The invention relates to the technical field of vertical take-off and landing aircrafts, and discloses a vertical take-off and landing aircraft and a flight method. The vertical take-off and landing aircraft comprises a fuselage, a propeller and an elevator. The propeller is located at the top of the fuselage and used for driving the vertical take-off and landing aircraft to vertically take off. The elevator is located on the aircraft body, can swing relative to the aircraft body and is used for driving the hovering vertical take-off and landing aircraft to conduct steering or overturning motion. In the take-off process of the vertical take-off and landing aircraft, the vertical take-off and landing aircraft can vertically take off through the propeller, and when the vertical take-off andlanding aircraft takes off to a certain height, the vertical take-off and landing aircraft can horizontally move or turn or turn over by changing the angle of the elevator and the rotating speed of the propeller on the vertical take-off and landing aircraft. Therefore, the vertical take-off and landing aircraft can perform normal flight motion through a relatively simple structure. The flight method comprises a takeoff step, a cruise step and a landing step.

    本发明涉及垂直起降飞行器技术领域,公开了一种垂直起降飞行器和飞行方法。垂直起降飞行器包括机身、螺旋桨和升降舵。螺旋桨位于机身的顶部,用于驱动垂直起降飞行器垂直起飞;升降舵位于机身上,升降舵能够相对机身摆动,用于带动悬停的垂直起降飞行器进行转向或翻转运动。在垂直起降飞行器起飞的过程中,通过螺旋桨,使得垂直起降飞行器可以垂直起飞,当垂直起降飞行器起飞到一定高度时,通过改变升降舵的角度,以及垂直起降飞行器上螺旋桨的转速,使得垂直起降飞行器可以实现平移、转向或翻转动作,从而使得垂直起降飞行器通过较为简洁的结构,便能够让垂直起降飞行器进行正常的飞行运动。飞行方法包括起飞步骤、巡航步骤和降落步骤。


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    Title :

    Vertical take-off and landing aircraft and flight method


    Additional title:

    一种垂直起降飞行器和飞行方法


    Contributors:
    SU SHANFEI (author) / LUAN TAO (author) / QIU XIZHI (author)

    Publication date :

    2020-12-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge