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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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