A multi-control-surface tail-supported vertical takeoff and landing aircraft belongs to the technical field of aircraft. The invention provides a multi-control-surface tail-supported vertical takeoff and landing aircraft. The multi-control-surface tail-supported vertical takeoff and landing aircraft is characterized by comprising an aircraft body, propellers, a controllable left wing, a controllable right wing, a controllable longitudinal wing, a takeoff and landing support frame, a left wing control device, a right wing control device and a longitudinal wing control device, the left wing control device is connected with the controllable left wing, and through the movement of the left wing control device, the controllable left wing or an included angle between a part of area of the controllable left wing and a plane formed by a transverse rolling shaft and a pitching shaft of the aircraft can be driven to change; the right wing control device is connected with the controllable right wing, and through movement of the right wing control device, the controllable right wing or an included angle between a part of area of the controllable right wing and a plane formed by a horizontal rolling shaft and a pitch shaft of the aircraft can be driven to change; the longitudinal wing control device is connected with the controllable longitudinal wing, and through the movement of the longitudinal wing control device, the controllable longitudinal wing or the included angle between a part of the area of the controllable longitudinal wing and a plane formed by a horizontal rolling shaft and a yaw shaft of the aircraft can be driven to change; the included angle formed by a plane formed by supporting points of the takeoff and landing supporting frame and a plane rolling shaft is larger than 60 degrees. The flight attitude of the aircraft can be stably controlled at a low speed, and runway-free takeoff and landing of the fixed-wing aircraft can be achieved.
多舵面尾部支撑垂直起落飞机属于飞行器技术领域。本发明提供了多舵面尾部支撑垂直起落飞机,其特征在于:所述多舵面尾部支撑垂直起落飞机包括飞机机身、推进器、可控左机翼、可控右机翼、可控纵机翼、起落支撑架、左机翼控制装置、右机翼控制装置、纵机翼控制装置;所述左机翼控制装置与所述可控左机翼连接,通过所述左机翼控制装置的运动,能够带动所述可控左机翼或其部分面积与飞机横滚轴及俯仰轴所形成平面的夹角角度发生变化;所述右机翼控制装置与所述可控右机翼连接,通过所述右机翼控制装置的运动,能够带动所述可控右机翼或其部分面积与飞机横滚轴及俯仰轴所形成平面的夹角角度发生变化;所述纵机翼控制装置与所述可控纵机翼连接,通过所述纵机翼控制装置的运动,能够带动所述可控纵机翼或其部分面积与飞机横滚轴及偏航轴所形成平面的夹角角度发生变化;所述起落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。本发明可以实现低速时能够稳定控制飞行姿态的飞机,可以实现固定翼飞机无跑道起落。
Multi-control-surface tail-supported vertical takeoff and landing aircraft
多舵面尾部支撑垂直起落飞机
2024-07-05
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2023
|European Patent Office | 2024
|European Patent Office | 2021
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