In order to solve the problem that in the prior art, the efficiency of a cruise mode and the tension of a hovering/vertical take-off and landing mode cannot be considered at the same time, the invention provides a tilting rotor wing with a bionic wavy front edge and a tilting rotorcraft, so that the efficiency of the tilting rotor wing in the cruise mode is guaranteed, and the lifting of the tension of the tilting rotor wing in a hovering/vertical take-off and landing mode can be realized. The tilting rotor wing comprises a tilting rotor blade, and the front edge of the tilting rotor blade iscomposed of a bionic wavy front edge and a non-bionic wavy front edge. According to the tilting rotor wing with a bionic wavy front edge and the tilting rotorcraft provided by the invention, the efficiency of the tilting rotor wing in a cruise mode is guaranteed, and the tension of the tilting rotor wing in a hovering/vertical take-off and landing mode can be improved.

    为了解决现有技术中倾转旋翼无法兼顾巡航模式的效率和悬停/垂直起降模式的拉力的问题,本公开提供了一种具有仿生波状前缘的倾转旋翼及倾转旋翼机,既保证倾转旋翼在巡航模式下的效率,又能实现倾转旋翼在悬停/垂直起降模式下拉力的提升。包括倾转旋翼桨叶,所述倾转旋翼桨叶的桨叶前缘由仿生波状前缘和非仿生波状前缘组成。本公开提供的一种具有仿生波状前缘的倾转旋翼及倾转旋翼机,既保证倾转旋翼在巡航模式下的效率,又能实现倾转旋翼在悬停/垂直起降模式下拉力的提升。


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    Title :

    Tilting rotor wing with bionic wavy front edge and tilting rotorcraft


    Additional title:

    具有仿生波状前缘的倾转旋翼及倾转旋翼机


    Contributors:
    LI ZHIPING (author) / PAN TIANYU (author) / HE LONG (author) / GONG XINYU (author)

    Publication date :

    2021-02-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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