A shroud assembly for an aircraft landing gear includes an aerodynamic shroud, a first support bracket assembly, and a second support bracket assembly. The first support bracket assembly is configured to couple with a structural member of an aircraft landing gear, support a first end of the aerodynamic shroud, and have a first position fixed relative to the structural member in x, y, and z directions. The first support bracket assembly has a first clamp configured to secure the first support bracket assembly relative to the structural member in an x-direction. The second support bracket assembly is configured to support the second end of the pneumatic cover and has a second position fixed relative to the structural member in the y-direction and the z-direction.

    一种用于飞行器起落架的罩组件包括气动罩、第一支撑托架组件和第二支撑托架组件。第一支撑托架组件被构造为与飞行器起落架的结构构件联接,支撑气动罩的第一端,并且具有在x方向、y方向和z方向上相对于结构构件固定的第一位置。第一支撑托架组件具有第一夹具,其被构造为在x方向上相对于结构构件固定第一支撑托架组件。第二支撑托架组件被构造为支撑气动罩的第二端并且具有在y方向和z方向上相对于结构构件固定的第二位置。


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    Titel :

    Acoustic enclosure of undercarriage


    Weitere Titelangaben:

    起落架隔声罩


    Beteiligte:
    FLYNN STEPHEN (Autor:in)

    Erscheinungsdatum :

    22.07.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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