A propeller mounting structure, a propeller, a power package, and an unmanned aerial vehicle. The propeller mounting structure (100) of the present disclosure is used to detachably mount the propeller (200) on a motor (10), and include a mounting seat (1), a lock member (2), and an elastic member (3). The mounting seat (1) is fixed at an end surface of the motor (10), and a motor shaft (20) of the motor (10) passes through the mounting seat (1). The mounting seat (1) is used to rotationally engaging with the propeller (200), and the elastic member (3) is connected with the lock member (2). The elastic member (3) is used to apply an elastic force to the lock member (2) along an axial direction of the motor shaft (20), such that at least part of the lock member (2) blocks the propeller (200) at an outer side in an engagement direction of the propeller (200). The present disclosure can realize a reliable mounting and connection of the propeller, and the assembly and disassembly are relatively simple.


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    Title :

    PROPELLER MOUNTING STRUCTURE, PROPELLER, POWER SET AND UNMANNED AERIAL VEHICLE


    Additional title:

    PROPELLERMONTAGESTRUKTUR, PROPELLER, ANTRIEBSAGGREGAT UND UNBEMANNTES LUFTFAHRZEUG
    STRUCTURE DE MONTAGE D'HÉLICE, HÉLICE, ENSEMBLE DE PUISSANCE ET AÉRONEF SANS PILOTE


    Contributors:
    HU BEN (author) / ZHANG SHENGXIN (author) / MO SONGQUAN (author) / WANG KUNDIAN (author) / LI LUXIN (author) / YU JIANFANG (author)

    Publication date :

    2021-03-10


    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 / F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen



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