C), the foreign matter was filtered out with a 50 μm filter, and then introduced into a composite lid of a crucible mold. -24- 201037840 Further, the raw material PET-5 was subjected to temperature. The mixture was dried under reduced pressure at 180 ° C under a vacuum of 5 mmHg for 2 hours, and supplied to the side of the heated extruder (a) at 29 5 ° C, and the foreign matter was filtered off with a 50 μm filter. And introduced into the composite cover of the Τ-type mold. Secondly, in the composite cover of the 模具-type mold, after the polymer from the extruder (a) and the polymer from the extruder (b) are layered and merged, Co-extruding flaky molten laminate sheets. However, controlling the extrusion of two extruders The aforementioned compounding ratio of the output: the extruder (a) layer / [extruder (a) layer + extruder (b) layer] should be 12%. Secondly, extruded into a T-die cover The flaky molten laminated sheet was solidified by contact cooling on a holding cylinder having a surface temperature of 20 ° C to obtain an unextended laminated film. Then, the unstretched film was subjected to a temperature of 85 t. After the preheating of the heating roller group, the heating roller group having a temperature of 90 ° C in the longitudinal direction (MD) is extended at a stretching ratio of 3.5 times, and then cooled by a roller group having a temperature of 25 ° C to obtain a uniaxial stretching. membrane. The two ends of the obtained uniaxially stretched film are clamped by a jig and guided to a preheating zone at a tenter temperature of 95 ° C, and then, at a temperature of 1 〇 5 ° C, the heating zone is continuously oriented for the long side direction. The vertical direction (TD) is extended at a stretching ratio of 4.0 times. Next, the step was continued, and heat treatment was carried out for 20 seconds at a heat treatment temperature (first heat treatment temperature) of 2 〇 5 ° C in the heat treatment zone in the tenter. Then, at a temperature of 180 ° C, the relaxation treatment is performed in the width direction (TD) at a relaxation rate of 3%, and the long-side direction (MD) is reduced by 1.5% due to the reduction of the clamp interval of the tenter. Relaxation. Next, after uniformly cooling to 25 ° C, the polyester film having a thickness of -25 to 201037840 125 μm can be obtained by rolling up. The (a) layer thickness of the obtained film was a layer thickness of ιιομιη. The evaluation results of the obtained film showed that the hydrolysis resistance of the film was evaluated as good. Further, the solar battery back sheet can be manufactured in the following manner. First, the two-layer laminated film obtained as described above was applied as an adhesive layer to 90 parts by weight of "TAKELACTM" - Α2 Tian Chemical Co., Ltd. and "ΑΚΕΝΑΤΕ·TM" A3 (manufactured by Mitsui Division) to the surface of (b) layer. , with a thickness of 12 μm, "HGTS" (the deposited layer of alumina deposited by Toray Film Processing Co., Ltd. as the second layer thereon, and bonded to the first layer and then coated on the second layer with the aforementioned adhesion A biaxially oriented polyester film (manufactured by Lumi rror Film Co., Ltd.) having the same thickness of 50 μm was bonded to the back sheet having a thickness of 187 μm on the adhesive layer. The evaluation results are shown in Table 1. The solution was evaluated as Further, since the (a) layer is located at the outermost layer, the UV resistance is good. 实施 Example 2 0 In addition to changing the average particle diameter 〇2 μιη titanium oxide (surface not stone type) to 30 parts by weight, the fluorescent whitening The amount of the agent "manufactured by 〇Β 4 达 达) was changed to 0.15 parts by weight and the ratio of the raw material pETd was mixed, and the mixture was dried under reduced pressure for 2 hours under a vacuum of 18 Torr, and then supplied to the outside of the extrusion. Again with the embodiment 19 The same method was used to form a film. The evaluation results of the obtained film are shown in the table. The 1 5 μιη - (b) is in the table. The first layer. 丨10 (Mitsui Takeda Chemical Co., Ltd. BarrialoxTM [PET Film) Opposite side. Adhesive layer, and don't "E20 (East, to make the water-resistant position of the total backboard, due to treatment, gold red j (Eastmanke 5 changed to 69.85 degrees 0.5mmHg out of the machine (a) side The hydrolysis resistance of the polyester film was evaluated as good as -26-201037840. Next, using the obtained polyester film, a back sheet was produced in the same manner as in Example 1. The evaluation results of the back sheet are shown in the table. The hydrolysis resistance of the back sheet was evaluated as good. Example 2 1 (raw material PET-6) In addition to using a rotary vacuum polymerization apparatus, heat treatment was performed at 230 r for 5 hours under a reduced pressure of 0.5 mmHg. Further, a polyester (polyethylene terephthalate) having an intrinsic viscosity [η] of 0.65 and a carboxyl terminal group concentration of 18 eq/ton was obtained in the same manner as in the raw material Ο PET-1. 10 parts by weight of the raw material PET-6 added 10 parts by weight of Stain Chemical manufactured by Sta Baxol P100 (polycarbodiimide) for mixing. The mixture is the raw material PET-7. In addition to 90 parts by weight of raw material PET-6 and 10 parts by weight of raw material Q PET·7 (equivalent to 1 part by weight) The carbodiimide was mixed and used as a raw material, and film formation was carried out in the same manner as in Example 6 to obtain a polyacetate film. The evaluation results of the obtained film are shown in the table. Evaluation of hydrolysis resistance of the film For the good. Then, using the obtained polyester film, a back sheet was produced in the same manner as in Example 1. The evaluation results of the backboard are listed in the table. The hydrolysis resistance of the back sheet was evaluated as good. Example 22 (raw material PET-8) -27- 201037840 In addition to the use of a rotary vacuum polymerization apparatus, in a reduced pressure environment of 55 mmHg, 'heat treatment at 270 ° C for 1 〇 0 hours, and The same procedure as the raw material PET-1 was carried out to obtain a polyester having an intrinsic viscosity [η] 2 and a carboxyl end group concentration of 8.0 eq/ton. A film was formed in the same manner as in Example 6 except that the above-mentioned raw material PET-8 was used as a raw material to obtain a polyester film. The evaluation results of the obtained film are shown in the table. The hydrolysis resistance of the film was evaluated as good. Next, using the obtained polyester film, a back sheet was produced in the same manner as in Example 1. The evaluation results of the backboard are listed in the table. The hydrolysis resistance of the back sheet was evaluated as good. Example 2 3 A film having a thickness of 1 2 5 μm was obtained in the same manner as in Example 6. The results of the evaluation are listed in the table. Further, the solar battery back sheet can be manufactured in the following manner. A film having a thickness of 125 μm obtained as described above was used as the first layer. Next, as the adhesion layer, 90 parts by weight of "TAKELACTM" - Α 310 (manufactured by Mitsui Takeda Chemical Co., Ltd.) and "ΑΚΕΝΑΤΕTM" A3 (manufactured by Mitsui Takeda Chemical Co., Ltd.) were applied to the surface of the first layer to a thickness of 12 μm BarrialoxTM. A deposited layer of HGTS (aluminum-deposited PET film manufactured by Toray Film Processing Co., Ltd.) is used as the second layer on the adhesive layer, and is bonded to the opposite side of the first layer, and then coated on the second layer with the aforementioned adhesion. The same adhesion layer was used, and a biaxially oriented polyester film "Lumirr〇rTM" S10 (manufactured by Toray Film Processing Co., Ltd.) having a thickness of 250 μm was bonded to the adhesion layer as a third layer. Next, the same adhesion layer as the above-mentioned adhesion layer -28-201037840 was applied to the third layer, and a biaxial alignment polyester film "LumirrorTM" Ε2〇 (manufactured by Toray Film Processing Co., Ltd.) having a thickness of 50 μm was attached to each other. On the adhesive layer, a back sheet having a total thickness of 43 μm was produced. The evaluation results of the back sheet are shown in the table. The hydrolysis resistance of the back sheet was evaluated as good. Example 24 A polyester film was obtained in the same manner as in Example 6 except that a polyester film having a thickness of 50 μm was used. The evaluation results of the film are shown in the table. Further, the solar battery back sheet can be manufactured in the following manner. A film having a thickness of 50 μm obtained as described above was used as the first layer. Next, as the adhesion layer, 90 parts by weight of "TAKELACTM"-A3 10 (manufactured by Mitsui Takeda Chemical Co., Ltd.) and "ΑΚΕΝ ATETM" A3 (manufactured by Mitsui Takeda Chemical Co., Ltd.) were applied to the first layer to a thickness of 12 μm BarrialoxTM. a deposited layer of "HGTS" (aluminum-deposited PET film manufactured by Toray Film Processing Co., Ltd.) as a second layer on the adhesive layer, and bonded to the opposite side of the first layer, and then coated on the second layer with the foregoing The adhesive layer having the same adhesion layer and a biaxially oriented polyester film having a thickness of 250 μm were bonded to each other on the adhesive layer as a third layer. The same adhesion layer as the above-mentioned adhesion layer was applied to the third layer, and a biaxially oriented polyester film "LumirrorTM" 20 (manufactured by Toray Film Processing Co., Ltd.) having a thickness of 188 μm was adhered to the adhesion layer. The back sheet having a total thickness of 500 μm was shown in Table 1. The hydrolysis resistance of the back sheet was evaluated as good. Examples 25 to 42 In addition to the film forming conditions listed in the table, Example 5 is the same -2 The method of 9-201037840 was carried out to obtain a polyester film. The evaluation results of the obtained film are shown in the table. The hydrolysis resistance of the film was evaluated as good. Next, the obtained polyester film was used and implemented. The back sheet was prepared in the same manner as in Example 1. The evaluation results of the back sheet are shown in the table. The hydrolysis resistance of the back sheet was evaluated as good. Comparative Example 1 (raw material PET-9) 100 parts by weight of terephthalic acid 0.08 parts by weight of calcium acetate and 0.03 parts by weight of antimony trioxide were added to a mixture of dimethyl formate and 60 parts by weight of ethylene glycol, and the mixture was heated and subjected to a transesterification reaction by a conventional method. Secondly, the transesterification was carried out. 0.16 parts by weight of lithium acetate and 0.11 part by weight of trimethyl phosphate were added to the reaction product, and then transferred to a polymerization reactor. Then, under a reduced pressure of 1 mmHg for slowly depressurizing the reaction under heating, Polymerization was carried out at 290 ° C according to the conventional method to obtain a polyester having an intrinsic viscosity [η] of 0.52. The polyester was cut into cubes each having a side length of 2 mm x 4 mm x 4 mm, and a rotary vacuum polymerization apparatus was used in a reduced pressure environment of .5 mmHg. The mixture was heat-treated at 203 ° C for 8 hours to obtain a polyester having an intrinsic viscosity [η] of 0.74 and a carboxyl end group concentration of 13 eq/ton. In addition to using the above-mentioned raw material PET-9 as a raw material, A film having a thickness of 125 μm was obtained in the same manner as in Example 1. The evaluation of the film revealed that the hydrolysis resistance was poor. Further, a back sheet having a thickness of 187 μm was produced in the same manner as in Example 1. The evaluation results are shown in the table. In the evaluation of the back sheet, it was found that the hydrolysis resistance was poor. -30- 201037840 Comparative Example 2 'In addition to the film forming conditions listed in the table, film formation was carried out in the same manner as in Comparative Example 1 to obtain a polymer. Ester film. The evaluation results of the obtained film are shown in the table, and in particular, the result of poor hydrolysis resistance appeared. Further, a back sheet was also produced in the same manner as in Example 1 to obtain a back sheet having a thickness of 187 μm. The results of the evaluation are listed in the table. In particular, the result of poor hydrolysis resistance has appeared. Comparative Example 3 A film was formed in the same manner as in Example 1 except for the film forming conditions listed in the table to obtain a polyester film. The evaluation results of the obtained film are shown in the table. In particular, the result of poor hydrolysis resistance has appeared. Further, a back sheet was also produced in the same manner as in Example 1 to obtain a thickness of 187 μm @@back sheet. The results of the evaluation are shown in Table 1 » especially the results of poor hydrolysis resistance. Comparative Example 4 A film was formed in the same manner as in Example 9 except for the film forming conditions listed in the table to obtain a polyester film. The evaluation results of the obtained film are listed in the table. In particular, the result of poor hydrolysis resistance has appeared. Further, a back sheet was also produced in the same manner as in Example 1 to obtain a thickness of 187 μm @@back sheet. The evaluation results are shown in Table 1. In particular, the result of poor hydrolysis resistance has appeared. Comparative Example 5 A film was formed in the same manner as in Example 5 except for the film forming conditions listed in the table to obtain a polyester film. The evaluation results of the obtained film are listed in the table -31 - 201037840 1 8 7 μ m. In particular, a result of poor hydrolysis resistance was observed. Further, a back sheet was produced by the method of Example 1 to obtain a thick back sheet. The evaluation results are shown in the table. In particular, there is a result of resistance to water.

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Ί 64 未滿足 〇 C0 ο CO CO CO 00 r^ CO T— 1實施例5 原料ΡΕΤ-2 C0 CO &lt;D CO in OD 1— in OJ t— 1— o 00 1— 卜 d ο ω 寸 CO CO 寸 CD 1«-» 6 滿足j CSJ tn 00 CO &gt;—· σ&gt; Γ- ω T— 實施例4 原料ΡΕΤ-1 C0 CO CD CO tn CM CM 紫 LH OJ T— CO r-* 220 卜 a ο C0 τ— 00 r— CM r— 0. 1 64 未滿足 00 eg r— LO &lt;N CO ω 卜 00 r— 實施例3 原料ΡΕΤ-1 C0 &lt;0 CO CO 〇 T— CN m in CM r— CO v— LO o CM r- o ο 00 r— 〇 CV4 寸 r— 寸 &lt;D τ- Ο 滿足 00 OJ 〇 LO LO Γ-· GO r— 寅施例2 原料ΡΕΤ-1 CO C0 CO CO tn o m U&gt; CM r— CO r— 〇 〇 CM 卜 d ο 00 τ*~ in &lt;Ν CD T— 寸 to τ α 未滿足 〇 C0 LO 卜 〇 00 CO p— 1實施例1 原料ΡΕΤ-1 Γ0 C0 Φ CO in CO t— 璀 ΙΛ CsJ T~~ CO r— 〇 00 1— 〇 ο 00 LO Γ ΟΟ I 0. 1 64| 滿足 cn CN o CO 〇 CO 00 . 00 τ— 原料 J MD延伸倍率(一) TD延伸倍率㈠ I 第1處理溫度rc) j MD鬆贼理 _度_) 殘基末端基濃度(eq/ton) 微小吸熱逢値溫度·Tmeatfc) I 固有黏度(dl/g) α. &amp; m If MD Q 1- 1 平面配向係數B2(-) I (B)公式的充她 1 波長400~700nm的平均反射率(%) 鎌72 •小時後 Y- I# II 1| 埘迎 m H-,s 1 m 1¾ | 薄片總厚度(&quot;m) I 晒 I 醤 細 150°C30 分 熱收縮率(%) feS s ? 蟀K·審 p|| s si lif -ero- 201037840 Ο ο 實施例14 | 原料PET-2 Ο 寸· tr&gt; ID o CJ m in &lt;N r— t— T— o o CM 卜 Ο ο ω τ— to 04 &lt;D τ— ΙΩ 卜 Τ Ο 滿足1 C0 CM Γ- CO o CNi CS( σ&gt; r- ω τ— 實施例13 原料PET-2 in η o 2 0.5 摧 LO CM T~* T— 〇 〇 CM rs d ο ω in CM CO r— 卜 ω r~ Ο 未滿足 〇 co LO 00 C〇 ο Oi 卜 00 τ— 實施例12 lL θ ω I® CO CO CD CO in CM CM m LO CSJ T*~ in 〇 CSJ CM 卜 ο 〇 00 τ- CJ) Τ'&quot; 09 二 廿 CD τ— ο 未滿足 00 (N ID ID oi ο CO Γ ΟΟ r— 實施例11 產® CO CO &lt;D CO 〇 CM 璀 ω CN r— in 20 5 卜 ο ο 00 τ— r— CM LO Τ·&quot; 寸 CD r— d 未滿足 Ο CO to 00 to ο ω 00 r— 實施例10 cl ^ W 0μ ϊΐ CO 00 (D 00 in 〇 CM m LO 〇j r— in 200 卜 〇· ο 00 τη» &lt;〇 CN τ— 寸 CD Τ Ο 未滿足 00 CM 〇 05 σ&gt; co σ&gt; 卜 00 r*&quot; 實施例9 —hi Μ α&lt; 蠢蠢 00 CO &lt;D CO in c〇 r— 璀 LO OJ r— 10 O co r— 卜 d ο ω τ— CO 寸 00 CO 寸 CO d 滿足 1— CO ID O U) co &lt;Si r^ 00 τ— |實施例8 原料PET-2 00 CQ CD CO LD CJ CM 摧 LO CM r— t— o CM CM ο ο C0 r— 卜 τ-* r~ r— 寸 CD r— d 未滿足 CD CM 00 in CM ο &lt;D 卜 00 r— 原料 MD延伸倍率卜) TD延伸倍率(一) ! 第i處理酿〇c) ! MD繫酿理 ! 麵度_) 翔基*S^®i度(叫/ton) 微賴臟値酿TmeatfC) I 固挪度(dl/g&gt; 登光X光測量的碟原子置(ppm) Q 2 TD | 平面配向係數叫) (B)公式的充她 波長400~700nm的平均反射率(%) 放置48 小麟 放置72 小時後 痤掛 II «ίΓ _降 's p m 5¾七 s« 駟滔 1 薄片總厚度(&quot;m) 1 150t30 分 熱收縮率(%) «s g _ H铢 p S i s si X g t lif 寸£ · 201037840 Ο 〇 實施例21 1 ! ai h-Q-UJ tor-Q- ^ h-龚4Q IgCD CO CO φ CO L〇 o CM 摧 in CM 二 〇 〇 CM &lt;0 6 Ο 00 r— 寸 CSi ΙΩ 1— 寸 CD 7~ d 細足J 0D CM in to 00 r— CD CO &gt;r— 實施例20 (參照說明書) U) CO ο 寸 LO 〇 CM L〇S &lt;N 二 1— τ— 200: | 0. 67| Ο r—· 寸 (D d CM d 0. 1 67 未滿足I 00 1-05 CO EQIH; •se 卜 卜 Γ0 00 00 r— 實施例19 (參照說明書&gt; LO CO ο ID o CM L〇3 CM r— r— 〇 〇 CM 03 CD 〇 ο τ— 寸 CD d 〇 卜 (D Τ Ο 未滿足 CsJO CO CQ 睡賠 ^-N CO 寸 CO 卜 00 τ— 實施例18 原料PET-5 i〇 CO ο 寸· iO o CnJ LO CM t— τ-~ 200 6 ο r— 寸 d OJ d 卜 (D y— 〇 未滿足 〇) CN CN O) 00 寸 σ&gt; 卜 00 T~~ 實施例17 原料PET-5 to CO ο LO o C\J 你 in CM T— 二 200 卜 d Ο 寸 CD 6 CM d 卜 CD r— d 未滿足 o CO r— cn 卜 寸 CD 卜 €0 T— 實施例16 原料PET-5 ΙΛ 03 ο ΙΩ o CNi m LO CvJ r~ 200 卜 d Ο r— 寸 CM CM CD 卜 to r— d 未滿足 00 CNJ 〇 O) 00 94 00 r~ |實施例15 原料ΡΕΤ·4 lO CO ο 寸 ΙΩ o CM 壊 LD Csl r— τ— τ— 200ί 1 d Ο τ~· CM CM CM (D 二 卜 CD r— d 未滿足 τ— CO 00 00 卜 CN σ&gt; Γ ΟΟ T*~ 原料 | MD延伸倍率㈠ 丄 掛 i m ;〇 !H | 第1處理酿。c) MOmmm 麒度(㈣ ; 羧基娜錄度(eq/ton) ! 1 —__________ 1 微小吸熱逢値溫度TmeaCC) 固雜度(dl/g) i m MD TD 平面配向係數B2(-) (B)公式的充雜 波長400~700nm的平均反射率(%) 放置48 /j僻後 if £ ? 18 O uij s g S| gl IS 薄片總厚度(&quot;m) | 1 醤 叢 150TC30 分 熱收縮率(%) 倾·ε? ? ^ κ:» p|| « Sft X g t lif m 201037840 ο ο 實施例28 1 原料ΡΕΤ-2 〇 CO CNi CO 〇 CO T— m in CNJ r— T~~ r— ir&gt; 卜 d 〇 00 04 a CO * CN 寸 ΙΟ Τ Ο 滿足l t- 00 τ- 00 03 CM in 00 00 實施例27 原料ΡΕΤ-2 LO 寸 to to ID T- 薬 in CM t-*· r- r- O to 卜 d o €0 T-· o (D 00 in h' 〇 τ- Ο 滿足 00 CN m σ&gt; CO LD 卜 cn 卜 GO r- 丨實施例26 原料ΡΕΤ-2 . CO CO o 寸 iO to r~ 摧 i〇 CM T- r~ r- o ΙΩ 卜 d o 00 1- CO ui 寸 U) N r~ d 滿足 ο CO ο 0) CO 寸 CO 0) CO r-* 實施例25 原料ΡΕΤ-2 · 00 00 CM in ΙΏ T- m in CM T~ T-~ r- o LO y— r-. d o 00 T~ 寸 CM CM CO τ- Ο 滿足 00 csl ο 00 o &lt;N 寸 CO 卜 CO r- 〇 o LO 實施例24 原料ΡΕΤ-2 CO CO CO CO in o 04 摧 o ID 1~ o o CM 卜 〇 〇 00 T- 寸 CM in y— 寸 iD τ- Ο 未滿足 04 CM ο 00 卜 CM l〇 實施例23 原料ΡΕΤ-2 CO CO &lt;£&gt; CO to o OJ 摧 to CM T- 二 200 卜 d o 00 r—· 寸 LO 寸 &lt;£&gt; r·· Ο 未滿足‘ 00 ο 00 00 寸 (D 卜 CO 寸 |實施例22 原料ΡΕΤ-8 ’ CO CO CO CO to o CNJ m LD (N r- r- 〇 o OJ OJ r- o 00 r- 寸 cs LO 寸 (Ο r- d 未滿足 〇 CO 〇 σ&gt; 寸 σ&gt; r- 00 原料 I MD延伸倍率(一) | TD延伸倍率㈠ | 第l處理溫度(t) 1 MD鬆麵理 1 娜度(&quot;m) 钱基娜讎度(eq/t〇n) 微小吸熱逢値溫度TmesitfC) 固有黏度(dl/g) 螢光X光測量的碟原子量(ppm) MD Q H 平面配向係數B2(-) (B)公式的充 波長400~700nm的平均反射率(%) 丨放置48 …小時後 放置72 小時後 II s « 一 #· e° fib sl 鹆芽 运β m 讀; m i: m 150°G30 分 MSI率(%) ig| p|| 111 朦北¢#1 鹤趣:劫 _9ε — 201037840 〇 o |實施例35 I 原料ΡΕΤ-2 ' 寸 to 〇 CM m IX) CM 1— r— to o CM Ο 〇 CO r— 寸 CO 1— CO CD 〇&gt; r~ 6 滿足 00 CvJ r~ CO 00 C\( in CO Γ ΟΟ 實施例34 原料ΡΕΤ-2 CM 计’ ο 谷 ο r— eg m ω CM r*- r— -t— 2 05 卜 d 〇 CD r-* &lt;〇 CM σ&gt; r— 〇 03 Τ Ο 滿足 〇 CO σ&gt; 卜 1C CN CO 00 卜 CO τ— 實ί®例33 原料ΡΕΤ-2 tn in 寸· ID 〇 m LO &lt;N r-· T— 2 00 卜 〇· 〇 00 产 tn CO &lt;N 00 CO σ&gt; -ρ- Ο 滿足 CO CM CM σ&gt; o LO 卜 σ&gt; Γ' 00 -τ~- 實施例32 原料ΡΕΤ-2 csj 'φ 〇 't i〇 〇 &lt;N m 10 CM t— 1— 200 卜 〇 o 00 1— 00 oj 0 01 σ&gt; 卜 Τ Ο 滿足 r*— CO ο Ο) 〇 CO LO Oi 卜 CO r- 實施例31 原料ΡΕΤ-2 in 寸 ΙΌ 寸· 〇 CO r— 璀 in &lt;N T~- T— LO 卜 t— 6 〇 CO r— 00 in CO in cn cn Τ Ο 滿足 CD CM CO σ&gt; T~ lO 卜 ω 卜 00 τ~ 實施例30 原料ΡΕΤ-2 ’ 00 CO Ο o CO 1— m ld eg T— T— LO 卜 i— 卜 〇 o CO r~ o to 04 寸· 卜 卜 τ- Ο 滿足, 〇 CO CM 05 o 寸 tn CD 卜 00 τ— |實施例29 原料ΡΕΤ-2 CO 00 CO CO 〇 00 r— m LO 04 T— T— LD 卜 r~ r- d 〇 CO T— to 寸 CD CO in ① ο 滿足 CD CNJ 00 00 LO CO CN Oi 卜 CO τ— 原料 1 MD延伸倍率(一) 1 TD延伸倍率(一) | 第i處理溫度re) I MD鬆賊理 1 鮮度(&quot;m) 羧基纖縫度(eq/tem) 微賴縫値酿TmeatCC) 固挪度(dl/g) 螢光X光測量的雜原子量&lt;ppm) MD Ll〇_1 平麵向係數Β2㈠ 1 (Β松式的充他 | Sft 400~700nm 的平均®^(%) 放置48 小時後 放置72 小時後 I裸 fi §« —ft si 粲萃 II 薄片總厚度(_ 1 150°C30 分 熱收縮率(%) 蜂 P遥· «si lif • Li_ m 201037840 〇 〇 實施例42 j 原料PET-2 to οι CD 04 in to r— m ιο (N 1— 〇 ιο r— 卜 6 Ο 00 r~ Ο 寸 CO CO 03 CNJ Τ Ο 未滿足| G) CM CO LO CM CM to 卜 00 r- 實施例41 原料PET-2 . ο Ο LO CSJ CM m m CN r- t- r~ 〇 CM 卜 〇 Ο 00 r— Oi τ- 00 T~ o cn d 未滿足 t- &lt;Τ) CNJ 00 CD 卜 卜 ω r— 實施例40 原料PET-2 〇 CO &lt;N CO LO 00 T~~ m LO &lt;N r- T- r-*· 〇 CO r— d Ο 〇0 r— Ο CO r~ CM 0. 1 54 未滿足 00 CsJ to 卜 卜 σ&gt; 卜 CO r~- 1實施例39 原料PET-2 . α&gt; CM 00 04 1 80 m in Oi 1— in 卜 i— 卜 d Ο 00 r- 00 〇i 00 T- m Τ Ο 未滿足 CO CO r- σ&gt; CM 00 卜 CO r- 實施例38 原料PET-2 CO &lt;N CO &lt;N o CO r- 摧 in CM 1- T*~ T&quot;· in to r~ 卜 ο 〇 00 τ— CO 寸 CD CO CM CO 产 d 未滿足 03 OJ ΙΛ GO ο CO 卜 00 τ-~ 實施例37 原料PET-2 tr&gt; 寸· LO in CNJ CM m LO CM T~ T~ 〇 CM Oi 卜 d Ο 〇0 r- in CM in CNJ 00 〇&gt; Τ Ο 滿足 00 CM T- ω 00 T— ΙΩ 00 卜 00 r- |實施例36 原料PET-2 CO 寸 CO 寸 I 225 摧 LO CM T- r- o CNJ CNi ο Ο αο τ- t- CM r- CM CO σ&gt; 〇 滿足 r— CO co CO ir- Oi 00 卜 00 r- 原料 1 MD延伸倍率(一) | TD延伸倍率㈠ I 第1處理溫度〇c&gt; MD鬆贼理 醇度(㈣ | 1 M' I 1 l 1 ΜΛ m 1 夢 § 固補度(dl/g&gt; 丨螢光X光測量的碟原子童(ppm) MD TD 平酿向係數B2(-) | (B)公式的充她 1 波長400~700nm的平均反射率(%) 幽返 卜A II II § m —* I齑 Ρ塗 ιη ψ· a 鹆芽 1 Η Sc S 薄片總厚度(&quot;m) | Φβ St si w探 Ms S _ t铢 p|| s Si X g t iif — 8ε — m 鲣 201037840〇-32- 201037840 Ο ο Example 7 1 Raw material ΡΕΤ-2 C0 CO CD CO ο CM m in CN T- r— r— LO 〇CN| d Ο 00 »— 〇> r—CO Two inches CO Τ Ο Not satisfied I τ 00 ΙΟ Ι Ω CD 卜 CO T - Example 6 Raw material ΡΕΤ-2 C0 00 to CO to o CN heap u> CJ r*~ T~ r- oo CM 卜 d Ο 00 7~ inch cs) LO Τ— 0. Ί 64 Not satisfied 〇C0 ο CO CO CO 00 r^ CO T—1 Example 5 Raw material ΡΕΤ-2 C0 CO &lt;D CO in OD 1—in OJ t— 1— o 00 1—bd ο ω 寸 CO CO inch CD 1«-» 6 satisfies j CSJ tn 00 CO &gt; —· σ &gt; Γ- ω T—Example 4 Raw material ΡΕΤ-1 C0 CO CD CO tn CM CM Purple LH OJ T— CO r -* 220 卜 a ο C0 τ — 00 r — CM r — 0. 1 64 Not satisfied 00 eg r— LO &lt; N CO ω 卜 r — Example 3 Raw material ΡΕΤ-1 C0 &lt;0 CO CO 〇T — CN m in CM r— CO v— LO o CM r- o ο 00 r— 〇CV4 inch r—inch&lt;D τ- Ο Meet 00 OJ 〇LO LO Γ-· GO r—寅Example 2 Raw materialΡΕΤ -1 CO C0 CO CO tn om U&gt; CM r— CO r— 〇〇CM 卜 d ο 00 τ*~ in &lt;Ν CD T—inch to τ α Not satisfied C0 LO 〇 00 CO p-1 Example 1 Raw material ΡΕΤ-1 Γ0 C0 Φ CO in CO t— 璀ΙΛ CsJ T~~ CO r— 〇00 1— 〇ο 00 LO Γ ΟΟ I 0. 1 64| Cn CN o CO 〇CO 00 . 00 τ — Raw material J MD stretching ratio (1) TD stretching ratio (I) I First processing temperature rc) j MD thief _ degree _) Residue end group concentration (eq/ton) Tiny Inhalation temperature · Tmeatfc) I Intrinsic viscosity (dl / g) α. &amp; m If MD Q 1- 1 Plane alignment coefficient B2 (-) I (B) formula for the average reflectance of the 1 wavelength of 400 ~ 700nm (%) 镰72 • After hours Y-I# II 1| Welcome m H-,s 1 m 13⁄4 | Total thickness of sheet (&quot;m) I Sun I 醤fine 150°C30 Heat shrinkage rate (%) feS s ? 蟀 K·审 p|| s si lif -ero- 201037840 Ο ο Example 14 | Raw material PET-2 Ο inch· tr&gt; ID o CJ m in &lt;N r — t — T— oo CM Ο ο ω τ — to 04 &lt; D τ — Ι Ω Τ Ο satisfy 1 C0 CM Γ - CO o CNi CS( σ > r- ω τ - Example 13 Raw material PET-2 in η o 2 0.5 Destruction LO CM T~* T— 〇〇CM rs d ο ω in CM CO r— Bu ω r~ Ο Not satisfied 〇co LO 00 C〇ο Oi 卜 00 τ— Example 12 lL θ ω I® CO CO CD CO in CM CM m LO CSJ T*~ in 〇CSJ CM οο 〇00 τ- CJ) Τ'&quot; 09 二廿CD τ— ο Not satisfied 00 (N ID ID oi ο CO Γ ΟΟ r—Example 11 Product CO CO &lt;D CO 〇CM 璀ω CN r— in 20 5 ο ο 00 τ — r— CM LO Τ·&quot; Inch CD r- d Not satisfied Ο CO to 00 to ο ω 00 r—Example 10 cl ^ W 0μ ϊΐ CO 00 (D 00 in 〇CM m LO 〇jr—in 200 〇 〇 ο 00 τη» &lt;〇CN τ—inch CD Τ Ο Not satisfied 00 CM 〇05 σ&gt; co σ&gt; 00 r*&quot; Example 9 - hi Μ α &lt; idiot 00 CO &lt; D CO in c〇r - 璀 LO OJ r - 10 O co r - 卜d ο ω τ—CO 00 00 CO 寸 CO d satisfies 1—CO ID OU) co &lt;Si r^ 00 τ— |Example 8 Raw material PET-2 00 CQ CD CO LD CJ CM Destroy LO CM r— t— o CM CM ο ο C0 r— 卜τ-* r~ r—inch CD r— d Not satisfied CD CM 00 in CM ο &lt;D 00 r—Material MD extension ratio TD extension ratio (1) ! 〇 〇 c) ! MD system brewing! Facial _) Xiang Ji * S ^ ® i degree (called / ton) micro Lai dirty brew TmeatfC) I Laerdal (dl/g&gt; Deng X-ray measurement of the disc atomic setting (ppm) Q 2 TD | plane alignment coefficient is called) (B) formula of the average reflectance of the wavelength of 400~700nm (%) placed 48 Xiaolin After 72 hours of placement, hang II <ίΓ _降's pm 53⁄4 s« 驷滔1 total thickness of sheet (&quot;m) 1 150t30 heat shrinkage rate (%) «sg _ H铢p S is si X gt lif inch £ · 201037840 Ο 〇 Example 21 1 ! ai hQ-UJ tor-Q- ^ h- Gong 4Q IgCD CO CO φ CO L〇o CM destroy in CM 〇〇 2 CM &lt;0 6 Ο 00 r - inch CSi Ι Ω 1—inch CD 7~ d Fine J 0D CM in to 00 r— CD CO &gt;r—Example 20 (Refer to the specification) U) CO ο 寸 LO 〇CM L〇S &lt;N 1-2 τ- 200 : | 0. 67| Ο r—· inch (D d CM d 0. 1 67 does not satisfy I 00 1-05 CO EQIH; • se 卜 Γ 0 00 00 r—Example 19 (Refer to the manual &gt; LO CO ο ID o CM L〇3 CM r— r— 〇〇CM 03 CD 〇ο τ—inch CD d 〇 ( (D Τ Ο not satisfied CsJO CO CQ sleep compensation ^-N CO inch CO 00 τ - Example 18 Raw material PET-5 i〇CO ο inch·iO o CnJ LO CM t— τ-~ 200 6 ο r—inch d OJ d Bu (D y - 〇 not satisfied 〇) CN CN O) 00 inch σ> 00 T~~ Example 17 Raw material PET-5 to CO ο LO o C\J You in CM T—two 200 b d Ο inch CD 6 CM d 卜 CD r - d not satisfied o CO r - cn 卜 inch CD 卜 € 0 - Example 16 raw material PET-5 ΙΛ 03 ο Ι Ω o CNi m LO CvJ r~ 200 卜 d Ο r - inch CM CM CD 卜 to r—d not satisfied 00 CNJ 〇O) 00 94 00 r~ |Example 15 Raw material ΡΕΤ·4 lO CO ο Ι Ι o CM 壊LD Csl r— τ— τ— 200ί 1 d Ο τ~· CM CM CM (D II Bu CD r - d not satisfied τ - CO 00 00 Bu CN σ &gt; Γ ΟΟ T*~ Raw materials | MD stretching ratio (1) 丄 im im ; 〇! H | 1st processing brewing. c) MOmmm 麒 degree ((4) ; carboxy 录 degree (eq/ton) ! 1 —__________ 1 Micro endothermic temperature TmeaCC) Solidity (dl/g) im MD TD Plane alignment coefficient B2(-) (B) The average reflectance (%) of the formula for the filling wavelength of 400~700nm is placed at 48 / j. If £ 18 O uij sg S| gl IS total thickness of the sheet (&quot;m) | 1 醤 150 150TC30 thermal shrinkage rate ( %) 倾·ε? ? ^ κ:» p|| « Sft X gt lif m 201037840 ο ο Example 28 1 Raw material ΡΕΤ-2 〇CO CNi CO 〇CO T— m in CNJ r— T~~ r— ir&gt卜d 〇00 04 a CO * CN ΙΟ ΙΟ Ο Meet l t 00 τ- 00 03 CM in 00 00 Example 27 Raw material ΡΕΤ-2 LO inch to to ID T- 薬in CM t-*· r- R- O to 卜do €0 T-· o (D 00 in h' 〇τ- Ο Meet 00 CN m σ&gt; CO LD 卜 卜 GO r- 丨Example 26 Raw material ΡΕΤ-2 . CO CO o inch iO To r~ 〇 i〇CM T- r~ r- o ΙΩ 卜 do 00 1- CO ui inch U) N r~ d Satisfy ο CO ο 0) CO 寸 CO 0) CO r-* Example 25 Raw material ΡΕΤ- 2 · 00 00 CM in ΙΏ T- m in CM T~ T-~ r- o LO y- r-. do 00 T~ inch CM CM CO τ- Ο Meet 00 csl ο 00 o &lt; N inch CO Bu CO r- 〇o LO Example 24 Raw material ΡΕΤ-2 CO CO CO CO in o 04 Destruction o ID 1~ oo CM Bu 00 T-inch CM in y-inch iD τ- Ο Not satisfied 04 CM ο 00 卜 〇 l Example 23 Raw material ΡΕΤ-2 CO CO &lt;£&gt; CO to o OJ Destroy to CM T- 二 200 卜do 00 r—· 寸 寸 寸&lt;£&gt; r·· Ο '00 00 00 00 inch is not satisfied (D 卜CO inch|Example 22 ΡΕΤ-8' CO CO CO CO o o CNJ m LD (N r- r- 〇o OJ OJ r- o 00 r- inch cs LO Inch (Ο r- d not satisfied 〇CO 〇σ> σσ> r- 00 Raw material I MD stretching ratio (1) | TD stretching ratio (1) | 1st processing temperature (t) 1 MD loose surface 1 degree (&quot ;m) Qian Ke Na degree (eq/t〇n) Micro heat absorption temperature TmesitfC) Intrinsic viscosity (dl/g) Atomic volume (ppm) measured by fluorescent X-ray MD QH Plane alignment coefficient B2(-) ( B) The average reflectance (%) of the formula for the charging wavelength of 400~700nm 丨 Placed for 48 hours and placed for 72 hours after II s « one #· e° fib sl 鹆 运 β β m read; mi: m 150°G30 points MSI rate (%) ig| p|| 111 朦北¢#1 鹤趣:劫_9ε — 201037840 〇o |Example 35 I Raw material ΡΕΤ-2 ' inch to 〇CM m IX) CM 1—r—to o CM Ο 〇CO r—inch CO 1—CO CD 〇> r~ 6 Meet 00 CvJ r~ CO 00 C \( in CO Γ 实施 Example 34 Raw material ΡΕΤ-2 CM meter' ο 谷ο r- eg m ω CM r*- r- -t— 2 05 卜d 〇CD r-* &lt;〇CM σ&gt; r— 〇03 Τ 〇 Satisfy 〇CO σ&gt; 卜1C CN CO 00 Bu CO τ— 实ί® Example 33 Raw material ΡΕΤ-2 tn in inch·ID 〇m LO &lt;N r-· T— 2 00 〇 〇 〇 00 Production tn CO &lt;N 00 CO σ&gt; -ρ- Ο satisfying CO CM CM σ&gt; o LO 卜 σ&gt; Γ' 00 -τ~- Example 32 Raw material ΡΕΤ-2 csj 'φ 〇'ti〇〇&lt;N m 10 CM t—1—200 卜〇o 00 1—00 oj 0 01 σ> Τ Τ 满足 meet r*—CO ο Ο) 〇CO LO Oi 卜 CO r- Example 31 Raw material ΡΕΤ-2 in inch ΙΌ inch · 〇CO r— 璀in &lt;NT~- T-LO 卜t-6 〇CO r— 00 in CO in cn cn Ο 满足 Meet CD CM CO σ> T~ lO ω 卜 00 τ~ Example 30 Raw material ΡΕΤ-2 ' 00 CO Ο o CO 1— m ld eg T— T— LO 卜 i — 卜〇 o CO r~ o to 04 inch · Bub τ- Satisfied, 〇CO CM 05 o inch tn CD 00 τ— |Example 29 Raw material ΡΕΤ-2 CO 00 CO CO 〇00 r— m LO 04 T— T— LD 卜 r~ r- d 〇CO T—to inch CD CO in 1 ο Meet CD CNJ 00 00 LO CO CN Oi Bu CO τ - Raw material 1 MD stretching ratio (1) 1 TD stretching ratio (1) | i-th processing temperature re) I MD squirrel 1 Freshness (&quot; m) carboxyl sulphide (eq/tem) micro-sand tasting TmeatCC) solidity (dl/g) amount of heteroatoms measured by fluorescent X-rays &lt;ppm) MD Ll〇_1 plane-direction coefficient Β2(1) 1 (Β Loose-filled | Sft 400~700nm average®^(%) placed after 48 hours and placed for 72 hours after I barefi §«-ft si extract II total thickness of sheet (_ 1 150 ° C 30 minutes heat shrinkage ( %) Bee P Yao · «si lif • Li_ m 201037840 〇〇Example 42 j Raw material PET-2 to οι CD 04 in to r— m ιο (N 1— 〇ιο r— 卜 6 Ο 00 r~ Ο inch CO CO 03 CNJ Τ Ο Not satisfied | G) CM CO LO CM CM to 00 r- Example 41 Raw material PET-2 . ο Ο LO CSJ CM mm CN r- t- r~ 〇CM 〇Ο 00 r— Oi Τ- 00 T~ o cn d not satisfied t- &lt;Τ) CNJ 00 CD 卜卜ω r- real Example 40 Raw material PET-2 〇CO &lt;N CO LO 00 T~~ m LO &lt;N r- T- r-*· 〇CO r- d Ο 〇0 r— Ο CO r~ CM 0. 1 54 Unsatisfied 00 CsJ to Bub σ&gt; Bu CO r~-1 Example 39 Raw material PET-2. α&gt; CM 00 04 1 80 m in Oi 1—in 卜i— 卜d Ο 00 r- 00 〇i 00 T - m Τ Ο not satisfied CO CO r- σ&gt; CM 00 Bu CO r- Example 38 Raw material PET-2 CO &lt;N CO &lt;N o CO r- destroyed in CM 1- T*~ T&quot;· in to r~ 卜ο 〇00 τ—CO inch CD CO CM CO production d not satisfied 03 OJ ΙΛ GO ο CO 00 τ ~~ Example 37 Raw material PET-2 tr> inch · LO in CNJ CM m LO CM T~ T ~ 〇CM Oi 卜d Ο 〇0 r- in CM in CNJ 00 〇&gt; Τ 满足 Meet 00 CM T- ω 00 T— ΙΩ 00 00 00 r- |Example 36 Raw material PET-2 CO Inch CO Inch I 225 Destroy LO CM T- r- o CNJ CNi ο Ο αο τ- t- CM r- CM CO σ> 〇 meet r- CO co CO ir- Oi 00 00 r- raw material 1 MD extension ratio (1) | TD extension Magnification (1) I 1st treatment temperature 〇c> MD squirrel alcoholicity ((4) | 1 M' I 1 l 1 ΜΛ m 1 Dream § Solidity (dl/g> 丨 fluorescent X-ray measurement of the atomic child ( Ppm) MD TD flat brewing coefficient B2(-) | (B) formula for the average reflectance of the 1 wavelength of 400~700nm (%) 幽回卜 A II II § m —* I齑Ρ涂ιη ψ· a鹆 1 1 Η Sc S total thickness of sheet (&quot;m) | Φβ St si w 探 Ms S _ t铢p|| s Si X gt iif — 8ε — m 鲣201037840

o D 比賴5 1 原料PET-2 Ο 寸 ο 寸 1 2 30| m in C\) T- T- T~ to CM CM 〇 ο 00 Ί- 00 r— r- r~- 00 05 t-· d 未滿足‘I 00 CM CO 寸 t— 03 寸 卜 〇0 τ- 比較例4 Η Μ Ah 亡竑 S1¾ Μ ^ CO CO &lt;〇 CO 2 30 m ID CM T~~ LO LD Csi 卜 d 〇 00 r- CO τ~ Ύ-r-- 0. 1 64 未滿足 00 CM 46 o CO 寸 卜 00 τ-· 比較例3 原料PET-1 CO CO to CO Ο CO Οί m U&gt; CM T- CO Τ'— LO CM f、 d Ο 00 τ- CO V- CN i― 0. 1 64 未滿足 Ο ¢0 (Μ 寸 o 寸 寸 卜 00 T- 比較例2 原料PET-9 CO CO &lt;0 CO m CM CM m lO OJ f- to r- 〇 CM CM 卜 6 Ο 00 ττ- σ) τ- CNJ r- 寸 to yr- o 未滿足 CO CM CO 寸 o 寸 寸 卜 CQ T- |比較例1 原料PET-9 CO CO &lt;£) CO ΙΟ 00 T- 摧 ΙΏ &lt;N r~ ΙΩ τ~· 〇 CO T- 卜 d ο 00 产 &lt;〇 00 寸 CO Ι Ο 滿足 σ&gt; CM LO 寸 o CD 寸 卜 00 τ- 原料 | MD延伸倍率㈠ | TD延伸倍率㈠ 第1處理酿rc) i MD鬆贼理 度(/m) _末端基濃度(eq/ton) 微小吸熱逢値溫度Tmeat(1C) 1 固有黏度(dl/g) g s If MD HP_ 平®B3向係數B2(-) (B)诚的充她 波長400~700nm的平均反射率(%) SI II 1| 1| 薄片總厚度(㈣) | 幽 潷 1 X 额 150t30 分 熱收縮率(%) p|| s s® ^ g t lif 鹦造:#! 嫌北您却 — 6· m 201037840 又,表格中「薄片」係指「背板」。 產業上之可利用性 本發明的膜可適合使用在使用背板之太陽電池。 【圖式簡單說明】 第1圖係求得薄膜之微小吸熱峰値溫度的示差掃描量熱 法(DSC )測量結果之一實施例示意圖。 【主要元件符號說明】 4E 〇 ❹ 〇 -40-o D 比赖 5 1 Raw material PET-2 Ο inch ο inch 1 2 30| m in C\) T- T- T~ to CM CM 〇ο 00 Ί- 00 r- r- r~- 00 05 t-· d Not satisfied 'I 00 CM CO inch t-03 inch 〇 〇 0 τ - Comparative example 4 Η Μ Ah 竑 竑 S13⁄4 Μ ^ CO CO &lt;〇CO 2 30 m ID CM T~~ LO LD Csi 卜d 〇00 R- CO τ~ Ύ-r-- 0. 1 64 Not satisfied 00 CM 46 o CO Inch 00 τ-· Comparative Example 3 Raw material PET-1 CO CO to CO Ο CO Οί m U&gt; CM T- CO Τ' — LO CM f, d Ο 00 τ- CO V- CN i― 0. 1 64 Not satisfied Ο ¢0 (Μ 寸 寸 inch 00 T- Comparative example 2 Raw material PET-9 CO CO &lt;0 CO m CM CM m lO OJ f- to r- 〇CM CM 卜6 Ο 00 ττ- σ) τ- CNJ r- inch to yr- o Not satisfied CO CM CO inch o inch inch CQ T- |Comparative example 1 Raw material PET-9 CO CO &lt;£) CO ΙΟ 00 T- Destroy &lt;N r~ ΙΩ τ~· 〇CO T- 卜d ο 00 Production &lt;〇00 inch CO Ι Ο Satisfy σ&gt; CM LO inch o CD inch 00 τ - Raw materials | MD stretching ratio (1) | TD stretching ratio (1) 1st processing rc) i MD thief ration (/m) _ end group concentration (eq/ton) Micro endothermic temperature Tmeat (1C) 1 Intrinsic viscosity ( Dl/g) g s If MD HP_ 平® B3 to the coefficient B2(-) (B) The average reflectance of the wavelength of 400~700nm (%) SI II 1| 1| total thickness of the sheet ((4)) | 幽潷1 X amount 150t30 Fractional heat shrinkage rate (%) p|| ss® ^ gt lif 雀造造:#! 嫌北你就— 6· m 201037840 Also, the “sheet” in the table means “backboard”. Industrial Applicability The film of the present invention can be suitably used in a solar cell using a back sheet. BRIEF DESCRIPTION OF THE DRAWINGS Fig. 1 is a schematic view showing an example of differential scanning calorimetry (DSC) measurement results of a micro endothermic peak temperature of a film. [Main component symbol description] 4E 〇 ❹ 〇 -40-

Claims (1)

201037840 七、申請專利祐圍· 1. 一種太陽電池用聚酯膜,其包含:羧基末端; 13eq/ton以下,且根據示差掃描量熱法(DSC) 微小吸熱峰値溫度Tmeta ( °C )爲220°C以下。 2. 如申請專利範圍第1項之太陽電池用聚酯膜,其 邊方向(MD)及其橫向(TD)於150°C、30分 縮率各爲0.6 %以下。 3. 如申請專利範圍第1項或第2項之太陽電池用聚 〇 ^ 中平面配向係數B2爲0.165以上。 4. 如申請專利範圍第1項至第3項中任一項之太陽 酯膜,其中根據螢光X光測定所求得之磷原子 200ppm 以上。 5. 如申請專利範圍第1項至第4項中任一項之太陽 酯膜,其中該微小吸熱峰値溫度Tmeta ( °C )爲 下。 _ 6.如申請專利範圍第1項至第5項中任一項之太陽 〇 酯膜,其中至少一側表面之波長400〜700nm的 率爲80%以上。 7. 如申請專利範圍第1項至第6項中任一項之太陽 酯膜,其中固有黏度在0.6〜1.2dl/g的範圍之間 8. 如申請專利範圍第1項至第7項中任一項之太陽 .酯膜,其中羧基末端基濃度爲12eq/ton以下。 9. 如申請專利範圍第1項至第8項中任一項之太陽 酯膜,其中聚酯層至少有2層。 i濃度爲 所求得之 中膜的長 鐘之熱收 酯膜,其 電池用聚 含有量爲 電池用聚 205。。以 電池用聚 平均反射 電池用聚 〇 電池用聚 電池用聚 -41- 201037840 10. 如申請專利範圍第1項至第9項中任一項之太陽電池用聚 酯膜,其中在125 °C、濕度100%的條件下放置48小時後 的平均伸度保持率爲5 0%以上。 11. 如申請專利範圍第1項至第10項中任一項之太陽電池用 聚酯膜,其中在125 °C、濕度100%的條件下放置72小時 後的平均伸度保持率爲10%以上。 12. 如申請專利範圍第1項至第11項中任一項之太陽電池用 _ 聚酯膜,其中Tmeta ( °C )與平面配向係數B2滿足以下 Ο 公式(B ) B2 g 0.00 0 86 xTmeta-0.002 86。 1 3 . —種製造如申請專利範圍第1項至第1 2項中任一項所記 載之太陽電池用聚酯膜的製造方法,其包含:針對未延伸 聚酯膜的至少一軸進行延伸後,以220°C以下的溫度進行 熱處理。 14.一種太陽電池背板,係至少包含1片如申請專利範圍第1 項至第12項中任一項所記載之太陽電池用聚酯膜。 Q 15.如申請專利範圍第14項之太陽電池背板,其中在125 °C、 濕度1 〇〇%的條件下放置48小時後的平均伸度保持率爲 5 0%以上。 16.—種太陽電池,係使用如申請專利範圍第14項或第15項 所記載之太陽電池背板所製成者。 I7·—種太陽電池用聚酯膜的製造方法,其包含:在具有羧基 末端基濃度爲13eq/ton以下之聚酯膜的製造方法中,針對 未延伸聚酯膜的至少一軸進行延伸後,以2 0 5 °C以下的溫 度進行熱處理。 -42- 201037840 18.如申請專利範圍第17項之太陽電池用聚酯膜的製造方 法,其中聚酯膜的羧基末端基濃度爲12eq/t〇n以下。201037840 VII. Application for patents. 1. A polyester film for solar cells, comprising: carboxyl terminal; 13 eq/ton or less, and according to differential scanning calorimetry (DSC), the micro endothermic peak temperature Tmeta (°C) is Below 220 °C. 2. For the polyester film for solar cells according to item 1 of the patent application, the side direction (MD) and the transverse direction (TD) thereof are 150 ° C and the 30-fold reduction ratio is 0.6% or less. 3. For the solar cell 聚 ^ in the patent application range 1 or 2, the plane alignment coefficient B2 is 0.165 or more. 4. The solar ester film according to any one of claims 1 to 3, wherein the phosphorus atom determined by the fluorescent X-ray measurement is 200 ppm or more. 5. The solar ester film according to any one of claims 1 to 4, wherein the micro endothermic peak temperature Tmeta (°C) is below. 6. The solar oxime ester film according to any one of claims 1 to 5, wherein the at least one surface has a wavelength of from 400 to 700 nm of 80% or more. 7. The solar ester film according to any one of claims 1 to 6, wherein the intrinsic viscosity is in the range of 0.6 to 1.2 dl/g. 8. In the first to seventh items of the patent application scope. Any of the solar ester films in which the carboxyl terminal group concentration is 12 eq/ton or less. 9. The solar ester film of any one of claims 1 to 8, wherein the polyester layer has at least 2 layers. The i-concentration is the heat-collecting ester film of the obtained film for a long period of time, and the battery has a polycondensation amount of the battery 205. . The use of a polyester film for a solar cell according to any one of the first to ninth aspects of the invention, wherein the film is at 125 ° C. The average elongation retention rate after standing for 48 hours under the conditions of 100% humidity was 50% or more. 11. The polyester film for a solar cell according to any one of claims 1 to 10, wherein the average elongation retention after leaving for 72 hours at 125 ° C and 100% humidity is 10%. the above. 12. For the solar cell _ polyester film according to any one of claims 1 to 11, wherein Tmeta ( °C ) and the plane alignment coefficient B2 satisfy the following formula B Formula (B) B2 g 0.00 0 86 xTmeta -0.002 86. The method for producing a polyester film for a solar cell according to any one of claims 1 to 2, further comprising: after extending at least one axis of the unstretched polyester film The heat treatment is performed at a temperature of 220 ° C or lower. A solar battery back sheet comprising at least one polyester film for a solar cell according to any one of claims 1 to 12. Q 15. For the solar cell backsheet of claim 14, the average elongation retention after leaving for 48 hours at 125 ° C and humidity of 1 〇〇% is more than 50%. 16. A solar cell produced by using a solar cell backsheet as recited in claim 14 or claim 15. A method for producing a polyester film for a solar cell, comprising: after extending at least one axis of the unstretched polyester film in a method for producing a polyester film having a carboxyl group-based group concentration of 13 eq/ton or less; The heat treatment is performed at a temperature of 20.5 ° C or lower. The method for producing a polyester film for a solar cell according to claim 17, wherein the polyester film has a carboxyl terminal group concentration of 12 eq/t 〇 n or less. -43--43-
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