Aileron driving structure for unmanned aerial vehicle
A technology of drive structure and aileron, applied in the field of wings, can solve problems such as easy failure of the drive structure and hindering the flight effect of drones, and achieve good protection, strong rigidity, and high precision.
Pending Publication Date: 2017-08-29
深圳市中航电科技有限公司
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Problems solved by technology
[0005] The purpose of the present invention is to provide a UAV aileron drive structure, aiming to solve the problem that the drive structure of the UAV aileron in the prior art is prone to failure and hinders the overall flight effect of the UAV
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[0019] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.
[0020] In the drawings of this embodiment, the same or similar symbols correspond to the same or similar components; The indicated orientation or positional relationship is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the referred device or element must have a specific orientation, or in a specific orientation. Construction and operation, so the words describing the positional relationship in the drawings are only for illustrative...
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The invention relates to the field of aerofoils and discloses an aileron driving structure for an unmanned aerial vehicle. The aileron driving structure comprises a vehicle body, ailerons, a link mechanism for driving the ailerons to swing and a server for driving the link mechanism to move; the link mechanism is respectively connected with the ailerons and the server; the vehicle body comprises a vehicle main body and the aerofoils; the aerofoils are connected with the vehicle main body; the ailerons are arranged on the aerofoils; the driving structure is positioned inside the vehicle body; due to no addition of windward area of the unmanned aerial vehicle, the problem that windward resistance is great if the driving structure is arranged outside the unmanned aerial vehicle is solved; the driving structure is not exposed, and a casing of the unmanned aerial vehicle plays a good protecting effect on the driving structure, so that the driving structure is not easy to damage; meanwhile, the driving structure adopts the link mechanism with high rigidity and efficiency to drive the ailerons, so that driving precision is higher.
Description
technical field [0001] The invention relates to the field of wings, in particular to an unmanned aerial vehicle aileron drive structure. Background technique [0002] The UAV aileron is located at the lower end of the wing and is an important part for controlling the flight path of the UAV. [0003] At present, in the control of the rudder surfaces (aileron rudder surface, elevator rudder surface, rudder rudder surface, flap rudder surface) of the UAV, a hinge is installed on the rudder surface to connect each rudder surface and its carrier, usually The two sides of the place must avoid the air and need to be made very thin in order to rotate normally. The rudder angle is installed on the rudder surface, and the steering gear is installed in the main body or fuselage of the rudder surface, and the rudder surface is driven to swing by the steering gear and the tie rod. [0004] In the prior art, the control of the traditional rudder surface increases the resistance of the a...
Claims
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Login to View More IPC IPC(8): B64C13/30
CPCB64C13/30B64U10/25Y02T50/40
Inventor孔垂红
Owner深圳市中航电科技有限公司