US2014349438A1PendingUtilityA1

Diaphragm sheet, and method for manufacturing solar cell module using diaphragm sheet

Assignee: NISSHINBO MECHATRONICS INCPriority: Jul 4, 2011Filed: Aug 6, 2014Published: Nov 27, 2014
Est. expiryJul 4, 2031(~4.9 yrs left)· nominal 20-yr term from priority
H10F 71/00H10F 19/80H10F 19/00H10F 19/804C08L 2203/206H01L 31/0481C08F 210/18H01L 31/18B30B 5/02B29C 66/7465B32B 37/1018B29C 66/91421B29K 2995/0083B29C 65/787B32B 37/0007B29C 65/18B29C 65/02B29C 66/342B29C 66/433B29C 66/0044B32B 2457/12B29C 66/81261B29C 66/81264B29C 66/8322B29C 66/81455B29C 66/919Y02E10/50B29C 66/71B32B 37/003B32B 37/1009
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Claims

Abstract

The performances and durability of a diaphragm sheet of a solar cell laminator are enhanced, and a favorable lamination work is stably performed over a long period of time. In addition, by stably performing sufficient and uniform lamination over a long period of time, a high-quality module is stably manufactured over a long period of time. A solar cell module is manufactured by using a diaphragm sheet formed of a composition containing an ethylene-propylene-diene rubber (EPDM), which is low in creep deformation and high in durability against an organic peroxide and a silane coupling agent.

Claims

exact text as granted — not AI-modified
1 . A diaphragm sheet to be used in a laminator for solar cell module manufacture using an ethylene vinyl acetate resin as an encapsulant, which comprises a composition containing an ethylene-propylene-diene rubber and which satisfies the following requirements (1) and (2):
 (1) swelling ratios with respect to an organic peroxide and a silane coupling agent contained in the encapsulant are not more than 20%; and   (2) a creep deformation of the diaphragm sheet at a hot plate temperature of 130° C. is not more than 3 mm.   
     
     
         2 . A diaphragm sheet to be used in a laminator for solar cell module manufacture using an ethylene vinyl acetate resin as an encapsulant, which comprises a composition containing an ethylene-propylene-diene rubber and which satisfies the following requirements (1) and (2):
 (1) a swelling ratio to tertiary-butyl peroxy-2-ethylhexyl carbonate and vinyl triethoxysilane contained in the encapsulant is not more than 20%; and   (2) a creep deformation of the diaphragm sheet at a hot plate temperature of 130° C. is not more than 3 mm.   
     
     
         3 . A method for manufacturing a solar cell module using an ethylene vinyl acetate resin as an encapsulant, which comprises
 a step of laminating solar cells with the encapsulant by a laminator using a diaphragm sheet,   the diaphragm sheet comprising a composition containing an ethylene-propylene-diene rubber and satisfying the following requirements (1) and (2):   (1) swelling ratios with respect to an organic peroxide and a silane coupling agent contained in the encapsulant are not more than 20%; and   (2) a creep deformation of the diaphragm sheet at a hot plate temperature of 130° C. is not more than 3 mm.

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