发明名称 Wing fold system rotating latch
摘要 An apparatus and method of a wing fold system may include a latch assembly (802) rotating an unfixed portion (808) of a wing, with respect to a fixed portion (810) of the wing, between a flight position (figure 8a) of the wing and a folded position (figure 8b) of the wing. A first portion of the wing may hold a rotating portion (806) of the latch assembly. A second portion of the wing may hold a secured portion (814) of the latch assembly. The rotating portion of the latch assembly may rotate between an open position and a closed position. A slot in the rotating portion may receive the secured portion of the latch assembly. A securing portion (820) of the rotating portion (806) may secure a secured portion (814) of the latch assembly. The latch assembly may prevent rotation of the second portion when the wing may be in the flight position.
申请公布号 EP2730500(A2) 申请公布日期 2014.05.14
申请号 EP20130189962 申请日期 2013.10.23
申请人 THE BOEING COMPANY 发明人 FOX, STEPHEN JOHN;KORDEL, JAN A;TOWNSEND, KEITH;LASSEN, MATTHEW AUGUST;GARDNER, MARK JOHN;GOOD, MARK STEVEN
分类号 B64C3/56;B64C23/06 主分类号 B64C3/56
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