The invention discloses an embedded aileron control mechanism for an unmanned aerial vehicle and the unmanned aerial vehicle, and the control mechanism comprises a pull rod which is arranged in a wing, and the shell end of the pull rod is hinged to the front end of the wing; the steering engine supporting rod is arranged in the wing, the middle of the steering engine supporting rod is hinged to the rear end of the wing, and the telescopic end of the pull rod is hinged to the lower end of the steering engine supporting rod; the steering engine push rod is arranged in the wing, one end of the steering engine push rod is hinged to the upper end of the steering engine support rod, the other end of the steering engine push rod is hinged to the aileron rocker arm rotationally arranged at the rear end of the wing, and the aileron rocker arm is connected with the aileron; the control mechanism is connected with the aileron rocker arm through the pull rod, the steering engine support rod and the steering engine push rod which are arranged in the wing, the whole control mechanism adopts an embedded design in the wing, the main bearing skin of the wing is not damaged, the design of an external fairing of the traditional wing can be cancelled, and the aerodynamic performance of the wing and the overall performance of the platform are improved.
本发明公开了一种无人机用内埋式副翼操纵机构及无人机,该操纵机构包括:拉杆,设置在机翼的内部,拉杆的壳体端与机翼的前端铰接;舵机支杆,设置在机翼的内部,舵机支杆的中部铰接在机翼的后端,拉杆的伸缩端与舵机支杆的下端铰接;舵机推杆,设置在机翼的内部,舵机推杆的一端与舵机支杆的上端铰接,舵机推杆的另一端与转动设置在机翼后端的副翼摇臂铰接,副翼摇臂与副翼连接;该操纵机构通过设置在机翼内部的拉杆、舵机支杆、舵机推杆与副翼摇臂连接,整体采用在机翼内的内埋式设计,不破坏机翼主承力蒙皮,能够取消传统机翼的外置整流罩设计,提升机翼气动性能和平台整体性能。
Embedded aileron control mechanism for unmanned aerial vehicle and unmanned aerial vehicle
一种无人机用内埋式副翼操纵机构及无人机
2022-06-28
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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