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
WO2013066533(A2)
申请公布日期
2013.05.10
申请号
WO2012US57486
申请日期
2012.09.27
申请人
THE BOEING COMPANY;GRIP, ROBERT ERIK;RAWDON, BLAINE KNIGHT;CROOKS, TAB HUNTER;STOIA, MICHAEL F.
发明人
GRIP, ROBERT ERIK;RAWDON, BLAINE KNIGHT;CROOKS, TAB HUNTER;STOIA, MICHAEL F.