A first aspect of the present invention provides an aircraft assembly comprising a wing and an engine mounting pylon. An aft end of the engine mounting pylon is connected to the wing by a spigot and at least one fastener. The aircraft assembly is configured such that, during operation of the aircraft assembly on an aircraft, the spigot transfers only lateral load between the engine mounting pylon and the wing and the at least one fastener transfers only vertical load between the engine mounting pylon and the wing.

    本发明的第一方面提供了包括机翼和发动机安装挂架的飞行器组件。发动机安装挂架的后端部通过套管和至少一个紧固件连接至机翼。飞行器组件构造成使得在飞行器上的飞行器组件的操作期间,套管仅在发动机安装挂架与机翼之间传递横向载荷,并且所述至少一个紧固件仅在发动机安装挂架与机翼之间传递竖向载荷。


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    Titel :

    AIRCRAFT WING-PYLON CONNECTION


    Weitere Titelangaben:

    飞行器机翼-挂架连接件


    Beteiligte:
    TULLOCH WILLIAM (Autor:in) / BROOMFIELD PAT (Autor:in)

    Erscheinungsdatum :

    2021-12-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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