The vertical take-off and landing manned aircraft comprises a right front hovering power system, a right front tilting power system, a right rear tilting power system, a right rear hovering power system, a vertical fin, a left rear hovering power system, a left rear tilting power system, a rear wing, a fuselage, an undercarriage, a left front tilting power system, a front wing and a left front hovering power system. The working method of the vertical take-off and landing manned aircraft comprises the following steps that S1, the aircraft takes off; s2, hovering the aircraft; s3, transitional flight of the aircraft; s4, the aircraft flies forwards; s5, landing the aircraft; under the condition of ensuring large power redundancy and large safety, the flying waste resistance in the forward flying state can be reduced, the endurance time of the aircraft is prolonged, meanwhile, in the transition flying process of the aircraft, four hovering power systems still work, the safety risk in the tilting process is reduced to a certain degree, and due to the fact that the number of propellers is large and the load of a propeller disc is small, the aircraft has the good stability. And the aerodynamic noise of the propeller can be greatly reduced.
本发明公开了一种垂直起降载人飞行器,包括有右前悬停动力系统,右前倾转动力系统,右后倾转动力系统,右后悬停动力系统,垂尾,左后悬停动力系统,左后倾转动力系统,后机翼,机身,起落架,左前倾转动力系统,前机翼,左前悬停动力系统;一种垂直起降载人飞行器的工作方法,包括有以下步骤:S1,飞行器的起飞;S2、飞行器的悬停;S3、飞行器过渡飞行;S4、飞行器前飞;S5、飞行器降落;本发明在保证动力冗余度较大,安全性较大的情况下,可以减少前飞状态的飞行废阻,提高飞机的续航时间,同时飞机过渡飞行过程,仍有4个悬停动力系统工作,一定程度上减少了倾转过程的安全风险,本飞行器由于螺旋桨较多,桨盘载荷较小,可以大幅减少螺旋桨气动噪声。
Vertical take-off and landing manned aircraft and working method thereof
一种垂直起降载人飞行器及其工作方法
2024-11-01
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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