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    DOOR LATCH SECURING DEVICE FOR AERIAL VEHICLE AND METHOD OF SECURING A DOOR STRUCTURE TO A FUSELAGE SKIN STRUCTURE OF AN AERIAL VEHICLE
    1.
    发明申请
    DOOR LATCH SECURING DEVICE FOR AERIAL VEHICLE AND METHOD OF SECURING A DOOR STRUCTURE TO A FUSELAGE SKIN STRUCTURE OF AN AERIAL VEHICLE 审中-公开

    公开(公告)号：WO2019209150A1

    公开(公告)日：2019-10-31

    申请号：PCT/SE2018/050427

    申请日：2018-04-26

    Applicant: SAAB AB

    Inventor： SCHUSTER, Samuel ,  STENDAL, Marcus ,  ALBERTSSON, Peter

    IPC: B64C1/14

    Abstract: The invention concerns an aerial vehicle (1) comprising a fuselage structure (3) having an aperture (7) and a door structure (5), which is latched and locked to the fuselage structure (3), and a method for securing the door structure (5) to the fuselage skin structure (3). An aperture perimeter (9) of the fuselage structure (3) surrounds the aperture (7). At least a portion of the aperture perimeter comprises (9) a door latch fitting securing device (13) having an elongated latch bar (15) configured for linear motion and engagement with a stationary latch fitting (11) of the door structure (5) in a latched position. The door latch fitting securing device (13) further comprises a rotatable lock member (17) configured for rotary motion for engagement with and for locking the elongated latch bar (15) in the latched position. An actuator device (19) is coupled to the door latch fitting securing device (13) via a translation mechanism (21) configured to convert rotary motion of the actuator device (19) into said linear motion and into said rotary motion.

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