发明名称 DIVIDER CURTAIN
摘要 <p>PROBLEM TO BE SOLVED: To provide a curtain divider for an aircraft interior containing pivot stow bins.SOLUTION: The curtain divider includes a first fabric curtain 132, having an outboard end 136 and an inboard end 138, which is attachable to the aircraft interior only at the outboard and inboard ends. The first fabric curtain includes a vertical portion 134, and a horizontal portion 148. The vertical portion has a substantially straight bottom edge 140, and an arcuate top edge 142 defining a space sufficient for opening the pivot stow bins. The horizontal portion is flexibly attached to the vertical portion along the top edge and extends from the outboard end to the inboard end, having a substantially continuous curvature. The horizontal portion is adapted to impart forward and aft stability to a curtain support member at the top edge.</p>
申请公布号 JP2014118144(A) 申请公布日期 2014.06.30
申请号 JP20130255687 申请日期 2013.12.11
申请人 BOEING CO 发明人 KENNETH M SLYTER;MORCOM PAUL W
分类号 B64D11/00 主分类号 B64D11/00
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