An unmanned aerial vehicle includes a fuselage body, a foldable wing assembly and a gear assembly. The foldable wing assembly, including a pair of opposing wing members, is coupled to the fuselage body and positionable in a stowed position and a deployed position. The gear assembly positions the wing members in a stowed position and a deployed position and include a support bracket assembly and a pair of opposing hinge members. The support bracket assembly is coupled to the fuselage body and including first and second support brackets forming a cavity therebetween and a pair of opposing hinge members. The pair of opposing hinge members are pivotably coupled to the support bracket assembly and positioned within the cavity. Each hinge member is coupled to a corresponding wing member and includes a set of gear teeth extending outwardly from an arcuate radially outer surface and coupled in a meshed arrangement.


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    Title :

    Foldable rotor blade assembly and aerial vehicle with a foldable rotor blade assembly


    Contributors:
    ZHANG LONG (author) / WANG ZHAOZHE (author) / LIU WEIQI (author) / CHENG XIAONAN (author) / ZHANG TONG (author)

    Publication date :

    2022-12-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    FOLDABLE ROTOR BLADE ASSEMBLY AND AERIAL VEHICLE WITH A FOLDABLE ROTOR BLADE ASSEMBLY

    ZHANG LONG / WANG ZHAOZHE / LIU WEIQI et al. | European Patent Office | 2020

    Free access