The invention relates to an aircraft sliding door (1) comprising: a door leaf (5) which is slidable in a switching direction between a closed position and an open position, respectively, and which has a door top part (5A) and a door bottom part (5B), the door top part (5A) and the door bottom part (5B) being arranged in a pulled-out state in the closed position and in a pushed-together state in the open position; a guide rail (9) inclined with respect to the opening/closing direction for guiding the door leaf (5) between a closed position and an open position; and a drive device (11) having an electric motor (12) for assisting the movement of the door leaf (5) from the open position to the closed position, in which the drive device (11) comprises a spindle (13), in particular a ball screw, which is connected to the electric motor (12) and which is inclined with respect to the opening/closing direction such that the door leaf (5) automatically shifts into the open position along the spindle (13) when the electric motor (12) is in a power-off state.

    本发明涉及一种飞行器滑动门(1),包括:门扇(5),其能够分别在开关方向上在关闭位置和打开位置之间滑动,并且具有门顶部部件(5A)和门底部部件(5B),门顶部部件(5A)和门底部部件(5B)布置成在关闭位置处于拉出状态并且在打开位置处于推合在一起的状态;导轨(9),其相对于开关方向倾斜,用于在关闭位置和打开位置之间引导门扇(5);以及驱动装置(11),其具有电动马达(12),用于辅助门扇(5)从打开位置移动到关闭位置,其中驱动装置(11)包括心轴(13),特别是滚珠丝杠,该心轴连接至电动马达(12)并相对于开关方向倾斜,使得当电动马达(12)处于断电状态时,门扇(5)沿着心轴(13)自动地转换到打开位置。


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    Titel :

    Aircraft sliding door


    Weitere Titelangaben:

    飞行器滑动门


    Beteiligte:
    SIESS MARTIN (Autor:in)

    Erscheinungsdatum :

    2024-02-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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