The invention provides a fixed-wing aircraft and a control method thereof, and relates to the technical field of fixed-wing aircrafts, the fixed-wing aircraft comprises an aircraft body, wings are connected to the two sides of the aircraft body; the front landing gear is rotationally arranged on the lower side of the front end of the aircraft body and comprises a first supporting column and a front propeller coaxially arranged on the first supporting column, the first supporting column is used for making contact with the ground, and the front propeller is located between the ground and the aircraft body when the first supporting column makes contact with the ground; the rear landing gear is rotationally arranged on the lower side of the rear end of the wing, the rear landing gear comprises a second supporting column and a rear propeller coaxially arranged on the second supporting column, the second supporting column is used for making contact with the ground, and the rear propeller is located between the ground and the aircraft body when the second supporting column makes contact with the ground; the function of an undercarriage is achieved through the first supporting column and the second supporting column, folding and unfolding of the undercarriage are achieved, vertical take-off and landing are achieved through the front propeller and the rear propeller, and the function of providing thrust during forward flight can be achieved through the folded rear propeller.

    本发明提供一种固定翼飞机及其控制方法,涉及固定翼飞机技术领域,包括:机体,机体的两侧连接有机翼;前起落装置,转动设置在机体的前端下侧,前起落装置包括第一支柱和同轴设置在第一支柱上的前螺旋桨,第一支柱用于与地面接触,且第一支柱与地面接触时前螺旋桨处于地面与机体之间;后起落装置,后起落装置转动设置在机翼的后端下侧,后起落装置包括第二支柱和同轴设置在第二支柱上的后螺旋桨,第二支柱用于与地面接触,且第二支柱与地面接触时后螺旋桨处于地面和机体之间;通过第一支柱和第二支柱起到起落架的作用,并实现起落架的收放,通过前螺旋桨和后螺旋桨实现垂直起降,并且通过收起后的后螺旋桨能够起到前飞时提供推力的功能。


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    Title :

    Fixed-wing aircraft and control method thereof


    Additional title:

    一种固定翼飞机及其控制方法


    Contributors:
    ZHANG GUANGLIN (author) / WANG ZHAORUI (author) / MU WEIHAO (author) / WEN KANG (author) / GAO LELE (author)

    Publication date :

    2024-06-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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