A frame for an aircraft (100), and an aircraft (100). The frame comprises: a body (10) and a fixing assembly (20). The fixing assembly (20) is provided on the body (10). The fixing assembly (20) comprises a fixing frame (210) and a fastening frame (220) spaced apart from each other in a first direction. The fixing frame (210) has two first assembly slots (2120) spaced apart from each other in a second direction. Each first assembly slot (2120) is suitable for accommodating a first arm (901). The fastening frame (220) comprises two second assembly slots (2220) spaced apart from each other in the second direction. Each second assembly slot (2220) is suitable for accommodating a second arm (902). The first direction is perpendicular to the second direction. The structure of the frame is simplified, thereby facilitating assembly and disassembly of an arm (90) of the aircraft (100).


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    Titel :

    FRAME FOR AIRCRAFT AND AIRCRAFT


    Weitere Titelangaben:

    RAHMEN FÜR FLUGZEUG UND FLUGZEUG
    CADRE POUR AÉRONEF ET AÉRONEF


    Beteiligte:
    WEN HAI JUN (Autor:in) / HE JIANBING (Autor:in) / PENG BIN (Autor:in)

    Erscheinungsdatum :

    26.01.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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