The invention relates to an aircraft capable of taking off and landing vertically and a control method thereof.The aircraft is provided with a lift fan system at least located at the front end of a fuselage and a vector thrust power system located on a main wing, and the flight requirement of the aircraft can be met by controlling the working states of the lift fan system and the vector thrust power system; the lift fan system is arranged on the aircraft body, and the space is large, so that the lift fan system can use a large-size fan so as to reduce the load of the whole propeller disc and reduce the take-off and landing energy consumption, and the vector thrust power system can provide course thrust for the aircraft while meeting the vertical take-off and landing function; the whole power system does not generate waste resistance during cruising, the cruising lift-drag ratio of the aircraft can be effectively improved, the endurance performance is improved, and therefore the flight speed and the operation efficiency of the aircraft are obviously improved.
本发明涉及一种可垂直起降的飞行器及其控制方法,该飞行器设置有至少位于机身的前端部分的升力风扇系统及位于主翼的矢量推力动力系统,通过控制二者的工作状态能够满足飞行器飞行需求,并且本发明中的升力风扇系统设置于机身,空间比较大,这样升力风扇系统可以使用大尺寸风扇从而降低整体桨盘负载、降低起降能耗,矢量推力动力系统在满足垂直起降功能的同时亦能为飞行器提供航向推力;整套动力系统在巡航时不产生废阻力,能有效提升飞行器巡航升阻比以及提升续航性能,从而明显提升飞行器的飞行速度和运营效率。
Aircraft capable of vertically taking off and landing and control method thereof
一种可垂直起降的飞行器及其控制方法
2022-07-22
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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