CN108133972B - 一种电极隔离结构体及一种太阳能电池组件 - Google Patents
一种电极隔离结构体及一种太阳能电池组件 Download PDFInfo
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- CN108133972B CN108133972B CN201611095308.4A CN201611095308A CN108133972B CN 108133972 B CN108133972 B CN 108133972B CN 201611095308 A CN201611095308 A CN 201611095308A CN 108133972 B CN108133972 B CN 108133972B
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- vinyl acetate
- eva
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- ethylene
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Abstract
本发明提供了一种可用于太阳能电池组件的电极隔离结构体,包括交联抗紫外EVA层,第一粘结层,聚酯树脂层和第二粘结层。在使用本发明提供的电极隔离结构体时,其抗紫外线性能和耐湿热老化性能都有所提高,解决了电极隔离结构体因长时间受紫外线照射而变黄影响太阳能电池组件的稳定性及美观性的技术问题。此外,电极隔离结构体和太阳能电池片、汇流条之间的粘结力有所提高,解决了电极隔离结构体容易在太阳能电池片,焊烙点处出现脱层等外观缺陷的技术问题。
Description
技术领域
本发明涉及太阳能电池组件领域,尤其涉及一种可用于太阳能电池组件的电极隔离结构体,以及一种包括电极隔离结构体的太阳能电池组件。
背景技术
如图1所示,一般太阳能电池组件包括玻璃2,两个EVA层3,被封装在所述两个EVA层3之间的太阳能电池片4以及背板5。为了防止太阳能电池片4的正极6和负极7接触发生短路,通常在正极6和负极7之间设置有电极隔离结构体8。为了提高太阳能电池组件的功率,可以选用紫外线透过的封装EVA材料作为EVA层3,但是,这样会导致被封装在EVA层3中的电极隔离结构体8受到紫外线照射而变黄,进而影响太阳能电池组件的稳定性及外观。此外,在正负汇流条及焊带结点处,常常存在锡渣堆砌,焊带与汇流条焊烙点面积过大,电极隔离结构体8在湿热老化过程中,容易在焊烙点处出现脱层等外观缺陷。
发明内容
本发明旨在提供一种可用于太阳能电池组件的电极隔离结构体,不仅具有良好的耐候性能(抗紫外线性能,耐湿热老化性能),而且提高了电极隔离结构体与太阳能电池、汇流条之间的粘结力。
根据本发明的一个方面,提供了一种电极隔离结构体,该电极隔离结构体包括:交联抗紫外EVA层,包括偶联剂、紫外线吸收剂、紫外线稳定剂、乙烯-醋酸乙烯酯EVA粒子、和重量百分比小于2%的过氧化类交联剂;第一粘结层,选自以下涂层的一种或它们的组合:含乙烯-醋酸乙烯酯EVA粒子的涂层、丙烯酸类涂层、氟树脂涂层、聚氨酯涂层、环氧树脂涂层;聚酯树脂层;和第二粘结层,包括乙烯-醋酸乙烯酯EVA粒子。
根据某些具体实施方式,在所述交联抗紫外EVA层中,所述乙烯-醋酸乙烯酯EVA粒子中醋酸乙烯酯的含量为5%~45%。
根据某些具体实施方式,所述交联抗紫外EVA层中的乙烯-醋酸乙烯酯EVA粒子的熔融流动指数大于10。
根据某些具体实施方式,所述交联抗紫外EVA层由0.5~1.5重量%过氧化类交联剂、0.5~1.5重量%偶联剂、0~5重量%紫外线吸收剂、0~5重量%紫外线稳定剂和90~99重量%乙烯-醋酸乙烯酯EVA粒子组成。
优选地,所述偶联剂选自硅烷类偶联剂或者钛酸酯类偶联剂。
优选地,所述交联抗紫外EVA层的厚度为50~500μm。
根据某些具体实施方式,所述第一粘结层为含乙烯-醋酸乙烯酯EVA粒子的涂层,其中,所述乙烯-醋酸乙烯酯EVA粒子中醋酸乙烯酯的含量为5%~45%。
优选地,所述第一粘结层由95~99重量%乙烯-醋酸乙烯酯EVA粒子,0~5重量%紫外线稳定剂和0~5重量%偶联剂组成。
根据某些具体实施方式,所述第一粘结层中的乙烯-醋酸乙烯酯EVA粒子的熔融流动指数为10~50。
根据某些具体实施方式,所述第二粘结层中的乙烯-醋酸乙烯酯EVA粒子的熔融流动指数为2~10。
根据某些具体实施方式,所述聚酯树脂层包括以下材料的一种或多种:聚对苯二甲酸乙二酯(PET)、聚萘二甲酸乙二醇酯(PEN)、聚碳酸酯(PC)、聚对苯二甲酸丁二醇酯(PBT)、聚甲基丙烯酸甲酯(PMMA)。
在使用本发明提供的电极隔离结构体时,其抗紫外线性能、耐湿热老化性能、电极隔离结构体和太阳能电池、汇流条之间的粘结力都有所提高,不仅解决了电极隔离结构体因长时间受紫外线照射变黄而影响太阳能电池组件的稳定性及美观性的技术问题,而且,同时也解决了电极隔离结构体在焊烙点处出现脱层等外观缺陷的问题。
根据本发明的另一个方面,还提供了一种太阳能电池组件,包括根据本发明提供的电极隔离结构体。
附图说明
为了让本发明的上述和其它目的、特征及优点能更加明显易懂,下面结合附图和具体实施方式对本发明作进一步说明。本领域技术人员应该理解,附图旨在示意性地阐明本发明的优选实施方式,图中各个部件并非按比例绘制。
图1为一种太阳能电池组件的结构示意图;
图2为根据本发明某些具体实施方式的电极隔离结构体的示意图。
具体实施方式
以下,将结合附图对根据本发明的一些具体实施方式进行更为详细的说明。应当理解,在不脱离本发明的范围或精神的情况下,本领域技术人员能够根据本说明书的教导设想其他各种实施方案并能够对其进行修改。因此,以下的具体方式是说明性的而非限制性的。
除非另外指明,否则本说明书和权利要求中使用的表示特征尺寸、数量和物理特性的所有数字均应理解为由术语“约”来修饰。因此,除非有相反的说明,否则本说明书和所附权利要求书中列出的数值参数均是近似值,根据本发明的教导,本领域普通技术人员能够适当改变这些近似值,获得所需特性。用端点表示的数值范围包括该范围内的所有数字,例如,1至5包括1、1.1、1.3、1.5、2、2.75、3、3.80、4和5等。
除非另外指明,否则实施例所用的原料,均为市售工业品,通过商业渠道可以购得。
名词解释
“熔融流动指数”:Melt Flow Index,MFI,按照ASTM D1238的测试方法,在载荷为2.16kg和190℃的条件下,测得熔体的流动速率。
电极隔离结构体
如图2所示,电极隔离结构体8从上至下依次包括:交联抗紫外EVA层81,第一粘结层82,聚酯树脂层83和第二粘结层84。其中,交联抗紫外EVA层81包括过氧化类交联剂、偶联剂、紫外线吸收剂、紫外线稳定剂和乙烯-醋酸乙烯酯EVA粒子,其中过氧化类交联剂的重量百分比小于2%;第一粘结层82可以选择含乙烯-醋酸乙烯酯EVA粒子的涂层;第二粘结层84包括乙烯-醋酸乙烯酯EVA粒子。
具体地,交联抗紫外EVA层81具有抗紫外线功能、粘结功能以及耐湿热老化性能,可由0.5~1.5重量%过氧化类交联剂、0.5~1.5重量%偶联剂、0~5重量%紫外线吸收剂、0~5重量%紫外线稳定剂和90~99重量%乙烯-醋酸乙烯酯EVA粒子等组成。其厚度介于50μm到500μm之间,优选为140μm。
发明人经研究发现,过氧化类交联剂的加入,能提高电极隔离结构体的交联性能,但如果含量过高,交联剂极易残存,导致太阳能电池组件在层压及湿热老化后,在电极隔离结构体附近会出现鼓包、脱层等外观缺陷。为了使电极隔离结构体同时具有良好的交联性能、抗紫外线功能以及耐湿热老化性能,交联抗紫外EVA层中的各组分之间需协同效应,并且交联抗紫外EVA层与电极隔离结构体的其他层之间需相互作用。过氧化类交联剂的含量优选为0.5~1.5重量%,偶联剂的含量优选为0.5~1.5重量%,紫外线吸收剂的含量优选为0.1~2重量%,紫外线稳定剂的含量优选为0.1~2重量%,乙烯-醋酸乙烯酯EVA粒子的含量优选为93-97重量%。
在交联抗紫外EVA层中,偶联剂可优选为硅烷偶联剂(KH550,KH560,KH570)、钛酸酯类偶联剂等。紫外线吸收剂可以选择水杨酸酯类、苯酮类、苯并三唑类、取代丙烯腈类、三嗪类等。例如,苯酮类的紫外线吸收剂可包括UV-9(2-羟基-4-甲氧基二苯甲酮)、UV-531(2-羟基-4-正辛氧基-二苯甲酮)、UV-24(2,2′-二羟基-甲氧基二苯甲酮)等,苯并三唑类的紫外线吸收剂可包括UV-326[(2′-羟基-3′-叔丁基-5′-甲基苯基)-5-氯代苯并三唑]、UV-P[2-(2′-羟基-5′-甲基苯基)苯并三唑]等,以及三嗪类的紫外线吸收剂可包括三嗪-5[2,4,6-三(2′-羟基-4′-正辛氧基苯基)-1,3,5-三嗪]等。紫外线稳定剂可包括受阻胺类等。典型的紫外线稳定剂可包括例如巴斯夫公司的TINUVIN 622,TINUVIN 770,TINUVIN 783,TINUVIN P,TINUVIN 788,还有氰特公司的CYASORB UV 1164,CYASORB UV 2126,CYASORBUV 3346,CYASORB UV 3853,及CYASORB THT系列产品等。交联剂的种类可以优选,是有机过氧化物引发剂如过氧化苯甲酰(BPO),过氧化苯甲酸叔戊酯(TAPA),过氧化3.3.5三甲基己酸叔丁酯(TBPMH),过氧化苯甲酸叔丁酯(TBPB),过氧化-2-乙基己基碳酸叔丁酯(TBEC),过氧化二异丙苯(DCP),过氧化叔丁基异丙苯(TBCP)等。可优选的乙烯-醋酸乙烯酯EVA粒子的熔融流动指数(MFI)大于10,其中醋酸乙烯酯(VA)的含量为5%~45%,有助于交联,例如,可以选用杜邦PV1300,PV1400Z,三星道达尔PV280。
第一粘结层82具有抗紫外线功能及粘结功能,可以由95~99重量%乙烯-醋酸乙烯酯EVA粒子,0~5重量%紫外线稳定剂和0~5重量%偶联剂组成。其厚度介于5μm到100μm之间,优选为30μm。
在第一粘结层中,所使用的偶联剂的种类可以是,硅烷类或钛酸酯类等。紫外线稳定剂可选用例如巴斯夫公司的TINUVIN 622,TINUVIN 770等,还有氰特公司的CYASORB UV1164,CYASORB UV 2126,及CYASORB THT系列产品等。可优选的乙烯-醋酸乙烯酯EVA粒子的熔融流动指数(MFI)大于10,更优选地,MFI为10~50,其中醋酸乙烯酯(VA)的含量为5%~45%,例如,可以选用台塑科技的TAISOX7660MEVA。
此外,第一粘结层也可以使用丙烯酸类涂层,氟树脂涂层,聚氨酯涂层,环氧树脂涂层,或者各类偶联剂涂层,其厚度可以为1~20μm。
聚酯树脂层83的厚度介于50μm到250μm之间。优选地,可以是白色的聚对苯二甲酸乙二酯(PET),更优选地,可以是耐候性能较好的抗水解用的PET。例如,可以选用东材科技的商品名为DS11的PET产品,且其厚度选为100μm。除此之外,还可以用聚碳酸酯(PC),聚萘二甲酸乙二醇酯(PEN),聚对苯二甲酸丁二醇酯(PBT),聚甲基丙烯酸甲酯(PMMA)作为聚酯树脂层。
第二粘结层84具有粘结及固定功能,其厚度介于5μm到100μm之间,优选为30μm。可优选的乙烯-醋酸乙烯酯EVA粒子的熔融流动指数(MFI)小于10,更优选地,MFI为2~10,其中醋酸乙烯酯(VA)的含量为5%~45%,例如,可以选用扬子巴斯夫的5110J EVA。
如图1所示,本发明的电极隔离结构体可以被设置在太阳能电池组件中的相邻太阳能电池片4的正极6和负极7之间,用于隔离正、负电极。太阳直射太阳能电池组件时,本发明的电极隔离结构体的交联抗紫外EVA层和第一粘结层可有效地阻隔紫外线,并且交联抗紫外EVA层能提供更好的粘结力和耐湿热性能。本发明的电极隔离结构体被应用于太阳能电池组件中时,更稳定,寿命更长,更好地隔离正、负电极,保护太阳能电池组件。
实施例
以下提供的实施例和对比例有助于理解本发明,并且这些实施例和对比例仅用于对本发明进行示例性说明,而不应将它们理解为对本发明范围的限制。除非另外指明,所有的份数和百分比均按重量计。
在本发明的实施例和对比例中采用的原料如表1所示。
表1
制备方法
本发明的电极隔离结构体的一种示例性的制备方法如下:
为了制备本发明的交联抗紫外EVA层,可以将EVA粒子3与过氧化类交联剂,偶联剂,紫外线吸收剂,紫外线稳定剂按一定比例,在常温(10~30℃)下混合搅拌均匀,加热后制备成交联抗紫外EVA膜。
同样的将EVA粒子2与偶联剂,紫外线稳定剂按一定比例,在常温(10~30℃)下混合搅拌均匀,加热后制备成第一粘结膜。
使用EVA粒子1,在聚酯树脂的一个面上制备30μm的第二粘结层。然后在聚酯树脂的另一个面上涂覆已经制备的30μm第一粘结膜。最后,在第一粘结膜上涂覆已经制备的140μm交联抗紫外EVA膜,制得电极隔离结构体样品。
本发明通过“紫外辐照测试”来评价电极隔离结构体的抗紫外线性能,通过“剥离力测试”来评价电极隔离结构体的粘结性能,通过“湿热老化测试”来评价电极隔离结构体的耐湿热老化性能。
紫外辐照测试
按照ASTM G154 cycle 1,将制得的电极隔离结构体样品,置于QUV加速老化箱体内,交联抗紫外EVA层朝向紫外光辐照灯源。
在150kWh/m2的累计紫外光辐照剂量下,用HUNTERLAB仪器按照ASTM E313测试电极隔离结构体的黄化指数(Yellowness Index,YI)。一般认为,YI小于10,电极隔离结构体的抗紫外线性能符合要求;YI小于5,电极隔离结构体的抗紫外线性能较好;YI小于3,电极隔离结构体的抗紫外线性能非常显著。
剥离力测试
将玻璃、封装EVA、太阳能电池片以及根据本发明的制备方法制得的电极隔离结构体样品,依次层叠热压后封装。然后,按照ASTM D903标准,使用INSTRON测试仪器来测试电极隔离体与电池片之间的剥离强度。
将玻璃、封装EVA、汇流条以及根据本发明的制备方法制得的电极隔离结构体样品,依次层叠热压后封装。然后,按照ASTM D903标准,使用INSTRON测试仪器来测试电极隔离体与汇流条之间的剥离强度。
一般认为,剥离强度大于5N/cm,电极隔离结构体的粘结力符合要求;玻璃强度大于10N/cm,电极隔离结构体的粘结力效果显著。测试中,如果电池片自身破裂而电极隔离结构体与电池片尚未分离,则认为电极隔离结构体的粘结力效果极佳。
湿热老化测试
将玻璃、封装EVA、汇流条、太阳能电池片以及根据本发明的制备方法制得的电极隔离结构体样品,如图1所示依次层叠热压后封装,制得太阳能电池组件样品。将太阳能电池组件样品分别置于85%湿度85℃温度的老化箱体内老化2000h。目测太阳能电池组件中,在电极隔离结构体处有无发生鼓包,脱层等外观不良,特别是在汇流条焊点与电极隔离结构体的重叠处。一般认为,出现鼓包、脱层等外观缺陷时,认为湿热老化性能不良;无鼓包、脱层等外观缺陷,则认为湿热老化性能合格。
实施例1
选用96.5重量%的EVA粒子3,1重量%过氧化类交联剂1,1重量%偶联剂1,1重量%紫外线吸收剂和0.5重量%紫外线稳定剂,根据本发明的制备方法制得交联抗紫外EVA层,厚度为140μm。选用98.5重量%EVA粒子2,1重量%偶联剂1,0.5重量%紫外线稳定剂制得第一EVA层,厚度为30μm。选用PET作为聚酯树脂层,选用EVA粒子1作为第二EVA层的原材料。
根据本发明的制备方法制得实施例1的电极隔离结构体样品。根据本发明的测试方法,对实施例1的样品进行测试,并且将各项测试结果记录于表4中。
实施例2~7
选用与实施例1相同的原材料以及制备方法,不同之处在于,交联抗紫外EVA层的各成分的比例不同,具体见表3。
根据本发明的制备方法分别制得实施例2~7的电极隔离结构体样品。根据本发明的测试方法,分别对实施例2~7的样品进行测试,并且将各项测试结果记录于表4中。
实施例8
不同于实施例4,在交联抗紫外EVA层中,选用过氧化类交联剂2和偶联剂2,其余原材料以及各原材料的比例均同实施例4。
根据本发明的制备方法制得实施例8的电极隔离结构体样品。根据本发明的测试方法,对实施例8的样品进行测试,并且将各项测试结果记录于表4中。
实施例9
不同于实施例4,在交联抗紫外EVA层中,选用过氧化类交联剂2,并且选用PC作为聚酯树脂层,其余原材料以及各原材料的比例均同实施例4。
根据本发明的制备方法制得实施例9的电极隔离结构体样品。根据本发明的测试方法,对实施例9的样品进行测试,并且将各项测试结果记录于表4中。
实施例10
不同于实施例9,选用PEN作为聚酯树脂层,其余原材料以及各原材料的比例均同实施例9。
根据本发明的制备方法制得实施例10的电极隔离结构体样品。根据本发明的测试方法,对实施例10的样品进行测试,并且将各项测试结果记录于表4中。
实施例11
不同于实施例4,选用丙烯酸类涂层作为第一粘结层。交联抗紫外EVA层、聚酯树脂层以及第二粘结层的原材料及配方均同实施例4。交联抗紫外EVA膜的制备方法同实施例4。
先在PET上涂覆厚度为3μm干膜的丙烯酸类涂层,然后在有涂层的PET上涂覆已经制备的交联抗紫外EVA膜,厚度为170μm。最后,在PET层另一面复合30μm第二粘结层,制得实施例11的电极隔离结构体样品。
根据本发明的测试方法,对实施例11的样品进行测试,并且将各项测试结果记录于表4中。
对比例1
不同于实施例1,在交联抗紫外EVA层中,仅使用EVA粒子3作为实验原料。
根据本发明的制备方法制得对比例1的电极隔离结构体样品。根据本发明的测试方法,对对比例1的样品进行测试,并且将各项测试结果记录于表4中。
对比例2
不同于实施例4,在交联抗紫外EVA层中,选用非过氧化类交联剂和偶联剂1,其余原材料以及各原材料的比例均同实施例4。
根据本发明的制备方法制得对比例2的电极隔离结构体样品。根据本发明的测试方法,对对比例2的样品进行测试,并且将各项测试结果记录于表4中。
对比例3~5
选用与实施例1相同的原材料以及制备方法,不同之处在于,交联抗紫外EVA层的各成分的比例不同,具体见表3。
根据本发明的制备方法分别制得对比例3~5的电极隔离结构体样品。根据本发明的测试方法,分别对对比例3~5的样品进行测试,并且将各项测试结果记录于表4中。
本发明的实施例和对比例的原材料如表2所示。
本发明的实施例和对比例的交联抗紫外EVA层中的各成分比例如表3所示。
表3
本发明的实施例和对比例的测试结果如表4所示。
表4
如表4所示,根据本发明的电极隔离结构体的抗紫外线性能符合要求,电极隔离结构体和太阳能电池片、汇流条之间的粘结力符合要求,并且电极隔离结构体的耐湿热老化性能也符合要求。
发明人经研究发现,在现有的电极隔离结构体中,添加交联抗紫外EVA层,并且交联抗紫外EVA层中的EVA粒子、过氧化类交联剂、偶联剂、紫外线吸收剂和紫外线稳定剂相互协同效应,能够同时提高抗紫外线性能以及电极隔离结构体的粘结强度。但是,如果过氧化类交联剂加入过多(如对比例3~5),过氧化类交联剂极易残存,则会导致太阳能电池组件在层压及湿热老化后,电极隔离结构体周围出现鼓包、脱层等外观缺陷,不符合要求。因此,为了使电极隔离结构体具有一定的抗湿热老化性能,过氧化类交联剂加入的含量应小于2%。
非过氧化类交联剂代替过氧化类交联剂加入交联抗紫外EVA层(如:对比例2),虽然也能一定程度上提高电极隔离结构体的粘结强度。但是,其粘结性能远不如过氧化类交联剂的加入。此外,太阳能电池组件在层压及湿热老化后,加入非过氧化类交联剂的电极隔离结构体周围会出现鼓包、脱层等外观缺陷,不符合要求。
当交联抗紫外EVA层中的紫外线吸收剂添加量达2%,紫外线稳定剂添加量达0.7%时,电极隔离结构体在150kWh/m2的紫外光辐照强度下,黄化指数能小于5。而未添加紫外线吸收剂和紫外线稳定剂的电极隔离结构体(如:对比例1)的黄化指数则会达到30以上。
其中,特别的,当过氧化类交联剂添加量为1重量%,偶联剂添加量为1重量%,紫外线吸收剂添加量为2重量%,紫外线稳定剂添加量为0.7重量%时,且第一粘结层为含乙烯-醋酸乙烯酯EVA粒子的涂层时,能够实现最佳技术效果,且最经济。
在本发明中,第一粘结层也可以选用耐候性的丙烯酸类涂层(如:实施例11),所制得的电极隔离结构体也能满足本发明的抗紫外线性能、粘结性能及耐湿热老化性能。但是,在实际使用中,电极隔离结构体的交联抗紫外EVA层与聚酯树脂层之间的剥离力没有第一粘结层选用含乙烯-醋酸乙烯酯EVA粒子的涂层强,且成本也相应较贵。
上述本发明的具体实施例仅例示性的说明了本发明的原理及其功效,而非用于限制本发明,熟知本领域的技术人员应明白,在不偏离本发明的精神和范围的情况下,对本发明所作的任何改变和改进都在本发明的范围内。本发明的保护范围,应以本发明所附的权利要求书所界定的范围为准。
Claims (12)
1.一种电极隔离结构体,包括:
交联抗紫外EVA层,包括0.5至1.5重量%的偶联剂、0.1至2重量%的紫外线吸收剂、0.1至2重量%的紫外线稳定剂、93至97重量%的乙烯-醋酸乙烯酯EVA粒子,和重量百分比为0.5至1.5重量%的过氧化类交联剂;
第一粘结层,选自以下涂层的一种或它们的组合:含乙烯-醋酸乙烯酯EVA粒子的涂层、丙烯酸类涂层、氟树脂涂层、聚氨酯涂层、环氧树脂涂层;
聚酯树脂层;和
第二粘结层,包括乙烯-醋酸乙烯酯EVA粒子。
2.根据权利要求1所述的电极隔离结构体,其特征在于:所述交联抗紫外EVA层中,所述乙烯-醋酸乙烯酯EVA粒子中醋酸乙烯酯的含量为5%~45%。
3.根据权利要求1或2所述的电极隔离结构体,其特征在于:所述交联抗紫外EVA层中的乙烯-醋酸乙烯酯EVA粒子的熔融流动指数大于10。
4.根据权利要求1所述的电极隔离结构体,其特征在于:所述交联抗紫外EVA层由0.5~1.5重量%过氧化类交联剂、0.5~1.5重量%偶联剂、0~5重量%紫外线吸收剂、0~5重量%紫外线稳定剂和90~99重量%乙烯-醋酸乙烯酯EVA粒子组成。
5.根据权利要求4所述的电极隔离结构体,其特征在于:所述偶联剂选自硅烷类偶联剂或者钛酸酯类偶联剂。
6.根据权利要求1所述的电极隔离结构体,其特征在于:所述交联抗紫外EVA层的厚度为50~500μm。
7.根据权利要求1所述的电极隔离结构体,其特征在于:所述第一粘结层为含乙烯-醋酸乙烯酯EVA粒子的涂层,其中,所述乙烯-醋酸乙烯酯EVA粒子中醋酸乙烯酯的含量为5%~45%。
8.根据权利要求7所述的电极隔离结构体,其特征在于:所述第一粘结层中的乙烯-醋酸乙烯酯EVA粒子的熔融流动指数为10~50。
9.根据权利要求7所述的电极隔离结构体,其特征在于:所述第一粘结层由95~99重量%乙烯-醋酸乙烯酯EVA粒子,0~5重量%紫外线稳定剂和0~5重量%偶联剂组成。
10.根据权利要求1或2所述的电极隔离结构体,其特征在于:所述第二粘结层中的乙烯-醋酸乙烯酯EVA粒子的熔融流动指数为2~10。
11.根据权利要求1所述的电极隔离结构体,其特征在于:所述聚酯树脂层包括以下材料的一种或多种:聚对苯二甲酸乙二酯(PET)、聚萘二甲酸乙二醇酯(PEN)、聚碳酸酯(PC)、聚对苯二甲酸丁二醇酯(PBT)、聚甲基丙烯酸甲酯(PMMA)。
12.一种太阳能电池组件,包括根据权利要求1~11中任一项所述的电极隔离结构体。
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