TW201100251A - Laminated polymer film and solar module made thereof - Google Patents

Laminated polymer film and solar module made thereof Download PDF

Info

Publication number
TW201100251A
TW201100251A TW099103379A TW99103379A TW201100251A TW 201100251 A TW201100251 A TW 201100251A TW 099103379 A TW099103379 A TW 099103379A TW 99103379 A TW99103379 A TW 99103379A TW 201100251 A TW201100251 A TW 201100251A
Authority
TW
Taiwan
Prior art keywords
ethylene
copolymer
solar cell
layer
film
Prior art date
Application number
TW099103379A
Other languages
Chinese (zh)
Inventor
qiu-ju Wu
Ruo-fei ZHAO
shi-jie Ren
Bo Xu
Original Assignee
Du Pont
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from PCT/US2009/048448 external-priority patent/WO2010101582A1/en
Application filed by Du Pont filed Critical Du Pont
Publication of TW201100251A publication Critical patent/TW201100251A/en

Links

Classifications

    • 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

Landscapes

  • Photovoltaic Devices (AREA)
  • Laminated Bodies (AREA)

Abstract

Disclosed is a laminated film having: (a) a substrate; and (b) a bonding layer of ethylene polymer on one major surface of the substrate wherein the bonding layer is placed directly on the substrate or there is a (c) primer layer between the substrate and bonding layer. Also disclosed is a solar module made of such a laminated polymer film.

Description

201100251 六、發明說明: 【發明所屬之技術領域】 本發明係關於在個別薄膜層之間具有改良的接合力的層 壓聚合物薄膜。層壓聚合物薄膜之各層間不但具有加強接 合力,且對於用以作為太陽能電池元件封裝件之乙稀-乙 酸乙烯酯共聚物具有改良的接合力。本發明亦關於以此種 層壓聚合物薄膜製成之太陽能模組。 【先前技術】 鑑於全球暖化,世界上各國政府對於節能與減排的需求 曰趨殷切。因此,尋求新能源以代替石化燃料成為亟待解 決之急迫性議題。 太陽能為乾淨、無污染且取用不盡之能源。迄今,太陽 能主要是以太陽能模組轉換為電力加以利用。電力之後用 於驅動電熱水器、電動車與衛星元件。 太陽能模組意指一種直接由光,特別是太陽光,產生電 能之光伏裝置。迄今,太陽能模組常見實例包含搭載結晶 矽太陽能電池,例如單晶矽太陽能電池、多晶矽太陽能電 池與奈米級太陽能電池,及薄膜太陽能電池,例如非晶矽 薄膜太陽能電池、碲化鎘薄膜太陽能電池與銅銦鎵硒薄膜 太陽能電池之模組。 結晶矽太陽能模組主要包含背板、封裝件、光伏電路與 前板。薄膜太陽能電池結構主要包含置於基材(例如,玻 璃板、聚合物板或不鏽鋼板)上的光伏電路、置於光伏電 路與基材之另一表面的封裝件、置於上述封裝上的前板或 146091.doc 201100251 背板。 封裝件使用於太陽能模組以與前板、光伏電路與/或背 板一起接合。以約15(TC進行的層壓操作中,融化的封裝 件流入太陽能電池内空隙以封裝太陽能電池。 迄今,S帛封裝材料包含乙婦_乙酸乙稀醋共聚物與離 子聚合物。不過’離子聚合物有缺點,包含高價、難以加 工與非常高的硬度。相比較下,乙烯-乙酸乙稀醋共聚物 (EVA)有易於加工、中等價格與具適當彈性之優點。因 此,此為目前最常使用之聚合性封裝材料。 太陽月b模、.且内月;I板之主要角色為保護太陽能電池對抗機 械:擊與磨損。為了充分利用入射光,前板必須在一定光 譜範圍具高透光度(例如:對於結晶石夕太陽能電池,為自 400至1,1〇〇奈米)。先前技術的太陽能模組中,前板主要為 玻璃(通常為厚度為3至4公楚之低鐵、淬火縫石(⑽㈣ flint)玻璃)或高分子材料構成。 太陽能模組内背板之主要角色為保護太陽能電池與封裝 件對抗濕度與乳化。於太陽能模組組合製程中,背板也用 作為機械阻障’避免刮傷與作為絕緣體。因此,背板必須 =優異的濕度阻障性質與彈性,及與封裝件具良好接合 強度’明免氧氣與濕度穿透進人太陽能模組。 太陽能模組的常見背板為多層層壓薄 (例如,聚醋基材)與位於基材表面之接合層。基材 上述層壓薄膜具有優異的之濕度與氧氣阻障性質, -基材(例如,聚醋基材)與接合層之間的接合強度並非完 146091.doc 201100251 全令人滿意。有時,於兩層間界面會發生脫層。 此外,接合層與封裝件,例如乙烯-乙酸乙_聚物 之間的接合強度也並非完全令人滿意。仍有改進空間。 因此,對於具有優異的濕度與氧氣阻障性質、在其層間 具優異的接合強度’與作為太陽能電池封裝件之乙稀-乙 酸乙稀酯樹脂間且侵里的垃人 n、的接合強度,以使接著劑與有機溶 劑用量能最低化的層壓薄膜,有其需求。 【發明内容】 所揭露者為層壓薄膜’具有優異的濕度與氧氣的阻障性 質、在其層間具優異的接合強度,與作為太陽能電池封裝 件之乙烯-乙酸乙烯酯樹脂間具優異的接合強度。 又揭露者為結w太陽能模組,使用本發明之層塵薄膜 作為背板。 使用本發明之層壓薄膜作 更揭露者為薄膜太陽能模組 為背板或前板。 Q 因此,所揭露者為層壓薄膜,包含·· ,該基材包 二酯與其混 ⑷-聚醋基材,包含一第一表面與一第二表面 含由聚苯二甲酸c2-6烷二酯 '聚萘二甲酸烷 合物或摻合物所成群組選出之聚合物。 (b)在该聚酯基材之第一表面上的一黏著層; ⑷在該聚醋基材之第二表面上的一底漆層,其中該底漆層 厚度小於0.99微米; ⑷在該底漆層上的-接合層,其中該接合層包含乙稀與選 自下述所成群組之-種或多種單體之共聚物:丙烯 146091.doc 201100251 烧醋、甲基丙烯酸cK4燒醋、甲基丙稀酸、甲基丙稀酸環 氧丙酯與順丁烯二酸酐;與 (6)在°亥黏著層上的-保護層,包含引張彈性模數大於15〇 Kpsi之氟聚合物。 所揭露者為太陽能模組,包含前板、背板與經乙稀-乙 酸乙烯醋共聚物材料封裝之光伏電路,其中該背板為由本 發明之層壓薄膜構成。 所揭露者為太陽能模組,包含置於玻璃板、聚合物或不 鐵鋼板上之光伏電路,及由本發明之層壓薄膜構成前板及/ 或背板。 【實施方式】 基材 本發明之層壓薄膜包含基材,其中該基材材質係選自聚 ::或含氟聚合物。層壓薄膜可包含單層或複數層之聚醋與 早層或複數層之含氟聚合物,例如兩層或複數層之聚醋與 含氟聚合物所成之層壓薄膜。在另一實施例中,聚醋或含 氣聚合物基材上yL· M a « 有金屬金屬氧化物及/或非金屬氧化物 之塗層。 因此’根據本發明之一具體實施例,基材可選自: ⑴聚醋’例如聚苯二甲酸k烧二醋、聚萘二甲酸C26 烷一醋或其二元共聚物、多元聚合物或混合物。 (ii)含氟聚合物; (叫於表面有金屬、金屬氧化物及/或非金屬氧化物之塗 層之聚酯或含氟聚合物;或 146091.doc 201100251 (IV)由上述一種或更多種材料所成之層壓薄膜。 聚酯基材 當使用聚酯製造基材時,對於使用之聚酯沒有特別限 制。可以為先雨技術之任何習知《酉旨。也可為層壓之雙層 或複數層聚醋薄膜。在一實施例中,聚醋基材總厚度為30 至350微米’杈佳為50至300微米,更佳為7〇至25〇微米。201100251 VI. Description of the Invention: TECHNICAL FIELD OF THE INVENTION The present invention relates to a laminated polymer film having improved bonding force between individual film layers. The layers of the laminated polymer film not only have a reinforcing bonding force but also have an improved joining force for the ethylene-vinyl acetate copolymer used as a solar cell element package. The invention also relates to a solar module made from such a laminated polymer film. [Prior Art] In view of global warming, the demand for energy conservation and emission reduction by governments around the world is growing. Therefore, the search for new energy to replace fossil fuels has become an urgent issue to be resolved. Solar energy is clean, non-polluting and uses inexhaustible energy. So far, solar energy has been mainly converted into electricity using solar modules. Electricity is then used to drive electric water heaters, electric vehicles and satellite components. A solar module means a photovoltaic device that produces electricity directly from light, especially sunlight. So far, common examples of solar modules include crystallization solar cells, such as single crystal germanium solar cells, polycrystalline solar cells and nano solar cells, and thin film solar cells, such as amorphous germanium thin film solar cells, cadmium telluride thin film solar cells. A module with a copper indium gallium selenide thin film solar cell. The crystallization solar module mainly comprises a back plate, a package, a photovoltaic circuit and a front plate. The thin film solar cell structure mainly comprises a photovoltaic circuit disposed on a substrate (for example, a glass plate, a polymer plate or a stainless steel plate), a package placed on the other surface of the photovoltaic circuit and the substrate, and placed on the package Board or 146091.doc 201100251 Backplane. The package is used in a solar module to interface with the front panel, the photovoltaic circuit, and/or the back panel. In a lamination operation of about 15 (TC), the melted package flows into the gap in the solar cell to encapsulate the solar cell. So far, the S帛 package material contains a polyethylene-acetic acid ethyl acetate copolymer and an ionic polymer. Polymers have disadvantages, including high cost, difficulty in processing, and very high hardness. In contrast, ethylene-ethylene acetate copolymer (EVA) has the advantages of ease of processing, medium price, and appropriate elasticity. Therefore, this is currently the most Polymeric packaging materials commonly used. Solar Moon b mode, and inner moon; The main role of I plate is to protect solar cells against machinery: impact and wear. In order to make full use of incident light, the front plate must be highly transparent in a certain spectral range. Luminosity (for example: for crystallized solar cells, from 400 to 1, 1 nanometer). In prior art solar modules, the front plate is mainly glass (usually 3 to 4 thick) Iron, quenched seam stone ((10) (four) flint) glass) or polymer material. The main role of the solar module inner back is to protect the solar cell and package against humidity and emulsification. In the solar module combination process, the back plate is also used as a mechanical barrier to avoid scratches and as an insulator. Therefore, the back plate must have excellent humidity barrier properties and elasticity, and good joint strength with the package. Oxygen and humidity penetrate into the solar module. The common backsheet of the solar module is a multi-layer laminated thin (for example, a polyester substrate) and a bonding layer on the surface of the substrate. The above laminated film of the substrate has excellent properties. Humidity and oxygen barrier properties, - the bonding strength between the substrate (for example, the polyester substrate) and the bonding layer is not satisfactory. 146091.doc 201100251 is all satisfactory. Sometimes, delamination occurs at the interface between the two layers. The bonding strength between the bonding layer and the package such as ethylene-acetic acid ethylene-polymer is not completely satisfactory. There is still room for improvement. Therefore, it has excellent humidity and oxygen barrier properties and is excellent in its interlayer. The bonding strength between the bonding strength 'and the ethylene-vinyl acetate resin as a solar cell package and the intrusion of the resin, so as to minimize the amount of the adhesive and the organic solvent. There is a need for a film. SUMMARY OF THE INVENTION The disclosed film is a laminate film having excellent barrier properties against humidity and oxygen, excellent joint strength between layers, and ethylene-vinyl acetate as a solar cell package. The resin has excellent joint strength. It is also disclosed that the solar module of the present invention uses the dust film of the present invention as the back sheet. The laminate film of the present invention is used as the back sheet or the front of the thin film solar module. The present invention is therefore a laminate film comprising: a substrate comprising a diester and a mixed (4)-polyacetate substrate comprising a first surface and a second surface comprising polyphthalic acid c2- a polymer selected from the group consisting of a 6-alkyl diester 'polynaphthalene dicarboxylate or a blend. (b) an adhesive layer on the first surface of the polyester substrate; (4) in the polyacetate a primer layer on the second surface of the material, wherein the primer layer has a thickness of less than 0.99 μm; (4) a bonding layer on the primer layer, wherein the bonding layer comprises ethylene and a group selected from the group consisting of Copolymer of one or more monomers: propylene 146091.doc 20110 0251 burnt vinegar, methacrylic acid cK4 vinegar, methyl acrylate, methyl propylene acrylate and maleic anhydride; and (6) protective layer on the adhesion layer, including the introduction A fluoropolymer having a modulus of elasticity greater than 15 〇 Kpsi. The disclosed system is a solar module comprising a front panel, a backsheet and a photovoltaic circuit encapsulated with a vinyl-vinyl acetate copolymer material, wherein the backsheet is comprised of the laminate film of the present invention. The disclosed embodiments are solar modules comprising photovoltaic circuits placed on glass sheets, polymers or non-ferrous steel sheets, and front and/or back sheets formed from the laminate film of the present invention. [Embodiment] Substrate The laminate film of the present invention comprises a substrate, wherein the substrate material is selected from the group consisting of poly-: or fluoropolymer. The laminate film may comprise a single layer or a plurality of layers of a fluoropolymer with an early layer or a plurality of layers of a fluoropolymer, for example, a laminate film of two or more layers of a mixture of a vinegar and a fluoropolymer. In another embodiment, the yL·M a « on the polyester or gas-containing polymer substrate is coated with a metal metal oxide and/or a non-metal oxide. Thus, in accordance with an embodiment of the present invention, the substrate may be selected from the group consisting of: (1) polyester vinegar such as polyphthalic acid k-burned vinegar, polynaphthalene dicarboxylic acid C26 alkaloid or its binary copolymer, multipolymer or mixture. (ii) a fluoropolymer; (a polyester or fluoropolymer having a coating of a metal, a metal oxide and/or a non-metal oxide on the surface; or 146091.doc 201100251 (IV) from one or more of the above A laminated film made of a plurality of materials. Polyester substrate When a substrate is produced using polyester, there is no particular limitation on the polyester to be used. It may be any conventional method of the prior art, or may be lamination. The double layer or the plurality of layers of the polyester film. In one embodiment, the polyester substrate has a total thickness of from 30 to 350 μm, preferably from 50 to 300 μm, more preferably from 7 to 25 μm.

適合用於基材之聚S旨材料之非限制性實例包含,例如, 聚苯二甲酸C2·6烧二醋,較佳為聚苯二甲酸C2.4烧二醋,如 ^對苯二甲酸乙二醋(PET)、聚對苯二甲酸丙二醋、聚對 苯二甲酸丁二酯、聚對苯二曱酸己二酯、聚鄰苯二甲酸乙 二酯、聚鄰苯二甲酸丙二酯、聚鄰苯二甲酸丁二酯、與聚 鄰苯二曱酸已二醋’較佳為聚對苯二甲酸乙二自旨;聚蔡二 曱酸C2_0烷二酯,較佳為聚萘二甲酸C24烷二酯,如聚举二 甲酸乙二1旨、聚萘二甲酸丙二醋與聚萘二甲酸丁二s旨:與 二種或更多種上述材料之共聚物及摻合物。 、適當之聚酯基材,可藉由鑄膜後以雙軸定向處理而形 成’以更增強機械強度與氣體阻障性質。該膜具有良好的 機械、介電與氣體阻障性質。 適當聚醋基材也可由市面購得,例如自E I.⑹p〇nt和 Nem〇urs and c〇mpany,威明頓,德拉瓦美國(「㈣⑽」) 可購得各種厚度的聚對苯4酸乙二醋板。 含氟聚合物基材 。適口用於製造基材之含氟聚合物並無特別限制。可以任 何先别技藝之f知含氟聚合物所形成之聚合物薄膜。合適 14609I.doc 201100251 之含氟聚合物之非限制性實例包含,氟乙烯聚合物;氟乙 烯與其他非氟化、部份氟化或全氟化單體之共聚物;偏二 氟乙烯聚合物;偏二氟乙烯與其他非氟化、部份氟化或全 氟化單體之共聚物;氯三氟乙烯聚合物;氯三氟乙烯與其 他非氟化、部份氟化或全氟化單體之共聚物;四氟乙烯聚 合物;四氟乙烯與其他非氟化、部份氟化或全氟化單體之 共聚物。 其他非氟化、部份氟化或全氟化單體之非限制性實例包 含,例如,乙烯、丙烯、氟乙浠、二氟化乙烯、偏二氟乙 烯、氣三氟乙烯、六氟丙稀、四氟乙稀、全氟炫氧基乙稀 基醚、全氟丙稀等。 合適作為基材的含氟聚合物亦可由市面購得,例如為購 自杜邦之Tedlar™聚氟乙烯或購自Dyneon LLC(奥克達爾, 明尼蘇達)之聚偏二氟乙浠、乙稀-四氟乙稀共聚物或四氟 乙烯/六IL丙烯/偏二氟乙稀共聚物。 含氟聚合物基材也可為雙層或複數層含氟聚合物之層壓 薄膜。在一實施例中,基材為由聚氟乙烯層與聚偏二氟乙 烯、乙稀-四氟乙稀共聚物或四氟乙烯-六氟丙浠/偏二氟乙 烯共聚物層所形成之層壓薄膜。 含氟聚合物基材總厚度為20至350微米,較佳為20至300 微米,更佳為20至250微米。 於其表面具有金屬、金屬氧化物及/或非金屬氧化物之塗 層之聚酯或含氟聚合物基材 該聚酯基材或含氟聚合物基材之一個或二個主要表面為 146091.doc 201100251 塗有單層或多層之選自金 之表面塗層。且屬乳化物與非金屬氧化物 含氟機屬塗層聚— 任:St:二?金,化物並無特別限制。可為 在 可白知金屬氧化物或非金屬氧化物。 化修〇 用之金屬氧化物或非金屬氧化物包含氧 -2)或氧化峰10χ,㈣,5·1.5)。這種氧化層 ο =用”氣相沈積(CVD)法沈積於聚醋或含筑聚合物 1 _埃(αΓ化層厚度—般為5°至4_埃(A),較佳為1⑽至 全t之金屬塗層並無特別限制。可為先前技術中習知之 因主:例如’銀箔、鋁箔或錫箔。當考量成本與其他 因素,一般使用銘箔。 金屬塗層的厚度益鞋則 乂广 度…特別限制。可為先前技術中常見之任 J旱度。在一實施例中,金屬塗層的厚度為5至50微米, ◎ 杈佳為7至25微米。 ”屬塗層(例如’銘冶)可利用本技術領域習知技術,層 =聚酿或含氣聚合物基材。例如,可使用黏著劑以利於 層壓製程。 ^表面”有金屬、金屬氧化物/非金屬氧化物塗層之聚 醋基材或含氟聚合物基材的總厚度為8至35〇微米,較佳為 10至300微米,更佳為12j_25h 層壓薄膜聚酯基材 本發月之層壓薄媒基材也可為由聚g旨與含氟聚合物所成 146091.doc 201100251 之層壓薄膜。可故 數声之含氣臂八層之聚醋與單一層或複 == 成之層麗薄膜。聚醋為舆該聚酿基材 才同之聚酉曰材料。可為由— 、 料所成之層壓物。在一實施;“材料或複數層聚酿材 η主 在貫知例中,於聚醋層之一個或兩個 主要表面上,層壓該含氟聚合物層。 在另一實施例中,聚|旨·含氟聚合物之層壓物為以交替 ,聚S旨層與含敦聚合物層所形成。聚醋層為由單—層聚 西曰或兩層、或複數層之聚酿所成之層壓物。含氣聚合物 :層壓物可為單一層含氟聚合物、或兩層,或複數層之含 II聚合物。 ㈣與含氟聚合物之層壓薄膜中,厚度可為本技術領域 揭露之任何習知厚度。在一實施例中,含氟聚合物層的厚 度為15至50微米’較佳為2〇至4〇微米。 聚酯-含氟聚合物之層壓薄膜基材的總厚度為3〇至35〇微 米,更佳為50至300微米,再更佳為7〇至25〇微米。 聚酯與含氟聚合物之層壓方法可為本技術領域之任何習Non-limiting examples of materials suitable for use in the substrate include, for example, polyphthalic acid C2·6 burnt vinegar, preferably polyphthalic acid C2.4 burnt vinegar, such as terephthalic acid Ethylene vinegar (PET), polytrimethylene terephthalate, polybutylene terephthalate, poly(p-phenylene terephthalate), poly(ethylene terephthalate), poly(phthalic acid) The diester, polybutylene phthalate, and poly(phthalic acid) diacetate are preferably polyethylene terephthalate; polycyanate C2-0 alkyl diester, preferably poly Naphthalene dicarboxylate C24 alkyl diester, such as polydiethylenedicarboxylate, poly(naphthalene dicarboxylate) and polynaphthalene dicarboxylate: copolymers and blends with two or more of the above materials Things. A suitable polyester substrate can be formed by biaxially oriented treatment after casting to enhance mechanical strength and gas barrier properties. The film has good mechanical, dielectric and gas barrier properties. Suitable polyacetal substrates are also commercially available, for example, from E I. (6) p〇nt and Nem〇urs and c〇mpany, Wilmington, Delaware USA ("(4)(10)")). Acid vinegar plate. Fluoropolymer substrate. The fluoropolymer suitable for the production of a substrate is not particularly limited. Any polymer film formed by a fluoropolymer can be known in any prior art. Non-limiting examples of suitable fluoropolymers of 14609I.doc 201100251 include, fluoroethylene polymers; copolymers of vinyl fluoride with other non-fluorinated, partially fluorinated or perfluorinated monomers; vinylidene fluoride polymers a copolymer of vinylidene fluoride with other non-fluorinated, partially fluorinated or perfluorinated monomers; chlorotrifluoroethylene polymer; chlorotrifluoroethylene and other non-fluorinated, partially fluorinated or perfluorinated a copolymer of monomers; a tetrafluoroethylene polymer; a copolymer of tetrafluoroethylene with other non-fluorinated, partially fluorinated or perfluorinated monomers. Non-limiting examples of other non-fluorinated, partially fluorinated or perfluorinated monomers include, for example, ethylene, propylene, fluoroacetam, ethylene difluoride, vinylidene fluoride, gas trifluoroethylene, hexafluoropropyl Dilute, tetrafluoroethylene, perfluorodecyl ether ether, perfluoropropene and the like. Fluoropolymers suitable as substrates are also commercially available, for example, TedlarTM polyvinyl fluoride available from DuPont or polyvinylidene fluoride available from Dyneon LLC (Oakdal, Minnesota), Ethylene-Four Fluoroethylene copolymer or tetrafluoroethylene/hexa-I-propylene/vinylidene fluoride copolymer. The fluoropolymer substrate can also be a laminate of two or more layers of fluoropolymer. In one embodiment, the substrate is formed of a polyvinyl fluoride layer and a polyvinylidene fluoride, ethylene-tetrafluoroethylene copolymer or a tetrafluoroethylene-hexafluoropropane/vinylidene fluoride copolymer layer. Laminated film. The fluoropolymer substrate has a total thickness of from 20 to 350 μm, preferably from 20 to 300 μm, more preferably from 20 to 250 μm. a polyester or fluoropolymer substrate having a coating of a metal, a metal oxide and/or a non-metal oxide on its surface, one or two major surfaces of the polyester substrate or fluoropolymer substrate are 146091 .doc 201100251 A single or multi-layered surface coating selected from gold. It is an emulsion and a non-metal oxide. The fluorine-containing coating is poly-plated: St: two-gold, and the compound is not particularly limited. It can be known as a metal oxide or a non-metal oxide. Metal oxides or non-metal oxides used for chemical modification include oxygen -2) or oxidation peaks 10, (4), 5.1.5). The oxide layer ο = deposited by a vapor deposition (CVD) method on a polyester or a building polymer 1 Å (the thickness of the Γ layer is generally 5 ° to 4 Å (A), preferably 1 (10) to The metal coating of the whole t is not particularly limited. It may be a conventional one known in the prior art: for example, 'silver foil, aluminum foil or tin foil. When considering the cost and other factors, the foil is generally used. The thickness of the metal coating is 益The breadth is particularly limited. It may be any conventional J drought. In one embodiment, the thickness of the metal coating is 5 to 50 microns, and ◎ is preferably 7 to 25 microns. It is possible to utilize a technique known in the art, layer = polymerized or gas-containing polymer substrate. For example, an adhesive may be used to facilitate the lamination process. ^ Surface" has metal, metal oxide / non-metal oxide The total thickness of the coated polyester substrate or fluoropolymer substrate is 8 to 35 Å, preferably 10 to 300 μm, more preferably 12 _25 h. The medium substrate may also be a laminated film of 146091.doc 201100251 which is formed of a fluoropolymer. The eight-layered vinegar of the air-containing arm is combined with a single layer or a layer of y============================================================================ The fluoropolymer layer is laminated on one or both of the major surfaces of the vine layer, in one embodiment; "material or a plurality of layers of granules η". The laminate of the fluoropolymer is formed by alternating the poly layer and the polymer layer. The vine layer is composed of a single layer or two layers, or a plurality of layers. A laminate formed by a brewing. A gas-containing polymer: the laminate may be a single layer of a fluoropolymer, or two layers, or a plurality of layers of a II-containing polymer. (IV) In a laminated film with a fluoropolymer The thickness may be any conventional thickness disclosed in the art. In one embodiment, the fluoropolymer layer has a thickness of from 15 to 50 microns', preferably from 2 to 4 microns. Polyester-fluoropolymer The laminated film substrate has a total thickness of from 3 Å to 35 Å, more preferably from 50 to 300 μm, still more preferably from 7 Å to 25 Å. Polyester and fluoropolymer layer The pressing method can be any of the prior art

知技術。在一實施例中,使用黏著劑以接合含氟聚合物層 至聚酯基材。 S 關於用以接合含氟聚合物層至聚酯層之黏著劑並無特別 限制。可為先前技術中習知之傳統黏著劑。在一實施例 中,使用聚胺酯黏著劑,其為以日本三菱製造之pp525〇與 15200兩種黏著劑,以重量比為8至10:1,較佳為9:1,混人 形成。 對於用以接合含氟聚合物至聚酯的黏著層厚度無特別限 146091.doc -10- 201100251 制,只要黏著強度符合需要即可。在一實施例中,黏著層 的厚度範圍為1至30微米,較佳為5至25微米,更佳為8至 18微米。 在:實施例中,使用兩層或多層之聚_/含說聚合物之 層塵薄膜作為基材。層壓薄膜選自下述所成組群:聚氣乙 稀/聚對苯二甲酸乙二醋層麗薄膜、聚偏二敦乙稀/聚對苯 二甲酸乙二酯層壓薄膜、聚氟乙烯/聚萘二曱酸乙二酯層 ❹壓薄膜、聚氟乙烯/聚對苯二甲酸乙二酯/聚氟乙烯層壓薄 膜、與聚對苯二甲gt乙二g旨/聚對苯二甲酸乙二酯/聚對苯 二曱酸乙二酯層壓薄膜。 在另一貫施例中,使用包含厚度為3至5〇微米之鋁箔層 之早層或多層之層壓薄膜作為基材。該基材之非限制性實 例包含,例如,聚氟乙烯/鋁箔/聚對苯二曱酸乙二酯。鋁 箔可利用黏著劑接合於含氟聚合物或聚酯表面。 在另一實施例中,使用於其表面具有金屬氧化物塗層之 〇 % S旨薄膜作為基材。該基材之非限制性實例,包含,例如 聚氟乙烯/氧化鋁/聚對苯二曱酸乙二酯/聚對苯二甲酸乙二 酉旨。 基材可包含數種類型的添加物,例如光穩定劑、熱穩定 劑、抗水解劑、表面修飾劑、螢光增亮劑、光線反射劑 (light reflecting agents)、顏料與色素。特別適合之添加物 為本技術領域習知所使用之添加物。當基材為層壓薄膜 (例如’聚醋層壓薄膜或聚酯—含氟聚合物之層壓薄膜)時, 添加物可視需要地添加到層壓薄膜之各層。 146091.doc 201100251 對於添加物的含量並無特別限制,只要添加物不對於基 材或層壓薄膜強度產生負面影響即可。 、土 接合層 層壓薄膜包含位於基材之主要表面的接合層,用以接合 背板至乙烯-乙酸乙烯酯共聚物封裝件。適合用於形成接 合層之材料為乙烯共聚物材料,其為選自下述組群者: 乙烯-甲基丙烯酸Cw烷酯共聚物與乙烯_丙烯酸Ci 4烷酯 共♦物,例如,乙烯_曱基丙烯酸曱酯共聚物、乙烯-丙烯 酸甲酯共聚物、乙烯-曱基丙烯酸乙酯共聚物、乙烯-丙烯 酸乙酯共聚物、乙烯-曱基丙烯酸丙酯共聚物、乙烯-丙烯 酸丙酯共聚物、乙烯-曱基丙烯酸丁酯共聚物、乙烯-丙烯 酸丁酯共聚物、與其兩種或更多種共聚物之混合物其中 各共聚物單元之總重量中,源於乙烯之共聚物單元計有 50%至99%,較佳為70%至95% ; 乙烯甲基丙烯酸共聚物、乙烯_丙浠酸共聚物與其摻合 物,其中各共聚物單元之總重量中,源於乙烯之共聚物單 元叶有50至99%,較佳為7〇至95〇/〇 ; 乙烯-順丁烯二酸酐共聚合物,其中各共聚物單元之總 重董中,源於乙烯之共聚物單元計有50至99❶/。,較佳為7〇 至 95 %; 由乙烯與至少二種選自下述之共-單體所形成之多元聚 合物·曱基丙烯酸Cl-4烷酯、丙烯酸烷酯、乙烯_甲基 丙烯酸、乙烯-丙烯酸與乙烯_順丁烯二酸酐,其非限制性 實例包含,例如,乙烯-丙烯酸甲酯-甲基丙烯酸之三聚物 146091.doc 201100251 (其中源於源於丙烯酸曱酯之共聚物單元計有2至30重量% 與源於甲基丙浠酸之共聚物單元計有1至3 0重量❹/〇)、乙烯-丙烯酸丁酯-曱基丙烯酸之三聚物(其中源於丙烯酸丁酯之 共聚物單元計有2至30重量%,源於曱基丙烯酸之共聚物 單元計有1至30重量%為)、乙烯-曱基丙烯酸丙酯-丙烯酸 之三聚物(其中源於曱基丙烯酸丙酯之共聚物單元計有2至 30重量%,與源於丙烯酸之共聚物單元計有1至3〇重量 %)、乙烯-丙烯酸曱酯-丙烯酸之三聚物(其中源於丙烯酸甲 酉旨之共聚物早元計有2至30重量%為,與源於丙烤酸之共 聚物單元計有1至30重量%)、乙烯-丙烯酸曱酯-順丁烯二 酸酐之三聚物(其中源於丙烯酸甲酯之共聚物單元計有2至 30重量% ’與源於順丁烯二酸酐之共聚物單元計有〇.2至1〇 重量%)、乙烯-丙烯酸丁酯-順丁烯二酸酐之三聚物(其中源 於丙烯酸丁酯之共聚物單元計有2至30重量%,與源於順 丁烯二酸酐之共聚物單元計有〇·2至1〇重量%)、與乙埽-丙 烯酸-順丁烯二酸酐之三聚物(其中源於丙烯酸之共聚物單 元計有2至3 0重量%,與源於順丁烯二酸酐之共聚物單元 計有0.2至10重量%); 由乙烯與甲基丙烯酸環氧丙酯與至少一種選自下述之 共-單體所形成之共聚物:甲基丙烯酸C14烷酯、丙烯酸 烧酯、乙烯-甲基丙烯酸、乙稀_丙稀酸與乙烯-順丁婦二酸 酐’其非限制性實例包含,例如,乙烯-丙烯酸丁醋-甲基 丙烯酸環氧丙酯之三聚物’其中源於丙烯酸丁酯之共聚物 單元計有2至30重量%,與源於曱基丙烯酸環氧丙酯之丑 146091.doc -13- 201100251 聚物單元計有1至15重量。/。;與上述兩種或更多種材料之 掺合物。 適合用於層壓薄膜之接合層厚度為丨〇至4〇〇微米,較佳 為40至200微米。 接合層可具有用以封裝太陽能模組(一般為聚乙烯_乙酸 乙烯醋、聚乙烯-丙烯酸甲醋、聚乙烯_丙烯酸丁醋、聚乙 烯-甲基丙烯酸酯、離子聚合物、聚胺酯或聚乙烯丁醛)的 封裝層且具有良好的黏著性質、良好的介電性質與抗老 化。 接合層可含有數種類型的添加物。適合的非限制性實例 包含光穩定劑、熱穩定劑、助滑劑、光線反射劑(1响 reflecting agents)與色素。 對於接合層内添加物的含量並無特別限制,只要添加物 不對於接合層,或層壓薄膜最終黏著性質產生負面影響即 可 〇 接合層可使用本技術領域 _ 一 -叹口土签何分迥之接 者法之非限制性實例包含,例如,於掩壓機中融化合適 之共聚物樹脂後利用擠壓成型模具以擠出方式將融化物塗 佈於基材表面,或㈣著劑將接合 ^一實施例中,接合層不使用黏著劑而接^基材,更 特疋5之,不使用以有機溶劑稀釋之黏著劑。 在一實施例中 °/〇之丙烯酸甲西旨 並由單一螺旋擠 ,將乙烯-丙烯酸甲酯共聚物(含有13重量 ,具有炫化指數9’由杜邦公司製造)融化 壓機於2贼擠出,接合至聚對苯二甲酸 146091,doc -14· 201100251 乙二酯(PET)基材。 此外接&層可為單一層材料或兩層或複數層材料之層 壓物,例如,本發明之接合層可為分別選自上述乙稀共聚 物材料之聚合物材料之2至8層,較佳為2至6層,更佳為2 至3層之層壓物。 在一實施例中,接合層為三層層壓物,其中一層為由選 自下述之聚合物材料所形成之聚合物板:乙烯-甲基丙烯 0 酸Cl_4烷酯共聚物、乙烯-丙烯酸Cm烷酯共聚物、乙烯-甲 基丙稀酸共聚物、乙烯_丙烯酸共聚物與乙烯_順丁烯二酸 酐共聚物。另—層係由乙烯與選自下述之至少兩種單體之 多元聚合物所形成之聚合物板:曱基丙烯酸Cm烷酯、丙 烯酸Cm烷酯、曱基丙烯酸、丙烯酸與順丁烯二酸酐。另 一層係聚合物板由乙烯與選自下述之至少一種共—單體之 含有甲基丙稀酸環氧丙g旨多元聚合物所形成之聚合物板: 甲基丙烯酸Ci·4烷酯、丙烯酸〇1_4烷酯、甲基丙烯酸、丙烯 〇 酸與順丁稀二酸酐。該三層聚合物板具有大約相同的厚 度,因此作為接合層之最終聚合物板具有厚度為10至400 微米,較佳為40至2〇〇微米。 在另一實施例中,接合層為雙層層壓物,其中一層為選 自下述聚合物材料所形成之聚合物板:乙烯-甲基丙烯酸 c]·4烷酯共聚物、乙烯_丙烯酸Ci_4烷酯共聚物、乙烯-尹基 丙烯酸共聚物、乙烯_丙烯酸共聚物、乙烯_順丁烯二酸酐 共聚物、由乙烯與選自下述之至少兩種單體所形成之共聚 物:甲基丙烯酸(:1·4烷酯、乙烯_丙烯酸Ci4烷酯、甲基丙 146091.doc 15 201100251 烯酸,丙烯酸、與順丁烯二酸酐;以及由乙烯與甲基丙烯 酸環氧丙酯與選自下述之至少一種共單體所形成之含有曱 基丙烯酸環氧丙酯共聚物:甲基丙烯酸Cw烷酯、丙烯酸 c,_4烷酯、甲基丙烯酸、丙烯酸與順丁烯二酸酐,與上述 兩種或更多種聚合物之摻合物。另一層為由選自下述之聚 合物材料所形成之聚合物板:聚乙烯、聚丙烯、乙烯_丙 烯共聚物、乙烯-甲基丙烯酸Ci *烷酯共聚物、乙稀_丙烯 酸匸!-4烷酯共聚物、乙烯_甲基丙烯酸共聚物、乙烯丙烯 酸共聚物、乙烯·順丁烯二酸酐共聚物、由乙烯與選自下 述之至少二種單體所形成之共聚物:甲基丙烯酸Cw烷 酉曰丙烯®^ C 1 _4烧自旨、曱基丙稀酸、丙浠酸與順丁稀二酸 酐;以及由乙烯與具有選自下述之至少一種共單體之曱基 丙烯酸環氧丙酯所形成之含有曱基丙烯酸環氧丙酯共聚 物:曱基丙烯酸(:1-4烷酯、丙烯酸(:1_4烷酯、曱基丙烯酸、 丙烯馱與順丁烯二酸酐,與上述兩種或更多種聚合物之摻 合物。 在另一實施例中,接合層為三層層壓物,其中一層為選 自下述之聚合物材料所形成之聚合物板:乙烯-曱基丙烯 酸<^_4烷酯共聚物、乙烯_丙烯酸C1_4烷酯共聚物、乙烯-曱 基丙烯酸共聚物、乙烯_丙烯酸共聚物、乙烯_順丁烯二酸 :共聚物、由乙烯與選自下述之至少二種單體所形成之共 ♦物.甲基丙烯酸Ci·4烷酯、丙烯酸酯、曱基丙烯酸、 丙烯酸與順丁稀二自請;以及由乙稀與具有選自下述之至 少—種共單體之甲基丙稀酸環氧丙r日所形成之含有曱基丙 146091.doc -16- 201100251 =酸環氧丙r日共聚物:曱基丙烯仏▲旨、丙烯酸心燒 0日、曱基丙烯酸、丙烯酸與順丁烯二酸針,與上述兩種或 更多種聚合物之摻合物。另一層為由選自下述之聚合物材 料所形成之聚合物板:聚乙稀、聚丙稀、乙稀_丙稀共聚 t、乙烯-甲基丙烯酸Ci-4烷酯共聚物、乙烯-丙烯酸Cl_4烷 酿共聚物、乙稀-甲基丙烯酸共聚物、乙稀.丙稀酸共: 物、乙烯-順丁婦二酸酐共聚物、由乙歸與選自下述之至 ❹〃 一種早體所形成之共聚物:甲基丙婦酸Cu院酉旨、丙稀 酸(^_4心旨、甲基丙稀酸、丙烯|、與順丁烯二酸肝;以 f由乙烯與具有選自下述之至少—種共單體之甲基丙稀酸 環氧丙醋所形成之含有甲基丙烯酸環氧丙酿共聚物:甲基 丙烯酸C“4烷酯、丙烯酸^烷酯、甲基丙烯酸、丙烯酸與 順丁烯二酸酐,與上述兩種或更多種聚合物之摻合物。另 一層是由選自下述之聚合物材料所形成之聚合物板:聚乙 烯、聚丙烯、乙烯-丙烯共聚物、乙烯_曱基丙烯酸Cw烷 Ο 醋共聚物、乙烯-丙烯酸C!-4烷酯共聚物、乙烯-甲基丙烯 酸共聚物、乙烯-丙烯酸共聚物、乙順丁烤二酸軒共聚 物、由乙烯與選自下述之至少二種單體所形成之共聚物Λ: 甲基丙婦酸Cw燒酯、丙烯酸Ci 4炫酯、甲基丙稀酸、丙烯 酸、與順丁稀二酸酐;以及由乙婦與具有選自下述之至少 一種共單體之甲基丙烯酸環氧丙酯所形成之含有尹基丙稀 酸環氧丙醋共聚物:甲基丙烯酸Cw烷醋、丙婦酸Ci4烷 酯、甲基丙烯酸、丙稀酸與順丁稀二酸野,或上述兩種或 更多種聚合物之搀合物。 146091.doc -17- 201100251 適合用於接合層之聚乙烯與聚丙烯包含高密度聚乙稀、 中密度聚乙烯、低密度聚乙烯、直鏈低密度聚乙稀、金屬 芳香類-衍生低密度聚乙烯與聚丙烯均聚物。 可使用兩種或更多種擠壓機藉由擠出_塗佈方式,使具 接合層之複數層層壓薄膜接合至本發明之基材。 '、 為了增加基材與接合層之間的接合強度,基材表面可為 經表面處理者。合適的表面處理方法並無限制,其可為本 技術領域之任何傳統方法。例如,其可為電晕處理、火焰 處理或底塗處理。合適底漆之非限制性實例包含亞胺 與胺底漆。 當底塗處理使用於基材表面之表面處理,對於所形成底 漆之最終厚度並無特別限制,可為本技術領域任何常見厚 度,只要底漆對於聚酯基材與接合層之間的接合強度不迭 成負面影響即可。底漆厚度一般為低於15微米,適當為 低於K2微米,較佳為低於m米,更佳為低於〇99微米, 最較佳為低於0.8微米,最適為低於〇.5微米。例如,底漆 厚度可低於0.45微来,极於他·止 " m 十㈣G揭,她塌或低於 在一實施例中,底漆厚度為0.01至0 99微米,適 〇.01至0.8微米,較佳為0.01至0.5微米。 士當所使用表面處理方法,例如為電暈處理或火焰處理 日守,接合層直接置於基材上。 於本發明’接合層直接置於基材上意指於接合層與基材 之間沒有施用塗層或層以改良該二者之間的接合強度。 146091.doc -18· 201100251 層壓薄膜於基材與接合層之間具高接合強度或剝離強 度。與本技術領域中可見之基材與接合層之間的接合強度 相比較,層壓薄膜之兩層間之接合強度較高,且根據丁型 剝離測試結果,接合強度可高達1 〇牛頓/公分。 層壓薄膜特別適合用於製備結晶矽太陽能模組之背板, 或薄膜太陽能模組之前板或背板。該種背板或前板不但具 有良好剝離強度,也可避免接合層與乙稀-乙酸乙烯酿共 0 聚物封裝層之間的脫層,此乃起因於接合層與乙烯-乙酸 乙烯s曰共聚物封裝層之間的高接合強度,且可以有效延長 太陽能模組之壽命。 本發明以下述例示之實施例進一步說明。 實施例 測試方法 1.層壓薄膜之基材與接合層之間的剝離強度測試。 層壓薄膜切為寬度為2.54公分、長度為1〇公分之樣品 〇 條,且接合層與基材分別固定於拉伸計之上方夾具與下方 夾具,以5英吋/分鐘之速度進行剝離測試。 2·接合層與乙稀-乙酸乙_旨共聚物封裝件之間的剝離強度 測試 層壓薄膜(具有緊鄰於封裝層之接合層)、乙稀乙酸乙稀 醋共聚物封裝層與-片玻璃以適當順序堆疊,並以層堡廢 合法於UOt之操作溫度,進行交聯反㈣分鐘。之後, 該樣品切為寬度為2.54公分、長度為1〇公分之條。背板層 昼涛膜與封裝件/玻璃層分別以固定於拉伸計之上方夹具 146091.doc -19- 201100251 與下方爽具’以5英吋/分鐘之速度進行剝離測試。 3.太陽能電池元件之濕熱老化測試 用以封農太陽能電池元件之製程,包含分類整理太陽能 電池、單面焊、依序焊(serial welding)、堆疊、層壓、元 件測試、定框與清潔。層壓太陽能電池元件之濕熱老化測 6式’係於環境室(climatic chamber) vC4〇i8(由 Vdtsch Industnetechnik GmbH,德國購得),根據晶矽太陽光電模 組測„式私準(IEC) 6丨2丨5第丨〇·丨3條進行。測試用太陽能電 池兀件係保持於濕熱環境1〇〇〇小時(85乞與相對濕 度)。之後,移開元件,且剝離乙烯_乙酸乙烯酯共聚物封 裝層。剝離之乙歸-乙酸乙烯醋共聚物封裝I,以卜仙 Ehner,美國,Lambda 95G紫外光/可見光/近紅外光光譜儀 (包含15〇公楚積分球)測試其黃化指數(yeii〇wing 以 ΔΥΙ): ’ "x A 1- I 〇 其中YG指未經濕熱條件處理 < G烯-乙酸乙烯酯共聚物封 裝層剝離後’以Lambda 950紫外伞曰, , '、卜光/可見光/近紅外光光古並 儀測得之消光值。γ指經、晶埶乞 1濕熱條件處理之乙烯-乙酸乙嫌 酯共聚物封裝層剝離後測得之消光 、* 、 950紫外光/可見光/近紅外光 k疋以Lambda 意指封裝件放置;^熱料時 减寺於零, ;:一,太_池具有優== 4 _太陽能電池輸出功率測試方法 146091.doc -20- 201100251 太陽能電池輸出功率係使用3500SLP元件測試系統測定 (由Spire Corporation,美國購得)。其係與由傳統之前板與 背板材料組裝之多晶矽太陽能電池比較。 5.層壓薄膜之接合層與層之間的接合強度測試方法 層壓薄膜切為寬度為2.54公分、長度為1 0公分之樣品 條,且頂層與底層分別固定於拉伸計之上方夹具與下方夾 具,以5英吋/分鐘之速度進行剝離測試。 比較例1 〇 於本例中,所使用之背板由具有PVF/PET/PVF構造之層 壓薄膜所製成,由Isovolta Group購得。PVF為聚偏二氟乙 烯之縮寫。 藉由使用上述方法,測得聚偏二氟乙烯與聚對苯二曱酸 乙二酯之間的剝離強度經測量為4牛頓/公分。 藉由使用上述方法,測得經層壓後,背板與EVA封裝層 之間的剝離強度經測量為4.5牛頓/公分。 Q 製備太陽能模組 下述元件為以下述順序堆疊後,於真空以熱壓進行層壓 以形成太陽能模組: -由 Dongguan CSG Solar Glass Co.,Ltd·購得 3 ·2公釐厚淬 火玻璃; -EVA封裝薄膜(500微米,用以製備光伏電池之Ruifu牌 EVA薄膜,R767,由 Ruiyang Photovoltaic Material Co_, Ltd.購得); -多晶矽光伏電路(125x125χ〇·3公釐,串聯72個電路); 146091.doc -21 - 201100251 -EV讀裝薄膜⑽微米,用以製備光伏電池之㈣讀 EVA4 m > R767 , ^Ruiyang Photovoltaic Material Co Ltd·購得);與 ’ _由上述比較例1之層壓薄膜所製成之背板。 " 述方法,組裝太陽能電池輸出功率經測定為 175 瓦。 藉由使用上述方法進行太陽能電池元件濕熱老化測試, 黃化指數ΔΥΙ經測定為〇 6。 實施例1 製備層壓薄膜與測試其性質 購自 I. du Pont de Nemours and Company,威明頓’德 拉瓦,美國(「杜邦」)之25微米厚之^^聚說乙稀薄 膜’與亦購自杜邦的200微米厚之聚對苯二甲酸乙二醋板 的主要表面接合。使用之黏著劑為pp525()/i5期聚胺醋黏 著劑之9:1(重量/重量)混合物,購自三菱,曰本。黏著層 為12微米厚。 由DaV1S Standard製造的擠出_塗佈機上,Ep⑽in p_ 1050(由日本觸媒株式會社製造)於聚對苯二甲酸乙二酯板 的另一主要表面塗佈作為〇.90微米厚底漆。之後,乙烯 基丙烯酸酯共聚物(80%為源自乙烯單體)層於29〇t:擠出_ 塗佈於經底塗之表面,厚度為75微米,以形成層壓薄膜。 藉由使用上述方法,聚對苯二p酸乙二酯板與乙烯 基丙烯酸酯共聚物層之間的剝離強度經測定為21牛頓/公 分。與比較例1所述之傳統層壓薄膜的剥離強度相比較, J 4609]. doc •22- 201100251 本發明之層壓薄膜增加四倍。 於環境為85°C與85%RH(相對濕度)的條件進行經加速之 濕熱老化1,000小時後,剝離強度經測定為12牛頓/公分。 藉由使用上述方法,乙烯-甲基丙烯酸酯共聚物層與乙 烯-乙酸乙烯酯共聚物封裝件之間的剝離強度經測定為8 j 牛頓/公分。比較傳統層壓薄膜(比較例〇與乙烯-乙酸乙烯 醋共聚物封裝件之剝離強度,本實施例之層壓薄膜與乙 烯-乙酸乙烯酯共聚物封裝件之間的剝離強度增加約16 倍。 製備太陽能模組 下述元件為以下述順序堆疊後,於真空以熱壓進行層壓 以形成太陽能模組: 由 Dongguan CSG Solar Glass Co_,Ltd.購得 3_2公釐厚淬 火玻璃; -EVA封裝薄膜(500微米,用以製備光伏電池之Ruifu牌 〇 ΕνΑ薄膜,R767,由 Ruiyang photov〇ltaic Material c〇..Know the technology. In one embodiment, an adhesive is used to bond the fluoropolymer layer to the polyester substrate. S There is no particular limitation on the adhesive for bonding the fluoropolymer layer to the polyester layer. It can be a conventional adhesive known in the prior art. In one embodiment, a polyurethane adhesive is used, which is an adhesive of pp 525 Å and 15200 manufactured by Mitsubishi, Japan, in a weight ratio of 8 to 10:1, preferably 9:1. There is no special limit on the thickness of the adhesive layer used to bond the fluoropolymer to the polyester, as long as the adhesion strength meets the requirements. In one embodiment, the thickness of the adhesive layer ranges from 1 to 30 microns, preferably from 5 to 25 microns, more preferably from 8 to 18 microns. In the examples, two or more layers of a polycrystalline film containing a polymer were used as the substrate. The laminate film is selected from the group consisting of polyethylene oxide/polyethylene terephthalate film, polyethylene terephthalate/polyethylene terephthalate laminate film, and polyfluoride. Ethylene/polyethylene naphthalate ethylene glycol layer laminated film, polyvinyl fluoride/polyethylene terephthalate/polyvinyl fluoride laminated film, and poly(p-phenylene terephthalate) A film of ethylene dicarboxylate/polyethylene terephthalate. In another embodiment, a laminate film comprising an early or a plurality of layers of an aluminum foil layer having a thickness of 3 to 5 μm is used as the substrate. Non-limiting examples of the substrate include, for example, polyvinyl fluoride/aluminum foil/polyethylene terephthalate. The aluminum foil can be bonded to the surface of the fluoropolymer or polyester using an adhesive. In another embodiment, a film having a metal oxide coating on its surface is used as the substrate. Non-limiting examples of the substrate include, for example, polyvinyl fluoride/alumina/polyethylene terephthalate/polyethylene terephthalate. The substrate may comprise several types of additives such as light stabilizers, heat stabilizers, hydrolysis inhibitors, surface modifiers, fluorescent brighteners, light reflecting agents, pigments and pigments. Additives which are particularly suitable are additives which are conventionally used in the art. When the substrate is a laminate film (e.g., a 'polyacetated laminate film or a polyester-fluoropolymer laminate film), the additives are optionally added to the respective layers of the laminate film. 146091.doc 201100251 There is no particular limitation on the content of the additive as long as the additive does not adversely affect the strength of the substrate or laminate film. The soil bonding layer laminate film comprises a bonding layer on the major surface of the substrate for bonding the back sheet to the ethylene-vinyl acetate copolymer package. Suitable materials for forming the bonding layer are ethylene copolymer materials selected from the group consisting of ethylene-methacrylic acid Cw alkyl ester copolymers and ethylene-acrylic acid Ci 4 alkyl esters, for example, ethylene. Ethyl methacrylate copolymer, ethylene-methyl acrylate copolymer, ethylene-ethyl methacrylate copolymer, ethylene-ethyl acrylate copolymer, ethylene-propyl methacrylate copolymer, ethylene-propyl acrylate copolymer a mixture of ethylene, butyl methacrylate copolymer, ethylene butyl acrylate copolymer, and two or more copolymers thereof, wherein the total weight of each copolymer unit is derived from the copolymer unit derived from ethylene. 50% to 99%, preferably 70% to 95%; ethylene methacrylic acid copolymer, ethylene-propionic acid copolymer and blend thereof, wherein the copolymer of ethylene is derived from the total weight of each copolymer unit The unit leaf has 50 to 99%, preferably 7 to 95 Å/〇; an ethylene-maleic anhydride copolymer, wherein the total weight of each copolymer unit is in the copolymer unit derived from ethylene. 50 to 99 ❶ /. Preferably, from 7 to 95%; a multi-polymer formed from ethylene and at least two co-monomers selected from the group consisting of alkyl alkyl acrylate, alkyl acrylate, ethylene methacrylate , ethylene-acrylic acid and ethylene-maleic anhydride, non-limiting examples of which include, for example, ethylene-methyl acrylate-methacrylic acid terpolymer 146091.doc 201100251 (wherein derived from the copolymerization of decyl acrylate) The material unit has 2 to 30% by weight of a terpolymer derived from a copolymer unit derived from methylpropionic acid (1 to 30% by weight), and a terpolymer of ethylene-butyl acrylate-mercaptoacrylic acid (which is derived from The copolymer unit of butyl acrylate is 2 to 30% by weight, and the copolymer unit derived from methacrylic acid is 1 to 30% by weight, and the terpolymer of ethylene-mercapto propyl acrylate-acrylic acid (wherein the source) The copolymer unit of propyl methacrylate has 2 to 30% by weight, and 1 to 3% by weight based on the copolymer unit derived from acrylic acid, and a terpolymer of ethylene-acrylic acid acrylate-acrylic acid (wherein The copolymer of methacrylate is 2 to 30% by weight, and is derived from The copolymer unit of the acrylic acid has 1 to 30% by weight of ethylene terephthalate-maleic anhydride terpolymer (in which the copolymer unit derived from methyl acrylate has 2 to 30% by weight' a copolymer of ethylene-butyl acrylate-maleic anhydride (a copolymer unit derived from butyl acrylate) with a copolymer unit derived from maleic anhydride: 2 to 1% by weight) a terpolymer having 2 to 30% by weight, based on the copolymer unit derived from maleic anhydride, 〇 2 to 1% by weight, and acetonitrile-acrylic acid-maleic anhydride (wherein 2 to 30% by weight of the copolymer unit of acrylic acid, 0.2 to 10% by weight based on the copolymer unit derived from maleic anhydride; and at least one selected from ethylene and propylene methacrylate Copolymers formed from the following co-monomers: C14 alkyl methacrylate, alkyl acrylate, ethylene-methacrylic acid, ethylene-acrylic acid and ethylene-cis-butane dianhydride, which are non-limiting Examples include, for example, ethylene-butyl acrylate-glycidyl methacrylate methacrylate, which is derived from propylene Namely butyl acrylate copolymer units of from 2 to 30 wt%, and Yue group derived from the glycidyl acrylate oligomer ugly 146091.doc -13- 201100251 meter unit 1 to 15 wt. /. a blend with two or more of the above materials. The bonding layer suitable for use in the laminate film has a thickness of from 丨〇 to 4 μm, preferably from 40 to 200 μm. The bonding layer may have a solar module for packaging (generally polyethylene_vinyl acetate, polyethylene-methyl vinegar, polyethylene butyl acrylate, polyethylene-methacrylate, ionic polymer, polyurethane or polyethylene) The encapsulating layer of butyraldehyde) has good adhesion properties, good dielectric properties and anti-aging. The tie layer can contain several types of additives. Suitable non-limiting examples include light stabilizers, heat stabilizers, slip agents, light reflecting agents, and pigments. The content of the additive in the bonding layer is not particularly limited as long as the additive does not adversely affect the final adhesive property of the bonding layer or the laminated film, and the bonding layer can be used in the technical field. Non-limiting examples of the method of splicing include, for example, squeezing a suitable copolymer resin in a masking machine, applying an extrusion method to the surface of the substrate by extrusion using an extrusion molding die, or (iv) applying a coating agent In the embodiment, the bonding layer is bonded to the substrate without using an adhesive, and more particularly, the adhesive diluted with an organic solvent is not used. In one embodiment, the ethylene/methyl acrylate copolymer (containing 13 weights, having a flammability index of 9' manufactured by DuPont) is melted by a single screw, and the melted press is extruded in 2 thieves. , bonded to polyterephthalic acid 146091, doc -14· 201100251 ethylene diester (PET) substrate. The bonding layer may be a single layer material or a laminate of two or more layers of materials. For example, the bonding layer of the present invention may be 2 to 8 layers of a polymer material selected from the above ethylene copolymer materials, respectively. It is preferably a laminate of 2 to 6 layers, more preferably 2 to 3 layers. In one embodiment, the bonding layer is a three-layer laminate, one of which is a polymer sheet formed of a polymer material selected from the group consisting of ethylene-methacrylic acid Cl_4 alkyl ester copolymer, ethylene-acrylic acid. A Cm alkyl ester copolymer, an ethylene-methyl acrylate copolymer, an ethylene-acrylic acid copolymer and an ethylene-maleic anhydride copolymer. Further, the layer is a polymer sheet formed of a multicomponent polymer of ethylene and at least two monomers selected from the group consisting of Cm alkyl acrylate, Cm alkyl acrylate, methacrylic acid, acrylic acid and butylene. Anhydride. The other layer of the polymer sheet is a polymer sheet formed of ethylene and at least one co-monomer containing methyl methacrylate propylene acrylate-based multicomponent polymer: Ci·4 alkyl methacrylate 〇1_4 alkyl acrylate, methacrylic acid, acrylic acid and cis-succinic anhydride. The three-layer polymer sheets have about the same thickness, so that the final polymer sheet as the bonding layer has a thickness of 10 to 400 μm, preferably 40 to 2 μm. In another embodiment, the bonding layer is a two-layer laminate, one of which is a polymer sheet formed from a polymer material selected from the group consisting of ethylene-methacrylic acid c]·4 alkyl ester copolymer, ethylene-acrylic acid. a Ci_4 alkyl ester copolymer, an ethylene-indenyl acrylic copolymer, an ethylene-acrylic acid copolymer, an ethylene-maleic anhydride copolymer, a copolymer of ethylene and at least two monomers selected from the group consisting of: Acrylic acid (:1. 4 alkyl ester, ethylene _acrylic acid Ci4 alkyl ester, methyl propyl 146091.doc 15 201100251 olefinic acid, acrylic acid, and maleic anhydride; and ethylene and propylene methacrylate A propylene-based propylene glycol acrylate copolymer formed from at least one comonomer: Cw alkyl methacrylate, c, _4 alkyl acrylate, methacrylic acid, acrylic acid and maleic anhydride, and a blend of two or more of the above polymers. The other layer is a polymer sheet formed from a polymeric material selected from the group consisting of polyethylene, polypropylene, ethylene-propylene copolymer, ethylene-methacrylic acid. Ci*alkyl ester copolymer, ethylene bismuth acrylate A-4 alkyl ester copolymer, an ethylene-methacrylic acid copolymer, an ethylene acrylic acid copolymer, an ethylene-maleic anhydride copolymer, a copolymer of ethylene and at least two monomers selected from the group consisting of: Cw alkene propylene methacrylate acrylate C 1 _4 burnt, mercapto acrylic acid, propionic acid and cis-succinic anhydride; and bismuth from ethylene and at least one comon selected from the group consisting of A glycidyl acrylate-containing propyl acrylate copolymer formed from propylene acrylate: methacrylic acid (: 1-4 alkyl ester, acrylic acid (: 1-4 alkyl ester, methacrylic acid, propylene oxime and maleic anhydride) a blend of two or more of the above polymers. In another embodiment, the tie layer is a three layer laminate, one of which is a polymer sheet formed from a polymeric material selected from the group consisting of: Ethylene-mercaptoacrylic acid <^_4 alkyl ester copolymer, ethylene-acrylic acid C1_4 alkyl ester copolymer, ethylene-mercaptoacrylic acid copolymer, ethylene-acrylic acid copolymer, ethylene-maleic acid: copolymer, ethylene a mixture of at least two monomers selected from the group consisting of: methacryl Acid Ci.4 alkyl ester, acrylate, methacrylic acid, acrylic acid and cis-butadiene; and methacrylic acid propylene-acrylic acid from ethylene and at least one comonomer selected from the group consisting of形成 丙 146 146091.doc -16- 201100251 = acid propylene-propylene copolymer: thiol propylene ▲ ▲, acrylic burning 0, methacrylic acid, acrylic acid and maleic acid needle a blend of two or more of the above polymers. The other layer is a polymer sheet formed of a polymer material selected from the group consisting of polyethylene, polypropylene, ethylene-propylene copolymer t, Ethylene-methacrylic acid Ci-4 alkyl ester copolymer, ethylene-acrylic acid Cl_4 alkylene copolymer, ethylene-methacrylic acid copolymer, ethylene. Acrylic acid: ethylene, cis-butane dianhydride copolymer And a copolymer formed by the combination of B and ❹〃 from the following: 甲基 甲基 妇 Cu 、 丙 丙 丙 、 、 、 、 、 、 、 、 、 、 、 、 、 、 、 、 、 、 、 、 、 、 And maleic acid; the content of f formed from ethylene and methyl acrylate acid propylene vinegar having at least one comonomer selected from the group consisting of Glycidoxy-based acrylic copolymer stuffed: methacrylic acid C "4 alkyl acrylate, ^ alkyl ester, methacrylic acid, acrylic acid and maleic anhydride, and the two or more polymers of the blend. The other layer is a polymer sheet formed of a polymer material selected from the group consisting of polyethylene, polypropylene, ethylene-propylene copolymer, ethylene-mercaptoacrylic acid Cw alkane vinegar copolymer, ethylene-acrylic acid C!-4 An alkyl ester copolymer, an ethylene-methacrylic acid copolymer, an ethylene-acrylic acid copolymer, an ethylene butyl bromide copolymer, a copolymer of ethylene and at least two monomers selected from the group consisting of: a propyl acetoate Cw octoate, a Ci 4 acrylate, a methyl acrylate, an acrylic acid, and a cis-succinic anhydride; and a methacrylic acid ring having at least one comon selected from the group consisting of a propyl acrylate-containing propylene-acrylic acid copolymer formed by oxypropyl acrylate: Cw alkane methacrylate, Ci4 alkyl acrylate, methacrylic acid, acrylic acid and cis-succinic acid field, or the above A composition of two or more polymers. 146091.doc -17- 201100251 Polyethylene and polypropylene suitable for bonding layers include high density polyethylene, medium density polyethylene, low density polyethylene, linear low density polyethylene, metal aromatics - derived low density Polyethylene and polypropylene homopolymer. A plurality of laminated films having a bonding layer may be bonded to the substrate of the present invention by extrusion-coating using two or more extruders. 'In order to increase the bonding strength between the substrate and the bonding layer, the surface of the substrate may be a surface treated person. Suitable surface treatment methods are not limited and can be any conventional method in the art. For example, it may be corona treatment, flame treatment or primer treatment. Non-limiting examples of suitable primers include imines and amine primers. When the primer treatment is applied to the surface treatment of the surface of the substrate, the final thickness of the formed primer is not particularly limited and may be any common thickness in the art as long as the primer is bonded to the polyester substrate and the bonding layer. The intensity does not overlap into a negative impact. The thickness of the primer is generally less than 15 microns, suitably less than K2 microns, preferably less than m meters, more preferably less than 〇99 microns, most preferably less than 0.8 microns, most preferably less than 〇.5. Micron. For example, the thickness of the primer can be less than 0.45 micrometers, which is extremely high, and it is less than or equal to the thickness of the primer. She collapses or falls below one embodiment. The thickness of the primer is 0.01 to 0 99 micrometers, which is suitable for .01 to 0.8 microns, preferably 0.01 to 0.5 microns. The surface treatment method used by the priest is, for example, corona treatment or flame treatment, and the bonding layer is directly placed on the substrate. Directly placing the bonding layer on the substrate of the present invention means that no coating or layer is applied between the bonding layer and the substrate to improve the bonding strength between the bonding layers. 146091.doc -18· 201100251 The laminated film has high joint strength or peel strength between the substrate and the bonding layer. The joint strength between the two layers of the laminate film is higher than that of the joint strength between the substrate and the bonding layer which can be seen in the art, and the joint strength can be as high as 1 〇 Newton/cm according to the butt peel test result. Laminated films are particularly suitable for use in the preparation of backsheets for crystalline germanium solar modules, or front or backsheets of thin film solar modules. The backsheet or the frontsheet not only has good peel strength, but also avoids delamination between the joint layer and the ethylene-vinyl acetate brewing copolyester encapsulation layer, which is caused by the joint layer and ethylene-vinyl acetate 曰The high bonding strength between the copolymer encapsulating layers can effectively extend the life of the solar module. The invention is further illustrated by the following exemplified examples. EXAMPLES Test Method 1. Peel strength test between the substrate of the laminate film and the bonding layer. The laminated film was cut into a sample purlin having a width of 2.54 cm and a length of 1 cm, and the bonding layer and the substrate were respectively fixed to the upper clamp and the lower clamp of the tensile tester, and the peeling test was performed at a speed of 5 inches per minute. . 2. Peel strength test between the bonding layer and the ethylene-acetate copolymer package laminate film (having a bonding layer adjacent to the encapsulation layer), ethylene acetate vinegar copolymer encapsulation layer and sheet glass Stacked in the appropriate order and cross-linked for four (four) minutes at the operating temperature of UOt. Thereafter, the sample was cut into strips having a width of 2.54 cm and a length of 1 cm. Backsheet layer The ruthenium film and the package/glass layer were peeled off at a speed of 5 inches per minute, respectively, to the upper clamp 146091.doc -19- 201100251 fixed to the tensile meter. 3. Hygrothermal aging test of solar cell components The process for encapsulating solar cell components includes sorting and sorting solar cells, single-sided welding, serial welding, stacking, lamination, component testing, framing and cleaning. The hygrothermal aging test of the laminated solar cell element is typed in the climatic chamber vC4〇i8 (purchased by Vdtsch Industnetechnik GmbH, Germany), according to the crystal solar module, IEC 6丨2丨5第丨〇·丨3. The solar cell test piece was kept in a hot and humid environment for 1 hour (85 乞 and relative humidity). After that, the component was removed and the ethylene-vinyl acetate was peeled off. Copolymer encapsulation layer. Stripped B-vinyl acetate vinegar copolymer package I, tested by Huang Ehner, USA, Lambda 95G UV/Vis/NIR spectrometer (including 15 〇 Gong Chu integrating sphere) to test its yellowing index (yeii〇wing to ΔΥΙ): ' "x A 1- I 〇 where YG means not treated under moist heat conditions < G-vinyl acetate copolymer encapsulation layer after stripping 'with Lambda 950 UV umbrella,, ', The extinction value measured by Buguang/visible/near-infrared light and ancient spectroscopy. γ refers to the extinction, *, 950 measured after the peeling of the encapsulation layer of ethylene-acetic acid ethyl ester copolymer treated by the wet heat condition of Jingjing 1. UV/visible/near-infrared light Lambda means the placement of the package; ^ when the hot material is reduced to zero, ;: one, too _ pool has excellent == 4 _ solar cell output power test method 146091.doc -20- 201100251 solar cell output power using 3500SLP components Test system measurements (available from Spire Corporation, USA) compared to polycrystalline tantalum solar cells assembled from conventional front and backsheet materials. 5. Bonding strength between bonded layers of laminate films. The film was cut into strips having a width of 2.54 cm and a length of 10 cm, and the top layer and the bottom layer were respectively fixed to the upper clamp and the lower clamp of the tensile tester, and the peeling test was performed at a speed of 5 inches per minute. Comparative Example 1 In this example, the backsheet used was made of a laminate film having a PVF/PET/PVF construction, available from Isovolta Group. PVF is an abbreviation for polyvinylidene fluoride. By using the above method, it was measured. The peel strength between polyvinylidene fluoride and polyethylene terephthalate was measured to be 4 Newtons/cm. By using the above method, the laminate between the back sheet and the EVA encapsulant layer was measured. Stripping The measurement was measured to be 4.5 Newtons/cm. Q Preparation of Solar Modules The following components were stacked in the following order and laminated under vacuum in a vacuum to form a solar module: - purchased by Dongguan CSG Solar Glass Co., Ltd. 3 · 2 mm thick tempered glass; - EVA packaging film (500 micron, Ruifu brand EVA film for photovoltaic cells, R767, purchased by Ruiyang Photovoltaic Material Co_, Ltd.); - Polycrystalline germanium photovoltaic circuit (125x125χ〇) · 3 mm, 72 circuits in series); 146091.doc -21 - 201100251 -EV read film (10) micron, used to prepare photovoltaic cells (4) read EVA4 m > R767, ^Ruiyang Photovoltaic Material Co Ltd· purchased) And a back sheet made of the laminated film of Comparative Example 1 above. " The method, assembly solar cell output power was determined to be 175 watts. The yellowing index ΔΥΙ was determined to be 〇 6 by performing the wet heat aging test of the solar cell element using the above method. Example 1 A laminate film was prepared and tested for properties from I. du Pont de Nemours and Company, Wilmington's Delaware, USA ("DuPont") 25 μm thick ^^ Polyethylene film 'and The main surface joint of a 200 micron thick polyethylene terephthalate plate purchased from DuPont. The adhesive used was a 9:1 (w/w) mixture of pp525()/i5 phase polyurethane adhesive, purchased from Mitsubishi, Sakamoto. The adhesive layer is 12 microns thick. On the extrusion-coater manufactured by DaV1S Standard, Ep(10)in p_ 1050 (manufactured by Nippon Shokubai Co., Ltd.) was coated on the other main surface of the polyethylene terephthalate sheet as a 90.90 μm thick primer. . Thereafter, a layer of a vinyl acrylate copolymer (80% derived from an ethylene monomer) was applied at 29 Torr: extrusion onto a primed surface to a thickness of 75 μm to form a laminate film. By using the above method, the peel strength between the polyethylene terephthalate acid ethyl ester plate and the vinyl acrylate copolymer layer was measured to be 21 Newtons/cm. Compared with the peel strength of the conventional laminate film described in Comparative Example 1, J 4609]. doc • 22 - 201100251 The laminate film of the present invention was increased by four times. After 1,000 hours of accelerated moist heat aging under conditions of 85 ° C and 85% RH (relative humidity), the peel strength was measured to be 12 Newtons/cm. By using the above method, the peel strength between the ethylene-methacrylate copolymer layer and the ethylene-vinyl acetate copolymer package was determined to be 8 j Newtons/cm. Comparing the peel strength of the conventional laminate film (comparative example with the ethylene-vinyl acetate copolymer package), the peel strength between the laminate film of the present embodiment and the ethylene-vinyl acetate copolymer package was increased by about 16 times. Preparation of Solar Module The following components were stacked in the following order and laminated under vacuum by vacuum to form a solar module: 3_2 mm thick tempered glass purchased by Dongguan CSG Solar Glass Co., Ltd.; - EVA packaging film (500 micron, Ruifu brand 〇ΕνΑ film for the preparation of photovoltaic cells, R767, by Ruiyang photov〇ltaic Material c〇..

Ltd.購得); -多晶矽光伏電路^25“25“·3公釐,串聯Μ個電路); -EVA封裝薄膜(5〇〇微米,用以製備光伏電池之尺⑴化牌 EVA 薄膜’ R767,由 Ruiyang Photovoltaic Material Co., Ltd.購得); ’ -上述實施例1揭露之層壓薄膜,具有面對上述eva薄膜 之上述乙烯甲基丙烯酸酯共聚物。 藉由使用上述方法,組裝太陽能電池輸出功率經測定為 146091.doc -23· 201100251 177 瓦。 太陽能電池元件之濕熱老化測試 藉由使用上述方法進行太陽能電池元件濕熱老化測試, 黃化指數ΔΥΙ計算結果為0.1。 比較例2 如日本專利第JP2008-108947號之實施例1所述之pet, 與曰本專利第JP2〇08-108947號之實施例1所述之乙稀-甲基 丙烯酸醋共聚物,經熱壓層壓之後,測試兩者間之剝離強 度。初始剝離強度為1.5牛頓/公分。經加速濕熱老化1,〇〇〇 小時後,剝離強度低於0.7牛頓/公分。 比較例3 如曰本專利第JP2008-108947號之實施例1所述之ΡΕτ, 與曰本專利第JP2008-108947號之實施例1所述之乙稀_甲基 丙烯酸酯共聚物,以聚胺酯黏著劑(聚酯為主的聚胺酯基 質與二異氰酸異佛爾酮酯(IPDI)與二異氰酸苯二曱酯(XDI) 混合固化劑)接合。兩者間之初始剝離強度為7 · 5牛頓/公 分。經加速濕熱老化後,剝離強度低於〇·8牛頓/公分。 實施例2 製備層壓薄膜與測試其性質 購自杜邦之25微米厚之Tedlar™聚氟乙稀薄膜與亦講自 杜邦的200微米厚之聚對苯二甲酸乙二酯板的主要表面接 合。使用之黏著劑為PP5250/I5200聚胺酯黏著劑之9:1(重 量/重量)混合物’購自三菱,日本。黏著層為丨2微米厚。 由Davis Standard製造的擠出-塗佈機上,Epomin p_ 146091.doc -24- 201100251 1050(由日本觸媒株式會社製造)於聚對苯二曱酸乙二酯板 的另一主要表面塗佈作為0.50微米厚底漆。之後,含有共 聚物總重量之5 % (重量/重量)的二氧化鈦添加物之乙烯-甲 基丙烯酸酯共聚物(80%為源自乙烯單體)層於290°C擠出-塗佈於經底塗之表面,以形成厚度為75微米之層壓薄膜。 藉由使用上述方法,聚對苯二甲酸乙二酯板與乙烯-甲 基丙烯酸酯共聚物層之間的剝離強度經測定為20牛頓/公 分。以85°C與85%RH的條件進行經加速濕熱老化1,000小 時後,剝離強度經測定為12牛頓/公分。 藉由使用上述方法,乙稀-甲基丙烯酸醋共聚物層與乙 烯-乙酸乙烯酯共聚物封裝件之間的剝離強度經測定為80 牛頓/公分。 製備太陽能模組 下述元件為根據下述順序堆疊,於真空以熱壓進行層壓 以形成太陽能模組: -由 Dongguan CSG Solar Glass Co·, Ltd.購得 3.2公釐厚淬 火玻璃; -EVA封裝薄膜(500微米,用以製備光伏電池之Ruifu牌 EVA薄膜,R767,由 Ruiyang Photovoltaic Material Co., Ltd.購得); -多晶矽光伏電路(125x125x0.3公釐,串聯72個電路); -EVA封裝薄膜(500微米,用以製備光伏電池之Ruifu牌 EVA薄膜,R767,由 Ruiyang Photovoltaic Material Co., Ltd.購得);與 146091.doc -25 - 201100251 上述實施例2揭露之層壓薄膜,(且 守、(具有面對上述EVA薄膜 之上述乙稀-甲基丙烯酸酯共聚物)。 藉由使用上述方法 177 瓦。 、卫I太陽鲍電池輸出功率經測定為 太陽能電池元件之濕熱老化測試 池元件之濕熱老化測 藉由使用上述方法進行太陽能電 試,黃化指數ΔΥΙ計算結果為〇1。 實施例3 製備層壓薄膜與其性質測試 購自杜邦之25微米厚之TedlarTM聚氟乙烯薄膜與亦購自 :邦的200微米厚之聚對苯二甲酸乙二酯板的主要表面接 =。使用之黏著劑為PP525〇/I52〇〇聚胺酯黏著劑之9以重 量/重量)混合物,購自三菱,曰本。黏著層為12微米厚。 由Davis Standard製造的擠出-塗佈機上,Ep〇min p_ 1 〇5〇(由日本觸媒株式會社製造)於聚對苯二甲酸乙二酯板 另一主要表面塗佈作為〇·45微米厚底漆。之後,乙烯-順丁 烯紅酐共聚物(80 %重量/重量為源自乙烯單體)與含有共 聚物總重置之5%(重量/重量)的二氧化鈦添加物之乙烯-甲 土丙烯馱S曰(80%重量/重量為源自乙烯單體)之丨:9(重量/重 里)此合物,擠出_塗佈於底漆表面以形成厚度乃微 壓薄膜。 曰 藉由使用上述方法,聚對苯二甲酸乙二酯板與接合層之 1的剝離強度經測定為23牛頓/公分。以85°C與的 ^、件進订經加速濕熱老化1,000小時後’剝離強度經測定 14609] .d〇c -26- 201100251 為12牛頓/公分·。 藉由使用上述方法,接合層與乙烯-乙酸乙烯酯共聚物 封裝層之間的剝離強度經測定為80牛頓/公分。 製備太陽能模組 下述元件為根據下述順序堆疊,於真空以熱壓進行層壓 以形成太陽能模組· -由 Dongguan CSG Solar Glass Co·, Ltd.購得 3.2公釐厚淬 火玻璃; (% -EVA封裝薄膜(500微米,用以製備光伏電池之Ruifu牌 EVA薄膜,R767,由 Ruiyang Photovoltaic Material Co., Ltd.購得); -多晶矽光伏電路(125x125x0.3公釐,串聯72個電路); -EVA封裝薄膜(500微米,用以製備光伏電池之Ruifu牌 EVA薄膜,R767,由 Ruiyang Photovoltaic Material Co., Ltd.購得);與 q -上述實施例3揭露之層壓薄膜,具有面對上述EVA薄膜 之上述共聚物混合物。 藉由使用上述方法,組裝太陽能電池輸出功率經測定為 178 瓦。 太陽能電池元件之濕熱老化測試 藉由使用上述方法進行太陽能電池元件之濕熱老化測 試,黃化指數AYI計算結果為0.1。 實施例4 購自杜邦之25微米厚之Tedlar™聚氟乙烯薄膜與亦購自 146091.doc -27- 201100251 杜邦的200微米厚之聚對苯二甲酸乙二酯板的主要表面接 合。使用之黏著劑為PP5250/I52〇〇聚胺酯黏著劑之9:ι(重 莖/重ΐ )混合物’購自三菱,日本。黏著層為12微米厚。 由DaWs Standard製造的擠出-塗佈機上,Ep〇min ρ_ 1050(由日本觸媒株式會社製造)於聚對苯二甲酸乙二酯板 另一主要表面塗佈作為0.48微米厚底漆。之後,乙烯-丙烯 酸丁酯-甲基丙烯酸三聚物(三單體之重量比例為 88.5.7.5.4)層,擠出_塗佈於底漆表面以形成厚度75微米之 層壓薄膜。 藉由使用上述方法,聚對苯二曱酸乙二酯板與接合層間 剝離強度經測定為25牛頓/公分。以85t與85%rh的條件 進行、..二加速/愚熱老化丨,小時後,剝離強度經測定為1 2 牛頓/公分。 藉由使用上述方法,接合層與乙烯-乙酸乙烯酯共聚物 封裝層之間的剝離強度經測定為82牛頓/公分。 製備太陽能模組 下述元件為根據下述順序堆疊,於真空以熱壓進行層壓 以形成太陽能模組: -由0〇1^柽1^11匸36 8〇1&犷01&55(2〇.,1^(1.購得3.2公釐厚淬 火玻璃; _ EVA封裝薄膜(50〇微米,用以製備光伏電池之Ruifu牌 EVA/專膜 ’ r767 ’ 由 Ruiyang photovoltaic Material Co., Ltd.購得); -夕日日石夕光伏電路(125><125><〇.3公釐,串聯72個電路); 146091.doc 201100251 -EVA封裝薄膜(500微米,用以製備光伏電池之如而牌 EVA薄膜,R767,由 Ruiyang Ph〇t〇v〇haic MateHal c〇,Ltd. purchased; - polycrystalline germanium photovoltaic circuit ^ 25 "25" · 3 mm, one circuit in series); - EVA packaging film (5 μm, used to prepare photovoltaic cell ruler (1) chemical EVA film 'R767 , obtained by Ruiyang Photovoltaic Material Co., Ltd.; '- The laminate film disclosed in the above Example 1 has the above ethylene methacrylate copolymer facing the above eva film. By using the above method, the assembled solar cell output power was determined to be 146091.doc -23·201100251 177 watts. Humidity heat aging test of solar cell elements The solar cell element damp heat aging test was carried out by using the above method, and the yellowing index ΔΥΙ was calculated to be 0.1. Comparative Example 2, as described in Example 1 of JP-A-2008-108947, the ethylene-methacrylic acid vinegar copolymer described in Example 1 of JP-A No. 08-108947, which is subjected to heat. After lamination, the peel strength between the two was tested. The initial peel strength was 1.5 Newtons/cm. After accelerated damp heat aging 1, after 〇〇〇 hours, the peel strength was less than 0.7 Newtons/cm. Comparative Example 3 The ΡΕτ described in Example 1 of JP 2008-108947, and the ethylene methacrylate copolymer described in Example 1 of JP 2008-108947, adhered with polyurethane. The polyester (polyester-based polyurethane matrix is bonded to isophorone diisocyanate (IPDI) and phenyl diisocyanate (XDI) mixed curing agent). The initial peel strength between the two was 7 · 5 Newtons / cm. After accelerated damp heat aging, the peel strength is less than 〇·8 Newtons/cm. Example 2 Preparation of a laminate film and testing of its properties A 25 micron thick TedlarTM polyvinyl fluoride film available from DuPont was bonded to the main surface of a 200 micron thick polyethylene terephthalate sheet also known from DuPont. The 9:1 (weight/weight) mixture of the adhesive used as the PP5250/I5200 polyurethane adhesive was purchased from Mitsubishi, Japan. The adhesive layer is 丨 2 microns thick. On the extrusion-coating machine manufactured by Davis Standard, Epomin p_ 146091.doc -24- 201100251 1050 (manufactured by Nippon Shokubai Co., Ltd.) was coated on the other main surface of the polyethylene terephthalate plate. As a 0.50 micron thick primer. Thereafter, a layer of ethylene-methacrylate copolymer (80% of which is derived from ethylene monomer) containing 5% by weight (wt/wt) of the total weight of the copolymer is extruded and coated at 290 ° C. The surface of the primer was applied to form a laminate film having a thickness of 75 μm. By using the above method, the peel strength between the polyethylene terephthalate sheet and the ethylene-methacrylate copolymer layer was determined to be 20 N/cm. After accelerated heat aging for 1,000 hours at 85 ° C and 85% RH, the peel strength was measured to be 12 Newtons / cm. By using the above method, the peel strength between the ethylene-methacrylic acid vinegar copolymer layer and the ethylene-vinyl acetate copolymer package was determined to be 80 N/cm. Preparation of Solar Modules The following components were stacked according to the following sequence, and vacuum laminated by hot pressing to form a solar module: - 3.2 mm thick tempered glass purchased by Dongguan CSG Solar Glass Co., Ltd.; - EVA Package film (500 micron, Ruifu brand EVA film for photovoltaic cells, R767, available from Ruiyang Photovoltaic Material Co., Ltd.); - polycrystalline germanium photovoltaic circuit (125x125x0.3 mm, 72 circuits in series); EVA encapsulating film (500 micron, Ruifu brand EVA film for preparing photovoltaic cells, R767, available from Ruiyang Photovoltaic Material Co., Ltd.); and 146091.doc -25 - 201100251 laminated film disclosed in the above embodiment 2 (and shou, (having the above-mentioned ethylene-methacrylate copolymer facing the above EVA film). By using the above method 177 watts, the Wei I solar abalone battery output power is determined as the hygrothermal aging of the solar cell element The wet heat aging test of the test cell components was carried out by using the above method for solar electric test, and the yellowing index ΔΥΙ was calculated as 〇 1. Example 3 Preparation of laminated film and its properties The 25-micron thick TedlarTM polyvinyl fluoride film purchased from DuPont was tested with the main surface of a 200 micron thick polyethylene terephthalate board also purchased from: State. The adhesive used was PP525〇/I52〇. A 9 wt/wt mixture of urethane adhesive was purchased from Mitsubishi, pp. The adhesive layer is 12 microns thick. On an extrusion-coating machine manufactured by Davis Standard, Ep〇min p_ 1 〇5〇 (manufactured by Nippon Shokubai Co., Ltd.) was coated on the other main surface of the polyethylene terephthalate sheet as 〇·45. Micron thick primer. Thereafter, the ethylene-malerene anhydride copolymer (80% w/w is derived from the ethylene monomer) and the ethylene-methane propylene oxime containing 5% (w/w) of the total reset of the copolymer. S曰 (80% w/w from ethylene monomer) 丨: 9 (w/w) of this compound, extruded _ coated on the surface of the primer to form a film of micro-pressure.脱 By using the above method, the peel strength of the polyethylene terephthalate sheet and the bonding layer was measured to be 23 Newtons/cm. After the accelerated heat and humidity aging for 1,000 hours at 85 ° C and ^, the peel strength was measured 14609]. d〇c -26- 201100251 was 12 Newtons/cm. By using the above method, the peel strength between the bonding layer and the ethylene-vinyl acetate copolymer encapsulating layer was determined to be 80 N/cm. Preparation of Solar Modules The following components were stacked in the following order, laminated under vacuum by hot pressing to form a solar module. - 3.2 mm thick tempered glass purchased by Dongguan CSG Solar Glass Co., Ltd.; -EVA packaging film (500 micron, Ruifu brand EVA film for photovoltaic cells, R767, available from Ruiyang Photovoltaic Material Co., Ltd.); - polycrystalline germanium photovoltaic circuit (125x125x0.3 mm, 72 circuits in series) - EVA encapsulating film (500 micron, Ruifu brand EVA film for preparing photovoltaic cells, R767, available from Ruiyang Photovoltaic Material Co., Ltd.); and q - laminated film disclosed in the above embodiment 3, having a surface The above copolymer mixture of the above EVA film. By using the above method, the assembled solar cell output power was determined to be 178 W. The damp heat aging test of the solar cell element was carried out by using the above method for the damp heat aging test of the solar cell element, yellowing The index AYI was calculated to be 0.1. Example 4 A 25 micron thick TedlarTM polyvinyl fluoride film purchased from DuPont was also purchased from 146091.doc -27-2 01100251 DuPont's 200 μm thick polyethylene terephthalate board is bonded to the main surface. The adhesive used is a PP5250/I52 〇〇 polyurethane adhesive 9: ι (heavy stem / heavy ΐ) mixture purchased from Mitsubishi , Japan. The adhesive layer is 12 μm thick. On the extrusion-coating machine manufactured by DaWs Standard, Ep〇min ρ_ 1050 (manufactured by Nippon Shokubai Co., Ltd.) is another main component of polyethylene terephthalate board. The surface was coated as a 0.48 micron thick primer. Thereafter, a layer of ethylene-butyl acrylate-methacrylic acid terpolymer (the weight ratio of the three monomers was 88.5.7.5.4) was extrusion-coated on the surface of the primer. A laminate film having a thickness of 75 μm was formed. By using the above method, the peeling strength between the polyethylene terephthalate plate and the bonding layer was determined to be 25 Newtons/cm. Under the conditions of 85 t and 85% rh, After two hours of acceleration/stupid heat aging, the peel strength was measured to be 1 2 Newtons/cm. By using the above method, the peel strength between the bonding layer and the ethylene-vinyl acetate copolymer encapsulating layer was determined to be 82 Newtons. /cm. Preparation of solar modules The following components are roots Stacked in the following order, vacuum laminated by vacuum to form a solar module: - 0〇1^柽1^11匸36 8〇1&犷01&55(2〇.,1^(1. Get 3.2 mm thick tempered glass; _ EVA packaging film (50 〇 micron, Ruifu brand EVA / film for the preparation of photovoltaic cells ' r767 ' purchased by Ruiyang photovoltaic Material Co., Ltd.); - 夕日日石夕Photovoltaic circuit (125><125><3 mm, 72 circuits in series); 146091.doc 201100251 -EVA package film (500 micron, for the production of photovoltaic cells such as EVA film, R767, by Ruiyang Ph〇t〇v〇haic MateHal c〇,

Ltd.購得);與 -上述實施例4揭露之層壓薄膜,具有面對上述eva薄膜 之上述三聚物。 藉由使用上述方法,組裝太陽能電池輸出功率經測定為 175 瓦。 〇 〇 太陽能電池元件之濕熱老化測試 藉由使用上述方法進行太陽能電池元件之濕熱老化測 試’黃化指數ΔΥΙ計算結果為〇」。 實施例5 購自杜邦之25微米厚之制„™聚氟乙烯薄膜與亦購自 杜邦的200微米厚之聚對苯二甲酸乙二g旨板的主要表面接 ^。使用之黏著劑為卯525〇/152〇〇聚胺醋黏著劑之9:丨(重 里重里)犯口物,購自二菱,日本。黏著層為! 2微米厚。 由製造的擠出-塗佈機上,Epomin P_ 1〇5一〇(由日本觸媒株式會社製造)於聚對苯二甲酸乙二醋板 另一主要表面塗佈作為〇·48微米厚底漆。之後,乙烯-丙烯 酸丁s旨-甲基丙烯酸環氧丙酿三聚物(25%(重量/重幻為源 产自丙賴丁醋單體與12%(重量/重量)為源自甲基丙稀酸環 氧單體)層,擠出-塗佈於底漆表面以形成層壓薄膜。 糟由使用上述方沐 @ m ^ t f本一甲酸乙二酯板與接合層之 間的剝離強度經測定為26牛頓/公分。以饥與85%RH的 條件進行經加速_老化1,_小時後,剝離強度經測定 146091.doc •29· 201100251 為11牛頓/公分。 藉由使用上述方法,接合層與乙烯-乙酸乙烯酯共聚物 封裝件之間的剝離強度經測定為80牛頓/公分。 製備太陽能模組 下述元件為根據下述順序堆疊,於真空以熱壓進行層壓 以形成太陽能模組: -由 Dongguan CSG Solar Glass Co.,Ltd.購得 3.2公爱厚淬 火玻璃; -EVA封裝薄膜(500微米,用以製備光伏電池之Ruifu牌 EVA 薄膜,R767,由 Ruiyang Photovoltaic Material Co·, Ltd.購得); -多晶矽光伏電路(125x125x0.3公釐,串聯72個電路); -EVA封裝薄膜(500微米,用以製備光伏電池之Ruifu牌 EVA 薄膜,R767,由 Ruiyang Photovoltaic Material Co., Ltd.購得);與 -上述實施例5揭露之層壓薄膜,具有面對上述EVA薄膜 之上述三聚物。 藉由使用上述方法,組裝太陽能電池輸出功率經測定為 178 瓦。 太陽能電池元件之濕熱老化測試 藉由使用上述方法進行太陽能電池元件之濕熱老化測 試,黃化指數AYI計算結果為0.1。 實施例6 購自杜邦之25微米厚之Tedlar™聚氟乙烯薄膜與亦購自 146091.doc -30- 201100251 杜邦的200微米厚之聚對苯二甲酸乙二醋板的主要表面接 2。使用之黏著劑為卯5250/15200聚胺醋黏著劑之9:1(重 里/重里)混合物’購自三菱,日本。黏著層為⑵鼓米厚。 由Davis Standard製造的擠出-塗佈機上,Ep〇min p_ 1050(由日本觸媒株式會社製造)於聚對苯二曱酸乙二醋板 另一主要表面塗佈作為〇·5微米厚底漆。之後,乙烯_丙烯 酸甲酯-順丁烯二酸酐三聚物(2〇%(重量/重量)為源自丙烯 酸甲酯單體與0.3%(重量/重量)為源自順丁烯二酸酐單體) 層,擠出-塗佈於底漆表面以形成層壓薄膜。 藉由使用上述方法,聚對苯二甲酸乙二酯板與接合層之 間的剝離強度經測定為26牛頓/公分。以85°c與85%RH的 條件進行經加速濕熱老化L000小時後,剝離強度經測定 為11牛頓/公分。 藉由使用上述方法,接合層與乙烯-乙酸乙烯酯共聚物 封裝件之間的剝離強度測定為8〇牛頓/公分。 製備太陽能模組 下述元件為根據下述順序堆疊,於真空以熱壓進行層壓 以形成太陽能模組: -由 Dongguan CSG Solar Glass Co.,Ltd.購得 3.2公釐厚淬 火玻璃; -ΕνΑ封裝薄膜(50〇微米,用以製備光伏電池之Ruifu牌 EVA薄膜’ R767 ’ 由 Ruiyang Photovoltaic Material Co., Ltd.購得); -多晶石夕光伏電路(125x125x0.3公釐,串聯72個電路); 146091.doc -31- 201100251 -題封㈣膜(_微米,用以製備光伏電池Ruifu牌EVA 薄膜,R767,由 Ruiyang ph〇t〇v〇haic ⑽ 購得);與 -上述實施例6揭露之層壓薄膜,具有面對上述跳薄膜 之上述三聚物。 藉由使用上述方法’組裝太陽能電池輸出功率經測定為 178 瓦。 太陽能電池元件之濕熱老化測試 使用上述方法進行太陽能電池元件之濕熱老化測試,黃 化指數ΔΥΙ計算結果為。 實施例7 購自杜邦之200微米厚的聚對苯二甲酸乙二酯板之主要 表面以電暈處理。 匕由Davis Standard製造的擠出-塗佈機上,乙稀-丙稀酸甲 -曰丨貝丁烯—酸酐三聚物(2〇%(重量/重量)為源自丙烯酸甲 7單體與0.3%(重量/重量)為源自順丁稀二酸肝單體)層, /出塗佈於聚對苯二甲酸乙二酯板之經電暈處理表面以 形成層壓薄膜。 稭由使用上述方法,聚對苯二曱酸乙二酯板與接合層之 間的剝離強度經測定為12牛頓/公分。以85t與85%1^1的 條件進行經加速濕熱老化1〇〇〇小時後,剝離強度經測定 為6牛頓/公分。 、7由使用上述方法,接合層與乙烯_乙酸乙稀酯共聚物 封名件之間的剝離強度經測定為8〇牛頓/公分。 146091.doc 201100251 製備太陽能模組 下述元件為以下述順序堆疊,且於真空以熱壓進行層壓 以形成太陽能模組。 -由 Dongguan CSG Solar Glass Co_, Ltd.購得 3.2公釐厚淬 火玻璃;The laminate film disclosed in the above Example 4 has the above-mentioned terpolymer facing the above eva film. By using the above method, the assembled solar cell output power was determined to be 175 watts. 〇 湿 Humidity heat aging test of solar cell elements The hygrothermal aging test of the solar cell element was carried out by the above method. The calculation result of the yellowing index ΔΥΙ was 〇”. Example 5 A 25 micron thick PTFE polyfluoroethylene film purchased from DuPont was bonded to the main surface of a 200 micron thick polyethylene terephthalate plate also purchased from DuPont. The adhesive used was 卯. 525〇/152〇〇 Polyamine vinegar adhesive 9: 丨 (重重重里) murder, purchased from Mitsubishi, Japan. Adhesive layer is! 2 microns thick. Made by extrusion-coating machine, Epomin P_1〇5〇(manufactured by Nippon Shokubai Co., Ltd.) was coated on the other main surface of polyethylene terephthalate board as a 〇·48 μm thick primer. After that, ethylene-acrylic acid butyl s-- Acrylic propylene-acrylic terpolymer (25% (weight/reciprocity is derived from propylene acetonitrile monomer and 12% (w/w) is derived from methyl acrylate epoxy monomer) layer, Extrusion-coating on the surface of the primer to form a laminate film. The peel strength between the board and the bonding layer was determined to be 26 Newtons/cm by using the above-mentioned square m@m^tf. After accelerated with aging conditions of 85% RH, after 1 hour, the peel strength was determined to be 146091.doc •29·201100251 was 11 Newtons/cm. In the above method, the peel strength between the bonding layer and the ethylene-vinyl acetate copolymer package was determined to be 80 N/cm. Preparation of Solar Module The following elements were stacked according to the following procedure, and laminated under vacuum by hot pressing. To form a solar module: - 3.2 Å thick tempered glass purchased by Dongguan CSG Solar Glass Co., Ltd.; - EVA packaging film (500 micron, Ruifu EVA film for photovoltaic cells, R767, by Ruiyang Photovoltaic Material Co·, Ltd. purchased; - polycrystalline germanium photovoltaic circuit (125x125x0.3 mm, 72 circuits in series); -EVA package film (500 micron, Ruifu EVA film for photovoltaic cells, R767, by Ruiyang Photovoltaic Material Co., Ltd. purchased; and the laminated film disclosed in the above Example 5, having the above-mentioned terpolymer facing the above EVA film. By using the above method, the assembled solar cell output power was determined to be 178. The heat and humidity aging test of the solar cell element is carried out by using the above method for the damp heat aging test of the solar cell element, and the yellowing index AYI is calculated. 0.1. Example 6 A 25 micron thick TedlarTM polyvinyl fluoride film purchased from DuPont and a major surface of a 200 micron thick polyethylene terephthalate plate also available from 146091.doc -30- 201100251 DuPont 2. The adhesive used was a 9:1 (Heavy/Heavy) mixture of 卯5250/15200 Polyurethane Adhesives, purchased from Mitsubishi, Japan. The adhesive layer is (2) drums thick. On an extrusion-coating machine manufactured by Davis Standard, Ep〇min p_ 1050 (manufactured by Nippon Shokubai Co., Ltd.) was coated on the other main surface of polyethylene terephthalate plate as a 〇·5 μm thick. Primer. Thereafter, ethylene-methyl acrylate-maleic anhydride trimer (2% by weight (weight/weight) is derived from methyl acrylate monomer and 0.3% (w/w) is derived from maleic anhydride single The layer is extruded-coated onto the surface of the primer to form a laminate film. By using the above method, the peel strength between the polyethylene terephthalate sheet and the bonding layer was measured to be 26 N/cm. After accelerated hythermal heat aging for 10,000 hours at 85 ° C and 85% RH, the peel strength was measured to be 11 Newtons/cm. The peel strength between the bonding layer and the ethylene-vinyl acetate copolymer package was determined to be 8 Newtons/cm by using the above method. Preparation of Solar Modules The following components were stacked in the following order, and vacuum laminated by hot pressing to form a solar module: - 3.2 mm thick tempered glass purchased by Dongguan CSG Solar Glass Co., Ltd.; - ΕνΑ Package film (50μm, Ruifu EVA film for PV cells 'R767' purchased by Ruiyang Photovoltaic Material Co., Ltd.); - Polycrystalline lithography circuit (125x125x0.3 mm, 72 in series) Circuit); 146091.doc -31- 201100251 - Title (four) film (_micron, used to prepare photovoltaic cell Ruifu brand EVA film, R767, purchased by Ruiyang ph〇t〇v〇haic (10)); and - the above embodiment The disclosed laminate film has the above-mentioned terpolymer facing the above-mentioned jump film. The assembled solar cell output power was determined to be 178 watts by using the above method. Humidity heat aging test of solar cell elements The wet heat aging test of solar cell elements was carried out by the above method, and the result of the yellowing index ΔΥΙ was calculated. Example 7 The main surface of a 200 micron thick polyethylene terephthalate board purchased from DuPont was treated with corona.乙 On the extrusion-coating machine manufactured by Davis Standard, ethylene-acrylic acid-mu-bee butene-anhydride terpolymer (2% by weight/weight) is derived from acrylic 7 monomer and 0.3% (w/w) is a layer derived from cis-buthanic acid liver monomer, and is applied to a corona-treated surface of a polyethylene terephthalate sheet to form a laminate film. Using the above method, the peel strength between the polyethylene terephthalate plate and the bonding layer was measured to be 12 Newtons/cm. The peeling strength was measured to be 6 Newtons/cm after accelerated damp heat aging for 1 hour at 85t and 85%. 7, by using the above method, the peel strength between the joint layer and the ethylene-vinyl acetate copolymer seal was measured to be 8 Newtons/cm. 146091.doc 201100251 Preparation of Solar Modules The following components were stacked in the following order and laminated under vacuum with a vacuum to form a solar module. - 3.2 mm thick tempered glass purchased by Dongguan CSG Solar Glass Co_, Ltd.;

-EVA封裝薄膜(5〇〇微米,用以製備光伏電池之尺以化牌 EVA薄膜,R767,由 Ruiyang Photovoltaic Material Co., Ltd.購得); _多晶矽光伏電路(125x125x0.3公釐,串聯72個電路); -EVA封裝薄膜(5〇〇微米,用以製備光伏電池之尺以化牌 EVA 薄祺,R767 ’ 由 Ruiyang Photovoltaic Material Co·, Ltd.購得);與 -上述實施例7揭露之層壓薄膜,具有面對上述EVA薄膜 之上述三聚物。 藉由使用上述方法,組裝太陽能電池輸出功率經測定為 175 瓦。 太陽能電池元件之濕熱老化測試 藉由使用上述方法進行太陽能電池元件之濕熱老化測 試’黃化指數ΔΥΙ計算結果為〇.1。 實施例8 睛自枝邦之25微米厚之TedlarTM聚氟乙烯薄膜與亦購自 杜邦的2〇〇微米厚之聚對苯二甲酸乙二酯板的主要表面接 合。使用之黏著劑為PP5250/I5200聚胺酯黏著劑之9:1(重 里/重置)視合物’購自三菱,日本。黏著層為12微米厚。 146091.doc •33· 201100251 由Davis Standard製造的擠出-塗佈機上,Ep〇min p_ 1〇5〇(由曰本觸媒株式會社製造)於聚對苯二曱酸乙二酯板 另—主要表面塗佈作為〇.5〇微米厚底漆。之後,兩乙烯共 聚物層擠出-塗佈於底漆表面以形成層壓薄膜:一層為乙 烯丙烯酸甲酯共聚物(2〇%(重量/重量)為源自丙烯酸甲酯 單體),另一層為含有5。/。二氧化鈦與丨0/〇二氧化石夕之乙烯_ 丙烯酸甲酯共聚物(6%(重量/重量)為源自丙烯酸曱酯單 體)。 藉由使用上述方法,接合層與聚對苯二甲酸乙二酯板之 間的剝離強度經測定為22牛頓/公分。以85。〇與85%RH的 條件進行經加速濕熱老化1,〇〇〇小時後,剝離強度經測定 為18牛頓/公分。 藉由使用上述方法,接合層與乙烯-乙酸乙烯酯共聚物 封裝件之間的剝離強度經測定為48牛頓/公分。 製備太陽能模組 下述元件為以下述順序堆疊,且於真空以熱壓進行層壓 以形成太陽能模組: -由0〇1^§\^]1€30 8〇^〇1383(3〇.,1^(1.購得3.2公釐厚淬 火玻璃; -EVA封裝薄膜(50〇微米,用以製備光伏電池之Ruifu牌 EVA薄膜 ’ R767,由 Ruiyang Photovoltaic Material Co.,-EVA encapsulating film (5 〇〇 micron, used to make photovoltaic cell ruler to make EVA film, R767, available from Ruiyang Photovoltaic Material Co., Ltd.); _ polycrystalline 矽 photovoltaic circuit (125x125x0.3 mm, series 72 circuits); - EVA package film (5 〇〇 micrometer for the preparation of photovoltaic cell ruler to make EVA thin enamel, R767 'purchased by Ruiyang Photovoltaic Material Co., Ltd.); and - above embodiment 7 The disclosed laminate film has the above terpolymer facing the above EVA film. By using the above method, the assembled solar cell output power was determined to be 175 watts. The damp heat aging test of the solar cell element The hygrothermal aging test of the solar cell element was carried out by using the above method. The calculation result of the yellowing index ΔΥΙ was 〇.1. Example 8 A 25 micron thick TedlarTM polyvinyl fluoride film from Aibang was bonded to the major surface of a 2 inch thick polyethylene terephthalate sheet also available from DuPont. The adhesive used was a 9:1 (gravity/reset) visor of PP5250/I5200 polyurethane adhesive, which was purchased from Mitsubishi, Japan. The adhesive layer is 12 microns thick. 146091.doc •33· 201100251 On an extrusion-coating machine manufactured by Davis Standard, Ep〇min p_ 1〇5〇 (manufactured by Sakamoto Co., Ltd.) on polyethylene terephthalate plate - The main surface is coated as a 〇.5 〇 micron thick primer. Thereafter, the two ethylene copolymer layers are extruded-coated on the surface of the primer to form a laminate film: one layer is an ethylene methyl acrylate copolymer (2% by weight (weight/weight) is derived from methyl acrylate monomer), and One layer contains 5. /. Titanium dioxide and 丨0/〇2 SiO2 ethylene methacrylate copolymer (6% (weight/weight) derived from decyl acrylate monomer). By using the above method, the peel strength between the bonding layer and the polyethylene terephthalate sheet was determined to be 22 Newtons/cm. Take 85. The accelerated heat and humidity aging was carried out under conditions of 85% RH, and after a few hours, the peel strength was measured to be 18 Newtons/cm. By using the above method, the peel strength between the bonding layer and the ethylene-vinyl acetate copolymer package was determined to be 48 N/cm. Preparation of the solar module The following components are stacked in the following order, and laminated under vacuum with a vacuum to form a solar module: - 0 〇 1 ^ § \ ^] 1 € 30 8 〇 ^ 〇 1383 (3 〇. , 1 ^ (1. purchased 3.2 mm thick tempered glass; - EVA packaging film (50 〇 micro, used to prepare photovoltaic cells of Ruifu EVA film 'R767, by Ruiyang Photovoltaic Material Co.,

Ltd.購得); -多晶矽光伏電路(125x 125x0.3公釐’串聯72個電路); -EVA封裝薄膜(5〇〇微米,用以製備光伏電池之Ruifu牌 146091.doc -34- 201100251 EVA 薄膜,R767,由 Ruiyang Photovoltaic Material Co., Ltd.購得);與 -上述實施例8揭露之層壓薄膜,具有面對上述EVA薄膜 之上述共聚物。 藉由使用上述方法,組裝太陽能電池輸出功率經測定為 178 瓦。 太陽能電池元件之濕熱老化測試 藉由使用上述方法進行太陽能電池元件之濕熱老化測 試,黃化指數ΔΥΙ計算結果為0.1。 由上述測試結果可觀察到本發明之層壓薄膜於其薄膜層 間具有改良的接合強度,且因而可抵抗脫層。當本發明之 層壓薄膜用於製造太陽能模組背板,背板與封裝層之間具 有改良的接合強度。結果為使用本發明層壓薄膜作為背板 之太陽能模組不但能延長使用壽命,也能具有改良的阻障 性質,以避免氧氣與濕氣穿透進入全部太陽能模組,因而 可得到相當好效果。 146091.doc 35-Ltd. purchased; - polycrystalline germanium photovoltaic circuit (125x 125x0.3 mm 'series 72 circuits); -EVA package film (5 μm, used to prepare photovoltaic cells Ruifu brand 146091.doc -34- 201100251 EVA A film, R767, available from Ruiyang Photovoltaic Material Co., Ltd.; and a laminated film disclosed in the above Example 8, having the above-mentioned copolymer facing the above EVA film. By using the above method, the assembled solar cell output was measured to be 178 watts. Humidity heat aging test of solar cell elements The wet aging test of solar cell elements was carried out by using the above method, and the yellowing index ΔΥΙ was calculated to be 0.1. From the above test results, it was observed that the laminate film of the present invention has improved joint strength between its film layers and thus is resistant to delamination. When the laminate film of the present invention is used to manufacture a solar module backsheet, there is improved joint strength between the backsheet and the encapsulation layer. As a result, the solar module using the laminated film of the present invention as a backing plate can not only prolong the service life, but also has an improved barrier property to prevent oxygen and moisture from penetrating into all the solar modules, thereby obtaining quite good effects. . 146091.doc 35-

Claims (1)

201100251 七、申請專利範圍: L 一種層壓薄膜,其包含· 含ΐ二Γ第—表面與一第二表面之聚醋基材,其包 二:逃所成組群之聚合物:聚笨二甲酸Μ二 ^奈二甲社2-6貌二酿,與其混合物或捧合物; Ο一於該聚8旨基材之第—表面上之黏著層; Ο201100251 VII. Patent application scope: L A laminated film comprising: a polyester substrate comprising a surface of the second surface and a second surface, the package 2: a polymer that escapes into a group: a poly 2 Μ Μ 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 二 (c)一於該聚醋基材之第二表面上之底漆層,其中該底 漆層厚度小於0.99微米; ()於為底漆層上之接合層,其中該接合層包含乙稀 :選自下述所成組群之一種或多種單體之共聚物:丙稀 1 4、元酉曰f基丙烯酸c&quot;烷酯、甲基丙烯酸、曱基丙 烯酸環氧丙酷與順丁稀二酸野;與 (e)於亥黏著層上之保護層,包含引張彈性模數大於 150 Kpsi之氟聚合物。 2.如申咕專利範圍第丨項所述之層壓薄膜,其中該聚酯基 材更包含金屬、金屬氧化物或非金屬氧化物之塗層。 3·如申明專利範圍第丨項所述之層壓薄膜,其中該苯二甲 酸C2.6烷二酯係選自下述所成組群:聚對苯二曱酸乙二 S曰、聚對苯二甲酸丙二酯、聚對苯二甲酸丁二酯、聚對 苯二甲酸己二酯、聚鄰苯二甲酸乙二酯、聚鄰苯二曱酸 丙一酉曰 '聚鄰苯二甲酸丁二酯與聚鄰苯二甲酸已二酯, 且該聚萘二甲酸C2·6烷二酯係選自下述所成組群〔聚萘 二甲酸乙二酯、聚萘二甲酸丙二酯與聚萘二甲酸丁二 酉旨。 146091.doc 201100251 4·如申請專利範圍第丨項所述之声 合物係選自下述所 一…專膜,其中該含氟聚 他非氟化、部份氣稀聚合物、氟乙歸與其 稀聚合物,,偏二氣r掄偽甘 /、聚物、偏二氟乙 化單體之共聚物.畜- 。卩知鼠化或全氟 物’虱二氟乙烯聚合物、 他非氟化、部份氟化或全氟化單體之乙稀與其 聚合物、四氣乙烯*甘π t /、忒物、四氟乙烯 體之共聚物。 知规化或全氟化單 5. 如申請專利範圍第4項之層壓薄膜 化、部份氣化或全氣化單體係選自下述非氣 π ^ r通所成組群:r 、、丙、、軋乙烯、二氟乙烯、偏二氟乙烯、氯三氟乙 烯、六款丙埽、四氟乙稀、全氣燒氧基乙 丙烯。 王既 6. 如申請專利範圍第i項所述之層壓薄臈,其中該聚醋基 材包含: &amp; (a) 包括一選自下述組群所成共聚物之層:苯二甲酸 CM烷二酯、聚萘二甲酸CM烷二酯與其混合物或摻合 物;與 (b) 包括一聚氟乙烯或聚偏二氟乙烯之層。 7·如申請專利範圍第1項所述之層壓薄膜,其中該接合層 包括一由乙烯與選自下述所成組群之一或多種單體之共 聚物:曱基丙烯酸甲酯、丙烯酸甲酯、曱基丙歸酸乙 酉曰、丙酸乙酷、甲基丙細酸丙醋、丙烤酸丙醋、甲美 丙烯酸丁酯、丙烯酸丁酯、甲基丙烯酸環氧丙酯與順丁 146091.doc 201100251 烯二酸酐。 8. 如申請專利範圍第7項所述之層壓薄膜’其中以該共聚 物之總重量為基準’該乙烯為5〇至99重量%。 9. 如申請專利範圍第丨項所述之層壓薄膜,其中該接合層 之共聚物係選自下述所成組群:乙烯_丙烯酸甲酯-曱基 丙烯酸三聚物、乙烯-丙烯酸丁酯_甲基丙烯酸三聚物、 乙烯-甲基丙烯酸丙酯·丙烯酸三聚物、乙烯-丙烯酸丁 酯-甲基丙稀酸環氧丙酯三聚物與乙烯_丙烯酸曱酯-順丁 烯二酸酐三聚物。 10.如申請專利範圍第9項所述之層壓薄膜,其中該共聚物 為乙烯-丙烯酸丁酯—曱基丙烯酸環氧丙酯三聚物,且以 該三聚物之重量為基準,丙烯酸丁酯為2至30重量%,甲 基丙烯酸環氧丙酯為丨至15重量%。 11.如申請專利範圍第丨項所述之層壓薄膜 具有10至400微米厚度。(c) a primer layer on the second surface of the polyester substrate, wherein the primer layer has a thickness of less than 0.99 microns; () is a bonding layer on the primer layer, wherein the bonding layer comprises ethylene: a copolymer of one or more monomers selected from the group consisting of: propylene 1, 4, fluorenyl acrylate, methacrylic acid, methacrylic acid, propylene acrylate, and cis-butyl Acid field; and (e) a protective layer on the adhesion layer of the hai, comprising a fluoropolymer having an elastic modulus greater than 150 Kpsi. 2. The laminate film of claim 3, wherein the polyester substrate further comprises a coating of a metal, a metal oxide or a non-metal oxide. 3. The laminate film according to the invention of claim 2, wherein the C2.6 alkyl diester is selected from the group consisting of: polyethylene terephthalate, polyethylene terephthalate, polypair Propylene phthalate, polybutylene terephthalate, poly(ethylene terephthalate), polyethylene phthalate, poly(phthalic acid) Butadiene ester and poly(phthalic acid) hexaester, and the poly(naphthalene dicarboxylate) C2·6 alkyl diester is selected from the group consisting of polyethylene naphthalate and polyethylene naphthalate. With the use of poly(naphthalene dicarboxylate). 146091.doc 201100251 4· The composition of the invention as described in the scope of claim 2 is selected from the group consisting of the following film, wherein the fluorine-containing poly-non-fluorinated, partially gas-soluble polymer, fluorine-containing And its dilute polymer, a copolymer of a partial gas, a rhodium, a polyglycol, a polymer, and a difluorinated monomer. Know the rat or perfluorinated 'fluorene difluoroethylene polymer, its non-fluorinated, partially fluorinated or perfluorinated monomer of ethylene and its polymer, tetraethylene ethylene * 甘 π /, sputum, a copolymer of tetrafluoroethylene. Oriented or perfluorinated single 5. The laminated thinned, partially gasified or fully vaporized single system according to item 4 of the scope of the patent application is selected from the group consisting of the following non-gas π ^ r pass groups: r , , C,, ethylene, difluoroethylene, vinylidene fluoride, chlorotrifluoroethylene, six propylene, tetrafluoroethylene, total gas oxyethylene propylene. The laminated enamel according to claim i, wherein the polyester substrate comprises: &amp; (a) comprising a layer of a copolymer selected from the group consisting of: phthalic acid a CM alkyl diester, a poly naphthalene dicarboxylic acid CM alkyl diester, a mixture or blend thereof; and (b) a layer comprising a polyvinyl fluoride or polyvinylidene fluoride. The laminate film according to claim 1, wherein the bonding layer comprises a copolymer of ethylene and one or more monomers selected from the group consisting of methyl methacrylate and acrylic acid. Methyl ester, mercaptopropionate, ethyl propionate, ethyl propyl acrylate, propyl acrylate, butyl acrylate, butyl acrylate, butyl methacrylate and cis-butyl 146091.doc 201100251 Adipic anhydride. 8. The laminate film of claim 7, wherein the ethylene is from 5 to 99% by weight based on the total weight of the copolymer. 9. The laminate film of claim 2, wherein the copolymer of the bonding layer is selected from the group consisting of ethylene methyl acrylate-mercapto acrylate terpolymer, ethylene butyl acrylate Ester_methacrylic acid terpolymer, ethylene-propyl methacrylate-acrylic acid terpolymer, ethylene-butyl acrylate-methyl propylene glycol propyl acrylate terpolymer and ethylene methacrylate-butylene Diacid anhydride trimer. 10. The laminate film of claim 9, wherein the copolymer is ethylene-butyl acrylate-glycidyl methacrylate terpolymer, and based on the weight of the terpolymer, acrylic acid The butyl ester is 2 to 30% by weight, and the glycidyl methacrylate is 丨 to 15% by weight. 11. The laminate film of claim 3, having a thickness of 10 to 400 microns. 12·如申請專利範圍第旧所述之層壓薄m該接合 為擠出-塗佈於該基材。 ★申印專利範圍第丨項所述之層壓薄膜,其中該接合 係—單層之乙稀與選自下述所成組群之一或多種單體· =聚物:丙烯酸Cl.4炫自旨、甲基丙烯酸Ci4g|、甲基丙) s文甲基丙烯酸環氧丙酯與順丁烯二酸酐。 14·如申請專利範圍第!項所述之層㈣膜,其中該接合3 =有2至8層之層壓物,其中該層壓物之各層為乙稀, ^下逑所成組群之一種或多種單體之共聚物:丙稀靡 I46091.doc 201100251 C 1 _ 4烧S旨、曱基丙嫌酿P w T岙那酼Ch烷酯、曱基丙烯酸、曱基丙烯 酸環氧丙酯、與順丁烯二酸酐。 15. 16. 17. 18. 如申„月專利範圍第!項所述之層壓薄膜,其中該接合層 更包含選自下述聚合物材料所形成之一或多種聚合物 n乙烯 '聚㈣ '乙烯_丙稀共聚物、乙稀_甲基丙 晞酸h以旨共聚物;乙歸_甲基丙烯酸共聚物;乙稀-順 丁稀酸酐共聚物;衍生自乙稀乙浠與選自下述之至少 兩種單體之共伞物.甲基丙烯酸烷酯、甲基丙烯 酸,丁浠二酸軒;由乙埽與具有選自下述之至少一 種共早體之曱基丙嫌酸提:g 歸駿衣乳丙酯所形成之含有曱基丙烯 酸環氧丙酯共聚物:甲A二&amp;私 甲基丙烯酸C!_4烷酯、曱基丙烯酸 與順丁烯二酸酐;與其摻合物, 其中該聚乙烯選自高密度聚乙烯、中密度聚乙烯、低密 度聚乙稀、直鏈低密度聚乙烯、金屬芳香類-衍生低密度 聚乙烯且該聚丙烯為聚丙烯均聚物。 如申請專利範圍第i項所述之層壓薄膜,其中該底漆層 包括一亞胺型或胺型底漆。 如申請專利範圍第i項所述之層壓薄膜,其中該接合層 包括聚胺酯。 一種太陽能電池模組,复白人丨s由 , ,、匕S順序由前方面對太陽側至 背-非面對太陽側的位置為⑷一前板,⑻以一聚合材料 封裝之-或多種太陽能電池,與⑷―背板,其中該前板 與月板之一或兩者為由申績直刹孟々闻&amp; 1 = 1两甲„月寻利|已圍第I項所述之層壓 薄膜所製成。 I4609l.doc 201100251 19 20. 21.G 22. 23.Ο 如:請專利範圍第18項所述之太陽能電池模組,其中該 ,陽能電池為以乙烯_乙酸乙烯醋共聚物封裝,且 背板為由申請專利範圍第1項所述之層壓薄膜所製成。^ 如申請專利範圍第18項所述之太陽能電池模組,其中該 太陽此电池為選自單晶矽太陽能電池、多晶矽太陽能電 池與奈米-石夕太陽能電池。 一種薄膜太陽能電池模組,其包含: 0)置於一玻璃板、聚合物板或不鏽鋼板上之薄膜太陽 能電池; (b) —層壓於該薄膜太陽能電池上之聚合性封裝件;與 (c) 層屋於該封裝件之背板或前板,其中該背板或前 板為由申請專利範圍第1項所述之層壓薄膜所製成。 如申請專利範圍第21項所述之薄膜太陽能電池模組,其 中該聚合性封裝件包括乙烯-乙酸乙烯酯共聚物。 如申請專利範圍第22項所述之薄膜太陽能電池模組,其 中該薄膜太陽能電池係選自非晶矽薄膜太陽能電池、碲 化編薄膜太陽能電池與銅銦鎵硒薄膜太陽能電池。 146091.doc 201100251 四、指定代表圖: (一) 本案指定代表圖為:(無) (二) 本代表圖之元件符號簡單說明: 五、本案若有化學式時,請揭示最能顯示發明特徵的化學式: (無) 146091.doc12. The laminate as described in the scope of the patent application is extruded to be applied to the substrate. The laminated film according to the item of the invention, wherein the bonding system is a single layer of ethylene and one or more monomers selected from the group consisting of: acrylic acid Cl. Self-purpose, methacrylic acid Ci4g|, methyl propyl) s methacrylate propyl methacrylate and maleic anhydride. 14·If you apply for a patent scope! The layer (four) film of the item, wherein the joint 3 = a laminate having 2 to 8 layers, wherein each layer of the laminate is ethylene, a copolymer of one or more monomers of the group of the lower jaw : Acetone 460 I46091.doc 201100251 C 1 _ 4 S S, 曱 丙 嫌 嫌 P P P P P 酼 酼 酼 酼 酼 酼 酼 酼 酼 酼 酼 酼 酼 酼 酼 酼 酼 Ch Ch Ch Ch Ch Ch Ch Ch Ch Ch Ch Ch Ch Ch Ch Ch Ch Ch Ch Ch Ch Ch Ch Ch Ch Ch Ch Ch Ch Ch Ch Ch 15. The laminated film of claim </ RTI> wherein the bonding layer further comprises one or more polymers selected from the group consisting of polymer n-ethylene (poly) 'ethylene-propylene copolymer, ethylene_methylpropionic acid h to copolymer; B-methacrylic acid copolymer; ethylene-cis-butyl anhydride copolymer; derived from ethyl acetophenone and selected from a common umbrella of at least two monomers of the following: alkyl methacrylate, methacrylic acid, butyl phthalate; acetaminophen and decanoic acid having at least one co-early substance selected from the group consisting of提: g 归 propyl acrylate containing methacrylic acid glycidyl acrylate copolymer: A A &amp; methacrylic acid C! 4 alkyl ester, methacrylic acid and maleic anhydride; a composition, wherein the polyethylene is selected from the group consisting of high density polyethylene, medium density polyethylene, low density polyethylene, linear low density polyethylene, metal aromatic-derived low density polyethylene, and the polypropylene is polypropylene homopolymer The laminated film of claim i, wherein the primer layer comprises an imine A laminate film according to the invention of claim 1, wherein the bonding layer comprises a polyurethane. A solar cell module, the white 丨s by, ,, 匕S sequentially from the front facing the sun side The position to the back-non-facing sun side is (4) a front plate, (8) encapsulated in a polymeric material - or a plurality of solar cells, and (4) - a back plate, wherein one or both of the front plate and the moon plate are 々孟々闻&amp; 1 = 1 two „月寻利| has been made of the laminated film described in item I. I4609l.doc 201100251 19 20. 21.G 22. 23. The solar cell module according to claim 18, wherein the solar cell is encapsulated with ethylene-vinyl acetate copolymer and the back The board is made of the laminated film described in claim 1 of the patent application. The solar cell module according to claim 18, wherein the solar cell is selected from the group consisting of a single crystal germanium solar cell, a polycrystalline germanium solar cell, and a nano-stone solar cell. A thin film solar cell module comprising: 0) a thin film solar cell placed on a glass plate, a polymer plate or a stainless steel plate; (b) a polymerizable package laminated on the thin film solar cell; c) The laminate is formed on the back sheet or the front panel of the package, wherein the back sheet or the front sheet is made of the laminated film described in claim 1 of the patent application. The thin film solar cell module of claim 21, wherein the polymerizable package comprises an ethylene-vinyl acetate copolymer. The thin film solar cell module according to claim 22, wherein the thin film solar cell is selected from the group consisting of an amorphous germanium thin film solar cell, a germanium braided thin film solar cell, and a copper indium gallium selenide thin film solar cell. 146091.doc 201100251 IV. Designated representative map: (1) The representative representative of the case is: (none) (2) The symbol of the symbol of the representative figure is simple: 5. If there is a chemical formula in this case, please reveal the best indication of the characteristics of the invention. Chemical formula: (none) 146091.doc
TW099103379A 2009-06-24 2010-02-04 Laminated polymer film and solar module made thereof TW201100251A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US2009/048448 WO2010101582A1 (en) 2009-03-03 2009-06-24 Laminated polymer film and solar module made thereof

Publications (1)

Publication Number Publication Date
TW201100251A true TW201100251A (en) 2011-01-01

Family

ID=44838273

Family Applications (1)

Application Number Title Priority Date Filing Date
TW099103379A TW201100251A (en) 2009-06-24 2010-02-04 Laminated polymer film and solar module made thereof

Country Status (1)

Country Link
TW (1) TW201100251A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2460266A1 (en) * 2009-07-31 2012-06-06 E. I. du Pont de Nemours and Company Cross-linkable encapsulants for photovoltaic cells

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2460266A1 (en) * 2009-07-31 2012-06-06 E. I. du Pont de Nemours and Company Cross-linkable encapsulants for photovoltaic cells
EP2460266A4 (en) * 2009-07-31 2013-07-17 Du Pont Cross-linkable encapsulants for photovoltaic cells

Similar Documents

Publication Publication Date Title
JP5632397B2 (en) Laminated polymer film and solar cell module made therefrom
JP5882937B2 (en) Photovoltaic module having a polyvinylidene fluoride backsheet
US20110247681A1 (en) Method for manufacturing multilayer films and solar panel backsheets formed thereof
US20120318344A1 (en) Photovoltaic module with chlorosulfonated polyolefin layer
JP5705643B2 (en) Polymer sheet for solar cell backsheet and solar cell module
TWI489644B (en) Resin composition, multi-layered film and photovoltaic module including the same
TW201217161A (en) Barrier assembly
US9450128B2 (en) Multi-layered film and photovoltaic modules comprising the same
JP5969594B2 (en) Back sheet for solar cell module and solar cell module including the same
US20120318354A1 (en) Photovoltaic module with chlorosulfonated polyolefin layer
TW201240816A (en) Multi-layered film and photovoltaic modules comprising the same
US20120328869A1 (en) Solar cell backsheet
WO2013033313A1 (en) Multilayer polyvinylidene films structures
TW201100251A (en) Laminated polymer film and solar module made thereof
TW201133890A (en) Solar cell module and production method for solar cell module
US20150040977A1 (en) Backsheet film with improved hydrolytic stability
JP2013033880A (en) Manufacturing method of solar cell back surface sealing material
TWI466776B (en) Multilayered film and photovoltaic modules having the same
JPH07202236A (en) Solar battery module
TWM411663U (en) Solar cell back plate structure
JP5696172B2 (en) Protective sheet for solar cell, method for producing the same, and solar cell module
JP2016213366A (en) Solar battery backside protection sheet
KR20120070091A (en) Solar cell backside protective sheet and solar cell module comprising the same
TW201215507A (en) Method for manufacturing multilayer films and solar panel backsheets formed thereof