An aircraft impeller (001) and an aircraft, relating to the field of aircraft drive components, the aircraft impeller (001) comprising a frame body (100) and a rotating wheel part (200); the frame body (100) comprises a mounting groove (130), the rotating wheel part (200) being fixedly arranged in the mounting groove (130); the mounting groove (130) has an axial centre line (105); the mounting groove (130) also has an open face and a bottom face (131) arranged opposite to one another; the rotating wheel part (200) comprises at least one vane (210) distributed around the axial centre line (105), the vane (210) comprising a windward face (211); at the connecting point of the windward face (211) and the open face, the angle of the tangent plane of the windward face (211) and the open face is an acute angle. The present aircraft impeller does not act excessively on the air, and saves energy sources.


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    Titel :

    AIRCRAFT IMPELLER AND AIRCRAFT


    Weitere Titelangaben:

    FLUGZEUGLAUFRAD UND FLUGZEUG
    ROUE À AILETTES D'AÉRONEF ET AÉRONEF


    Beteiligte:
    TANG LIANGLUN (Autor:in)

    Erscheinungsdatum :

    2024-05-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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