An aircraft propulsion system includes: an engine assembly including a fan that moves air; and a cowl surrounding at least a portion of the engine assembly when the cowl is in a closed position. The fairing includes an outer surface disposed remote from the engine assembly, the outer surface providing an aerodynamic surface. The aircraft propulsion system also includes a cowl mechanism connected to the cowl and configured to guide the cowl from the closed position to an open position along a path of movement. In the open position, the entire cowl is arranged further away from a horizontal plane through an axis of rotation of the fan than in the closed position.

    一种飞行器推进系统,包括:发动机组件,其包括使空气运动的风扇;以及整流罩,当所述整流罩处于关闭位置时,所述整流罩围绕所述发动机组件的至少一部分。该整流罩包括远离发动机组件布置的外表面,该外表面提供空气动力表面。所述飞行器推进系统还包括整流罩机构,所述整流罩机构连接到所述整流罩并且被配置为沿着移动路径将所述整流罩从所述关闭位置引导到打开位置。在该打开位置中,该整个整流罩被布置为比在该关闭位置中更远离穿过该风扇的旋转轴线的水平面。


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    Titel :

    Aircraft engine nacelle fairing mechanism


    Weitere Titelangaben:

    飞行器发动机机舱整流罩机构


    Beteiligte:
    SOSNOWSKI DANIEL (Autor:in) / WILL THOMAS (Autor:in) / KLINGLER ROBERT (Autor:in)

    Erscheinungsdatum :

    08.07.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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