The invention relates to an aircraft, and particularly discloses a vertical take-off and landing fixed-wing aircraft. The vertical take-off and landing fixed-wing aircraft comprises a fuselage, wings and a power system, the power system comprises a main power module and an auxiliary power module, and the auxiliary power module comprises a first power unit for providing vertical thrust; the main power module comprises an adjusting plate and at least one second power unit, and the second power unit is arranged on the adjusting plate; and the adjusting plate is rotatably and movably connected with the fuselage and/or the wings, the adjusting plate has at least two position states relative to the fuselage, in the first position state, the second power unit provides horizontal thrust, and in the second position state, the second power unit provides vertical thrust. According to the vertical take-off and landing fixed-wing aircraft, the thrust direction of the main power module is changed through the adjusting plate, vertical take-off and landing of the aircraft are achieved, and meanwhile the advantage of high navigational speed of the fixed-wing aircraft is taken into account.
本发明涉及一种飞行器,具体公开了一种垂直起降固定翼飞行器。该垂直起降固定翼飞行器包括机身、机翼和动力系统,所述的动力系统包括主动力模块和辅助动力模块,所述的辅助动力模块包括提供竖直推力的第一动力单元;所述的主动力模块包括调整板和至少一个第二动力单元,所述的第二动力单元设置在调整板上;所述的调整板与机身和/或机翼旋转活动连接,且所述的调整板相对于机身至少具有两个位置状态,第一位置状态下,所述的第二动力单元提供水平推力,第二位置状态下,所述的第二动力单元提供竖直推力。以上所述的垂直起降固定翼飞行器通过调整板改变主动力模块的推力方向,实现飞行器的垂直起降,并同时兼顾固定翼飞行器的高航速优点。
Vertical take-off and landing fixed-wing aircraft
一种垂直起降固定翼飞行器
2021-12-24
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |