The invention relates to an active lift augmentation tandem wing type ground effect aircraft, and relates to the field of ground effect aircrafts. The defects that a stable take-off environment is needed, take-off time is long, and operation is complex are overcome. An active lift-increasing tandem wing type ground effect aircraft comprises a machine body, a cockpit is formed in the middle of the top of the machine body, connecting pieces symmetrically arranged in the direction of the machine body are fixedly installed on the front side and the rear side of the machine body correspondingly, and wing structures are fixedly connected to the connecting pieces on the front side and the connecting pieces on the rear side correspondingly; the inclination angle between the wing structures fixed to the connecting pieces on the front side of the aircraft body and the ground, the inclination angle between the wing structures fixed to the connecting pieces on the rear side of the aircraft body and the ground and the inclination angle between the wing structures fixed to the connecting pieces on the rear side of the aircraft body are larger than the inclination angle of the front-side wings. By means of the tandem wing type layout, the inclination angles of the paddles, the front wing structure and the rear wing structure relative to the ground are increased, and when the aircraft runs, the aircraft can obtain the maximum lift force compensation under the influence of the ground effect.
本发明涉及一种主动增升串翼式地效飞行器,涉及地效飞行器领域。为了克服需要稳定的起飞环境,起飞时间长,操作复杂的缺点。一种主动增升串翼式地效飞行器,包括有机体,机体顶部中间开设有驾驶舱,机体前侧与后侧均固定安装有沿机体方向对称设置的连接片,前侧连接片与后侧连接片均固定连接有机翼结构,与机体前侧的连接片相固定的机翼结构与地面的倾斜角,与机体后侧的连接片相固定的机翼结构与地面的倾斜角,前侧机翼倾斜角大于后侧倾斜角,通过将飞行器自身设备载重设置在机体前侧。本发明通过串翼式布局,增大桨叶和前后机翼结构与地面倾斜角度,在飞行器运行时,受到地面效应的影响下,飞行器能够获得最大的升力补偿。
Active lift-augmentation tandem wing type ground effect aircraft
一种主动增升串翼式地效飞行器
2025-03-04
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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