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A kind of front wing tilting mechanism for unmanned aerial vehicle and unmanned aerial vehicle

A technology of tilting mechanism and unmanned aerial vehicle, applied in the field of unmanned aerial vehicle, can solve the problems of increasing the failure risk of the front wing tilting mechanism, large internal stress, etc.

Active Publication Date: 2019-11-15
GOERTEK ROBTICS CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At the same time, due to the large internal stress in the front wing, the failure risk of the front wing tilting mechanism will also be greatly increased

Method used

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  • A kind of front wing tilting mechanism for unmanned aerial vehicle and unmanned aerial vehicle
  • A kind of front wing tilting mechanism for unmanned aerial vehicle and unmanned aerial vehicle
  • A kind of front wing tilting mechanism for unmanned aerial vehicle and unmanned aerial vehicle

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Embodiment Construction

[0025] Various exemplary embodiments of the present invention will now be described in detail with reference to the accompanying drawings. It should be noted that the relative arrangements of components and steps, numerical expressions and numerical values ​​set forth in these embodiments do not limit the scope of the present invention unless specifically stated otherwise.

[0026] The following description of at least one exemplary embodiment is merely illustrative in nature and in no way taken as limiting the invention, its application or uses.

[0027] Techniques, methods and devices known to those of ordinary skill in the relevant art may not be discussed in detail, but where appropriate, such techniques, methods and devices should be considered part of the description.

[0028] In all examples shown and discussed herein, any specific values ​​should be construed as exemplary only, and not as limitations. Therefore, other instances of the exemplary embodiment may have dif...

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Abstract

The invention discloses a front wing tilting mechanism for an unmanned aerial vehicle. Connected at one end, the base is configured to fix the power assembly of the UAV, and can rotate relative to the fixing fixture with the rotation of the front wing rod, and the fixing rod is configured to be fixedly connected to the main structure of the UAV , one end of the fixing rod is fixedly connected with the fixing fixture. A technical effect of the present invention is that it can drive the power assembly fixed by the mechanism to rotate.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and more specifically relates to a front wing tilting mechanism for an unmanned aerial vehicle and the unmanned aerial vehicle. Background technique [0002] UAV is the abbreviation of unmanned aircraft, which is an unmanned aircraft operated by radio remote control equipment and self-contained program control device, or operated completely or intermittently by the on-board computer. Because of its low cost, high efficiency, no risk of casualties, strong survivability, good maneuverability, and convenient use, it is currently widely used in various industries, such as military, film and television industries. [0003] In the aerospace field, the front wing of the UAV can place the horizontal stable surface in front of the main wing. It can generate vortex above the main wing, which can increase the stall angle of attack. In addition to generating vortex, the movable front wing ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C39/12B64C39/02B64C3/38
CPCB64C3/385B64C39/02B64C39/12B64U10/25B64U50/19
Inventor 侯铭硕
Owner GOERTEK ROBTICS CO LTD