Embedded aileron control mechanism for unmanned aerial vehicle and unmanned aerial vehicle

Abstract

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.

Description

technical field [0001] The invention belongs to the technical field of aileron manipulation of unmanned aerial vehicles, and more particularly relates to an embedded aileron manipulation mechanism for unmanned aerial vehicles and an unmanned aerial vehicle. Background technique [0002] The aileron control mechanism is an important component of the UAV wing. In the prior art, the thickness of the wing is small. In order to improve the driving force arm of the steering gear, the control mechanism is usually arranged outside the wing, which affects the aircraft to a certain extent. The aerodynamic performance of the wing and the overall performance of the platform. SUMMARY OF THE INVENTION [0003] The purpose of the present invention is to aim at the deficiencies existing in the prior art, and to provide an embedded aileron control mechanism for an unmanned aerial vehicle and an unmanned aerial vehicle. The steering gear push rod is connected to the aileron rocker arm, and...

AI Technical Summary

Problems solved by technology

[0002] The aileron control mechanism is an important component of the UAV wing. In the prior art, the thickness of the wing is small. In order to improve the driving force arm of the steering gear, the control mechanism is usually arranged outside the wing, which affects the aircraft to a certain extent. The aerodynamic performance of the wing and the overall performance of the platform

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