发明名称 STRAIN ISOLATION LAYER ASSEMBLIES AND METHODS
摘要 In an embodiment of the disclosure, there is provided a strain isolation layer assembly. The assembly has a rigid solar layer; a strain isolation layer having a discontinuous configuration, a vertical rigidity, and a horizontal shear flexibility; and an underlying substrate layer. The strain isolation layer is coupled between the rigid solar layer and the underlying substrate layer to form a strain isolation layer assembly, such that the strain isolation layer isolates the rigid solar layer to reduce one or more strains induced on the rigid solar layer.
申请公布号 EP2774185(A2) 申请公布日期 2014.09.10
申请号 EP20120779212 申请日期 2012.09.27
申请人 THE BOEING COMPANY 发明人 GRIP, ROBERT ERIK;RAWDON, BLAINE KNIGHT;CROOKS, TAB HUNTER;STOIA, MICHAEL F.
分类号 H01L31/048 主分类号 H01L31/048
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