The invention relates to the technical field of tail vanes of fixed-wing unmanned aerial vehicles, in particular to a tail vane locking device of a vertical take-off and landing fixed-wing unmanned aerial vehicle, which comprises a fixed-wing unmanned aerial vehicle main body, and a rudder locking balance assembly is arranged behind the fixed-wing unmanned aerial vehicle main body; the rudder locking balance assembly comprises a gear, the outer wall of the gear is meshed with a gear ring, the interior of the gear ring is connected with a first nut pair, and the periphery of the gear ring is provided with a shell. The rudder clamping block clamps a tail rudder of the fixed-wing unmanned aerial vehicle body, the situation that the tail rudder suddenly operates in the take-off and landing process, consequently, the fixed-wing unmanned aerial vehicle body spins, and air crash accidents are caused is avoided, the balance block is arranged, and the second nut pair drives the balance block to move in the direction away from the tail rudder, so that the whole body is balanced; and the overall inclination phenomenon in the landing stage is avoided.
本发明涉及固定翼无人机的尾舵技术领域,具体为一种垂直起降固定翼无人机的尾舵锁舵装置,包括固定翼无人机主体,所述固定翼无人机主体的后方设置有锁舵平衡组件;锁舵平衡组件,所述锁舵平衡组件包括齿轮,所述齿轮的外壁啮合有齿环,所述齿环的内部连接有一号螺母副,所述齿环的外围设置有壳体,本发明锁舵装置通过卡舵块和转辊的设置,减少了固定翼无人机主体的磨损,卡舵块卡住固定翼无人机主体的尾舵,避免起降过程中尾舵突然运作,导致固定翼无人机主体发生自旋,避免引发坠机事故,通过平衡块的设置,二号螺母副带动平衡块向远离尾舵的方向移动,使得整体到达平衡,避免起落阶段整体出现倾斜的现象。
Tail vane locking device of vertical take-off and landing fixed-wing unmanned aerial vehicle
一种垂直起降固定翼无人机的尾舵锁舵装置
2024-03-22
Patent
Elektronische Ressource
Chinesisch
IPC: | B64U |
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