A frame for an aircraft, and an aircraft. The frame includes: a body and a fixing assembly. The fixing assembly is provided on the body. The fixing assembly includes a fixing frame and a fastening frame spaced apart from each other in a first direction. The fixing frame has two first assembly slots spaced apart from each other in a second direction. Each first assembly slot is suitable for accommodating a first arm. The fastening frame includes two second assembly slots spaced apart from each other in the second direction. Each second assembly slot is suitable for accommodating a second arm. The first direction is perpendicular to the second direction. The structure of the frame is simplified, thereby facilitating assembly and disassembly of an arm of the aircraft.


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    Title :

    FRAME FOR AIRCRAFT AND AIRCRAFT


    Contributors:
    WEN HAI JUN (author) / HE JIANBING (author) / PENG BIN (author)

    Publication date :

    2022-01-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen



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