The invention provides a rotor structure, an aircraft and a flight control method, and particularly relates to the technical field of aircrafts. The flight control method is used for controlling flight of the aircraft, the aircraft comprises at least one rotor wing structure, each rotor wing structure comprises at least one paddle, and the flight control method comprises the following steps that when the horizontal component speed of the aircraft is larger than a first set threshold value, the rotor wing structure is driven to rotate; and the extension direction of the blades is controlled to be parallel or approximately parallel to the course of the aircraft. The flight control method can reduce the aerodynamic resistance of the aircraft in the cruise mode and increase the effective navigation time of the aircraft.

    本发明提供一种旋翼结构、飞行器及飞行控制方法,具体涉及飞行器技术领域。本发明的飞行控制方法,用于控制飞行器飞行,其中,所述飞行器包括有至少一个旋翼结构,所述旋翼结构包括至少一个桨叶,所述飞行控制方法包括如下过程:在所述飞行器的水平分速度大于第一设定阈值时,控制所述桨叶的延伸方向与所述飞行器的航向平行或近似平行。本发明飞行控制方法可以降低飞行器在巡航模式下的气动阻力,增加飞行器的有效航行时间。


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    Titel :

    Rotor wing structure, aircraft and flight control method


    Weitere Titelangaben:

    一种旋翼结构、飞行器及飞行控制方法


    Beteiligte:
    CHEN YENYU (Autor:in) / XIE SHAIMING (Autor:in) / YU XIN (Autor:in) / ZHANG ZIQIAN (Autor:in) / QU HUMIN (Autor:in) / LI TANG (Autor:in) / WEN JINLONG (Autor:in)

    Erscheinungsdatum :

    05.07.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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