The invention relates to a vertical take-off and landing aircraft adopting special fixed wings, which belongs to the technical field of vertical take-off and landing airplanes, and comprises an aircraft body, and a set of coaxial reverse propeller power device is arranged at the front end of the aircraft body. A front upper rudder wing and a front lower rudder wing are symmetrically arranged on the front portion of the aircraft body up and down, a left wing and a right wing are symmetrically arranged on the left side and the right side of the middle of the aircraft body, a left empennage and a right empennage are arranged on the left side and the right side of the rear portion of the aircraft body, and an upper empennage and a lower empennage are arranged on the upper side and the lower side of the rear portion of the aircraft body. A left anti-lift wing is arranged in the middle of the upper portion of the left wing, a right anti-lift wing is arranged in the middle of the upper portion of the right wing, and during vertical take-off and landing, lateral thrust f2 generated when the left anti-lift wing and the right anti-lift wing synchronously open by a certain angle can counteract lateral thrust f1 generated by the left wing and the right wing, so that the aircraft can keep balanced during vertical take-off and landing.
本发明为一种采用特殊固定翼的垂直起降飞机,属于垂直起降飞机技术领域,包括机体,所述机体前端设有一套所述共轴反桨动力装置,所述机体前部上下对称设有前上舵翼和前下舵翼、中部左右两侧对称设有左机翼和右机翼、后部左右两侧设有左尾翼和右尾翼、后部上下两侧设有上尾翼和下尾翼,所述左机翼上方中部设有左反升力翼,所述右机翼上方中部设有右反升力翼,垂直起降时,所述左反升力翼与所述右反升力翼同步张开一定角度产生的侧向推力f2可抵消所述左机翼和所述右机翼产生的所述侧向推力f1,有利于垂直起降时所述飞机保持平衡。
Vertical take-off and landing aircraft adopting special fixed wings
一种采用特殊固定翼的垂直起降飞机
2024-12-06
Patent
Electronic Resource
Chinese
Vertical take-off and landing aircraft with parallel wings
European Patent Office | 2022
|European Patent Office | 2022
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