The invention discloses a total-distance-controllable tailstock type vertical takeoff and landing aircraft and belongs to the technical field of aircrafts. The invention provides a collective-pitch-controllable tailstock type vertical takeoff and landing aircraft which is characterized in that the collective-pitch-controllable tailstock type vertical takeoff and landing aircraft comprises an aircraft body, propellers, a controllable horizontal left wing, a controllable horizontal right wing, a controllable longitudinal wing, a tailstock type supporting frame and a power device; the thruster is a propeller type thruster with a controllable total pitch; all or partial areas of the controllable horizontal left wing, the controllable horizontal right wing and the controllable longitudinal wing can be controlled to move; the ratio of the movable part area of the controllable longitudinal wing to the profile projection of the aircraft is not less than 20%, or the ratio of the movable part areas of the controllable horizontal left wing and the controllable horizontal right wing to the profile projection of the aircraft is not less than 20%; the included angle between the plane formed by the supporting points of the tailstock type supporting frame and the plane rolling shaft is larger than 60 degrees. According to the invention, the fixed-wing aircraft can take off and land without runways in windy weather.
总距可控尾座式垂直起落飞机属于飞行器技术领域。本发明提供了总距可控尾座式垂直起落飞机,其特征在于,总距可控尾座式垂直起落飞机包括飞机机身、推进器、可控水平左机翼、可控水平右机翼、可控纵向机翼、尾座式支撑架、动力装置;推进器为总距可控制的螺旋桨式推进器;可控水平左机翼、可控水平右机翼、可控纵向机翼其全部或部分面积可以控制运动;可控纵向机翼可运动部分面积与飞机外廓投影之比不小于20%,或者可控水平左机翼、可控水平右机翼可运动部分面积与飞机外廓投影之比不小于20%;尾座式支撑架的支撑点所形成平面与飞机横滚轴形成夹角大于60度。本发明可以实现固定翼飞机在大风天气无跑道起落。
Tailstock type vertical takeoff and landing aircraft with controllable total pitch
总距可控尾座式垂直起落飞机
2024-10-25
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2024
|European Patent Office | 2023
|European Patent Office | 2021
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