TW201244915A - Process for producing solar cell sealing sheet - Google Patents

Process for producing solar cell sealing sheet Download PDF

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Publication number
TW201244915A
TW201244915A TW101111289A TW101111289A TW201244915A TW 201244915 A TW201244915 A TW 201244915A TW 101111289 A TW101111289 A TW 101111289A TW 101111289 A TW101111289 A TW 101111289A TW 201244915 A TW201244915 A TW 201244915A
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Taiwan
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sheet
solar cell
sealing sheet
temperature
embossing
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TW101111289A
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Chinese (zh)
Inventor
Yoshiyuki Oka
Makoto Nakahara
Makoto Sato
Takashi Ichinomiya
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Toray Industries
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Publication of TW201244915A publication Critical patent/TW201244915A/en

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    • 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

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  • Shaping Of Tube Ends By Bending Or Straightening (AREA)

Abstract

The present invention is a process for producing a solar cell sealing sheet, the process comprising conducting the following steps (a), (b), and (c) in the this order: a step (a) in which a resin composition that has been melted by heating is formed into a sheet and then cooled to obtain a web sheet; a step (b) in which at least one surface of the web sheet obtained in the step (a) is heated for 22-55 seconds to elevate, during this heating, the temperature of this surface to a temperature not lower than the melting point of the resin composition that constitutes this surface; and a step (c) in which the surface of the web sheet which has been heated in the step (b) is made to have a temperature within a specific range, and an embossing roller is subsequently pushed against this surface to form an embossed pattern in the surface. Thus, a solar cell sealing sheet which suffers little heat shrinkage and in which a distinct embossed pattern has been formed can be efficiently produced at low cost.

Description

201244915 六、發明說明: 【發明所屬之技術領域】 本發明係關於一種太陽電池密封片材之製造方法。尤其是 關於一種較佳用於製造加熱收縮較小、且於表面形成有清晰 之突起之太陽電池密封片材的片材之製造方法。 【先前技術】 近年來,就資源之有效利用或環境污染之防止等方面而 言’將太陽光直接轉換為電能之太陽電池受到關注而進行有 各種開發。通常,太陽電池係於玻璃基板所代表之受光面保 護材與稱為底層片材之背面保護材之間以太陽電池密封片 材(以下記為密封片材)將太陽電池單元密封的構成。 作為太陽電池模組之主流即結晶矽型太陽電池通常係以 如下方式製造。首先,依序積層玻璃基板、密封片材、太陽 電池單元(矽發電元件)、密封片材及底層片材。該密封片材 通常由乙烯-乙酸乙烯酯共聚合體(以下記為 EVA(ethylene-vinyl acetate copolymer))所構成。繼而,利用 真空層壓機於真空下加熱該積層體’將密封片材加熱炫融而 使其交聯硬化。以此方式而製造各構成構件無氣泡地接著之 太陽電池模組。 於此種太陽電池模組之製造中’若密封片材於加熱時之收 縮較大’則有時由於該收縮變形而矽發電元件破損,或單元 之位置偏移。因此,要求密封片材於加熱時之收縮較小。進 101111289 3 201244915 、年來4 了、,ΌΒΘ石夕之資源有效利用、或適於太陽電池模 組普及之降低成本,㈣發電元狀厚錢得料· ^ 左右’進而變得易於破損。因此,使密封片材之加熱收縮較 小之要求變得進㈣烈。因此,正研究減小密則材之加孰 收縮率之各種方法。(例如,專利文獻1)β 又’除對上述製造時之要求以外,關於太陽電池模組,為 可於製造後長期使用,而其可靠性亦極為重要4為於經長 ,使用之太陽電池模組中產生之代表性之異常,有太陽電池 單兀與ί&封片材之間之剝離、膨脹等外觀不良、或伴隨其之 發電量之降低。該等異常現象之理由並不明確’正就構成密 封片材之原材料方面進行研究。例如,正研究調整構成密封 片材之EVA之黏度的方法(專利文獻幻,或為提昇太陽電池 單元與雄封片材之接著強度而添加矽烷偶合劑之方法(專利 文獻3)等。 進而,亦正就密封片材之構造方面進行各種研究。為防止 伴隨長期使用而產生之膨脹等,使剛製造之模組内部之各構 成構件儘可能以無氣泡之狀態而接著較為重要。於是,為於 真空層合時容易排放空氣,而嘗試於密封片材之表面上形成 壓紋形狀等各種突起或凹處。又,該等突起或凹處有時亦係 為防止太陽電池單元由於層合時之壓製壓力而破損,或提昇 密封片材之處理性等目的而形成。關於壓紋紋樣,針對其來 狀或深度等提出有詳細之提案(專利文獻4、5)。 101111289 4 201244915 如上所述,於製造密封片材時,減少密封片材之加熱收 縮、且於密封片材之表面上形成清晰之壓紋形狀較為重要。 作為此前所提出之方法,揭示有:於澆鑄使用雙軸擠出機等 擠出機自τ字模擠出之片材時,於喷嘴正下方於片材上形 成壓紋形狀,其後視需要進行減少加熱收縮之退火處理的方 法(專利文獻6)。 [先前技術文獻] [專利文獻] 專利文獻1 專利文獻2 專利文獻3 專利文獻4 專利文獻5 專利文獻6 曰本專利特開 曰本專利特開 曰本專利特開 曰本專利特開 曰本專利特開 曰本專利特開 2000-084996 號公報 2002-170971 號公報 2000-183382 號公報 2006-134970 號公報 2002-185027 號公報 2010-100032 號公報 【發明内容】 (發明所欲解決之問題) 專利文獻6之製造方法係於製造步驟中之片材(以下記為 步驟片材)之表面上形成壓紋形狀之後,對該步驟片材進行 退火處理。因此,若為減少密封片材之加熱收縮而將步驟片 材充分加熱,則會由於該加熱而形成於步驟片材之表面上之 壓紋形狀變形。相反,若為保持壓紋形狀而減弱步驟片材之 加熱,則退火處理變得不充分。如此,於專利文獻6之製造 101111289 5 201244915 之減少與明確地形成壓紋形狀非 方法中’同時貫現加熱收墙 常困難。 又’作為減少密封片材之 ^ ^ _ 熱收縮之方法,通常如專利令 獻1中所揭不般而利用如下方、去.、 」文 器搬送樹脂薄膜時,使人σ側於以具有複數之麵之輪送 周速等,使步驟片材收縮而·、^周速快於出口側之輥之 士、 。 延伸,故而加熱收縮之去降尤 充为,必需歷經1〜2分鐘之長時 除不 焚寻間而貫施退火處理。 又,多數情況下由EVA所椹忐令一 u u 汀構成之密封片材中含有交聯 劑’由於步驟片材之成形溫度為低溫’故而於步驟片材中車 多地殘存有殘留應變。並且,多數情況下該殘留應變於寬巾s 之步驟片材之寬度方向上不均勻。若對此種狀態之步驟片材 如上所述地進行退火處理,則產生片材之平面性受損, 、,厚度 變得不均勻,或退火處理中步驟片材變得彎彎曲曲等異常 進而,以複數之輥對此種狀態之步驟片材進行夾持加 /至建續 地實施壓紋加工等非常困難。 因此,本發明之目的在於提供一種可充分減少密封片材之 加熱收縮、且於密封片材之表面上形成清晰之壓紋形狀 造方法^ (解決問題之手段) 為解決上述課題,本發明之太陽電池密封片材之製造方去 之特徵在於:依序進行下述步驟(a)、步驟(b)及步驟(c)。 101111289 6 201244915 步驟(a):使藉由加熱而炫融之樹脂組成物成形為片材 狀,繼而藉由冷卻而獲得步驟片材之步驟; 步驟(b).將上述步驟⑷中所獲得之步驟片材之至少一個 表面加熱22〜55秒鐘,於該加熱中使該表面之溫度達到構 成該表面部分之樹脂組成物之熔點以上的溫度之步驟; 步驟(c):使於上述步驟(b)中經加熱之步驟片材之表面成 為(構成上述表面部分之樹脂組成物之熔點_1〇。〇〜(構成上 述表面部分之樹脂組成物之熔點+20。〇之溫度,繼而對該表 面按壓壓紋親而於該表面上形成壓紋形狀之步驟。 (發明效果) 根據本發明,可以低成本且效率良好地製造加熱收縮較 小、且形成有清晰之壓紋形狀之太陽電池密封片材。 【實施方式】 [太陽電池密封片材之製造方法] 本發明之太陽電池密封片材之製造方法係依序進行下述 步驟(a)、步驟(b)及步驟(c)。 步驟(a):使藉由力口熱而炼融之樹脂組成物成开;為片材 狀,繼而藉由冷卻而獲得步驟片材之步驟。 步驟(b):將上述步驟(a)中所獲得之步驟片材之至少〜烟 表面加熱22〜55秒鐘’於該加熱中使該表面之溫度達到構 成該表面部分之樹脂組成物之熔點以上的溫度之步驟。 步驟(c):使於上述步驟(b)中經加熱之步驟片材之表面成 101111289 7 201244915 為(構成上述表面部分之樹脂組成物之熔點_10^)〜(構成上 述表面部分之樹脂組成物之溶點+20。〇之溫度,繼而對該表 面上按壓壓紋輥而於該表面上形成壓紋形狀之步驟。 以下,針對本發明之太陽電池密封片材之製造方法,—面 參照圖式一面進行說明。圖1係表示本發明之製造方法之— 之實施態樣的概略模式圖。 [步驟(a):製膜步驟] 首先,針對步驟(a)進行說明。步驟(a)係使原料樹脂成形 為片材狀並將其冷卻而獲得步驟片材之步驟。以下,將步驟 0)稱為製膜步驟。 於圖1中之製膜步驟中,設置有:於高溫下使原料樹脂與 添加劑熔化並進行混練之擠出機11、減少樹脂之壓力變動 而使片材之厚度穩定化之齒輪泵31、將經混練之熔融樹脂 擠出為片材狀之模具12、使所擠出之高溫之步驟片材冷卻 固化而成形為固體之步驟片材的拋光輥13a、13b及13C。 作為擠出機11,可使用單軸擠出機或雙軸擠出機。就生 產性或樹脂與添加劑之混練性等方面而言,較佳為使用雙軸 擠出機。於使用單軸擠出機之情形時,由於擠出機内充滿樹 脂’故而擠出機前端之模具部分中之壓力變動相對較小,因 此並非必需設置齒輪泵31等定量供給裝置。於使用雙軸擠 出機之情形時,由於擠出機内並非充滿之狀態,故而較佳為 於擠出機與模具之間設置齒輪泵31等定量供給裝置。 10Π11289 8 201244915 關於技入擦出機u中之原料樹脂及添加劑,可投入預先 利用混合機錢拌器等進行混合者,亦可將各自分別投入。 又,亦可使用於擠出機之中途側飼添加劑、或若為液體之添 加劑則以注入泵等進行添加之方法等。 混練原料樹脂與添加劑時之溫度係依據所使用之樹脂之 種類或黏度而定,但較佳為(原料樹脂之熔點職Η原料 樹脂之賴職)之範ι再者,於本發日种,所謂炼點係 於-差掃描熱量測定(DSC,贿⑽如丨 —㈣中以和min進行升溫時之吸熱峰值溫度。作 為密封片材,於為通常所使用之跳片材之情形時,多數 情形下為使隱交聯而含有有機過氧化物作為添加劑。因 此’必需留意儘量使有機過氧化物不分解而進行混練。因 此’作為樹脂溫度,例如於炼點為7代左右之隱之情形 時,。較佳為於8G〜13G°C之範圍㈣行轉。更佳為100〜 〇C之範®未滿8GC時’存在混練性不充分而添加劑之 均句分散性降低之可雜。其結果為,存在密封片材之外觀 變差之可能性。若超過13()ΐ,則有時於調配有有機過氧化 物之情形時有機過氧化物分解,密封片材之品質不穩定,此 外連續生產性亦降低。 再者,於圖1之步驟中,作為將步驟片材進行製膜之方法 而設置有擠出機,但亦可使用利㈣输之成形等已知之不 同方法。 101111289 9 201244915 利用擠出機11等使原料樹胎金4 &與添力嗜純魏練之炼融 樹脂係使用模具12擠出為片材狀。 ^201244915 VI. Description of the Invention: [Technical Field of the Invention] The present invention relates to a method of manufacturing a solar cell sealing sheet. More particularly, it relates to a method for producing a sheet which is preferably used for producing a solar cell encapsulating sheet having a small heat shrinkage and having a sharp protrusion formed on the surface. [Prior Art] In recent years, solar cells that directly convert sunlight into electric energy have been developed in various aspects in terms of effective use of resources or prevention of environmental pollution. In general, a solar cell is configured by sealing a solar cell unit with a solar cell sealing sheet (hereinafter referred to as a sealing sheet) between a light-receiving surface protective material represented by a glass substrate and a back surface protective material called a back sheet. As a mainstream of solar cell modules, a crystalline germanium type solar cell is usually manufactured in the following manner. First, a glass substrate, a sealing sheet, a solar cell unit (tantalum power generation element), a sealing sheet, and an underlayer sheet are sequentially laminated. This sealing sheet is usually composed of an ethylene-vinyl acetate copolymer (hereinafter referred to as EVA (ethylene-vinyl acetate copolymer)). Then, the laminated body was heated under vacuum by a vacuum laminator', and the sealing sheet was heated and fused to be cross-linked and hardened. In this way, the solar cell module in which each constituent member is bubble-free is manufactured. In the manufacture of such a solar cell module, "if the sealing sheet shrinks when heated", the power generating element may be broken due to the shrinkage deformation, or the position of the unit may be shifted. Therefore, the sealing sheet is required to have a small shrinkage upon heating. Into 101111289 3 201244915, the year has come, and the resources of the Shishixi are effectively utilized, or the cost is reduced for the popularization of the solar cell module, and (4) the power generation is thick and the material is good, and then it becomes easy to break. Therefore, the requirement that the heat shrinkage of the sealing sheet is small is made four (4). Therefore, various methods for reducing the shrinkage rate of the dense material are being studied. (For example, Patent Document 1) β, in addition to the requirements for the above-mentioned manufacturing, the solar cell module can be used for a long period of time after manufacture, and its reliability is extremely important. The representative anomalies generated in the module are poor appearance such as peeling and expansion between the solar cell unit and the ί& sealing sheet, or a decrease in the amount of power generation accompanying it. The reason for these anomalies is not clear, and research is being conducted on the raw materials constituting the sealing sheet. For example, a method of adjusting the viscosity of the EVA constituting the sealing sheet (a patent document, or a method of adding a decane coupling agent to enhance the adhesion strength between the solar cell unit and the male sheet) (Patent Document 3), etc. Various studies have been conducted on the structure of the sealing sheet. In order to prevent expansion and the like accompanying long-term use, it is important that the constituent members inside the module to be manufactured are as air-free as possible. It is easy to discharge air during vacuum lamination, and attempts to form various protrusions or recesses such as an embossed shape on the surface of the sealing sheet. Moreover, the protrusions or recesses are sometimes used to prevent solar cells from being laminated due to lamination. The pressing pressure is broken, or the sealing sheet is raised for the purpose of rationality, etc. Regarding the embossing pattern, a detailed proposal is proposed for the shape or depth thereof (Patent Documents 4 and 5). 101111289 4 201244915 In the manufacture of the sealing sheet, it is important to reduce the heat shrinkage of the sealing sheet and form a clear embossed shape on the surface of the sealing sheet. The method proposed in the prior art discloses that when a sheet extruded from a τ-shaped die is cast using an extruder such as a twin-screw extruder, an embossed shape is formed on the sheet directly under the nozzle, and the rear view is required to be reduced. Method for annealing treatment by heat shrinkage (Patent Document 6) [Prior Art Document] [Patent Document] Patent Document 1 Patent Document 2 Patent Document 3 Patent Document 4 Patent Document 5 Patent Document 6 Patent Application Patent Publication No. Japanese Laid-Open Patent Publication No. 2000-084996, No. 2002-170971, No. 2000-183382, No. 2006-134970, No. 2002-185027 SUMMARY OF THE INVENTION (Problems to be Solved by the Invention) The manufacturing method of Patent Document 6 is to anneal the sheet after forming an embossed shape on the surface of a sheet (hereinafter referred to as a step sheet) in the manufacturing step. Therefore, if the step sheet is sufficiently heated to reduce the heat shrinkage of the sealing sheet, the embossed shape formed on the surface of the step sheet due to the heating is deformed. On the other hand, if the heating of the step sheet is weakened in order to maintain the embossed shape, the annealing treatment becomes insufficient. Thus, the reduction in the manufacture of 101111289 5 201244915 of Patent Document 6 and the non-method of clearly forming the embossed shape are simultaneously It is often difficult to heat the wall. In addition, as a method of reducing the heat shrinkage of the sealing sheet, it is usually used as follows in the patent order, and the following method is used to transfer the resin film. The person σ is placed on the side of the wheel with a plurality of faces, and the step sheet is contracted, and the peripheral speed is faster than that of the roller on the outlet side, so that the heat shrinkage is particularly high. It must be annealed for a period of 1 to 2 minutes, unless it is not burned. Further, in many cases, the EVA has a cross-linking agent contained in the sealing sheet composed of a ruthenium. Since the forming temperature of the step sheet is low, there is a residual strain remaining in the step sheet. Further, in many cases, the residual strain is uneven in the width direction of the step sheet of the wide towel s. When the step sheet of such a state is annealed as described above, the planarity of the sheet is impaired, the thickness becomes uneven, or the sheet of the step in the annealing process becomes abnormal, such as bending and bending. It is very difficult to perform the embossing process, such as the step of adding/removing the step sheet of the state in a plurality of rolls. Accordingly, an object of the present invention is to provide a method for sufficiently reducing the heat shrinkage of a sealing sheet and forming a clear embossed shape on the surface of the sealing sheet. (Means for Solving the Problems) In order to solve the above problems, the present invention The manufacturing method of the solar cell sealing sheet is characterized in that the following steps (a), (b) and (c) are sequentially performed. 101111289 6 201244915 Step (a): forming a resin composition which is smelted by heating into a sheet form, and then obtaining a step sheet by cooling; Step (b). Obtaining the above obtained in the step (4) At least one surface of the step sheet is heated for 22 to 55 seconds, and the temperature of the surface is brought to a temperature above the melting point of the resin composition constituting the surface portion during the heating; step (c): in the above step ( b) the step of heating the step of the sheet becomes (the melting point of the resin composition constituting the surface portion, 〇 〇 ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( The step of pressing the embossing surface to form an embossed shape on the surface. (Effect of the Invention) According to the present invention, it is possible to manufacture a solar cell seal having a small heat shrinkage and a clear embossed shape at low cost and with high efficiency. [Embodiment] [Method for Producing Solar Cell Sealing Sheet] The method for producing a solar cell sealing sheet of the present invention is to sequentially perform the following steps (a), (b) and (c). (a): forming a resin composition which is fused by heat of the mouth; forming a sheet, and then obtaining a step sheet by cooling. Step (b): in the above step (a) The at least one of the obtained step sheets is heated to a temperature of 22 to 55 seconds in which the temperature of the surface reaches a temperature higher than a melting point of the resin composition constituting the surface portion. Step (c): The surface of the step of heating in the above step (b) is 101111289 7 201244915 (the melting point of the resin composition constituting the surface portion _10^)~ (the melting point of the resin composition constituting the surface portion +20). The step of pressing the embossing roll on the surface to form an embossed shape on the surface. Hereinafter, the method for producing the solar cell sealing sheet of the present invention will be described with reference to the drawings. 1 is a schematic view showing an embodiment of the production method of the present invention. [Step (a): Film forming step] First, the step (a) will be described. In the step (a), the raw material resin is formed into a sheet. The material is shaped and cooled to obtain a step sheet In the following, the step 0) is referred to as a film forming step. In the film forming step in Fig. 1, an extruder 11 is provided which melts and kneads the raw material resin and the additive at a high temperature to reduce the pressure of the resin. The gear pump 31 that stabilizes the thickness of the sheet, the mold 12 that extrudes the kneaded molten resin into a sheet shape, and the step sheet that is extruded at a high temperature is cooled and solidified to form a solid sheet. Polishing rolls 13a, 13b, and 13C. A single-axis extruder or a twin-screw extruder can be used as the extruder 11. In terms of productivity, kneading of the resin and the additive, etc., it is preferable to use a double shaft. In the case of using a single-screw extruder, since the pressure in the mold portion of the extruder front end is relatively small because the extruder is filled with the resin, it is not necessary to provide a quantitative supply device such as the gear pump 31. In the case of using a twin-screw extruder, since the inside of the extruder is not full, it is preferable to provide a quantitative supply device such as a gear pump 31 between the extruder and the mold. 10Π11289 8 201244915 The raw material resin and the additive in the technical-injection machine u can be put into a premixed mixer or the like, or they can be separately supplied. Further, it is also possible to use a side-feed additive in the middle of the extruder or a method of adding it by an injection pump or the like in the case of a liquid additive. The temperature at which the raw material resin and the additive are kneaded is determined depending on the kind or viscosity of the resin to be used, but it is preferably (the raw material resin is the melting point of the raw material resin). The so-called refining point is the endothermic peak temperature of the differential scanning calorimetry (DSC, bribe (10), such as 丨-(4), and the temperature is raised by min. As the sealing sheet, in the case of the commonly used hopping sheet, most In this case, an organic peroxide is contained as an additive for the concealment. Therefore, it is necessary to pay attention to mixing the organic peroxide as much as possible without decomposition. Therefore, as the resin temperature, for example, the refining point is about 7 generations. Preferably, it is in the range of 8G to 13G °C (four), more preferably 100~ 〇C of the standard® is less than 8GC, and there is a lack of kneading and a decrease in the uniformity of the additive. As a result, there is a possibility that the appearance of the sealing sheet is deteriorated. When it exceeds 13 (), the organic peroxide may be decomposed when the organic peroxide is blended, and the quality of the sealing sheet is unstable. In addition, continuous productivity Further, in the step of Fig. 1, an extruder is provided as a method of forming a step sheet, but a known different method such as forming of a profit can be used. 101111289 9 201244915 Using extrusion The machine 11 and the like are used to extrude the raw material tree gold 4 & and the force-purifying Wei Lian refining resin into a sheet shape using the mold 12. ^

字模或圓形模具等。平板狀之模I作為模具12,可使用T 寬度而形成寬幅之形狀,故^ ^依闕欲擠出之片材 女裳於擠出機上則成為T 型,因而統稱為T字模。又,於T _ 、T予模中,由於在模具之 寬度方向上滯留時間或流速等不同 冰 ’故而易於產生厚薄不均 (uneven thickness) 4 問題’或於弗 办a + l re 、中於加熱步驟片材時 寬度方向上之厚度不均等。為解決、丄、 、上4問題較佳為使用圓筒 狀:圓形模具。圓形模具係用於將樹㈣出為圓筒狀並藉由 將其切開而成形為片材狀之圓符灿+ 叫问狀之模具,片材寬度向 上之物性易於變得相對均勻。 又,於使用T字模之情形時, κ用银數之擠出機擠出不 同之樹脂組成物’亦可藉由進料掇 寸模組方式或多模方式等丘擠 出方法而將步㈣材製成積層構 万式^、擠 占. « . „ 战藉由製成此種積層構 成,可按各層作為密封片材而將必 調節添加·而降低成本。^雜分離’或可藉由 使用模具12所擠出之步驟片材係__n13b、 13c成形為片材狀。拋光輥係用於以一 對概對炼融樹脂夾持 行片材之厚度及表面性之賦形之包含複數之 驟片材搬送裝置。構成該裝置 < 各棍具備調整為適於 熔融树脂之冷卻或賦形性之溫度 Ρ <錢構、或調整各輥間之間 隙及加壓壓力之機構。又,較佳為, 硯硌要而藉由流入冷卻 101111289 201244915 水等調溫水而防止步驟片材之黏著提昇成形性。較佳為冷卻 水之溫度調整為0〜3(rc之範圍。由於依據所使用之樹脂之 組成不同而有時高溫之樹脂易於黏著於輥之表面,故而較佳 為拋光輥中位於最上游侧之拋光輥13a於表面上捲附矽橡 膠等而提昇脫模性。進而為提昇搬送性,亦較佳為將位於最 上游側之拋光輥13a之對向輥13b設為具有梨皮狀之表面形 態的金屬輥。較佳為,梨皮狀之面粗糙度為jisb〇6〇1_1994 中斤疋義之10點平均粗糙度rz為2〜口爪左右的範圍。 於在抛光親13a之表面上捲附石夕橡膠等且將對向輥既設為 具有梨皮狀之表面形態之金屬輥的情形時,拋光輥13a之表 之夕橡膠之厚度較佳為3〜10 mm,更佳為4〜8 mm。若 夕橡膠之厚度未滿3 mm,則有時梨皮狀之紋樣之轉印不充 a步驟片材黏著於用以搬送步驟片材之自由輥等。若石夕橡 膠之厚度超過1Gmm,财時由於源自炫賴狀熱蓄積於 橡膠表面而樹脂黏著於輥。 [步驟(b):退火處理步驟] +繼而針對步驟⑻綺說明。步驟⑻之目的在於去除製膜 乂驟中所成形之步驟片材所具有之殘留應變,減少步驟片材 之加熱收縮。於步驟(b)中,可列舉_面利用設置於退火爐 之中之加熱器16進行加熱,一面使步驟片材通過複數之 送輥17上等方法。以下,將步驟(b)稱為退火步驟。 用以加熱步驟片材之加熱器16只要為可加熱步驟片材者 >01111289 201244915 則無特別限定,可使用陶 熱器等公知之方半六%,、益、不鏽鋼加熱器、護套加 於可於片材之厚度;力,片^ 佳地使用利用熱風或蒸汽等執媒之;:而較佳…亦可較 觸之方法等。該等加熱方法可單較n與經加熱之輥接 而使用。 之用’亦可組合幾種方法 用以搬送步驟片材之搬送輥17 片材,故而較佳為脫模加熱之步驟 塗金屬藉由壓紋加工或者喷 :或金屬氧化物等化合物而於表面上設置有凹凸之金 :乂、可使用塗佈有聚四氟乙稀、全i乙稀丙烯共聚物、全 氟燒氧基燒烴等氟樹脂之1¾ ^或者,亦可使用於金屬親之表 面上捲附有經脫模性之塗佈處理之紙或薄膜等的輥。該等脫 模性之賦予手段無需特別限定,可使用先前公知之方法。作 為5亥等親之脫模性之程度,較佳為依據JIS Z〇237_2009中規 定之方法,對於Nichiban股份有限公司製造之透明膠帶之 剝離強度為5 N/mm以下之材質。又,爐内之搬送輥17可 配合步驟片材之收縮而個別地控制其速度,由於效率良好地 去除加熱收縮故而較佳。 關於加熱器16及搬送輥17,設置於退火爐丨5之中儘可 能減少與外部氣體之接觸由於可使爐内之溫度穩定、使步驟 片材之熱處理穩定故而較佳。又,較佳之態樣之一為以使爐 内之溫度均勻地穩定化為目的而對爐内供給熱風。 101111289 12 201244915 較佳為,進而視需要於退火爐15之上游設置一對軋輥 14。藉由設置軋輥14可阻斷退火處理步驟對製膜步驟之影 響,故而較佳。具體而言,可防止加熱步驟片材時之收縮對 製膜步驟造成影響,或使步驟片材對退火步驟之供給穩定 化。 又,較佳為於退火爐15之出口與壓紋輥20之間設置片材 取出親18。片材取出幸昆18發揮自退火爐15中取出步驟片 材之作用。若無片材取出輥18,則有時於退火爐内之輥π 中最靠出口側之輥與壓紋加工輥20之間步驟片材被拉伸而 產生變形。又,於退火處理時,由於有時若於步驟片材之加 熱收縮中於步驟片材之寬度方向上有不岣則產生褶皺等,故 而為去除該槽皺,亦較佳為片材取出棍18為擴幅幸昆(弓形彎 曲輥)。又’片材取出輥18較佳為與爐内之搬送輥π相同, 賦予有脫模性。 又,關於片材取出輥18,若其表面溫度過低,則有時供 給於壓紋輥之步驟片材冷卻而壓紋形狀之轉印性降低。相反 地,若表面溫度過高,則有時步驟片材黏著於片材取出輥 18而步驟片材之搬送變得困難。因此,片材取出輥18之表 面溫度較佳為進行溫度調整至20〜80¾之範圍。進而較佳 為設為與退火爐出口之步驟片材之溫度相等或其以下之表 面溫度。若片材取出輥18之表面溫度高於自退火燐出來之 步驟片材之表面溫度,則有時步驟片材黏著於輥。 101111289 13 201244915 為防止步驟片材之溫度降低’較佳為退火爐15與壓紋輕 20之距離儘可能較短。因此,片材取出輥18亦可設置複數 根,但較佳為更少,較佳為至多設為3根以下,更佳為1 或2根。 於連續進行退火處理步驟及後續之步驟(〇時,較佳為對 退火爐15出來之步驟片材之表面溫度、及於步驟⑷中導入 壓紋輥中之步驟材之表面溫度進行控制。因此,為正確把 握步驟片材之表面溫度,而測定退火爐15之出口部分、及 即將進行壓紋加I前之步驟片材之表面溫度,因此較佳為設 置非接觸式紅外線溫度言十33。進而較佳為於退火爐15中設 置複數之非接觸式溫度計來測定步驟片材之表面溫度。 於退火處理步驟中,將步驟片材之至少一個表面之最高溫 度加熱至成為構成該表面部分之樹脂組成物之熔點以上的 溫度。於後續之步驟⑷中’對該經加熱之側之表面實施壓 、文加工此處所明「構成表面部分之樹脂組成物」,於步 驟片材為單層片材之情形時係指構成該步驟片材之樹脂組 成物於步驟片材為積層有複數之層之積層片材之情形時係 =構成經加熱之側之表面之層的樹脂組成物。即便實施最高 溫度只能為未滿樹脂組成物之熔點之溫度的退火處理 ,減少 加熱收縮率之效果亦不充分,必需進行長期之處理。又,表 t Γ7 /皿度較佳為(構成加熱之側之表面部分之樹脂組成 物的熔點+5。〇〜Γ椹士 α V再战加熱之側之表面部分之樹脂組成物 101111289 201244915 的熔點+35t)之溫度範圍内。若退火處理中之溫度過高,則 ν / 著於搬送輕’或平面性降低’由於該等肩因,有 :Κ麦角之步驟(c)中產生稽敏。例如,於為以炼點為71°c • 之A树月曰所構成之步驟片材之情形時,退火處理步驟中 :之表面之最高達到溫度較佳為76〜1G6°C之範圍。 純步驟片材之時間,即使步驟片材滯留於退火爐内之時 門為2 55 U里之範圍内。該加熱時間係對於經抛光棍u 冷卻之步驟片材而使步驟片材之表面溫度達到炼點溫度以 上斤品要之時間、與於達到炫點溫度以上後進行用以減少加 ,、、、收縮之退火處理之時間的合計。若加熱時間未滿η秒 知則加熱收縮之去除不充分。即便加熱時間超過^秒鐘 進行加熱’亦由於效絲和而只是徒勞地延長退火之長度。 加熱時間^下限較佳為22秒鐘以上,更佳為Μ秒鐘以上。 八要可充刀地去除加熱收縮,則加熱時間之上限以較短為 宜’較佳為45秒、鐘以下,更佳為4〇秒鐘以下。 [步驟(c).壓紋加工步驟] 繼而針對步驟(e)進行說明。步驟(e)係對藉由於退火步驟 中之加熱而成為高溫狀態之步驟片材實施壓紋加工而於步 驟片材表面上形成壓紋形狀的步驟。於步驟(c)中,設置有 用以於步驟片材上形成壓紋形狀之壓紋輥2〇、祕對向輥 19、及冷卻輕21。以下,將該步驟(c)稱為壓紋加工步驟。 於堅、、文親20之表面上,對應欲於步驟片材上升多成之壓紋 101111289 15 201244915 形狀而實施將該壓紋形狀反轉之雕刻。形成於步驟片材上之 壓紋形狀係不規則形狀或幾何紋樣等,視需要決定即可。但 是,若壓紋形狀之形成不充分,則有可能於步驟片材之搬送 時或捲成I昆狀時易於產生黏連,或於製成太陽電池模組時空 氣難以排放而導致於模組内產生氣泡。實施於壓紋輥之表面 上之雕刻的紋樣可採用半球形,或三角錐、四角錐、六角錐、 圓錐等錐形,或使該等之頂部扁平之梯形。又,亦可為該等 形狀混合之紋樣。於該等中,較佳為半球形及/或四角錐形。 此處,所謂「半球形及四角錐狀」,意指半球形與四角錐形 混合之紋樣之雕刻。就於將密封片材向太陽電池單元按壓時 不易施加集中負荷且可均勻地分散負荷方面而言,較佳為半 球形。又,就不易產生密封片材之反射光之不均、表面品質 優異方面而言,較佳為四角錐形。並且,為表現該半球形與 四角錐形兩者之特徵’亦較佳為使半球形與四角錐形混合之 紋樣。於使半球形與四角錐形混合之情形時,各自之比例依 據更追求哪—者之特徵而任意決定即可。特佳為全部為半球 雕亥丨過冰之情形時,於壓紋加工時需較 大之壓製壓力,設備變撂士拥 亏乂品罕父 u 大I。因此,壓紋輥之雕刻之深度 雖亦依據步驟片材之屋痒 早度而疋,但較佳為65〜350 μπι之範 圍内。再者,所謂壓紋輥 μ ^ 心至疆峨之表面(未^ 1之^表不自壓紋親之中 (未實施雕刻之部分)之距離、與自麗紋輥 101111289 201244915 之中。至雕刻之凹部(凹陷部分)之最深部分之距離的差。該 雕刻之深度係藉由依據JIS B〇6〇l(2001)並利用表面粗縫度 測疋機所測定之最大高度Pz(㈣而表示。 車乂佳為’於壓紋親之表面上進而實施有深度為1〜20 μηι 处藉由以貫知有此種微小之凹處之壓紋輕i%行壓紋加 工,而於片材之表面上形成微小之突起。其結果為,片材之 滑動性提昇而變得易於操作,另外,藉由微小之突起而光發 生散射使片材之白色性提昇,因此畴異料之檢查較為容 易。此種微小之凹處可藉由於對壓紋絲岭_刻之後實 =知之喷射處理等而容㈣形成。微小之㈣之深度可藉 由噴射加X時之粒子尺寸或壓力條件而進行調整。 :於與壓_對向之對_19,為提昇壓紋棍表面 有=ΓΓΓ之轉印性,較佳為使·金屬輥上捲附 有·者。·_之_,存切橡勝、腈_ =膠等,並無特別限定,但較佳為依據心咖福 之類型Α硬度為65〜85。之範圍之橡膠。低於65。或超過 85。,均有時壓紋形狀之轉印性降低。於該等橡膠之中,由 於與在高溫下易於黏著之步驟片材之脫模 為石夕橡膠。 難故而最佳 於壓紋加1步驟中,將供給至壓、味之步驟 理步驟情加熱之表㈣溫度設為(構錢表樹^ 物之熔點.賊)〜(構成該表面之樹脂組成 〇成 101111289 17 201244915 之’皿度範圍内。若未滿(樹脂組成物mi代),則壓紋形 狀之轉印1±降低。若超過(樹脂組成物之熔點,則退 火乂驟中之步驟片材之溫度過高,於退火步驟中易於產生稍 敵等。例如’於表面側之層為以溶點A 71°C之EVA樹脂構 成之情形時’壓紋加卫時之表面溫度設為61〜9rc之範圍 内。 進而,壓紋輥20之擠壓壓力較佳為使對步驟片材施加之 線壓力為150〜500 N/cm之範圍。更佳為200〜 範圍。若線壓力未滿150 N/cm,則有時壓紋形狀之轉印性 降低。若欲附加超過5〇〇 N/cm之線壓力,.則產生使設備大 型化之需要,於該情形時對向橡膠輥之壽命降低。 於圖2中所示之先前之技術中,壓紋輥13ly之擠壓壓力高 至線壓力為1〇〇 N/cm左右即足夠。推測其原因如下:例如 於使用熔點為71 °C之EVA樹脂之情形時,自τ字模所擠出 之樹脂之溫度多數情形下為l〇〇〜12〇°c之範圍,由於為高 溫狀態故而於壓紋形狀之轉印中線壓力為1〇〇 N/cm左右即 足夠。另一方面,於本發明之製造方法中,於如上所述(樹 脂組成物之熔點_10。〇〜(樹脂組成物之熔點+2(rc)之溫度 範圍内進行壓紋加工。如此,若壓紋加工時之步驟片材之表 面溫度變低,則難以使壓紋形狀轉印,因此較佳為提高於壓 紋加工中必需之擠壓壓力。即,較佳為使線壓力為i 5 0 N/ c m 以上。再者,本發明中所謂之線壓力,係以輥之擠壓負重除 101111289 201244915 以粮之面長而得之值。 進而,如上所述於相對低溫下之壓紋加工中,為提昇壓紋 形狀之轉印性,較佳為使步驟片材環繞於壓紋輥20上。具 ; 體而言’對壓紋輥之包角較佳為30〜270。之範圍。若只賦 - 予較Ά之壓紋則包角度未滿30。亦可’但為賦予較深、且、青 晰之形狀之壓紋,較佳為將包角度設為30。以上。再者,包 角可簡便地根據步驟片材32與壓紋輥20相接之部分之圓弧 之長度、與壓紋輥之圓周的比率進行計算。例如,於包角為 90。之情形時,意指步驟片材與相當於壓紋輥之圓周之1/4 之長度的部分相接。 該壓紋加卫步驟中之壓紋輥2G之表面溫度較佳為(構成 轉印壓紋形&一側之表面部分之樹脂組成物之炫點_2〇°c ) 以下。若壓紋輥之溫度較低,則步驟片材之脫模性良好,步 驟片材不易纏繞於親上。其結果為,自壓紋㈣步驟片材制 離時之負載減輕,可獲得品質更佳之太陽電池密封片材。’ I 使步·材自敎輥脫模之後,冷卻親21冷卻步驟 :#材、使步驟>}材之表面溫度迅速降低至室溫附近。’ ;V方式製膜、藉由退火處理去除加熱收縮、邢# 紋形狀之步驟月奸v ^战壓 月材32進行缺點檢查或將步驟片材 答為所i:宮麻乂&寸調 ’’’、 a之後’利用纏繞機等纏繞為輥狀或剪裁為 長度之切割片材,用於太陽電池模組之製造中。.、、、的 [太陽電池密封片材] 101111289 201244915 繼而,針對太陽電池密封片材進行說明。密封片材較佳為 於表面上具有高度為6G〜3⑻μιη之獨立之突起。藉由於密 封片材之表面上具有獨立之高度為6G帅以上之突起,於製 造太陽,池模組時之真空層合時,可將殘留於密封片材與太 陽電池早7L之間之空氣自多個方向有效地去除,從而抑制氣 泡之產生。進而,可使密封片材對太陽電池單元之按壓壓力 分散:抑制單元破裂之產生。若密封片材表面之形狀並非獨 立之突起而為連續之凹槽形狀,則於直入凹槽内之方向上之 脫氣不充分’殘留之空氣形成氣泡。又,若突起之高度為 300 μιη以下,則可抑制真空層合時負重集中於突起之頂 部’從而防止太陽電池單元破裂。此處,所謂「獨立之突起」, 係於著眼於突起之底面時下述底邊之長度D為%〜綱〇 μπι之範圍之突起。 又’關於獨立之突起,較佳為於以平板夾住密封片材並於 厚度方向上賦予5G kPa之勤進行壓縮使突起變形,而突 起之頂部與平板相接之區域擴大時,來自⑽鄰接之突起之 2個ε域間確保2〇〜8〇〇 μχη之間隙。 獨立之突起較佳為突起之高度⑺與突起之底邊長度(d) 〇l更佳為015〜〇 8〇。若t/d比未滿 〇.〇5,則有時密封片材之緩衝性不充分。若⑽比超過〇鄭 則有時發生負重集中於突起之卿而產生單元破裂。突起之 南度τ仙如下方式而敎。首先,對在單面上有突起之 101111289 20 201244915 情形進行說明。將密封片材有突 大起一側之面設為A面,將 無大起一側之面設為B面。如jgj ) a 圖3中所示般,將自A面之Font or circular mold, etc. The flat mold I is used as the mold 12, and the width of the T can be used to form a wide shape. Therefore, the sheet to be extruded is a T-shaped mold on the extruder, and is collectively referred to as a T-shaped mold. In addition, in the T _ and T pre-modes, it is easy to produce a thickness unevenness due to the retention of time or flow rate in the width direction of the mold. The thickness in the width direction is not uniform when the sheet is heated. For solving the problem of 丄, 、, and upper 4, it is preferable to use a cylindrical shape: a circular mold. The circular mold is used to form the tree (four) into a cylindrical shape and to form a sheet-like round-shaped can-like mold by cutting it, and the physical properties of the sheet width tend to become relatively uniform. Moreover, in the case of using a T-shaped mold, κ can extrude different resin compositions by an extruder with a silver number, and can also be stepped by a feed-in module or a multi-mode extrusion method. The material is made into a layered structure, and it is squeezed. « . „ By making such a laminated structure, it is possible to reduce the cost by adding each layer as a sealing sheet, and to reduce the cost. The step sheet __n13b, 13c extruded by the mold 12 is formed into a sheet shape. The polishing roll is used for the inclusion of a pair of smelting resin to sandwich the thickness and surface properties of the sheet material. A sheet conveying device. The device is constructed. Each of the sticks has a mechanism for adjusting the temperature of the molten resin to be cooled or shaped, and the mechanism for adjusting the gap between the rolls and the pressing pressure. Preferably, it is preferable to prevent the adhesion of the step sheet by the inflow of cooling water such as cooling 101111289 201244915 water, etc. It is preferable to adjust the temperature of the cooling water to 0 to 3 (the range of rc. The composition of the resin used is different and sometimes the resin of high temperature is easy The polishing roller 13a on the most upstream side of the polishing roller is preferably wound with a rubber or the like on the surface to improve the mold release property, and further enhances the conveyability, and is preferably located on the most upstream side. The counter roller 13b of the buffing roller 13a is a metal roll having a pear-like surface shape. Preferably, the surface roughness of the pear-like surface is jisb〇6〇1_1994, and the 10-point average roughness rz of the pinch is 2 ~ 左右 左右 左右 左右 左右 左右 左右 左右 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在The thickness of the rubber is preferably from 3 to 10 mm, more preferably from 4 to 8 mm. If the thickness of the rubber is less than 3 mm, the transfer of the skin of the pear skin is sometimes not applied to the sheet of the step. The free roller of the step sheet is conveyed. If the thickness of the stone rubber exceeds 1 Gmm, the resin is adhered to the roller due to the heat accumulated from the sloping heat. [Step (b): Annealing step] + Then Step (8) 绮 Description. The purpose of step (8) is to remove the shape formed in the film forming step The residual strain of the sheet material is reduced, and the heat shrinkage of the step sheet is reduced. In the step (b), the step sheet is heated by the heater 16 provided in the annealing furnace, and the step sheet is passed through the plurality. The method of feeding the roller 17 or the like. Hereinafter, the step (b) is referred to as an annealing step. The heater 16 for heating the sheet of the step is not particularly limited as long as it is a step of heating the sheet > 01111289 201244915, and ceramic heat can be used. Half of the known, such as a half, 6%, Yi, stainless steel heaters, jackets can be added to the thickness of the sheet; force, film ^ use the hot air or steam to use the media;: and better... The method of contact, etc. These heating methods can be used in combination with n and heated rolls. The method of 'can also be used to transfer the sheet of the conveying roller 17 of the step sheet. Therefore, it is preferred to apply the metal in the step of mold release heating by embossing or spraying: or a compound such as metal oxide. The gold is provided with a bump: 乂, a fluororesin coated with a polytetrafluoroethylene, a full i propylene propylene copolymer, a perfluoroalkoxy oxyhydrocarbon, or the like may be used, or may be used for the metal. A roll of a release coated paper or film or the like is attached to the surface. The means for imparting such mold release property is not particularly limited, and a conventionally known method can be used. The degree of release property of the 5 HAI and the like is preferably a material having a peeling strength of 5 N/mm or less for the scotch tape manufactured by Nichiban Co., Ltd. according to the method specified in JIS Z〇237_2009. Further, the conveying roller 17 in the furnace can be individually controlled in accordance with the shrinkage of the step sheet, and it is preferable to remove the heat shrinkage efficiently. It is preferable that the heater 16 and the conveying roller 17 are disposed in the annealing furnace 5 as much as possible to reduce the contact with the outside air, because the temperature in the furnace can be stabilized and the heat treatment of the step sheet is stabilized. Further, one of the preferred aspects is to supply hot air to the furnace for the purpose of uniformly stabilizing the temperature in the furnace. 101111289 12 201244915 Preferably, a pair of rolls 14 are provided upstream of the annealing furnace 15 as needed. It is preferable to set the roll 14 to block the influence of the annealing treatment step on the film forming step. Specifically, it is possible to prevent the shrinkage at the time of heating the sheet from affecting the film forming step or to stabilize the supply of the step sheet to the annealing step. Further, it is preferable to provide a sheet take-out 18 between the exit of the annealing furnace 15 and the embossing roll 20. The sheet is taken out and the Kun Kun 18 functions as a step of taking out the step sheet from the annealing furnace 15. If the sheet take-up roll 18 is not provided, the sheet may be stretched and deformed between the roll on the exit side and the embossing roll 20 in the roll π in the annealing furnace. Further, in the annealing treatment, wrinkles or the like may occur in the width direction of the step sheet during the heat shrinkage of the step sheet, and therefore, it is preferable to remove the wrinkles. 18 is the expansion of the lucky Kun (bow bending roller). Further, the sheet take-up roll 18 is preferably the same as the transfer roll π in the furnace, and is provided with mold release property. Further, when the surface temperature of the sheet take-up roll 18 is too low, the sheet to be supplied to the embossing roll may be cooled, and the transfer property of the embossed shape may be lowered. On the other hand, if the surface temperature is too high, the step sheet may be adhered to the sheet take-up roll 18 and the conveyance of the step sheet may become difficult. Therefore, the surface temperature of the sheet take-up roll 18 is preferably adjusted to a temperature of 20 to 803⁄4. Further, it is preferably set to a surface temperature equal to or lower than the temperature of the step sheet of the annealing furnace outlet. If the surface temperature of the sheet take-up roll 18 is higher than the surface temperature of the step sheet from the annealing, the step sheet sometimes adheres to the roll. 101111289 13 201244915 To prevent the temperature of the step sheet from decreasing, it is preferable that the distance between the annealing furnace 15 and the embossing light 20 is as short as possible. Therefore, the sheet take-up roll 18 may be provided with a plurality of roots, but is preferably less, preferably at most 3 or less, more preferably 1 or 2. In the continuous annealing step and the subsequent step (when the crucible is used, it is preferable to control the surface temperature of the step sheet from which the annealing furnace 15 comes out, and the surface temperature of the step material introduced into the embossing roll in the step (4). In order to accurately grasp the surface temperature of the step sheet, the exit portion of the annealing furnace 15 and the surface temperature of the sheet immediately before the embossing plus I are measured. Therefore, it is preferable to provide a non-contact infrared temperature. Further preferably, a plurality of non-contact thermometers are provided in the annealing furnace 15 to measure the surface temperature of the step sheet. In the annealing step, the highest temperature of at least one surface of the step sheet is heated to become the surface portion. The temperature above the melting point of the resin composition. In the subsequent step (4), the surface of the heated side is subjected to pressure, and the "resin composition constituting the surface portion" as described herein is processed, and the sheet is a single layer in the step. In the case of a material, it means that the resin composition constituting the sheet of the step is heated in the case where the step sheet is a laminated sheet having a plurality of layers laminated. The resin composition of the layer on the side of the surface. Even if the annealing treatment is carried out at a temperature at which the maximum temperature is only the melting point of the resin composition, the effect of reducing the heat shrinkage rate is insufficient, and it is necessary to carry out long-term treatment. The Γ7 / dish degree is preferably (the melting point of the resin composition constituting the surface portion on the side of the heating + 5 + 〇 ~ Γ椹 α α V and the resin portion of the surface portion of the heating side 101111289 201244915 melting point + 35t) Within the temperature range, if the temperature in the annealing treatment is too high, then ν / in the transfer lighter 'or flatness' is due to the shoulder cause, and there is a sensitivity in the step (c) of the buckwheat horn. For example, In the case of a step sheet composed of a refining point of 71 °c • A-tree, the highest surface temperature in the annealing step is preferably in the range of 76 to 1 G 6 ° C. At the time, even if the step sheet stays in the annealing furnace, the door is in the range of 2 55 U. The heating time is for the step sheet cooled by the polishing rod u, so that the surface temperature of the step sheet reaches the refining point temperature. The time required for the above pounds, After the glaze temperature is reached, the total time for annealing, shrinkage, and shrinkage is reduced. If the heating time is less than η seconds, the heat shrinkage is not sufficiently removed. Even if the heating time exceeds ^ seconds, the heating is performed. Also because of the effect of the wire and only in vain to extend the length of the annealing. The heating time ^ lower limit is preferably 22 seconds or more, more preferably more than Μ seconds. Eight to fill the knife to remove the heat shrinkage, the upper limit of the heating time The shorter one is preferably '45 seconds, less than the clock, more preferably less than 4 seconds. [Step (c). Embossing processing step] Next, step (e) will be explained. Step (e) is a loan a step of forming an embossed shape on the surface of the step sheet by performing embossing on the step sheet which becomes a high temperature state by heating in the annealing step. In the step (c), it is provided to form an embossing on the step sheet. The shape of the embossing roller 2, the secret counter roller 19, and the cooling light 21. Hereinafter, this step (c) is referred to as an embossing step. On the surface of Yu Jian and Wen Qin 20, the engraving of the embossed shape is reversed in accordance with the shape of the embossing 101111289 15 201244915 which is desired to rise in the step sheet. The embossed shape formed on the step sheet is an irregular shape or a geometric pattern, and may be determined as needed. However, if the formation of the embossed shape is insufficient, there is a possibility that adhesion may occur easily during the conveyance of the step sheet or when it is rolled into a shape, or the air may be difficult to be discharged when the solar cell module is formed. Air bubbles are generated inside. The engraved pattern applied to the surface of the embossing roll may be a hemispherical shape, or a triangular pyramid, a quadrangular pyramid, a hexagonal cone, a cone or the like, or a trapezoidal shape which flattens the top. Further, it may be a pattern in which the shapes are mixed. Among these, it is preferably a hemispherical shape and/or a quadrangular pyramid shape. Here, the term "hemispherical and quadrangular pyramidal" means engraving of a pattern in which a hemisphere and a quadrangular pyramid are mixed. The semi-spherical shape is preferable in that it is difficult to apply a concentrated load when the sealing sheet is pressed against the solar cell unit and the load can be uniformly dispersed. Further, in terms of the unevenness of the reflected light of the sealing sheet and the excellent surface quality, it is preferably a quadrangular pyramid. Further, in order to express the characteristics of both the hemispherical shape and the quadrangular pyramid shape, it is preferable to mix the hemispherical shape and the quadrangular pyramid shape. In the case where the hemispherical shape and the tetragonal pyramid are mixed, the respective ratios may be arbitrarily determined depending on which characteristics are sought. It is especially good for all hemispheres. When the ice is overlaid, the pressing pressure is required for the embossing process, and the equipment becomes a gentleman. Therefore, the depth of engraving of the embossing roll is also determined by the early itching of the sheet, but it is preferably in the range of 65 to 350 μm. Furthermore, the so-called embossing roller μ ^ heart to the surface of the 峨 ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( ( The difference in the distance between the deepest part of the concave portion (the concave portion) of the engraving. The depth of the engraving is determined by the maximum height Pz ((4) measured according to JIS B〇6〇l (2001) and using the surface rough seam measuring machine.乂 乂 为 为 为 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于 于As a result, minute protrusions are formed on the surface of the material. As a result, the slidability of the sheet is improved and it becomes easy to handle, and the light is scattered by the minute protrusions to increase the whiteness of the sheet, so the inspection of the domain dissimilar material is performed. It is relatively easy. Such a small recess can be formed by the embossing of the embossed silk ridge, etc., and the depth of the micro (4) can be determined by the particle size or pressure condition when the X is added by spraying. Make adjustments: _19 against pressure _ opposite, to enhance the surface of the embossed stick There is a transfer property of ΓΓΓ, and it is preferable that the metal roll is attached to the roll. The ___, the cut rubber, the nitrile _ = glue, etc., is not particularly limited, but is preferably based on the heart Fu type is a rubber with a hardness of 65 to 85. It is less than 65 or more than 85. The transferability of the embossed shape is reduced. Among these rubbers, it is easy to adhere to it at high temperatures. The step of releasing the sheet is Shi Xi rubber. It is difficult to use the step of adding the pressure to the tempering step, and the temperature is set to (the temperature) is set to (the temperature of the tree) Melting point. Thief) ~ (The composition of the resin constituting the surface is 10111111289 17 201244915 within the range of the degree of the dish. If it is not full (resin composition mi generation), the transfer of the embossed shape is reduced by 1 ± if exceeded (resin The melting point of the composition is such that the temperature of the sheet in the annealing step is too high, and it is easy to generate a slight enemy in the annealing step. For example, the layer on the surface side is composed of EVA resin having a melting point of A 71 ° C. When the surface temperature of the embossing is set to be in the range of 61 to 9 rc. Further, the pressing pressure of the embossing roller 20 Preferably, the line pressure applied to the step sheet is in the range of 150 to 500 N/cm, more preferably in the range of 200 to 1. If the line pressure is less than 150 N/cm, the transfer property of the embossed shape may be lowered. If a line pressure exceeding 5 〇〇 N/cm is to be added, there is a need to increase the size of the apparatus, in which case the life of the facing rubber roller is lowered. In the prior art shown in Fig. 2, embossing It is sufficient that the pressing pressure of the roller 13ly is as high as about 1 〇〇N/cm. The reason is presumed to be as follows: for example, in the case of using an EVA resin having a melting point of 71 ° C, the resin extruded from the τ-shaped mold The temperature is in the range of l〇〇~12〇°c in many cases, and it is sufficient that the transfer line center pressure is about 1 N/cm in the embossed shape due to the high temperature state. On the other hand, in the production method of the present invention, embossing is carried out as described above (the melting point of the resin composition is _10. 〇~ (the melting point of the resin composition + 2 (rc)). When the surface temperature of the step sheet in the embossing process is lowered, it is difficult to transfer the embossed shape. Therefore, it is preferable to increase the pressing pressure necessary for the embossing process. That is, it is preferable to make the line pressure i 5 . 0 N/cm or more. Further, the line pressure in the present invention is a value obtained by dividing the negative load of the roll by 101111289 201244915 by the length of the grain. Further, the embossing at a relatively low temperature as described above. In order to improve the transferability of the embossed shape, it is preferred that the step sheet is wrapped around the embossing roll 20. The body wrap angle of the embossing roll is preferably in the range of 30 to 270. If only the embossing is applied to the embossing, the angle of the package is less than 30. It is also possible to provide a deeper and clearer shape, preferably by setting the angle of the package to 30 or more. The wrap angle can be simply according to the length of the arc of the portion where the step sheet 32 is in contact with the embossing roll 20, and the embossing roll The ratio of the circumference is calculated. For example, in the case where the wrap angle is 90, it means that the step sheet is in contact with a portion corresponding to a length of 1/4 of the circumference of the embossing roll. The surface temperature of the embossing roll 2G is preferably (below the swell point _2 〇 °c of the resin composition constituting the surface portion of the transfer embossing & one side). If the temperature of the embossing roll is low, the step The release property of the sheet is good, and the step sheet is less likely to be entangled on the pros. The result is that the load on the embossing (four) step sheet is reduced, and a solar cell sealing sheet having better quality can be obtained. · After the material is released from the roll, the cooling pro 21 cooling step: #材,使步骤>} the surface temperature of the material is rapidly lowered to near room temperature. 'V-film formation, annealing treatment to remove heat shrinkage, Xing #纹形的步步月 v ^战压月材32 to perform a defect check or to answer the step sheet as i: 宫麻乂& inch''', a after 'winding with a winding machine, etc. Cut into length cut sheets for use in the manufacture of solar cell modules. Battery sealing sheet] 101111289 201244915 Next, a description will be given of a solar cell sealing sheet. The sealing sheet is preferably a protrusion having a height of 6 G to 3 (8) μm on the surface, since the surface of the sealing sheet has an independent height. For the protrusion of 6G handsome, when the vacuum is laminated in the solar module and the pool module, the air remaining between the sealing sheet and the solar battery 7L can be effectively removed from multiple directions, thereby suppressing the generation of bubbles. Further, the pressing pressure of the sealing sheet against the solar cell unit can be dispersed: the occurrence of cracking of the unit can be suppressed. If the shape of the surface of the sealing sheet is not a separate protrusion and is a continuous groove shape, the direction is straight into the groove. The degassing on the surface is insufficient. The residual air forms bubbles. Further, when the height of the projections is 300 μm or less, it is possible to suppress the load from being concentrated on the top portion of the projections during vacuum lamination, thereby preventing the solar cell from being broken. Here, the "independent protrusion" is a protrusion in which the length D of the following bottom side is in the range of % to 〇 μπι when focusing on the bottom surface of the protrusion. Further, regarding the independent protrusion, it is preferable to compress the protrusion by sandwiching the sealing sheet with a flat plate and imparting 5 G kPa in the thickness direction, and the protrusion is extended from the (10) abutment when the top portion of the protrusion is extended to the flat plate. The gap between 2 〇 and 8 〇〇 μχ is ensured between the two ε domains of the protrusion. The independent protrusion is preferably such that the height of the protrusion (7) and the length of the base of the protrusion (d) 〇l are preferably 015 to 〇 8 。. If the t/d ratio is less than 〇.〇5, the cushioning properties of the sealing sheet may be insufficient. If the ratio of (10) exceeds that of Zheng Zheng, there is a case where the load is concentrated on the protrusion and the unit is broken. The south of the protrusion is the following way. First, the case of 101111289 20 201244915 having a protrusion on one side will be described. The surface on which the sealing sheet has the protruding side is referred to as the A surface, and the surface on the side where the sealing sheet is not raised is referred to as the B surface. As jgj) a as shown in Figure 3, will be from the A side

突起之頂點至B面之距離設為T imax’將自A面之無突起之 部分至B面之距離設為Tmini τ_與之差為突起 之向度T。繼而,對在兩面上有突起之情形進行說明。將密 封片材之一面設為A面,將另一而< 从 乃 面设為B面。如圖4中所 示般,將自A面之突走&之頂赴E ^ 犬趣之概至B面之無突起之部分的距 離設為TAmax,將自b面之窣 之大起之頂點至A面之無突起之 部分的距離設為TBmax,將白A r X财自A面之無突起之部分至B面 之無突起之部分的距離設為Tmin。該τα_與Tmin之差 為A面之突起之高度TA ’ TBmax與Tmin之差為B面之突 起之高度TB。所謂突起之底邊之長度,係圖5中所示之突 起之外周直徑D。再者’於突起之底面之形狀為三角形或六 角形等多角形、_形之情形時,突起之底邊之長度為包含 底面之形狀之最小正圓的直徑。關於上述之Tmax、Tmin、 D可藉由利用立體顯微鏡之片材之觀察而測定。 理想之突起之高度T係如上所述為6〇〜300 μιη。於突起 之高度Τ為60 μηι之情形時,突起之底邊D之長度較佳為 75〜1200 μιη,更佳為75〜400 μιη。於突起之高度T為3〇〇 μιη之情形時,突起之底邊〇之長度較佳為375〜6000 μιη, 更佳為375〜2000 μηι。 獨立之突起之個數較佳為片材單側之面積每1 cm2為40 101111289 21 201244915 〜I00個°更佳為4G〜11⑻個。若獨立之突起未滿40個 則有夺產生單元破裂或氣泡。若超過23GG個/cm2, 則有時上述之T/D比增大,由於負重集中於突起頂部而產 生單元破裂。 密封片材較佳為於阶之溫水中放置丨分剌片材行進 方向之加熱收縮率為3〇%以下。更佳為Μ%以下。此處, ^胃「放置於溫水中」,於密封片材之比重較小而密封片材 丁浮於/皿7jC之表面上之情形時,係、指不自上方按壓密封片材 使其沉入溫水中而以該漂浮著之狀態放置。另—方面,於密 子片材之比重^大而密封片材沉人溫水之中之情形時係指 不自下方支樓密封片材而以該沉人之狀態放置。又,所謂「片 材行進方向」’係指於密封丨材之製造步驟巾步驟#材行進 之方向。於太陽電池模組之製造中之通常之真空層合步驟 中’於到密封片材充分溶融為止期間,不對片材加壓而以無 負重狀態進行抽空’進行密封片材之熔融及脫氣。此時,由 於密封>;材於80°C左右之高溫下暴露於無負重狀態下,故 而產生也封片材之收縮,結果產生單元之破裂或位置偏差。 本發明者等人著眼於單元之破裂或位置偏差而進行研究,結 果發現.若於再現於真空層壓機内之無負重狀態下將步驟片 材放置1刀知時片材行進方向之加熱收縮率為π%以下,則 可進而抑制單元之破裂。所謂再現於該真空層壓機内之狀 態’係將步驟片材放置於8G。之溫水_之狀態。再者,與片 101111289 22 201244915 !之正交之方向的加熱收縮率與行進方向相比微 並無特別限定,但較佳為5%以下。 獨立之突起之形狀較佳為半球形,或三角錐 一 角錐、圓錐等錐形,或使該等之頂部為匕 =rtr,。於謝,二= 池二:突起混合之表面形狀。就於對太陽電 勻地分散負重方面而言,較佳為半球形。又,就不重易= :光之不均、表面品質優異方面而言,亦較佳為四角錐形。 车^為表現該等半球形及四角錐形兩者之特徵,亦較 =四Γ形混合之形狀。於使半球形與四角錐形混合 主自之比例依據更追求哪-者之特徵而任意決定 特佳為全部為半球形之紋樣。 且本t月之密封片材較佳為於具有獨立之突起之面上進而 八有冋度為i〜15 μιη之突起。藉由具有此種微小之突起, 片,之π動性提昇而易於操作。又,藉由微小之突起而光發 生散射使片材之白色性提昇,因此附著異物等之檢查較為容 总。 此種微小> * + •^大起可藉由繼退火步驟之後實施壓故加工之 m 達成。於在實施壓紋加卫後實施利用加 熱之退火處理的先前方法中,有時高度為數10 μηι以上之較 101111289 23 201244915 大突起於加熱處理後亦殘存於片材中,但高度為數阿左右 之微小突起隨著熱處理而消失。 再者’微小之突起之高度細如下方式所測定之數值。依 據JISB〇6〇1(2〇〇1)並使用周知之雷射顯微鏡,❹ KEYENCE股份有限公司製造之雷射顯微鏡VK_X100等, 以働倍率拍攝片材表面。於所獲得之影像之粗糖度 將截斷值為議mm時之^值設為微小之突起之高 度。 於本申請案中,作為對用以抑制太陽電池之單元破裂之密 封片材之緩衝性進行評價的指標,採用將密封片材且有 ^面於厚度方向壓縮刚哗時片材的回彈應力。針對太陽 電η元破裂性舆密封片材 研九’結果發現單元之破裂受到 kpa以下。再者,上述之回彈 _力較佳為70 使用具有壓縮位移方面為5师以如下方式而獲得: 秒万面為5 μιη以下、壓縮負荷方面為The distance from the apex of the protrusion to the B surface is set to T imax', and the distance from the portion having no protrusion of the A surface to the surface B is Tmini τ_ and the difference is the directionality T of the protrusion. Next, a case where there are protrusions on both sides will be described. One side of the sealing sheet is set to the A side, and the other side is set to the B side. As shown in Fig. 4, the distance from the top of the A side to the top of the E ^ dog's interest to the non-protruding part of the B side is set to TAmax, which will be from the height of the b side. The distance from the vertex to the portion of the A surface where no protrusion is formed is TBmax, and the distance from the portion where there is no protrusion of the A surface to the portion where the protrusion is not formed on the B surface is Tmin. The difference between the τα_ and Tmin is the height TA of the protrusion A of the A surface, and the difference between Tmin and Tmin is the height TB of the B surface. The length of the bottom edge of the projection is the outer peripheral diameter D as shown in Fig. 5. Further, when the shape of the bottom surface of the protrusion is a polygonal shape such as a triangle or a hexagon, or a _ shape, the length of the bottom side of the protrusion is the diameter of the smallest perfect circle including the shape of the bottom surface. The above-mentioned Tmax, Tmin, and D can be measured by observation of a sheet using a stereoscopic microscope. The height T of the ideal protrusion is 6 〇 to 300 μηη as described above. When the height 突起 of the protrusion is 60 μηι, the length of the bottom edge D of the protrusion is preferably 75 to 1200 μηη, more preferably 75 to 400 μηη. When the height T of the protrusion is 3 〇〇 μιη, the length of the bottom edge of the protrusion is preferably 375 to 6000 μηη, more preferably 375 to 2000 μηι. The number of independent protrusions is preferably that the area of one side of the sheet is 40 101111289 per 1 cm 2 21 201244915 ~ I00 pieces and more preferably 4G to 11 (8) pieces. If there are less than 40 independent protrusions, there is a break in the cell or bubbles. If it exceeds 23 GG/cm2, the above-mentioned T/D ratio may increase, and the unit may be broken due to the concentration of the load on the top of the projection. The sealing sheet is preferably placed in the warm water of the order, and the heat shrinkage rate in the direction in which the sheet is branched is 3% or less. More preferably Μ% or less. Here, ^the stomach is "placed in warm water", when the sealing sheet has a small specific gravity and the sealing sheet is floated on the surface of the dish 7jC, the system does not press the sealing sheet from above to sink it. It is placed in warm water and placed in this floating state. On the other hand, in the case where the proportion of the dense sub-sheet is large and the sealing sheet is in the warm water, it means that the sheet is not sealed from the lower branch and placed in the state of the sinking. Further, the "sheet traveling direction" means the direction in which the material of the sealing coffin is processed. In the usual vacuum lamination step in the manufacture of the solar cell module, the sheet is pressed and the material is not subjected to the load-bearing state during the period in which the sealing sheet is sufficiently melted, and the sealing sheet is melted and degassed. At this time, since the sealing material is exposed to a no-load state at a high temperature of about 80 ° C, shrinkage of the sheet is also caused, resulting in cracking or positional deviation of the unit. The inventors of the present invention conducted research by focusing on the rupture or positional deviation of the unit, and as a result, found that if the step sheet is placed in a no-load state in a vacuum laminator, the sheet is placed in a direction of heating. When the rate is π% or less, the cracking of the unit can be further suppressed. The state reproduced in the vacuum laminator is to place the step sheet at 8G. The state of warm water _. Further, the heat shrinkage ratio in the direction orthogonal to the sheet 101111289 22 201244915 ! is not particularly limited as compared with the traveling direction, but is preferably 5% or less. The shape of the individual protrusions is preferably hemispherical, or a pyramidal cone, a cone or the like, or the top of the elements is 匕 = rtr. Thanks, two = pool 2: the surface shape of the protrusions. It is preferably hemispherical in terms of uniformly distributing the weight of the sun. Further, in terms of unevenness of light and excellent surface quality, it is preferably a quadrangular pyramid. The car ^ is characterized by the characteristics of both the hemispherical and the quadrangular pyramid, and is also in the shape of a mixed shape of four quadrangles. In order to mix the hemispherical shape and the quadrangular pyramid, the ratio of the main self is determined arbitrarily according to the characteristics of which one is pursued. The best is a hemispherical pattern. And the sealing sheet of the present month is preferably a protrusion having an independent protrusion and further having a degree of twist of i 15 μm. It is easy to operate by having such minute protrusions and sheets, and the π dynamic property is improved. Further, since the light is scattered by the minute projections to improve the whiteness of the sheet, the inspection of adhering foreign matter or the like is uniform. Such a small > * + • ^ large can be achieved by performing the pressing process m after the annealing step. In the prior method in which the annealing treatment by heating is performed after the embossing is applied, the height is 10 μηη or more, and the large protrusions of 101111289 23 201244915 remain in the sheet after the heat treatment, but the height is about several angstroms. The minute protrusions disappear with heat treatment. Furthermore, the height of the tiny protrusions is as follows. The surface of the sheet was taken at a magnification of 雷 according to JISB〇6〇1 (2〇〇1) using a well-known laser microscope, a laser microscope VK_X100 manufactured by KEYENCE Co., Ltd., etc. The crude sugar content of the obtained image is set to a value of a small protrusion when the cutoff value is mm. In the present application, as an index for evaluating the cushioning property of the sealing sheet for suppressing cracking of the unit of the solar cell, the rebound stress of the sheet when the sealing sheet is pressed and the steel sheet is compressed in the thickness direction is used. . For the solar η element rupture 舆 sealing sheet, the results of the discovery of the unit rupture are below kpa. Furthermore, the above-mentioned rebound _ force is preferably 70. The use of the compression displacement is obtained by the following five divisions in the following manner: the second plane is 5 μιη or less, and the compression load is

Pa以下之分解度的壓縮試驗裝置,將扁平之加壓端子以 mm/s之加壓速度_糾材具有聽之面於厚度方向上力 壓1〇,日寺,測定此時片材之回彈應力㈣。若密封口 之回彈應料70 kPa以下,則可藉由以使具有突起之面與 太陽電池單it相接之方式積層並進行真空層合而抑制太陽 電池單it之破裂。再者,與㈣片材具有突起之面相反側之 面的形狀無特贿定,但就防止製造太陽電池模組時密封片 101111289 24 201244915 材之黏著等方“言,祕為具有 微小之突起。 ΙΟμιη左右之 密封片材之厚度較佳為5〇〜 _,特佳為·〜。於更佳為⑽〜誦 又若m 或於作業性之觀點上出現問題。 超過1500 _,則有時生產性之降低或密接性之降低 成為問題。再者,於僅於密封 4接11之降低 形時,密則狀厚衫自U 形財突起之情 ^之厚度為自4之頂點至與具有突起之面相 面的距離°於在㈣片材之兩面上形成有突起之情形 時’密封片狀厚度為自-面之突起之概絲反面之突起 之頂點的距離。 如上所述,對於在密封片材之表面上正確地形成獨立之突 起’或將密封片材之加熱收縮率抑制於特定之範圍内,較佳 為利用本發明之製造方法製造密封片材。 [構成太陽電池密封片材之原料] 繼而,針對構成密封片材之樹脂組成物進行說明。再者, 較佳為至少構成形成有突起—側之表面部分之樹脂組成物 滿足下文所㈣之樹脂組成物的組鱗。#然,更佳為構成 步驟片材之所有樹脂組成物滿足τ文所說明之樹脂組成物 的組成等。 構成密封片材之樹脂組成物較佳為含有聚烯烴系樹脂。作 為聚烯烴系樹脂,可舉出··均聚聚丙烯、與以丙烯為主成分 101111289 25 201244915 之其他草體之共聚合體、乙烯-丙烯丁烯三元共聚合體等聚 丙烯系樹脂,低密度聚乙烯、超低密度聚乙烯、直鏈狀低密 度聚乙烯、中密度聚乙烯、高密度聚乙烯、與以乙烯為主成 分之其他單體之共聚合體等聚乙烯系樹脂,聚烯烴系熱塑性 彈性體等。作為與以乙烯為主成分之其他單體之共聚合體 可舉出:乙烯-α-烯烴共聚合體、乙烯_不飽和單體共铲八 體。作為α-烯烴,可舉出:α-烯烴為乙烯、丙烯、丨丁稀° 異丁烯、1-戊烯、2_曱基-1-丁烯、3-曱基_丨_丁烯、丨·已烯 ^庚烯、1-辛烯、1-壬烯、1-癸烯等。作為不飽和單體可 舉出:6酸乙烯酯、丙烯酸、曱基丙烯酸、丙烯酸曱酯、可 基丙烯酸甲酯、丙烯酸乙酯或乙烯醇等。又,較佳 ^ 心態樣之 -為視需要於該等輯烴㈣脂中❹魏化合物、竣 環氧丙基化合物等而使少量共聚合或進行改質。 久5 於該等聚_系樹脂中,就作為太陽電池密封材而U 重要之透明性、或與太陽電池單元之接著性等觀點而:,奢 佳為使㈣乙触殘和魏化合物對乙烯·乙酸乙歸㈣ 聚合體、乙H丙騎甲g旨共聚合體、低密度聚乙^ 行改質以。於使用乙烯·乙酸乙稀§旨共聚合 ^ 酸甲_聚切之情科,絲合成分之丙树 40質量%之範圍。 住馬15〜 又, 物。關 101111289 26 201244915 解而產生自由基者,則可使用任意者,考慮製造太陽電池密. 封片材時之溫度、製成太陽電池模組時之加熱貼合溫度、及 交聯劑本身之貯存穩定性等而選擇即可。特佳為半生期為 ίο小時之分解溫度為7(rc以上者。作為此種有機過氧化物 之例’可舉出’ l1-二(過氧化第三己基)環己烧、正丁基4,4-二-(過氧化第三丁基)戊酸醋、2,5_二甲基_2,5_二(過氧化第三 丁基)己燒、—·第二丁基過氧化物、二·第三己基過氧化物、 2,5-二甲基-2,5_二(過氧化第三丁基)己炔_3、二玻_過氧 化物—(4_第二丁基環己基)過氧化二碳酸醋、四曱 基丁基過氧化·2-乙基己酸醋、第三己基過氧化_2•乙基己酸 ::::丁基過氧化_2_乙基己動旨、第三己基過氧化異丙 基㈣㈣、二㈣三丁基環己基)過氧化二碳酸酷 丁基過氧化-3,5,5-三甲基己酸醋、第 乐二 酽、笛一 丁… 第二丁基過氧化月桂酸 酉曰红丁基過氧化-2-乙基己基單碳酸醋、第三丁 化-2·乙基己酸酯、第三丁基過氧化異 ^ ° 氧化乙酸目旨、第:孩缝似4、 紅丁基過 μ A b異錢_、第三絲過氧化_2· 土己酸S旨、第三戊基過氧化正辛 ="三戊基一基己基上A compression test device with a degree of decomposition below Pa, which presses the flat pressure terminal at a pressurization speed of mm/s. The correction material has a hearing surface pressed in the thickness direction by 1 〇, and the temple is measured. Elastic stress (four). If the rebound of the sealing port is 70 kPa or less, the solar cell can be prevented from being broken by laminating and laminating the surface having the projections in contact with the solar cell. Furthermore, the shape of the surface opposite to the side of the (4) sheet having the protrusion surface is not limited, but the sealing sheet 101111289 24 201244915 is prevented from being adhered when the solar cell module is manufactured. The thickness of the sealing sheet around ΙΟμιη is preferably 5〇~ _, especially preferably ~. It is more preferably (10)~诵 and if m or problems arise from the viewpoint of workability. More than 1500 _, sometimes The decrease in productivity or the decrease in the adhesion is a problem. Moreover, in the case of the lowering of the seal 4, the thickness of the dense thick shirt from the U-shaped prominence is from the apex of the 4 to the The distance from the face of the protrusion is the distance from the apex of the protrusion on the opposite side of the ruler of the self-face protrusion when the protrusion is formed on both sides of the (four) sheet. As described above, for the seal It is preferable to form the sealing sheet by the manufacturing method of the present invention by forming the independent protrusions ' on the surface of the sheet correctly or suppressing the heat shrinkage ratio of the sealing sheet within a specific range. [Constructing the solar cell sealing sheet Raw material] The resin composition constituting the sealing sheet is described. Further, it is preferable that at least the resin composition constituting the surface portion on which the protrusion-side is formed satisfies the grouping of the resin composition of the following (4). The resin composition constituting the step sheet satisfies the composition of the resin composition described in the above-mentioned article. The resin composition constituting the sealing sheet preferably contains a polyolefin resin. Examples of the polyolefin resin include Homopolymeric polypropylene, copolymer with other grasses containing propylene as main component 101111289 25 201244915, polypropylene resin such as ethylene-propylene butene ternary copolymer, low density polyethylene, ultra low density polyethylene, linear Polyethylene-based resin such as a low-density polyethylene, a medium-density polyethylene, a high-density polyethylene, and a copolymer of another monomer containing ethylene as a main component, a polyolefin-based thermoplastic elastomer, etc. Examples of the copolymer of the other monomer include an ethylene-α-olefin copolymer and an ethylene-unsaturated monomer. The α-olefin is an α-olefin. Alkene, propylene, butyl ketone isobutylene, 1-pentene, 2-hydrazino-1-butene, 3-mercapto-indene-butene, fluorene-hexene, heptene, 1-octene, 1- Terpene, 1-decene, etc. Examples of the unsaturated monomer include vinyl acetate, acrylic acid, methacrylic acid, decyl acrylate, methyl methacrylate, ethyl acrylate or vinyl alcohol. Good ^ mentality - in order to make a small amount of copolymerization or modification in the hydrocarbon (tetra) lipids, such as oxime compounds, oxime epoxy propyl compounds, etc. As a solar cell sealing material, U is important for transparency, or adhesion to solar cells, etc.: Luxury is to make (4) B-resistance and Wei compound to ethylene-acetic acid (4) polymer, B-H- riding Agglomerates, low-density polyethylene, and modified. In the case of using ethylene-acetic acid, the copolymerization of the acid A-poly-cutting, the silk synthesis is in the range of 40% by mass of the C. Live horse 15 ~ again, things. Guan 101111289 26 201244915 Anyone who generates free radicals can use any one of them, considering the manufacture of solar cell dense. The temperature at the time of sealing the sheet, the heating and bonding temperature when making the solar cell module, and the storage of the crosslinking agent itself. Select the stability and so on. It is particularly preferable that the decomposition temperature of the half-life is ίο hours is 7 (rc or more. As an example of such an organic peroxide, 'l1-two (peroxide third hexyl) cyclohexane, n-butyl 4 , 4-di-(t-butylperoxy peroxide) valeric acid vinegar, 2,5-dimethyl-2,5-di(t-butylperoxide) hexane,-·second butyl peroxide , bis-thyl hexyl peroxide, 2,5-dimethyl-2,5-di(t-butylperoxy)hexyne _3, bis- _ peroxide - (4_ second butyl Cyclohexyl)peroxydicarbonate, tetradecylbutyl peroxide, 2-ethylhexanoic acid vinegar, third hexyl peroxide, -2-ethylhexanoic acid::::butyl peroxy-2_ethyl Auxiliary, third hexyl peroxy isopropyl (tetra) (tetra), di(tetra)cyclobutylcyclohexyl) peroxydicarbonate, butyl peroxy-3,5,5-trimethylhexanoic acid vinegar, Flute-butyl... Dibutyl peroxy laurate ruthenium butyl peroxy-2-ethylhexyl monocarbonate, third butane-2-ethylhexanoate, tert-butyl peroxide ° Oxidized acetic acid purpose, the first: the child is like 4, red butyl over μ A b _, the third wire peroxide _2 · S purpose, the third n-octyl-amylperoxy = " on a three-pentyl hexyl

氧化一 Γ_'τ基)環己烧、乙基3,3-二(過 氧化第二丁基)丁酸醋、α二(過氧化 W 該等有機過氧化物亦可組合2種以上使用。該;:烷等。 物之含量相對於聚烯烴系樹脂:1、過氧化 101111289 負量份較佳為01〜5 s 27 201244915 里知更佳為0.1〜3質量份’特佳為〇 2〜2質量份。若有 機過氧化物之含量未滿(M質量份,财時無法使聚稀烴系 樹脂交聯。即便含有超過5質量份,該含有效果亦較低,並 且存在未分解之有機過氧化物殘存於密封片材中而成為經 年劣化之原因的可能性。 構成密封片材之樹脂組成物亦可進而含有交聯助劑、石夕燒 系偶合劑、光穩定劑、紫外線吸收劑、抗氧化劑等。 交聯助劑為於分子内具有複數個不飽和鍵之多官能性單 體’用於與由有機過氧化物之分解所產生之活性自由基化合 物進行反應,而使聚烯烴系樹脂均勻地且效率較佳地交聯。 作為該等交聯助劑之例,可舉出:異氰尿酸三烯丙酯、氰尿 酸三烯丙酯、三羥曱基丙烷三(甲基)丙烯酸酯、季戊四醇三 (甲基)丙烯酸酯、三[(曱基)丙烯醯氧基乙基]異氰尿酸酯、 一經曱基丙烧四(甲基)丙婦酸醋、季戊四醇四(曱基)丙婦酸 酯、季戊四醇乙氧基四(曱基)丙烯酸酯、二季戊四醇五(甲基) 丙烯酸酯、二季戊四醇六(甲基)丙烯酸酯、二乙烯基苯等。 該等交聯助劑可分別單獨使用,亦可併用2種以上。再者, 於本發明中,「(甲基)丙烯酸酯」意指「丙烯酸酯或甲基丙 稀酸S旨」。 於該等交聯助劑之中,特佳為異氰尿醆三烯丙醋、三0甲 基丙烧三(曱基)丙稀酸酯。添加該等交聯助劑之情形時之含 量相對於聚烯烴系樹脂10〇質量份較佳為〇〜5質量份。更 101111289 28 201244915 佳為0.1〜3質量份’特佳為0.3〜3質量份。即便含有超過 5質量份,效果之提昇亦微小’且成為成本上升之要因。 矽烷系偶合劑較佳為用以提昇太陽電池密封片材與太陽 電池單元、底層片材、玻璃等各種構件之接著性。添加矽烷 系偶合劑之情形時之含量相對於聚烯烴系樹脂1〇〇質量 份,較佳為〇.〇5〜2質量份之範圍。若未滿〇 〇5質量份則含 有效果較小。即便含有超過2質量份接著性之提昇效果亦較 小。作為矽烷系偶合劑並無特別限定,例如可舉出:具有選 自曱基丙烯醯氧基、丙烯醯氧基、環氧基、疏基、腺基、異 級醋基、胺基、經基中之至少i種官能基之烧氧基石夕烧化 δ物作為其具體例’可舉& : 基丙烯酿氧基丙基甲基 二曱氧基魏、γ_曱基丙騎氧基丙基三f氧基魏、了_甲 基丙烯酿氧基丙基甲基二乙氧基魏、γ_甲基丙烯醢氧基丙 基三曱氧基雜等含有甲基丙雜氧基之絲基魏化合 物’γ-丙烯醯氧基丙基三曱氧基魏等含有㈣醯氧基之烧 氧基石夕烧化合物,γ_環氧丙氧基丙基三甲氧基㈣、γ_環氧 丙氧基丙基二乙氧基錢、ρ_(3,4_環氧基環己基)乙基三甲 祕石夕烧等含有環氧基之絲基戟化合物,㈣ 丙基三甲 氧基#、γ·威丙基三乙氧基魏等含㈣基之錄基石夕炫 物γ脲基丙基二乙氧基石夕炫、脈基丙基三甲氣基石夕 烧等含有脲基之科基錢化合物,γ•異減縣丙基三乙 氧土夕炫γ_異氰酸能基丙基三f氧基魏、γ·異氰酸醋基 Ι011Ι1289 29 201244915 丙基f基二甲氧基㈣等含有異氰酸酯基之絲基石夕炫化 合物,γ_(2_胺基乙基)胺基丙基P基二f氧基矽烷、γ·(2_胺 基乙基)胺基丙基三f氧基矽烷、广胺基丙基三^氧基矽烷 等含有私基之燒氧基石夕烷化合物,广羥丙基三,氧基矽烷、 γ-羥丙基二乙氧基矽烷等含有羥基之烷氧基矽烷化合物 等。其中,就與聚烯烴系樹脂之相溶性之觀點而言,較佳為 含有曱基丙_氧基找氧基魏化合物,進而較佳為丫_ 曱基丙烯醯氧基丙基三曱氧基矽烷。 構成密封片材之樹脂組成物較佳為進而含有紫外線吸收 劑。紫外線吸收劑係吸收照射光中有害之紫外線並於分子内 轉換為無害之熱能,從而防止高分子中之光劣化起始之活性 種被激發者。作為紫外線吸收劑,可使用已知者。例如,可 使用二苯基酮系、苯并三唾系、三、水揚酸系、氛基丙 烯酸醋系等。可❹該等之1種,亦可將2種以上組合而使 用0 作為二苯基酮系紫外線吸收劑,例如可舉出:2,2 ,·二經基 Μ··二(經甲基)二苯基嗣、2上二經基从二㈣乙基): 本基_、2’2’-二經基_3,3’_二甲氧基·5,5Ι_二(經曱基)二笨基 酮、2,2’·二經基·3 3'- **甲备a产 土 土 3,3 一甲氧基_5,5丨_二(2_羥乙基)二苯基蜩、 2,2’_二經基_3,3·_二(經曱基)你二曱氧基二苯基鋼、n -祕-3,3,·二(2·經乙基)_5,5••二甲氧基二苯基酮、π二經 基一曱氧基二苯基酮等。 101111289 201244915 作為本并二a坐糸紫外線吸收劑,例如可舉出:2_[2,_經基 -5’-(羥甲基)苯基]·2Η_苯并三唑、2_[2,_羥基_5、2•羥乙基)苯 基]2Η-本并二η坐、2_[2’-經基·5'-(3-經丙基)苯基]_2η_苯并三 唑、2-[2,-羥基_3|·甲基_5,_(羥甲基)苯基]_2扎苯并三唑、2_[2,· 羥基-3·-甲基·5·_(2_羥乙基)苯基]_2Η_苯并三唑、2[2·_羥基 -3L曱基-5,-(3-羥丙基)苯基]-2Η-苯并三唑、2—[2, ·羥基·3,·第 三丁基_5’-(羥甲基)苯基]_2Η_苯并三唑、2_[2,_羥基_3,_第三丁 基-5 -(2-經乙基)本基]_2Η-苯并三β坐、2-[2’-經基_3,_第三辛基 -5’-(羥甲基)苯基;|_2H-苯并三唑、2-[2,-羥基·3,_第三辛基 -5’-(2-羥乙基)苯基]_2Η-苯并三唑、2_[2,_羥基_3•-第三辛基 -5-(3-技丙基)本基]-2Η-苯弁三β坐等,或者2 2'·亞曱基雙 [6-(2Η-苯并三唑-2-基)-4-(羥甲基)苯酚]、2,2,_亞曱基雙 [6-(2H-笨并三唑_2_基)冬(2_羥乙基)苯酚]、亞甲基雙 [6-(2H-苯并三唑-2-基)-4-(3-羥丙基)苯酚]、2,2,_亞甲基雙 [6-(2H-苯并三唑-2-基)-4-(4-羥基丁基)苯酚]、3,3_{22,·雙 [6-(2H-苯并三唑-2-基)-1 -羥基_4_(2_羥乙基)苯基]丨丙烷、 2,2-{2,2’-雙[6-阳-苯并三嗤-2-基)-1_經基|(2_經乙基)苯 基]}丁烧、2,2-氧基雙[6-(2H-苯并三唾_2_基)_4_(2·經乙基) 苯紛]、2,2,-雙[6-(肌苯并三唾_2_基)_4_(2_紅基)苯紛]胺 等。 作為二畊系紫外線吸收劑,例如可舉出:2_(2_羥基羥 曱基苯基)-4,6-二苯基-均三啩、2_(2_羥基斗羥曱基笨 101111289 31 201244915 基M,6-雙(2,4-二曱基苯基)_均三♦、印·經基_4♦經乙基) 苯基]-4,6-一苯基-均二畊、2必經基_4_(2經乙基)苯基]♦ 雙(2,4-二甲基苯基均三啡、2_[2·經基邻_經基乙氧基)苯 基]-4,6-二苯基-均三畊、2·[2_羥基_4_(2·羥基乙氧基)苯 基Η,6-雙(2,4-二甲基苯基)_均三β井、2_[2_經基·4_(3_經基丙 氧基)苯基Η,6-二苯基-均三β丼、2_[2_經基_4(3_經基丙氧基) 苯基]-4,6-雙(2,4-二甲基苯基)_均三讲、2 [2_經基_4·⑷經基 丁基)苯基]-4,6-二苯基_均三啡、2_[2_經基冬(4羥基丁基) 苯基Η,6-雙(2,4-二甲基苯基)_均三畊、2_[2_經基冰⑷經基 丁氧基)苯基]-4,6_二苯基-均三畊、2_[2_經基邻_經基丁氧 基)苯基Η,6·雙(2,4_二曱基苯基)_均三啡、2_(2經基4經甲 基苯基)-4,6-雙(2-經基-4-甲基苯基)_均三σ井、2_[2_經基_4·(2· 羥乙基)苯基Η,6·雙(2_羥基I甲基苯基)_均三畊、2_[2•經基 4-(2-羥基乙氧基)笨基]_4,6_雙(2_羥基-‘曱基苯基)·均三 啡、2-[2-羥基_4-(3·羥丙基)苯基]_4,6_雙(2_羥基_4_曱基苯 基)-均三啡、2-[2-羥基-4-(3-羥基丙氧基)苯基]_4,6_雙(2_羥基 •4-曱基苯基)_均三〇井等。 作為水揚酸系紫外線吸收劑,可舉出:水揚酸苯酯、水揚 酸對第三丁基苯酯、水楊酸對辛基苯酯等。 作為氰基丙稀酸酯系紫外線吸收劑,可舉出:2_乙基己基 2-氰基-3,3’-二苯基丙烯酸酯、乙基_2_氰基·3,3,·二苯基丙烯 酸酯等。 101111289 32 201244915 添於°亥等紫外線吸收劑中,就紫外線吸收效果及紫外線吸收 劑本身之著色之觀點而言,最佳為二苯基鲷系之紫外線吸收 劑。 : 於添加上述紫外線吸收劑之情形時,相對於聚烯烴系樹脂 * 1〇0 f量份較佳為0.〇5〜3質量份。更佳為0.05〜2.〇質量 伤若含I未滿0.05質量份則含有效果較低,若超過3質 量份則有著色傾向。 構成密封片材之樹脂組成物較佳為進而含有光穩定劑。光 穩定劑係捕制聚合物有害之自由隸且不產生新自由基 者。作為光穩定劑,較佳地使用受阻胺系光穩定劑。 作為^:阻胺系光穩定劑,可舉出:癸二酸雙(2,2,6,6_四甲 基-1(辛氧基)-4-哌啶基)酯、包含匕卜二曱基乙基氫過氧化物 與辛烷之反應生成物70質量%及聚丙烯3〇質量%者、雙 (U,2,6,6-五曱基L定基;^3,5.雙.二甲基乙基)4經 基苯基]曱基]丁基丙二酸酯、雙(1,2,2,6,6_五曱基_4_哌啶基) ; 癸二酸酯與甲基-1,2,2,6,6-五曱基_4_哌啶基癸二酸酯混合 • 物、雙(2,2,6,6-四曱基-4-哌啶基)癸二酸酯、四(2,2,6,6-四曱 基-4-哌啶基)-1,2,3,4-丁烷四羧酸酯、四^2,2,6,6-五曱基-4- 口底咬基)-1,2,3,4-丁烷四羧酸酯、2,2,6,6_四曱基冰哌啶基 -1,2,3,4-丁烷四羧酸酯與十三烷基丁烷四羧酸酯之 /«j合物、1,2,2,6,6-五甲基_4_σ底咬基_i,2,3,4-丁烧四缓酸酯與 十三院基-1,2,3,4-丁烷四羧酸酯之混合物、聚[^(丨丄^四 101111289 33 201244915 曱基丁基)胺基-1,3,5-三讲-2,4-二基}{(2,2,6,6-四甲基·4_哌 咬基)亞胺基}六亞曱基{(2,2,6,6-四曱基-4-哌啶基)亞胺 基}]、琥珀酸二曱酯與4-羥基-2,2,6,6-四曱基小哌咬乙醇之 聚合物、Ν,Ν,,Ν”,Ν,,,-四-(4,6-雙-(丁基-(Ν-曱基-2,2,6,6-四曱 基旅咬冰基)胺基)-三畊-2·基)-4,7-二氮雜癸烷_ι,10_二胺與 上述號拍酸二曱錯及4-經基-2,2,6,6-四甲基-Ι-d底咬乙醇之 聚合物之混合物、二丁基胺_1,3,5-三畊·Ν,Ν,-雙(2,2,6,6-四甲 基-4-哌啶基-1,6-六亞曱基二胺與]SK2,2,6,6_四甲基_4_哌啶 基)丁基胺之縮聚物等。上述受阻胺系光穩定劑可單獨使用 1種,亦可將2種以上混合而使用。 於s玄#之中’作為受阻胺系光穩定劑,較佳為使用:雙 (1,2,2,6,6-五曱基-4-0底咬基)癸二酸醋與甲基_1,2,2,6,6_五甲 基-4-哌啶基癸二酸酯之混合物、以及甲基_4_哌啶基癸二酸 西曰、雙(2,2,6,6-四甲基-4-旅咬基)癸二酸自旨。又,受阻胺系 光穩定劑較佳為使用熔點為6〇。(:以上者。 添加受阻胺系光穩定劑之情形時之含量相對於聚烯烴系 樹脂100質量份,較佳為0 05〜3 〇質量份。更佳為〇 〇5〜 1.0質量份。於含量未滿〇.05質量份時,穩定化效果不充分, 即便含有超過3.0質量份,亦成為著色或成本上升之要因。 另外,作為已知之添加劑,亦可於不妨礙本發明之效果之 範圍内視需要而含有抗氧化劑、難燃劑、難燃助劑、可塑劑、 潤滑劑、著色劑等。 101111289 34 201244915 [太陽電池模組] 太陽電池模組係由受光面保護材、背面保護材、及配置於 °玄又光面保護材與背面保護材之間且利用密封片材而密封 太陽電池單元之層所構成。作為此處所使用之密封片材,可 使用利用本發明之製造方法所獲得之密封片材,亦可使用上 述於表面上具有獨立之突起之密封片材。 於利用本發明之製造方法所獲得之密封片材中,使上述構 成之材料積層一體化時之加熱收縮較小。因此,太陽電池單 元與密封片材之間、受光面保護材與密封片材之間、背面保 護材與密封片材之間於成形時之殘留應力較小,形成歷經長 期之耐久性優異之太陽電池模組。 又,上述於表面上具有獨立之突起之密封片材由於可使於 使上述構成之材料積層一體化時對太陽電池單元之按壓力 分散,故而可使太陽電池單元與密封片材之間之殘留應力較 小。又,亦無雄、封材中之氣泡之殘存。因此,形成歷經長期 之耐久性優異之太陽電池模組。 [實施例] 將本實施例中所使用之測定法示於下文。只要並無特別說 明’則測定η數均設為5,並採用平均值。 (1)片材之厚度 將成形之密封片材於寬度方向上測定任意2〇處之厚度, 求出平均尽度。測疋器係使用Mitutoyo公司製造之厚产規 101111289 35 201244915 (547-301型)。關於密封片材之厚度,於僅於密封片材之單 面上形成有突起之情形時,測定自突起之頂點至與具有突起 之面相反侧之面的距離。於在密封片材之兩面上形成有突起 之情形時,測定自一面之突起之頂點至相反面之突起之頂點 的距離。 (2)突起高度 於與製造時片材之移動方向(以下簡稱為MD方向)成直角 之方向(寬度方向)上,以通過突起之頂部之方式切割密封片 材。利用立體顯微鏡跨及片材之整個寬度而觀察經切割之密 封片材之厚度方向剖面。 於密封片材之單面上有突起之情形時,將密封片材有突起 一側之面設為A面,無突起一側之面設為B面。如圖3中 所示般,將自A面之突起之頂點至B面之距離設為Tmax, 自A面之無突起之部分至B面之距離設為Tmin。然後,利 用式⑴計算突起之高度T。 • Τ(μιη)= Tmax-Tmin· * -(i) 於密封片材之兩面上有突起之情形時,將密封片材之一面 設為A面,另一面設為B面。如圖4中所示般,將自A面 之突起之頂點至B面之無突起之部分的距離設為TAmax, 自B面之突起之頂點至A面之無突起之部分的距離設為 TBmax,自A面之無突起之部分至B面之無突起之部分的 距離設為Tmin。然後,利用式(ii)計算A面之突起之高度 101111289 36 201244915 ΤΑ,利用式(iii)計算B面之突起之高度TB。 • TA(pm)=TAmax-Tmin...⑴) • TB(pm) = TBmax_Tmin. ·.(出)。 (3) 壓紋輥之紋樣深度 依據JIS B0601(2001)’於基準長度為2〇 mm、負重為〇 75 mN、測疋速度為〇·3 mm/s之測定條件下測定壓紋輥之表 面。測定係使用Mitutoyo公司製造之小塑表面粗糙度測定 器SJ401,並使用圓錐為60。、前端曲率半徑為2 μιη之金剛 石觸針進行測定》以該測定值作為壓紋輥之紋樣深度ρζ值 (μιη)。 (4) 壓紋轉印率 以上述(2)中所測定之突起高度τ(μιη)(或者,宍起高度 ΤΑ(μιη)或突起高度τΒ(μιη))除以上述(3)中所測定之壓紋輥 之紋樣深度ρζ的值作為壓紋轉印率。 •壓紋轉印率(%) = Τ/Ρζχ100。 (5) 加熱收縮率 自也、封片材切下一邊為120 mm之平面正方形之試驗片。 於該試驗片上,於製造時之TD方向中央部,空出100 mm 之間隔劃兩條平行之TE)方向之直線(5 cm)。然後,於將各 直線6等分之位置(分別為5處)標出記號。 繼而’將試驗片於加熱至80。(:之溫水中放置60秒鐘。於 密封片材之比重較小而密封片材漂浮於溫水之表面的情形 101111289 37 201244915 時,以該漂浮著之狀態放置。於密封片材之比熏較大而密封 片材沉入溫水之中之情形時,以該沉入之狀態放置。經過 60秒鐘後,自溫水中取出試驗片,使其於2〇ΐ之常溫水中 浸潰冷卻10秒鐘後,去除片材表面之水分。 利用游標卡尺,測定自劃於試驗片上之一條直線上所標出 之5處各個記號至另一條直線上所標出之對向之各個記號 的間隔A(mm) ’並基於下述式算出加熱收縮率,求出5處 之平均值。 •加熱收縮率(%)=(100-Α)/100χ100。 (6) 構成密封片材之樹脂組成物之熔融流動速率 依據JISK7210(1999)「塑膠-熱塑性塑膠之熔融質量流率 (MFR ’ Melt mass-flow rate)及熔融體積流,meh volume-flow rate)之試驗方法」,於溫度為19〇。(:、負荷為2.16 kg之試驗條件下對樹脂組成物進行測定。 (7) 突起之底邊長度(D) 利用立體顯微鏡觀察片材具有突起之面,測定底邊長度 (D)。於突起之底面之形狀為三角形或六角形等多角形、或 橢圓形之情形時,測定包含上述形狀之最小正圓之直徑。 (8) 單元破裂性 自密封片材切下2片一邊為180 mm之平面正方形之試驗 片。於多晶太陽電池單元(3條型匯流排' 尺寸為i56mm見 方、厚度為200 μπι)上焊接連接體(厚度為280 、寬度為 101111289 38 201244915 2 mm)’製成附有連接體之太陽電池單元。準備玻璃板(尺寸 為180 mm見方、厚度為3mm)及聚酯製太陽電池底層片材 (尺寸為180mm見方、厚度為24〇μιη)。於玻璃板上依序積 層密封片材、太陽電池單it、密封片材、底層>1材。此時, 以密封片材具有突起之面與太陽電池單元相接之方式進行 積層。將該積層體於溫度145。(:、抽空30秒鐘、壓製1分 鐘、壓力S持10分鐘之條件下進行真空層合,製作太陽電 池模組。利用太陽電池£L(Electroluminescence,電致發光) 影像檢測裝置對崎得之太陽電域組_發絲像,並測 疋單元破裂u卩之總龜裂之長度(mm)。將該試驗重複 3次而 求出總龜裂長度之平均值。 (9) 氣泡個數 藉由目視數出上述(8)中所製作之太陽電池模組中之氣泡 個數。求出3次試驗之平均值。 (10) 回彈應力 自密封片材切下一邊為120 mm之平面正方形之試驗片。 繼而,使用Kato Tech公司製造之壓縮試驗機KES FB_3, 藉由直徑16 111111之扁平加壓端子以速度2〇叫/肌自試驗片 具有突起之面對密封片材加壓,測定於厚度方向上加壓1〇〇 μιη時之片材之回彈應力(kpa)。將該試驗重複3次而求出回 彈應力之平均值。 (實施例1) 101111289 39 201244915 依照圖1中所示之制 方法製成太陽電池密封片材 步驟(a):製膜步_Oxidized mono- _' τ base) cyclohexene, ethyl 3,3-di(t-butyl peroxide) butyric acid vinegar, α 2 (peroxide W) These organic peroxides may be used in combination of two or more kinds. The content of the substance is relative to the polyolefin resin: 1. The peroxidation amount is 101111289. The negative amount is preferably 01 to 5 s. 27 201244915 The best known is 0.1 to 3 parts by mass. 2 parts by mass. If the content of the organic peroxide is not sufficient (M parts by mass, the polyolefin resin may not be crosslinked at the time of the product. Even if it contains more than 5 parts by mass, the effect is low and there is an undecomposed organic The peroxide remains in the sealing sheet and may cause deterioration over the years. The resin composition constituting the sealing sheet may further contain a crosslinking assistant, a sinter coupling agent, a light stabilizer, and an ultraviolet absorbing agent. Agent, antioxidant, etc. The crosslinking assistant is a polyfunctional monomer having a plurality of unsaturated bonds in the molecule for reacting with an active radical compound produced by decomposition of an organic peroxide to cause polymerization The olefin-based resin is uniformly and efficiently crosslinked. Examples of the crosslinking auxiliary agent include: triallyl isocyanurate, triallyl cyanurate, trishydroxypropyl propane tri(meth)acrylate, pentaerythritol tri(meth)acrylate, and three [ (fluorenyl) propylene oxiranyl ethyl] isocyanurate, thioglycolic acid tetrakis(methyl) propyl acetoacetate, pentaerythritol tetrakis(yl) propyl acrylate, pentaerythritol ethoxy tetra (曱) (A) acrylate, dipentaerythritol penta (meth) acrylate, dipentaerythritol hexa (meth) acrylate, divinyl benzene, etc. These crosslinking assistants may be used singly or in combination of two or more. In the present invention, "(meth) acrylate" means "acrylate or methacrylic acid S". Among these crosslinking assistants, particularly preferred is isocyanuric triene The vinegar and the trimethyl propyl ketone tris(mercapto) acrylate are preferably 〇 5 parts by mass based on 10 parts by mass of the polyolefin resin when the crosslinking assistant is added. 101111289 28 201244915 preferably 0.1 to 3 parts by mass 'extra good to 0.3 to 3 parts by mass. Even if it contains more than 5 parts by mass The improvement of the effect is also small and becomes a factor of cost increase. The decane coupling agent is preferably used to improve the adhesion of solar cell sealing sheets to various components such as solar cells, underlying sheets, and glass. Adding a decane coupling agent The content in the case of the polyolefin resin is preferably in the range of 5 to 2 parts by mass based on 1 part by mass of the polyolefin resin. If it is less than 5 parts by mass, the effect is small. Even if it contains more than 2 parts by mass. The effect of improving the adhesion is also small. The decane coupling agent is not particularly limited, and examples thereof include a fluorenyloxy group selected from a mercapto propylene group, an acryloxy group, an epoxy group, a sulfhydryl group, and an gland group. A specific example of the alkoxy sulphate, an amine group, and at least one of the functional groups in the group, as a specific example thereof, can be mentioned as follows: γ 曱 丙 丙 氧基 氧基 氧基 氧基 氧基 氧基 f f 了 了 了 _ 氧基 氧基 氧基 氧基 氧基 氧基 氧基 氧基 氧基 氧基 氧基 氧基 氧基 氧基 氧基 氧基 氧基 氧基 氧基 氧基 氧基 氧基 氧基a methyl-propionyl-containing silk-based Wei compound 'γ-acryloxypropyltrioxane Kewei et al. (A) anthracene-based alkoxylated compound, γ-glycidoxypropyltrimethoxy (tetra), γ-glycidoxypropyl diethoxy, ρ_(3,4 _Epoxycyclohexyl)ethyltrimethylpyrazine and other silk-based fluorene compounds containing epoxy groups, (iv) propyltrimethoxy#, γ·weipropyl triethoxy Wei, etc.夕炫物 γ-ureidopropyl diethoxy sulphur, ketone propyl trimethyl sulphate, etc., containing urea-based keel-based compounds, γ•iso-counter propyl triethoxy sulphate γ _ Cyanic acid propyl tri-foxy- Wei, γ-isocyanate Ι 011 Ι 1289 29 201244915 propyl f-dimethoxy (IV) and other isocyanate-containing silk-based compound, γ_(2-aminoethyl) Alkoxypropyl P-based bis-oxy decane, γ·(2-aminoethyl)aminopropyltri-f-oxydecane, broadly-aminopropyltrimethoxy decane, etc. a hydroxy alkane compound such as a hydroxy alkane compound, a polyhydroxypropyl group, a oxy decane or a γ-hydroxypropyl diethoxy decane. Among them, from the viewpoint of compatibility with the polyolefin resin, it is preferred to contain a mercaptopropoxy-oxyl-wei compound, and further preferably a mercaptopropenyloxypropyltrimethoxy group. Decane. The resin composition constituting the sealing sheet preferably further contains an ultraviolet absorber. The ultraviolet absorbing agent absorbs harmful ultraviolet rays in the illuminating light and converts them into harmless heat energy in the molecule, thereby preventing the active species of the light in the polymer from being excited. As the ultraviolet absorber, a known one can be used. For example, a diphenyl ketone type, a benzotrisal system, a tris, a salicylic acid type, an aryl acrylate vinegar type, etc. can be used. One type of these may be used, and two or more types may be used in combination, and 0 may be used as the diphenyl ketone-based ultraviolet absorber. For example, 2, 2, di-diyl ruthenium (m-methyl) may be mentioned. Diphenyl hydrazine, 2 upper di-based groups from di(tetra)ethyl): benzyl, 2'2'-di-diyl-3,3'-dimethoxy-5,5 Ι_bis (thiol) Phenyl ketone, 2,2'·dimensyl·3 3'- **A prepared a soil 3,3 monomethoxy _5,5 丨 _ bis (2 hydroxyethyl) diphenyl hydrazine , 2,2'_di-based _3,3·_ two (by fluorenyl) your di-oxydiphenyl steel, n-secret-3,3, · two (2·ethyl)_5, 5••Dimethoxydiphenyl ketone, π-dipyridyl-methoxy-diphenyl ketone, and the like. 101111289 201244915 As the ultraviolet absorber of the present invention, for example, 2_[2,_transyl-5'-(hydroxymethyl)phenyl]·2Η_benzotriazole, 2_[2,_ Hydroxy _5, 2 hydroxyethyl) phenyl] 2 Η - Benzene η sit, 2_[2'-radio- 5'-(3-propyl) phenyl]_2η_benzotriazole, 2 -[2,-hydroxy_3|·methyl_5,_(hydroxymethyl)phenyl]_2 benzotriazole, 2_[2,·hydroxy-3·-methyl·5·_(2_ Hydroxyethyl)phenyl]_2Η_benzotriazole, 2[2·_hydroxy-3Lindolyl-5,-(3-hydroxypropyl)phenyl]-2Η-benzotriazole, 2-[2 , hydroxy·3,·t-butyl-5'-(hydroxymethyl)phenyl]_2Η_benzotriazole, 2_[2,_hydroxy_3,_t-butyl-5-(2- Ethyl)benzyl]_2Η-benzotriazine, 2-[2'-carbyl-3,_t-octyl-5'-(hydroxymethyl)phenyl;|_2H-benzotriazole , 2-[2,-hydroxy·3,_t-octyl-5'-(2-hydroxyethyl)phenyl]_2Η-benzotriazole, 2_[2,_hydroxy_3•-third octane -5-(3-Technylpropyl)benzyl]-2Η-benzoquinone tris[beta] or the like, or 2 2'·indolyl bis[6-(2Η-benzotriazol-2-yl)-4- (hydroxymethyl) phenol], 2, 2, _ fluorenylene bis [6-(2H- stupid Triazol-2-yl) winter (2-hydroxyethyl)phenol], methylene bis[6-(2H-benzotriazol-2-yl)-4-(3-hydroxypropyl)phenol], 2,2,_methylenebis[6-(2H-benzotriazol-2-yl)-4-(4-hydroxybutyl)phenol], 3,3_{22,·double [6-(2H -benzotriazol-2-yl)-1 -hydroxy_4_(2-hydroxyethyl)phenyl]indole propane, 2,2-{2,2'-bis[6-cation-benzotriazine- 2-yl)-1_transcarbyl|(2_ethyl)phenyl]}butyring, 2,2-oxybis[6-(2H-benzotrisyl-2-yl)_4_(2· Ethyl) Benzene], 2,2,-bis[6-(musobenzotrisin-2-yl)_4_(2_erythryl)benzene]amine. Examples of the second-tillage ultraviolet absorber include: 2-(2-hydroxyindoleylphenyl)-4,6-diphenyl--tris-trimium, 2-(2-hydroxy hydroxy hydroxy phenyl) 101111289 31 201244915 M,6-bis(2,4-dimercaptophenyl)_all three ♦, imprinted by warthene _4♦ by ethyl) phenyl]-4,6-monophenyl-average tillage, 2 Must be based on _4_(2-ethyl)phenyl]♦ bis(2,4-dimethylphenyl-tris-morphine, 2_[2-trans-iso-p-ethylethoxy)phenyl]-4, 6-diphenyl-average three-plowing, 2·[2-hydroxy_4_(2·hydroxyethoxy)phenylhydrazine, 6-bis(2,4-dimethylphenyl)_-s-tri-β well, 2_[2_经基·4_(3_Pyrylpropoxy)phenylhydrazine, 6-diphenyl-s-tris-β丼, 2_[2_trans-based-4(3-pyridyloxy)benzene 4-[6,6-bis(2,4-dimethylphenyl)-distributed, 2 [2_carbyl-4-(4)-butylbutyl)phenyl]-4,6-diphenyl _Homotriene, 2_[2_ via acetyl (4-hydroxybutyl) phenyl hydrazine, 6-bis (2,4-dimethylphenyl) _ three tillage, 2_[2_ via base ice (4) Butyloxy)phenyl]-4,6-diphenyl-average three-pile, 2_[2_trans-iso-butyryloxy)phenylindole, 6·bis(2,4-diyl) Phenyl)--tri-ephthyl, 2-(2-based 4-methyl-phenyl)-4,6-bis(2-yl--4 -Methylphenyl)_all three sigma wells, 2_[2_transcarbyl_4·(2·hydroxyethyl)phenylhydrazine, 6·bis(2-hydroxylmethylphenyl)_three tillage, 2_[2•transyl 4-(2-hydroxyethoxy)phenyl]_4,6-bis(2-hydroxy-'mercaptophenyl)·-trientrine, 2-[2-hydroxy-4-( 3-hydroxypropyl)phenyl]_4,6-bis(2-hydroxy-4-indolylphenyl)-memenorphin, 2-[2-hydroxy-4-(3-hydroxypropoxy)phenyl ]_4,6_bis(2-hydroxy-4-indolylphenyl)_all three wells and the like. Examples of the salicylic acid-based ultraviolet absorber include phenyl salicylate, p-tert-butylphenyl salicylate, p-octylphenyl salicylate, and the like. Examples of the cyanoacrylate-based ultraviolet absorber include 2-ethylhexyl 2-cyano-3,3'-diphenylacrylate and ethyl-2-cyano-3,3, Diphenyl acrylate and the like. 101111289 32 201244915 It is preferably a diphenyl fluorene-based ultraviolet absorber from the viewpoint of the ultraviolet absorbing effect and the coloring of the ultraviolet absorbing agent itself. In the case where the above ultraviolet absorber is added, it is preferably from 0.5 to 3 parts by mass based on the amount of the polyolefin resin * 1 〇 0 f. More preferably, it is 0.05 to 2. 〇 mass. If the wound contains less than 0.05 parts by mass, the effect is low, and if it exceeds 3 parts by mass, the coloring tendency tends. The resin composition constituting the sealing sheet preferably further contains a light stabilizer. Light stabilizers are those that capture the harmful effects of the polymer and do not produce new free radicals. As the light stabilizer, a hindered amine light stabilizer is preferably used. Examples of the:-resistance-based light stabilizer include bis(2,2,6,6-tetramethyl-1(octyloxy)-4-piperidyl) sebacate, and The reaction product of mercaptoethyl hydroperoxide and octane is 70% by mass and the polypropylene is 3% by mass, and double (U, 2, 6, 6-pentamethyl L-based; ^3, 5. double. Dimethylethyl) 4 phenylphenyl] decyl] butyl malonate, bis(1,2,2,6,6-pentacylidene-4-piperidinyl); sebacate Methyl-1,2,2,6,6-pentamethyl-4_piperidinyl sebacate mixture • Bis(2,2,6,6-tetradecyl-4-piperidinyl) Sebacate, tetrakis(2,2,6,6-tetradecyl-4-piperidinyl)-1,2,3,4-butanetetracarboxylate, tetra^2,2,6,6 - 曱, ,, -4-, 4-butane, tetrabutyl phthalate, 1,2,6,6-tetradecyl-piperidinyl-1,2,3, 4-butane tetracarboxylate and tridecylbutane tetracarboxylate/«j, 1,2,2,6,6-pentamethyl_4_σ bottom bite _i,2,3 , a mixture of 4-butane sulphate and thirteen-yard-1,2,3,4-butane tetracarboxylate, poly[^(丨丄^四101111289 33 201244915 decylbutyl)amine -1,3,5-three-talk-2,4-diyl}{(2,2,6,6-tetramethyl-4-indanyl)imine }六亚曱基{(2,2,6,6-tetradecyl-4-piperidinyl)imido}], dinonyl succinate and 4-hydroxy-2,2,6,6-tetra Polymers, hydrazine, hydrazine, hydrazine, hydrazine, hydrazine, hydrazine, hydrazine, hydrazine, hydrazine, hydrazine, hydrazine, hydrazine, hydrazine, hydrazine, hydrazine, hydrazine, hydrazine, hydrazine, hydrazine, hydrazine, hydrazine, hydrazine, hydrazine曱基基旅基冰基)Amino)-三耕-2·yl)-4,7-diazadecane_ι,10-diamine with the above-mentioned acenaphthyl quinone and 4-carbyl- 2,2,6,6-tetramethyl-Ι-d bottom bite ethanol polymer mixture, dibutylamine_1,3,5-three tillage·Ν,Ν,-double (2,2,6 a polycondensate of 6-tetramethyl-4-piperidinyl-1,6-hexamethylenediamine and [SK2,2,6,6-tetramethyl-4-pyridinyl)butylamine The hindered amine-based light stabilizer may be used singly or in combination of two or more. In the case of s 玄#, as a hindered amine-based light stabilizer, it is preferably used: double (1, 2, a mixture of 2,6,6-pentamethyl-4-0 bottom bite) azelaic acid vinegar with methyl-1,2,2,6,6-pentamethyl-4-piperidinyl sebacate And methyl 4-(piperidinyl azelaic acid bismuth, bis(2,2,6,6-tetramethyl-4-Benbityl) azelaic acid. Further, hindered amine light stabilizer It is preferred to use a melting point of 6〇 (In the case where the hindered amine-based light stabilizer is added, the content is preferably 0. 05 to 3 parts by mass based on 100 parts by mass of the polyolefin-based resin. More preferably 〇 〜 5 to 1.0 parts by mass. When the content is less than 5.00 parts by mass, the stabilizing effect is insufficient, and even if it contains more than 3.0 parts by mass, it becomes a cause of coloring or cost increase. Further, as a known additive, an antioxidant, a flame retardant, a flame retardant auxiliary, a plasticizer, a lubricant, a colorant or the like may be contained as needed within a range not inhibiting the effects of the present invention. 101111289 34 201244915 [Solar battery module] The solar cell module is composed of a light-receiving surface protective material, a back protective material, and a solar cell unit that is disposed between the quartz and the surface protective material and the back protective material and sealed with a sealing sheet. The layer is composed. As the sealing sheet used herein, a sealing sheet obtained by the production method of the present invention can be used, and a sealing sheet having independent projections as described above can also be used. In the sealing sheet obtained by the production method of the present invention, the heat shrinkage when the above-mentioned constituent materials are laminated is small. Therefore, the residual stress between the solar cell unit and the sealing sheet, between the light-receiving surface protective material and the sealing sheet, and between the back surface protective material and the sealing sheet is small, forming a sun having excellent durability over a long period of time. Battery module. Further, since the sealing sheet having the independent projections on the surface thereof can disperse the pressing force of the solar battery cells when the materials of the above-described constituent layers are integrated, the residual between the solar battery cells and the sealing sheets can be caused. The stress is small. Moreover, there is no residual of the bubbles in the male and the sealing materials. Therefore, a solar cell module excellent in durability over a long period of time is formed. [Examples] The assays used in the examples are shown below. Unless otherwise specified, the number of measured η was set to 5, and the average value was used. (1) Thickness of sheet The thickness of the formed sealing sheet was measured at any two turns in the width direction to determine the average end. The measuring device is a thick product specification 101111289 35 201244915 (model 547-301) manufactured by Mitutoyo Corporation. Regarding the thickness of the sealing sheet, when a projection is formed only on one surface of the sealing sheet, the distance from the vertex of the projection to the surface opposite to the surface having the projection is measured. In the case where protrusions are formed on both surfaces of the sealing sheet, the distance from the apex of the protrusion of one surface to the apex of the protrusion of the opposite surface is measured. (2) Protrusion height The sealing sheet is cut by the top of the projection in a direction (width direction) at right angles to the moving direction of the sheet at the time of manufacture (hereinafter simply referred to as the MD direction). The thickness direction cross section of the cut sealing sheet was observed by a stereo microscope across the entire width of the sheet. When there is a projection on one surface of the sealing sheet, the surface on the side where the sealing sheet has the projection is the A surface, and the surface on the side where the projection is not formed is the B surface. As shown in Fig. 3, the distance from the vertex of the protrusion on the A surface to the surface B is Tmax, and the distance from the portion of the A surface where there is no protrusion to the surface B is Tmin. Then, the height T of the protrusion is calculated using the formula (1). • Τ (μιη) = Tmax-Tmin· * - (i) When there are protrusions on both sides of the sealing sheet, one side of the sealing sheet is set to the A side and the other side is the B side. As shown in FIG. 4, the distance from the vertex of the protrusion of the A surface to the portion of the B surface where no protrusion is formed is set to TAmax, and the distance from the vertex of the protrusion of the B surface to the portion of the A surface where no protrusion is formed is TBmax. The distance from the non-protrusion portion of the A surface to the non-protrusion portion of the B surface is set to Tmin. Then, the height of the protrusion of the A surface is calculated by the formula (ii) 101111289 36 201244915 ΤΑ, and the height TB of the protrusion of the B surface is calculated by the formula (iii). • TA(pm)=TAmax-Tmin...(1)) • TB(pm) = TBmax_Tmin. ·.(out). (3) The depth of the embossing roller is determined according to JIS B0601 (2001)'. The surface of the embossing roller is measured under the conditions of a reference length of 2 mm, a load of 〇75 mN, and a measuring speed of 〇·3 mm/s. . The measurement was carried out using a small plastic surface roughness measuring device SJ401 manufactured by Mitutoyo Co., Ltd., and a cone of 60 was used. The diamond stylus with a front end radius of curvature of 2 μη is measured. The measured value is used as the embossing depth ρ ζ (μιη) of the embossing roll. (4) The embossing transfer rate is determined by dividing the protrusion height τ (μιη) (or the height 宍 (μιη) or the protrusion height τ Β (μιη)) measured in the above (2) by the above-mentioned (3) The value of the pattern depth ρ 压 of the embossing roller is used as the embossing transfer rate. • Embossing transfer rate (%) = Τ / Ρζχ 100. (5) Heat shrinkage rate Test piece of a flat square of 120 mm on one side of the sealing sheet. On the test piece, at the center of the TD direction at the time of manufacture, a straight line (5 cm) in the direction of two parallel TEs was drawn at intervals of 100 mm. Then, the positions where the respective straight lines 6 are equally divided (5 places respectively) are marked. The test piece was then heated to 80. (: The warm water is placed for 60 seconds. When the sealing sheet has a small specific gravity and the sealing sheet floats on the surface of the warm water, 101111289 37 201244915, it is placed in the floating state. The ratio of the sealing sheet is smoked. When the sealing sheet is large and sinks into warm water, it is placed in the state of sinking. After 60 seconds, the test piece is taken out from the warm water, and it is immersed and cooled in a room temperature of 2 Torr. After a second, remove the moisture on the surface of the sheet. Using a vernier caliper, measure the interval A from each of the five marks marked on one of the straight lines on the test piece to the opposite mark marked on the other line ( (mm) The heating shrinkage rate is calculated based on the following formula, and the average value of the five points is obtained. • The heat shrinkage rate (%) = (100 - Α) / 100 χ 100. (6) Melting of the resin composition constituting the sealing sheet The flow rate is based on JISK7210 (1999) "Test method for MFR 'melt mass-flow rate and melt volume flow rate, meh volume-flow rate" at a temperature of 19 Torr. (: The resin composition was measured under the test conditions of a load of 2.16 kg. (7) Length of the bottom side of the protrusion (D) The surface of the sheet having the protrusion was observed by a stereoscopic microscope, and the length of the bottom side (D) was measured. When the shape of the bottom surface is a polygonal shape such as a triangle or a hexagon, or an elliptical shape, the diameter of the smallest perfect circle including the above shape is measured. (8) Unit rupture The two sides of the self-sealing sheet are cut into 180 mm. Test piece of flat square. Soldering joint (thickness 280, width 101111289 38 201244915 2 mm) on a polycrystalline solar cell unit (3 types of busbars 'i56mm square, thickness 200 μπι) Solar cell with connector. Prepare glass plate (180 mm square, thickness 3 mm) and polyester solar cell back sheet (180 mm square, thickness 24 〇μιη). The laminated sealing sheet, the solar cell sheet, the sealing sheet, and the bottom layer were laminated. At this time, the sealing sheet was laminated so that the surface of the sealing sheet was in contact with the solar cell unit. The laminated body was placed at a temperature of 145. (:, The solar cell module was fabricated by vacuuming for 30 seconds, pressing for 1 minute, and pressure S for 10 minutes to form a solar cell module. Using a solar cell £L (Electroluminescence) image detecting device for the solar electric field of Saki Group _ hair image, and measure the length (mm) of the total crack of the unit rupture u 。. Repeat the test three times to find the average value of the total crack length. (9) Number of bubbles by visual number The number of bubbles in the solar cell module produced in the above (8) was determined. The average value of the three tests was obtained. (10) Rebound stress A test piece of a flat square having a side of 120 mm cut from the sealing sheet Then, using the compression tester KES FB_3 manufactured by Kato Tech Co., Ltd., the flat pressure terminal of diameter 16 111111 was pressed at a speed of 2 〇/ muscle from the test piece with a protrusion facing the sealing sheet, and measured in the thickness direction. The rebound stress (kpa) of the sheet when the pressure was increased by 1 〇〇μηη. The average value of the rebound stress was obtained by repeating the test three times. (Example 1) 101111289 39 201244915 According to FIG. Method for making solar cell sealing sheet (a) : film making step _

使用雙軸擠出機作A 為擠出機11,將包含EVA(乙酸乙稀酯 含量:28質量。/0、熔 流動速率:15 g/10 min,熔點:71 °C)l〇〇質量份、第二τ甘. 一丁基過氧化-2-乙基己基單碳酸酯(1小 時半生期溫度:11 ^ 。# ^ C)0·7質量份、異氰尿酸三烯丙酯0.3 質里知、γ-甲基内稀酿氧基丙基三曱氧基魏Μ質量份、 2-經基·4-曱氧基二苯_ Q3質量份、雙(1,2,⑽-五甲基 -4♦定基)癸二酸_ 〇丨f量份之樹脂組成物供給至設定為 8〇°c之擠出機η㈣行㈣鱗。雜鱗之樹脂组成物 自連接於擠出機11之保持為航之Τ字模12擠出。再者, 所使用之Τ字模之開幅為i細匪,開口間隙為〇 8賴。 將以上述方式擠出之樹脂組成物藉由保持為2(TC之拋光 輥13a、13b、13c進行冷卻固化而製成片材狀。再者,自τ 字模吐出時之步驟片材之溫度為1Grc。又,此時之步驟片 材之寬度為1150mm,厚度為450μιη,搬送速度為1〇m/mine 步驟(b):退火處理步驟 繼而’於表1中記載之條件下實施退火處理。 加熱時使用陶瓷加熱器16,搬送輥π使用將直徑15〇mm 且於表面上塗佈有“Teflon(註冊商標),,之金屬輥以輥之中 心間距成為200 mm之間隔而設置者。退火爐15係使用於 SUS製之殼體上纏繞有隔熱材者。又,自退火爐η之入口 101111289 40 201244915 下部及出口下部以1 m/sec之風速吹入熱風。 步驟(c).壓紋加工步驟 依照表1中記載之條件,繼退火處理之後而實施壓紋加 工0 壓紋加工係藉由使自退火爐搬送之步驟片材通過紋樣深 度120 μιη的壓紋輥2〇、與纏繞有厚度1〇 mm之硬度75。之 矽橡膠的壓紋對向輥19之間而實施。 評價所獲得之太陽電池密封片材之加熱收縮率及壓紋轉 印率。將結果示於表1中。如表1中所示,可獲得加熱收縮 率非b小並且清晰地轉印有壓紋紋樣之太陽電池密封片材。 (實施例2) 除將步驟(b)中之熱風之溫度料87ΐ、將加熱器溫度設 為320°C、將爐内滯留時間設為29秒鐘以外,以與實施例i 相同之方法製成密封片材。由於步驟片材之表面溫度下降, 故而加熱收縮率稍微變大,又壓紋轉印率稍微變低^ 但可與 實施例1同樣轉得加熱㈣轉常小並且清晰地轉印有 壓紋紋樣之太陽電池密封片材。 (實施例3) 除將步驟(b)中之熱風之溫度設為贼、將加熱器溫度設 為300°C、將爐内滯留時間設為30秒鐘、將線壓力設U〇 N/cm以外’讀實施例丨㈣之方法製成密封諸。由於 步驟片材之表面溫度進而下降,故而加熱收縮麵微變大, 101111289 41 201244915 又壓紋轉印率稍微變低,但可與實施例1同樣地獲得加熱收 縮率非常小並且清晰地轉印有壓紋紋樣之太陽電池密封片 材。 (實施例4) 除將步驟(c)中之線壓力設為200 N/cm以外,以與實施例 3相同之方法製成密封片材。壓紋轉印率稍微變低,但可與 實施例3同樣地獲得清晰地轉印有壓紋紋樣之太陽電池密 封片材。 (實施例5) 除將步驟(b)中之熱風溫度設為110°C、將爐内滯留時間設 為27秒鐘、將步驟⑷中之線壓力設為200 N/cm以外,以 與實施例1相同之方法製成片材。由於步驟片材之表面溫度 上升,故而可獲得加熱收縮率變得非常小且壓紋轉印率亦清 晰之太陽電池密封片材。 (實施例6) 除將步驟(c)中對壓紋輥之包角設為45。以外,以與實施例 5相同之方法製成密封片材。由於包角變淺,故而壓紋轉印 率變得稍淺,但為具有良好之外觀之片材。 (實施例7) 除將步驟(b)中之步驟片材之搬送速度設為7 m/min、將熱 風溫度設為110°C、將加熱器溫度設為300°C、將爐内滯留 時間設為39秒鐘、將步驟⑷中之線壓力設為120 N/cm以 101111289 42 201244915 外,以與實施例1相同之方法製成密封片材。由於步驟片材 之加熱時間變長,表面溫度變高,故而加熱收縮率大大降 低,即便線壓力較低亦可製成清晰之壓紋形狀之片材。 (比較例1〜5) 除使用表2中所示之條件以外,以與實施例1相同之方法 製成太陽電池密封片材。 (比較例6、7) 利用圖2中所示之先前之製造方法,自T字模擠出後立 即實施壓紋加工,繼而進行退火處理。退火處理裝置設為與 實施例1相同者,緊接於T字模後之壓紋輥13b'使用紋樣 深度為120 μιη之親。 101111289 43 201244915 【II 實施例7 寸 卜 CO (N 〇 8 cn 〇 OS 〇〇 v〇 00 00 實施例6 δ § 〇 cn CN 〇 T—Η 〇 tn m 〇 Os On ON α; 00 00 o CN 3 實施例5 寸 〇 CO CN 〇 ο m 8 〇\ ON 〇\ ON 00 〇〇 8 CN r—Η 實施例4 〇 ο ΓΛ CN ο m ΓΛ P 〇\ VO ο o CN 實施例3 δ 〇 ο m CN g 8 m rn ΓΛ (N <7; ο 寸 ,_·Η 實施例2 〇 ο m CN SS 闵 m ir> 00 m 00 in 〇\ i〇 m 實施例1 **Η 〇 ο m CN ΓΟ as 沄 m v〇 cK oo 沄 m 〇 CN »-Η S3 項目 Τ字模出口處續脂之M(°c) 步驟片材之厚度_ 步驟片材之搬送速度(m/min) 退火爐15入口處之步驟片材之表面溫度(°C) 熱風雜(°〇 加熱器16之表面溫度(°C) 退火爐内之步驟片材之表面之最高溫度(°C) 退火爐出口處之步驟片材之表面溫度(°C) 退火爐内之步驟片材之滯留時間(秒) 退火爐15出口處之步驟片材之速度(m/min) 壓紋輥20入口處之步驟片材之表面溫度(°C) 壓紋輥20之溫度(°C) 壓紋輥20之線壓力(N/cm) 對壓紋親20之包角(°) 壓紋輥之紋樣之深度Τηι(μχη) 加熱收縮率(%) 壓紋轉印率(%) 製膜步驟 退火處理步驟 壓紋加工步驟 片材特性 片材製 成步驟 寸寸 ; s-UIOl 201244915 【(Nd 比車交例7 寸 〇 Τ—^ m <N 00 VO ο (Ν CS Ο; 1 1 Ο <Ν 1 3 pj 比較例6 〇 〇 m (N § ο ΓΟ rn CS cK 1 1 Ο f—Η 1 |比較例5 1 寸 cn CN S τ—Η 8 寸 14·4 1 m oo VO m CR 比較例4 〇 Ο m CN ρ CN 00 CN 〇< Q 们 Γ—^ 寸 r»H 00 m 比較例3 ! 寸 ο m CN ο Ο ^Τ) ο CN Os ON Ό uo ir> 寸 T-H r-H in <N 比較例2 寸 ο ^Η cn CN 00 s (Ν s <N α< OO <n § r-H 無樣品 i無樣品 丨比較例1 〇 ο r-H CO (N 00 VO g (Ν vo CN cK oo 寸 項目 T字模出口處之樹脂之溫度(°C) 步驟片材^J?·度(μηι) 步驟片材之搬送速度(m/min) 退火爐15入口處之步驟片材之表面溫度(°C) 熱風溫度(°C) 加熱器16之表面溫度(°C) 退火爐内之步驟片材之表面之最高溫度(°C) 退火爐出口處之步驟片材之表面溫度(°C) 退火爐内之步驟月材之滯留時間(秒) 退火爐15出口處之步驟片材之速度(m/min) 壓紋親20入口處之步驟片材之表面溫度(°C) 壓紋親20之溫度(°C) 壓紋報20之線壓力(N/cm) 對壓紋報20之包角(°) 壓紋報之紋樣之深度Tm(pm) 加熱收縮率(%) 壓紋轉印率(%) 製膜步驟 退火處理步驟 壓紋加工步驟 片材特性 片材製 成步驟 5寸 68-11101 201244915 (結果) 如表1中所示,實施例1〜7中製成之太陽電池密封片材 係加熱收縮率較小,且壓紋轉印率較高,壓紋形狀清晰地轉 印。 使用該等太陽電池密封片材並以先前公知之方法製成太 陽電池模組,結果,於模組製成時,並未產生單元偏移、單 元破裂、或氣泡混入等異常。 於比較例1中,由於退火處理時之溫度、壓紋輥20入口 處之片材溫度均較低,故而加熱收縮率較大,壓紋轉印率較 低。於比較例3 t,由於將退火爐出口與壓紋輥入口之間擴 大’故而片材之溫度降低,壓紋轉印率降低。於比較例4 中’由於退火爐内之片材表面溫度較低,故而無法充分減少 加熱收縮率。 於比較例2中,步驟片材纏繞於壓紋輥上,無法獲得樣品。 於比較例5中,由於退火處理時間較短,故而無法充分減 少太陽電池密封片材之加熱收縮。 於比較例6、7中,由於利用拋光輥賦予壓紋形狀故而壓 紋形狀清晰,但若欲使加熱收縮減少則壓紋形狀變形,若欲 保持壓紋形狀則無法使加熱收縮減少。 (實施例8) 步驟(a):製膜步驟 將包含EVA(乙醆乙烯隨含量:28質量%、熔融流動速率: 101111289 46 201244915 15 g/l〇 min(190°C)、熔點:7Γ〇1〇〇質量份、第三丁基過 氧化-2-乙基己基單碳酸酯(1時間半生期溫度:119。匸)〇 7質 . 量份、異氰尿酸三稀丙酉旨〇.3質量份、γ_甲基丙烯醯氧基两 ; 基三甲氧基石夕烧0.2質量份、L羥基-4-甲氧基二笨基酮〇 3 . 質量份、雙(丨,2,2,6,6·五曱基-4-哌啶基)癸二酸酯〇1質量份 之樹脂組成物供給至設定為8 〇。匸之雙軸擠出機而進行熔融 混練。將經混練之樹脂組成物自連接於雙軸擠出機之保持為 105°C之Τ字模擠出。再者,Τ字模之開幅為13〇〇 mm,開 口間隙為0.8 mm。 將該EVA片材藉由保持為2〇°C之拋光輥進行冷卻固化。 再者,EVA片材自τ字模吐出時之片材溫度為i〇7°C。又, 此時之片材寬度為1150 mm,片材之厚度為450 μπι,片材 搬送速度為10 m/min。繼而,連續實施退火處理、壓紋加 工。 步驟(b):退火處理步驟 乂 退火處理係藉由通過於SUS製之殼體上纏繞有隔熱材之 ! 退火爐内而進行,該退火爐設置有表面溫度設定為350°c之 陶瓷加熱器,並將直徑為150 mm且於表面上塗佈有 "Teflon(註冊商標)"之金屬耗以親之中心間距成為250 mm 之間隔而設置。又,自爐之入口下部及出口下部以1 m/sec 之風速吹入熱風。 步驟(c):壓紋加工步驟 101111289 47 201244915 壓紋加工係藉由使自退火爐取出之片材通過紋樣深度為 180 μπι且具有450個/cm2之直徑46〇 μιη且為半球形之凹型 之雕刻紋樣的壓紋親、與纏繞有厚度10 mm之硬度75。之石夕 橡膠的對向輥之間而實施。 再者,上述製造條件之詳細情況如下。Using a twin-screw extruder as A for extruder 11, it will contain EVA (ethyl acetate content: 28 mass. /0, melt flow rate: 15 g/10 min, melting point: 71 °C) Part, second τ Gan. monobutyl peroxy-2-ethylhexyl monocarbonate (1 hour and half-life temperature: 11 ^. # ^ C) 0·7 parts by mass, triallyl isocyanurate 0.3 Lizhi, γ-methyl-endo-oxypropyltrimethoxy oxime, mass fraction, 2-perylene 4-methoxydiphenyl _ Q3 parts by mass, bis(1,2,(10)-penta The resin composition of the base of the adipic acid 癸 量 量 供给 is supplied to an extruder η (four) row (four) scale set to 8 ° ° C. The resin composition of the squama is extruded from the extruder 11 and held by the stencil. Furthermore, the opening width of the Τ font used is i fine, and the opening gap is 〇8 赖. The resin composition extruded in the above manner is formed into a sheet shape by being cooled and solidified by the polishing rolls 13a, 13b, and 13c of TC. Further, the temperature of the sheet when the film is ejected from the τ font is 1Grc. Further, the step sheet at this time has a width of 1150 mm, a thickness of 450 μm, a transport speed of 1 μm/mine, and a step (b): an annealing treatment step followed by an annealing treatment under the conditions described in Table 1. The ceramic heater 16 is used, and the transfer roller π is provided with a diameter of 15 mm and coated with "Teflon (registered trademark) on the surface, and the metal rolls are provided at intervals of a center pitch of the rolls of 200 mm. The 15 series is used for the insulation of the casing made of SUS. In addition, the hot air is blown at a wind speed of 1 m/sec from the lower part of the annealing furnace η 101111289 40 201244915 and the lower part of the outlet. Step (c). The processing steps are performed according to the conditions described in Table 1, and the embossing is performed after the annealing treatment. The embossing process is performed by passing the step sheet conveyed from the annealing furnace through the embossing roll 2 of the pattern depth of 120 μm, and wound with The hardness of 1〇mm is 75. The embossing of the glue was carried out between the opposed rolls 19. The heat shrinkage rate and the embossing transfer rate of the obtained solar cell sealing sheet were evaluated. The results are shown in Table 1. As shown in Table 1, The heat shrinkage rate is not small and the embossed solar cell sealing sheet is clearly transferred. (Example 2) The temperature of the hot air in the step (b) was 87 ΐ, and the heater temperature was set to 320 ° C. The sealing sheet was formed in the same manner as in Example i except that the residence time in the furnace was set to 29 seconds. Since the surface temperature of the step sheet was lowered, the heat shrinkage ratio was slightly increased, and the embossing transfer rate was increased. It is slightly lower. However, it can be heated in the same manner as in Example 1 (4) to turn the solar cell sealing sheet which is often small and clearly transferred with an embossed pattern. (Example 3) Except the temperature of the hot air in the step (b) It is set as a thief, and the temperature of the heater is set to 300 ° C, the residence time in the furnace is set to 30 seconds, and the line pressure is set to be U 〇 N / cm. The method of reading Example 丨 (4) is sealed. The surface temperature of the sheet is further lowered, so that the heat shrinkage surface becomes slightly larger, 101111289 41 20124 Further, in the same manner as in Example 1, a solar cell sealing sheet having a very small heat shrinkage ratio and clearly transferred with an embossed pattern was obtained in the same manner as in Example 1. (Example 4) c) The pressure of the line was set to 200 N/cm, and a sealing sheet was produced in the same manner as in Example 3. The embossing transfer rate was slightly lowered, but the transfer was clearly obtained in the same manner as in Example 3. An embossed solar cell sealing sheet. (Example 5) The hot line temperature in the step (b) was set to 110 ° C, the residence time in the furnace was set to 27 seconds, and the line pressure in the step (4) was used. A sheet was produced in the same manner as in Example 1 except that it was set to 200 N/cm. Since the surface temperature of the step sheet rises, a solar cell sealing sheet having a very small heat shrinkage ratio and a clear embossing transfer rate can be obtained. (Example 6) The wrap angle of the embossing roll in the step (c) was set to 45. A sealing sheet was produced in the same manner as in Example 5 except for the method. Since the wrap angle becomes shallow, the embossing transfer rate becomes slightly shallow, but it is a sheet having a good appearance. (Example 7) The holding speed of the sheet in the step (b) was set to 7 m/min, the hot air temperature was set to 110 ° C, the heater temperature was set to 300 ° C, and the residence time in the furnace was set. A sealing sheet was prepared in the same manner as in Example 1 except that the line pressure in the step (4) was set to 120 N/cm to 101111289 42 201244915. Since the heating time of the step sheet becomes long and the surface temperature becomes high, the heat shrinkage rate is greatly lowered, and even if the line pressure is low, a clear embossed sheet can be produced. (Comparative Examples 1 to 5) A solar cell sealing sheet was produced in the same manner as in Example 1 except that the conditions shown in Table 2 were used. (Comparative Examples 6 and 7) Using the previous production method shown in Fig. 2, embossing was immediately performed after extrusion from the T-die, followed by annealing treatment. The annealing treatment apparatus was set to be the same as in the first embodiment, and the embossing roll 13b' immediately after the T-shaped mold used a protruding depth of 120 μm. 101111289 43 201244915 [II Example 7 Inch Bu CO (N 〇8 cn 〇OS 〇〇v〇00 00 Example 6 δ § 〇cn CN 〇T-Η 〇tn m 〇Os On ON α; 00 00 o CN 3 Embodiment 5 Inch 〇CO CN 〇ο m 8 〇\ON 〇\ON 00 〇〇8 CN r—Η Example 4 〇ο ΓΛ CN ο m ΓΛ P 〇 VO ο o CN Example 3 δ 〇ο m CN g 8 m rn ΓΛ (N <7; ο inch, _·Η Example 2 〇ο m CN SS 闵m ir> 00 m 00 in 〇\ i〇m Example 1 **Η 〇ο m CN ΓΟ as沄mv〇cK oo 沄m 〇CN »-Η S3 Item M at the exit of the stencil mold M (°c) Step thickness of the sheet _ Step sheet conveying speed (m/min) Step at the entrance of the annealing furnace 15 Sheet surface temperature (°C) Hot air miscellaneous (°〇 Surface temperature of heater 16 (°C) The maximum temperature of the surface of the sheet in the annealing furnace (°C) The surface of the sheet at the exit of the annealing furnace Temperature (°C) Retention time of the sheet in the annealing furnace (seconds) Step speed of the sheet at the exit of the annealing furnace 15 (m/min) Step sheet at the entrance of the embossing roller 20 Surface temperature (°C) Temperature of embossing roll 20 (°C) Line pressure of embossing roll 20 (N/cm) Wrap angle of embossing pro 20 (°) Depth of embossing roll Τηι(μχη Heating shrinkage rate (%) embossing transfer rate (%) film forming step annealing process step embossing processing step sheet property sheet making step inch; s-UIOl 201244915 [(Nd than car case 7 inch inch —^ m <N 00 VO ο (Ν CS Ο; 1 1 Ο <Ν 1 3 pj Comparative Example 6 〇〇m (N § ο ΓΟ rn CS cK 1 1 Ο f—Η 1 | Comparative Example 5 1 inch Cn CN S τ—Η 8 inch 14·4 1 m oo VO m CR Comparative Example 4 〇Ο m CN ρ CN 00 CN 〇< Q Γ—^ 寸 r»H 00 m Comparative Example 3 ! inchο m CN ο Ο ^Τ) ο CN Os ON Ό uo ir> Inch TH rH in <N Comparative Example 2 Inch ο ^Η cn CN 00 s (Ν s <N α< OO <n § rH No sample i no sample丨Comparative example 1 〇ο rH CO (N 00 VO g (Ν vo CN cK oo inch temperature of the resin at the exit of the T-die) (°C) Step sheet ^J?·degree (μηι) Step sheet conveying speed (m/min) Step at the entrance of the annealing furnace 15 Sheet surface temperature (°C) Hot air temperature (°C) Surface temperature of heater 16 (°C) Maximum temperature of the surface of the sheet in the annealing furnace (°C) Step sheet at the exit of the annealing furnace Surface temperature (°C) Step in the annealing furnace Residual time of the moon (seconds) Step speed of the sheet at the exit of the annealing furnace 15 (m/min) Step surface of the embossing pro 20 inlet sheet (° C) embossing pro 20 temperature (°C) embossing report 20 line pressure (N / cm) embossing report 20 wrap angle (°) embossed report depth Tm (pm) heating shrinkage ( %) embossing transfer rate (%) film forming step annealing treatment step embossing processing step sheet property sheet forming step 5 inch 68-11101 201244915 (Results) As shown in Table 1, Examples 1 to 7 The prepared solar cell sealing sheet has a small heat shrinkage ratio, a high embossing transfer rate, and a clear transfer of the embossed shape. Using these solar cell sealing sheets and forming a solar battery module by a conventionally known method, as a result, no abnormality such as cell offset, cell breakage, or bubble mixing occurred during the manufacture of the module. In Comparative Example 1, since the temperature at the time of the annealing treatment and the sheet temperature at the entrance of the embossing roll 20 were both low, the heat shrinkage ratio was large and the embossing transfer rate was low. In Comparative Example 3 t, since the temperature between the annealing furnace outlet and the embossing roller inlet was enlarged, the temperature of the sheet was lowered, and the embossing transfer rate was lowered. In Comparative Example 4, since the surface temperature of the sheet in the annealing furnace was low, the heat shrinkage ratio could not be sufficiently reduced. In Comparative Example 2, the step sheet was wound around the embossing roll, and the sample could not be obtained. In Comparative Example 5, since the annealing treatment time was short, the heat shrinkage of the solar cell sealing sheet could not be sufficiently reduced. In Comparative Examples 6 and 7, the embossed shape was obtained by the use of the buffing roll, and the embossed shape was clear. However, if the heat shrinkage was to be reduced, the embossed shape was deformed, and if the embossed shape was to be maintained, the heat shrinkage could not be reduced. (Example 8) Step (a): The film forming step will contain EVA (ethylene hydride content: 28% by mass, melt flow rate: 101111289 46 201244915 15 g/l 〇 min (190 ° C), melting point: 7 Γ〇 1 part by mass, tert-butylperoxy-2-ethylhexyl monocarbonate (1 time half-life temperature: 119. 匸) 〇 7 mass. Parts, isocyanuric acid tris-propyl hydrazine. Parts by mass, γ-methacryloxyloxy; 0.2 parts by weight of trimethoxycarbazide, L-hydroxy-4-methoxydipyridyl ketone 3. Part by mass, bis (丨, 2, 2, 6 The resin composition of 1 part by mass of hexamethylene-4-piperidinyl) sebacate was supplied to a twin-screw extruder set to 8 Torr. The melt-kneading was carried out by mixing the resin. The material was extruded from a twin-axis extruder maintained at 105 ° C. Further, the opening of the Τ-shaped mold was 13 〇〇 mm, and the opening gap was 0.8 mm. The EVA sheet was maintained by The polishing roller of 2 ° ° C is cooled and solidified. Further, the sheet temperature of the EVA sheet when ejected from the τ-shaped mold is i 〇 7 ° C. Further, the sheet width at this time is 1150 mm, and the thickness of the sheet is 450 μπι, The material conveying speed is 10 m/min. Then, the annealing treatment and the embossing processing are continuously performed. Step (b): Annealing treatment step The annealing treatment is performed by winding a heat insulating material through a casing made of SUS! It is carried out in a furnace equipped with a ceramic heater having a surface temperature of 350 ° C and a metal having a diameter of 150 mm and coated with "Teflon(registered trademark)" The center-to-center spacing is set at intervals of 250 mm. Further, hot air is blown at a wind speed of 1 m/sec from the lower part of the inlet of the furnace and the lower part of the outlet. Step (c): embossing processing step 101111289 47 201244915 By embossing The sheet taken out from the annealing furnace passes through a embossing pattern having a grain depth of 180 μm and having a diameter of 450 Å μm of 450/cm 2 and a concave shape of a hemispherical concave shape and a hardness of 75 mm wound with a thickness of 75 mm. The eccentric rubber is applied between the opposing rolls. Further, the details of the above manufacturing conditions are as follows.

退火爐入口處之片材表面溫度:23 °C 熱風溫度:93°C 退火爐内之片材表面之最高溫度:90°C 退火爐出口處之片材表面溫度:90°C 退火爐内之片材滯留時間:28秒鐘 退火爐15出口處之片材速度:9.6 m/min 壓紋輥入口處之片材表面溫度:78。〇 壓紋輥溫度:15°C 壓紋輥之線壓力:350 N/cm 對壓紋輥之包角:120。。 對所獲得之密封片材之加熱收縮率、回彈應力、模組製造 時之單元破裂性、及氣泡個數進行評價。將結果示於表3 中。如表3中所示,為片材加熱收縮率較小且模組製造時之 單元破裂、氣泡較少之密封片材。 (實施例9) 除將步驟(c)中之壓紋輥變更為紋樣深度120 且具有 450個/cm2之直徑460 μιη且為半球形之凹型之雕刻紋樣的 101111289 48 201244915 壓紋親以外’以與實施例8相同之方式製成密封片材。所獲 得之密封片材係如表3中所示,為片材加熱收縮率較小且模 組製造時之單元破裂、氣泡較少之密封片材。 • (實施例10) • 除將步驟(e)中之壓紋輥變更為紋樣深度300 μιη且具有 450個/cm2之直徑46〇 μηι且為半球形之凹型之雕刻紋樣的 壓紋輥以外’以與實施例8相同之方式製成密封片材。所獲 付之密封片材係如表3中所示,為片材加熱收縮率較小且模 組製造時之單元破裂、氣泡較少之密封片材。 (實施例11) 除將步驟(e)中之壓紋輥變更為紋樣深度則_且具有 兆0個/cm之直徑33〇 μιη且為半球形之凹型之雕刻紋樣的 ”外,以與實施例8相同之方式製成密封片材。所獲 付之密封片材係如表3巾所示,為片材加熱收縮率較小且模 組製造時之單元破裂、氣泡較少之密封片材。 (實施例12) , 除將步驟⑷中之壓紋輥變更為紋樣深度180 μιη且具有 840個/cm2之外周直徑46〇 μιη且為四角錐形之凹蜇之雕刻 紋樣的壓紋輥以外,以與實施例8相同之方式製成密封片 材。 所獲得之密封片材係如表3中所示,為於模組製造時產生 若干單元破裂但片材加熱收縮率較小且氣泡較少之密封片 101111289 49 201244915 材。 (實施例13) 不實施退火處理,利用紅外線加熱器將片材表面溫度加熱 除“外’以與實施例⑶同 之方式製成密封片材。 戶斤獲得之密封片材係如表3中所示,為片材之加熱收縮率 較大並於模組製造時產生若干單元破裂但氣泡較少之密封 片材。 (實施例14) 除將EVA樹脂變更為熔融流動速率為1〇 g/i〇之eva 樹脂以外’以與實施例8相同之方法冑成密封片材。所獲得 之密封片材係如表3中所示,為於模組製造時產生若干之單 元破裂但片材加熱收縮率較小且氣泡較少之密封片材。 (實施例15) 除將步驟(c)中之壓紋輥變更為紋樣深度ι8〇 μιη且具有45 個/cm2之外周直徑2000 μηι且為四角錐形之凹型之雕刻紋 樣的壓紋輥以外,以與實施例8相同之方式製成密封片材。 所獲得之密封片材係如表3中所示,為片材加熱收縮率較 小並於模組製造時產生若干單元破裂但氣泡較少之密封片 材。 (參考例1) 除不實施壓紋加工以外,以與實施例8相同之方式製成實 101111289 50 201244915 施至退火處理之密封片材並供於評價。 所獲得之密封片材係如表4中所示,為片材之加熱收縮率 較小但模組製造時之單元破裂、氣泡大量產生之密封片材。 (參考例2) 除將步驟(c)中之壓紋輥變更為紋樣深度18〇卜111且具有於 輥之旋轉方向上連續之半圓形之凹槽(凹槽寬μιη)之雕 刻紋樣的壓紋輥以外,以與實施例8相同之方式製成密封片 材。 所獲得之密封片材係如表4中所示,為片材加熱㈣率較 小且模組製造時之單元破裂較少但氣泡較多之密封片材。 (參考例3) 除將步驟⑷中之壓喃變更為紋樣深度5()卿且且有45〇 個W之直徑_卿且為半球形之凹型之雕刻紋樣的屋紋 輕以外’以與實施例8相同之方式製成密封片材。 所獲得之密封片材係如表4中所示,為片材加熱收縮率較 小但模組製造叙單元破H錄k密封片材。 (參考例4) 除將步驟⑷中之輥變更為紋樣深度i8Q _且且有 4r5〇〇^C^ 卜,以與貫施例8相同之方式製成密封片材。 所獲得之密封片材係如表4中所 斤’、為片材加熱收縮率較 小且氣泡較少但於模組製造時單元破裂财之密封片材。 101111289 201244915 (參考例5) 除將步驟(c)中之壓紋輥變更為紋樣深度180 μιη且具有7 個/cm2之直徑3800 μιη且為半球形之凹型之雕刻紋樣的壓 紋輥以外,以與實施例8相同之方式製成密封片材。 所獲得之密封片材係如表4中所示,為片材加熱收縮率較 小但模組製造時之單元破裂、氣泡較多之密封片材。 101111289 52 201244915 【£嵴】 實施例15 四角錐I 〇 2000 0.08 in CO ο 實施例14 〇 半球 450 460 0.33 實施例13 半球 450 460 0.33 ο 實施例12 »Ti 四角錐 840 I 0.33 <N m ο 實施例11 1半球 980 250 330 0.76 cn 〇 ο 實施例10 1半球| 450 250 460 0.54 o ο 實施例9 1半球1 450 〇 460 0.22 | (Ν »n o ο |實施例8 1 1半球1 450 150 460 | 0.33 | o ο 單位 | g/10 min 個/cm2 ί 1 kPa i EVA樹脂之熔融流動速率 突起之形狀 突起之個數 突起之高度Τ 突起之底邊之長度D Τ/D比 加熱收縮率 回彈應力 單元破裂性(龜裂長度) 氣泡個數 1參考例5 I l半球I 卜 3800 I 0.04 I 215 寸 |參考例4 1 1半球| 4500 I 1.00 I (Ν CN σ\ 〇〇 〇 |參考例3 1 |半球| 450 〇 460 0.09 CN 00 00 寸 參考例2 連續凹槽形狀 t Γ-Η 1 1 m (N CN 〇 ΓΛ 參考例1 無突起 1 1 1 1 (N 220 單位 1 g/10 min 個/cm2 1 I kPa 1 學 EVA樹脂之熔融流動速率 突起之形狀 突起之個數 突起之高度Τ 突起之底邊之長度D T/D比 加熱收縮率 回彈應力 單元破裂性(龜裂長度) 氣泡個數 【寸1 -s-llsl 201244915 (產業上之可利用性) 本發明可非常適合地用於太陽電池密封片材之製造方法 中。尤其是,由於減少加熱收縮且具有清晰之壓紋紋樣,故而 可防止模組製造時之單元之位置偏差、氣泡混入模組内等,且 可顯著提昇模組之生產性。 【圖式簡單說明】 圖1係表示本發明之太陽電池密封片材之製造方法之一例 的概略模式圖。 圖2係表示先前之太陽電池密封片材之製造方法之一例的 概略模式圖。 圖3係說明測定於單面上形成有突起之太陽電池密封片材 之突起之高度之方法的圖。 圖4係說明測定於兩面上形成有突起之太陽電池密封片材 之突起之高度之方法的圖。 圖5係表示突起之底邊之長度d的圖。 【主要元件符號說明】 1 步驟片材 11 雙軸擠出機 12 模具 13a 拋光輥(表面無雕刻加工) 13b 拋光輥(表面無雕刻) 13b' 壓紋輥(表面有雕刻加工) 101111289 54 201244915 13c 拋光輥(表面無雕刻加工) 14 軋輥 15 退火爐 16 加熱器 17 搬送輥 18 片材取出報 19 壓紋對向輥 20 壓紋輥 21 冷卻輥 31 齒輪果 32 片材搬送方向 33 非接觸式紅外線溫度計 101111289 55Sheet surface temperature at the inlet of the annealing furnace: 23 °C Hot air temperature: 93 °C Maximum temperature of the surface of the sheet in the annealing furnace: 90 °C Surface temperature at the exit of the annealing furnace: 90 °C Annealing furnace Sheet residence time: sheet speed at the exit of the annealing furnace 15 at 28 seconds: 9.6 m/min. Sheet surface temperature at the entrance of the embossing roll: 78. 〇 embossing roll temperature: 15 °C Line pressure of embossing roll: 350 N/cm Wrap angle of embossing roll: 120. . The heat shrinkage ratio, the rebound stress, the cell cracking property at the time of module manufacture, and the number of bubbles were evaluated for the obtained sealing sheet. The results are shown in Table 3. As shown in Table 3, it is a sealing sheet in which the sheet heat shrinkage rate is small and the unit is broken and bubbles are small at the time of module manufacture. (Example 9) In addition to changing the embossing roll in the step (c) to a pattern depth of 120 and having a diameter of 450/cm 2 of 460 μm and a hemispherical concave pattern of 101111289 48 201244915 A sealing sheet was produced in the same manner as in Example 8. The obtained sealing sheet was as shown in Table 3, and was a sealing sheet in which the sheet heat shrinkage rate was small and the unit was broken at the time of manufacture of the mold, and the bubbles were small. • (Example 10) • Except that the embossing roll in step (e) was changed to an embossing roll having a pattern depth of 300 μm and having a diameter of 450/cm 2 46〇μηι and a hemispherical concave pattern. A sealing sheet was produced in the same manner as in Example 8. The obtained sealing sheet was as shown in Table 3, and was a sealing sheet in which the heat shrinkage rate of the sheet was small and the unit was broken and bubbles were small at the time of manufacture of the module. (Example 11) Except that the embossing roll in the step (e) was changed to the depth of the pattern, and the embossed pattern having a diameter of 0.3 Å/cm and a concave shape of a hemispherical shape was used, A sealing sheet was prepared in the same manner as in Example 8. The obtained sealing sheet was as shown in Table 3, and was a sealing sheet having a small heat shrinkage rate of the sheet and a cell breakage and less bubbles in the manufacture of the module. (Example 12), except that the embossing roll in the step (4) was changed to an embossing roll having a embossed pattern having a groove depth of 180 μm and having a peripheral diameter of 46 Å/cm 2 and a square pyramid shape A sealing sheet was produced in the same manner as in Example 8. The obtained sealing sheet was as shown in Table 3, in order to cause a number of cells to be broken during the manufacture of the module, but the sheet had a smaller heat shrinkage ratio and a smaller bubble. (10) The sealing sheet was prepared in the same manner as in the example (3) except that the annealing treatment was not carried out, and the surface temperature of the sheet was heated by an infrared heater except "outside". The sealing sheet obtained by the household is as shown in Table 3, which is a sheet having a large heat shrinkage ratio and a sealing sheet in which a plurality of cells are broken but bubbles are small at the time of module manufacture. (Example 14) A sealing sheet was formed in the same manner as in Example 8 except that the EVA resin was changed to an eva resin having a melt flow rate of 1 〇 g / i. The obtained sealing sheet was as shown in Table 3, which was a sealing sheet in which a plurality of unit cracks were produced at the time of module manufacture, but the sheet had a small heat shrinkage ratio and a small number of bubbles. (Example 15) Except that the embossing roll in the step (c) was changed to a embossing roll having a embossed pattern of a pattern depth of ι8 〇μηη and having a peripheral diameter of 2000 μm and having a square pyramid shape of a rectangular shape, A sealing sheet was produced in the same manner as in Example 8. The obtained sealing sheet was as shown in Table 3, and was a sealing sheet having a small heat shrinkage rate of the sheet and a number of cell cracks but less bubbles in the manufacture of the module. (Reference Example 1) A sealing sheet which was subjected to annealing treatment was prepared and evaluated for evaluation in the same manner as in Example 8 except that embossing was not carried out. The obtained sealing sheet was as shown in Table 4, and was a sealing sheet in which the heat shrinkage rate of the sheet was small but the unit was broken at the time of manufacture of the module, and a large amount of bubbles were generated. (Reference Example 2) Except the engraved pattern in which the embossing roll in the step (c) is changed to the embossing depth of 18 111 111 and has a semicircular groove (groove width μιη) continuous in the rotation direction of the roll. A sealing sheet was produced in the same manner as in Example 8 except for the embossing roll. The obtained sealing sheet was as shown in Table 4, and was a sealing sheet in which the sheet was heated at a small (four) rate and the unit was broken at the time of module manufacture but the bubbles were large. (Reference Example 3) In addition to changing the embossing in the step (4) to a grain depth of 5 () and having a diameter of 45 WW, which is a hemispherical concave pattern, the pattern is lighter than A sealing sheet was produced in the same manner as in Example 8. The obtained sealing sheet was as shown in Table 4, and the heat shrinkage rate of the sheet was small, but the module manufacturing unit broke the H-k sealing sheet. (Reference Example 4) A sealing sheet was produced in the same manner as in Example 8 except that the roll in the step (4) was changed to the pattern depth i8Q_ and 4r5〇〇^^^. The obtained sealing sheet was as shown in Table 4, and was a sealing sheet in which the sheet had a small heat shrinkage ratio and a small number of bubbles but the unit was broken at the time of module manufacture. 101111289 201244915 (Reference Example 5) Except that the embossing roll in the step (c) is changed to an embossing roll having a pattern depth of 180 μm and having a diameter of 3800 μm and a hemispherical concave pattern, A sealing sheet was produced in the same manner as in Example 8. The obtained sealing sheet was as shown in Table 4, and was a sealing sheet in which the sheet had a small heat shrinkage ratio but the unit was broken and the bubbles were large at the time of module manufacture. 101111289 52 201244915 [Example] Example 15 Quadrilateral I 〇 2000 0.08 in CO ο Example 14 Hemisphere 450 460 0.33 Example 13 Hemisphere 450 460 0.33 ο Example 12 » Ti Teeth 840 I 0.33 < N m ο Example 11 1 Hemisphere 980 250 330 0.76 cn 〇ο Example 10 1 Hemisphere | 450 250 460 0.54 o ο Example 9 1 Hemisphere 1 450 〇 460 0.22 | (Ν »no ο | Example 8 1 1 Hemisphere 1 450 150 460 | 0.33 | o ο unit | g/10 min / cm2 ί 1 kPa i EVA resin melt flow rate protrusion shape protrusion number of protrusions Τ length of the bottom side of the protrusion D Τ / D ratio heating shrinkage Rebound stress unit rupture (crack length) Number of bubbles 1 Reference Example 5 I l Hemisphere I Bu 3800 I 0.04 I 215 inch | Reference Example 4 1 1 Hemisphere | 4500 I 1.00 I (Ν CN σ\ 〇〇〇| Reference Example 3 1 | Hemisphere | 450 〇460 0.09 CN 00 00 Inch Reference Example 2 Continuous groove shape t Γ-Η 1 1 m (N CN 〇ΓΛ Reference example 1 No protrusion 1 1 1 1 (N 220 unit 1 g/ 10 min / cm2 1 I kPa 1 Learn the melt flow of EVA resin The height of the number of protrusions of the shape protrusions Τ The length of the bottom side of the protrusions DT/D ratio Heat shrinkage rate Rebound stress unit rupture (crack length) Number of bubbles [inch 1 -s-llsl 201244915 (Industry UTILITY) The present invention can be suitably used in a method for manufacturing a solar cell sealing sheet. In particular, since the heat shrinkage is reduced and a clear embossing pattern is provided, the positional deviation of the unit during module manufacturing can be prevented. Fig. 1 is a schematic view showing an example of a method for producing a solar cell sealing sheet of the present invention. Fig. 2 is a schematic view showing an example of a method for producing a solar cell sealing sheet of the present invention. A schematic view showing an example of a method for producing a solar cell sealing sheet of the prior art. Fig. 3 is a view for explaining a method of measuring the height of a projection of a solar cell sealing sheet having a protrusion formed on one surface. A diagram of a method of forming the height of the protrusion of the protruding solar cell sealing sheet on both sides. Fig. 5 is a view showing the length d of the bottom side of the protrusion. [Description of main component symbols] 1 Step sheet 11 Double-axis extruder 12 Mold 13a Polishing roller (surface without engraving) 13b Polishing roller (no engraving on the surface) 13b' Embossing roller (surface engraving) 101111289 54 201244915 13c Polishing roller (surface without engraving) 14 Roller 15 Annealing furnace 16 Heater 17 Transfer roller 18 Sheet removal report 19 Embossed counter roller 20 Embossing roller 21 Cooling roller 31 Gear fruit 32 Sheet conveying direction 33 Non-contact infrared Thermometer 101111289 55

Claims (1)

201244915 七、申請專利範圍: -種太陽電池密封片材之製造方法,其依 驟⑷、步驟(b)及步驟(c) : 步藉由加熱而料之樹脂組成物 狀,繼而藉由冷卻而獲得步驟片材之步驟; 片材 步驟(b):將上述步驟(a)中 ’ 表面加熱㈣秒鐘,於該一-個 成該表面部分之韻組成物切點 ^面之狐度達到構 步驟⑷:使於上述步驟(b)中經加熱:步:度片::表 為(構成上述表面部分之樹脂組成物之炫點挑)〜(構成上 述表面部分之樹脂組成物之魅·.c)之溫度,繼而對該表 面按壓壓紋輥而於該表面上形成壓紋形狀之步驟。 2.如申請專利範圍第i項之太陽電池密封片材之製造方 法其中,於上述步驟(c)中,於以上述墨紋報按壓上述步 驟片材之表面時,使施加於該表面上之線壓力為⑼〜伽 N/cm。 3’如申μ專利fc圍第1或2項之太陽電池密封片材之製造 方法’其巾’於上述步驟⑷巾,独上述壓純按壓上述 步驟片材之表面時,使該壓紋輥之表面溫度成為(構成上述 表面部分之樹脂組成物之熔點_2〇ΐ)以下。 4’如U利fcS)第1至3項中任—項之太陽電池密封月 材之製其中’於上述步驟⑷中,使料軸或雙轴 101111289 56 201244915 擠出機將上述藉由加熱而熔融之樹脂組成物自模具擠出並 成形為片材狀。 5. 如申請專利範圍第!至4項中任—項之太陽電池密封片 材之製造方法,其中,構成上述表面部分之樹脂la成物含有 聚烯烴系樹脂及有機過氧化物。 6. -種太陽電池密封片材,其係利用申請專利範圍第ι至 5射任-項之製造方法所獲得之太陽電池密封片材,且 構成上述表面部分之樹脂組成物含有聚稀煙系樹脂, 形成有上述壓紋形狀之表面具有4〇〜23〇〇個/cm2之高度 60〜·μΐη之獨立之突起,且該獨立之突起之高度(τ)與底 邊長度(D)之比(T/D)為〇.〇5〜〇 8〇。 — 7. 如申5月專利範圍第6項之太陽電池密封片材,其中,於 將上述太陽電池密封諸於_之溫水中放置丨分鐘時,、 口亥在封片材之片材行進方向之加熱收縮率為以下。 8·如中請專利範圍第6或7項之太陽電池密封片材,其 中,上述獨立之突起之形狀為半球形及/或 四角錐形。 9. 如申叫專利範圍第6至8項中任—項之太陽電池密封片 材’其中’於將上述太陽電池密封片材具有上述突起之面於 該密封片材之厚度方向上壓縮刚哗時,片材之回彈應力 為70 kPa以下。 10. 如申請專利範圍第6至9項中任—項之太陽電池密封 片材,其中’ _L述太陽電池密封片#具有突起之面進而具有 101111289 57 201244915 咼度為1〜15 μιη之突起。 u.—種太陽電池模組, 受光面保護材, 为面保護材,及 其係由如下部分所構成: 配置於該受光面保護材與背面保護材之間、利用申請專利 範圍第6至1〇項中任一項之太陽電池密封片材而密封太陽 電池單元的層。 101111289 58201244915 VII. Patent application scope: - A method for manufacturing a solar cell sealing sheet, which is according to step (4), step (b) and step (c): step by heating the resin composition, and then cooling Step of obtaining a step sheet; sheet step (b): heating the surface of the step (a) in the above step (a) for four seconds, and forming a flop of the surface of the rhyme composition of the surface portion (4): heating in the above step (b): step: degree sheet:: the table is (the sleek point of the resin composition constituting the surface portion) ~ (the enchantment of the resin composition constituting the surface portion described above. The temperature, which in turn presses the embossing roll against the surface to form an embossed shape on the surface. 2. The method for manufacturing a solar cell sealing sheet according to the invention of claim i, wherein in the step (c), when the surface of the step sheet is pressed by the ink mark, the surface is applied to the surface The line pressure is (9) ~ gamma N / cm. 3', the method for manufacturing a solar cell sealing sheet according to claim 1 or 2, wherein the embossing roller is used in the above step (4), and the surface of the sheet is pressed by the above-mentioned step. The surface temperature is equal to or lower than the melting point of the resin composition constituting the surface portion. 4', such as Uli fcS), the solar cell sealing material of any one of items 1 to 3, wherein in the above step (4), the shaft or the biaxial 101111289 56 201244915 extruder will be heated by the above The molten resin composition is extruded from a mold and formed into a sheet shape. 5. If you apply for a patent scope! The method for producing a solar cell encapsulating sheet according to any one of the preceding claims, wherein the resin la composition constituting the surface portion contains a polyolefin resin and an organic peroxide. 6. A solar cell sealing sheet obtained by using the solar cell sealing sheet obtained by the manufacturing method of the patent application No. 1-5 to 5, and the resin composition constituting the surface portion contains a poly-smoke system The resin, the surface on which the embossed shape is formed has a height of 60 · 23 〇〇 / cm 2 of the independent protrusion, and the ratio of the height (τ) of the independent protrusion to the length of the base (D) (T/D) is 〇.〇5~〇8〇. — 7. The solar cell sealing sheet according to item 6 of the patent scope of May, wherein, when the solar cell is sealed in the warm water of _ for a minute, the direction of the sheet of the sealing sheet is The heat shrinkage ratio is as follows. 8. The solar cell sealing sheet of claim 6 or claim 7, wherein the independent protrusions have a hemispherical shape and/or a quadrangular pyramid shape. 9. The solar cell encapsulating sheet according to any one of claims 6 to 8 wherein the solar cell sealing sheet has the above-mentioned protrusion surface is compressed in the thickness direction of the sealing sheet. When the sheet has a rebound stress of 70 kPa or less. 10. The solar cell sealing sheet according to any one of claims 6 to 9, wherein the solar cell sealing sheet has a raised surface and further has a protrusion of 101111289 57 201244915 having a twist of 1 to 15 μm. u.—The solar cell module, the light-receiving surface protection material, and the surface protection material, and the system thereof are composed of the following parts: disposed between the light-receiving surface protection material and the back surface protection material, and the application patent scopes 6 to 1 A solar cell sealing sheet according to any one of the preceding claims, wherein the layer of the solar cell unit is sealed. 101111289 58
TW101111289A 2011-03-31 2012-03-30 Process for producing solar cell sealing sheet TW201244915A (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105683276A (en) * 2013-11-05 2016-06-15 希爱化成株式会社 Method for manufacturing solar-cell sealing material

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105683276A (en) * 2013-11-05 2016-06-15 希爱化成株式会社 Method for manufacturing solar-cell sealing material

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