The invention discloses a tailstock type vertical take-off and landing fixed-wing unmanned aerial vehicle. The fixed-wing unmanned aerial vehicle comprises a fuselage, wings, a take-off and landing driving assembly, a cruise driving assembly and an empennage assembly, wherein the two wings are respectively arranged on two sides of the fuselage, and one end of each wing is fixedly connected with the fuselage; the take-off and landing driving assembly comprises a main rotor wing and a first driving element, the first driving element is used for driving the main rotor wing to rotate, and the main rotor wing is used for providing lift force for lifting and hovering for the fuselage; the cruise driving assembly is connected to the tail of the fuselage, a second driving element is used for driving the auxiliary rotor to rotate, a pitching driving element is used for adjusting a pitching angle of a rotating shaft of the auxiliary rotor, the auxiliary rotor is used for providing thrust for the fuselage during level flight, and the auxiliary rotor is further used for providing pitching force for the fuselage during lifting; a first empennage is fixedly connected with the fuselage, and a control rudder can swing relative to the first empennage. The tailstock type vertical take-off and landing fixed-wing unmanned aerial vehicle can provide pitching force capable of being accurately adjusted during vertical take-off and landing.
本发明公开了一种尾座式垂直起降固定翼无人机,包括机身、机翼、起降驱动组件、巡航驱动组件和尾翼组件;两个机翼分别置于机身的两侧,各机翼的一端与机身固定连接;起降驱动组件包括主旋翼和第一驱动元件,第一驱动元件用于驱使主旋翼旋转,主旋翼用于为机身提供升降和悬停的升力;巡航驱动组件连接于机身的尾部,第二驱动元件用于驱使副旋翼旋转,俯仰驱动元件用于调整副旋翼的旋转轴的俯仰角度,副旋翼用于为机身提供平飞时的推力,副旋翼还用于为机身提供升降时的俯仰力;第一尾翼与机身固定连接,控制舵能够相对第一尾翼摆动。本发明的尾座式垂直起降固定翼无人机能够在垂直起降时提供可精确调节的俯仰力。
Tailstock type vertical take-off and landing fixed-wing unmanned aerial vehicle
尾座式垂直起降固定翼无人机
2021-12-03
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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