The invention discloses an aircraft power assembly. The aircraft power assembly comprises a base, a first connecting part and a first driving device. The base is provided with a first mounting surface, the first connecting part is provided with a first end surface and a second end surface which are arranged back to back, the first end surface is attached and detachably connected to the first mounting surface, the second end surface is attached and connected to the first driving device, and the first end surface and the second end surface of the first connecting part are obliquely arranged; the first end face is detachably connected to the first mounting face, so that the first connecting part can be detached from the base and rotated, and the tilting direction of the first driving device is quickly changed.

    本发明公开了一种航空器动力组件,包括基座、第一连接部件和第一驱动装置;基座设有第一安装面,第一连接部件具有相背设置的第一端面和第二端面,第一端面贴合并可拆卸地连接于第一安装面,第二端面贴合并连接于第一驱动装置,第一连接部件的第一端面和第二端面倾斜设置,这使得第一驱动装置与第一安装面是相互倾斜的,由于第一端面可拆卸地连接于第一安装面,因此可将第一连接部件从基座上拆下并转动,以快速改变第一驱动装置的倾转方向。


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    Titel :

    Aircraft power assembly


    Weitere Titelangaben:

    航空器动力组件


    Beteiligte:
    HU HUAZHI (Autor:in) / HE DANIAN (Autor:in) / JIANG GUOJUN (Autor:in)

    Erscheinungsdatum :

    04.04.2023


    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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