Aircraft door comprising an engaging mechanism providing engagement between an external opening/closing lever and an internal opening/closing lever

    公开(公告)号:US12071215B2

    公开(公告)日:2024-08-27

    申请号:US17759655

    申请日:2021-01-26

    申请人: LATECOERE

    IPC分类号: B64C1/14

    CPC分类号: B64C1/1423

    摘要: An aircraft door including an external opening/closing lever (7) and an internal opening/closing lever (9) which are coupled by an engaging mechanism (12) which includes: a stop (24) which entrains a counter-stop (23) when the internal opening/closing lever (9) is in its closed position and the external opening/closing lever (7) is pivoted from its closed position to its open position; a lug (22) that rotates as one with the internal opening/closing lever; an engaging pawl (15) which is spaced apart from the path of the lug (22) in a passive position, and disposed on the path of the lug (22) in an active position; a support base (16) designed to push the engaging pawl (15) back into its passive position when the external opening/closing lever (7) is in its closed position.

    Plane Door Frame Canopy
    3.
    发明公开

    公开(公告)号:US20240092503A1

    公开(公告)日:2024-03-21

    申请号:US18273463

    申请日:2022-01-21

    IPC分类号: B64F1/00

    CPC分类号: B64F1/005 B64C1/1423

    摘要: A removable canopy, such as for placement above an entry into a vehicle, includes a brace having releasable mounting features for mounting to the vehicle. The canopy further includes a linkage extending from the brace and convertible from a folded configuration to an extended configuration and a cross bar connected to the linkage so as to be nearer the brace when the linkage is in the folded configuration than when the linkage is in the extended configuration. A sheet is connected to the cross bar and the linkage so as to be folded when the linkage is in the folded configuration and extended when the linkage is in the extended configuration.