Wing capable of being automatically folded and unfolded, unmanned aerial vehicle and control method for unmanned aerial vehicle

An automatic retractable and unmanned aerial vehicle technology, applied in the field of aircraft, can solve the problems of unsightly integrated wings and excessive energy consumption, and achieve the effects of reducing impact, reducing energy consumption, and improving flight time.

Pending Publication Date: 2019-11-29
深圳飞马机器人科技有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The embodiment of the present application provides an automatic retractable wing, unmanned aerial vehicle and its control method, which can pull the retractable wing slider group through the screw rod, so as to solve the problems of unsightly appearance and excessive energy consumption of the integrated wing

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  • Wing capable of being automatically folded and unfolded, unmanned aerial vehicle and control method for unmanned aerial vehicle
  • Wing capable of being automatically folded and unfolded, unmanned aerial vehicle and control method for unmanned aerial vehicle
  • Wing capable of being automatically folded and unfolded, unmanned aerial vehicle and control method for unmanned aerial vehicle

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Embodiment Construction

[0021] In order to make the purpose, features and advantages of the present application more obvious and understandable, the technical solutions in the embodiments of the present application will be clearly and completely described below in conjunction with the drawings in the embodiments of the present application. Obviously, the described The embodiments are only some of the embodiments of the present application, but not all of them. Based on the embodiments in this application, all other embodiments obtained by those skilled in the art without making creative efforts belong to the scope of protection of this application.

[0022] see Figure 1 to Figure 6 , figure 1 A sectional view of an automatically retractable wing provided for an embodiment of the present application; figure 2 A cross-sectional view of an automatically retractable wing provided for an embodiment of the present application; image 3 A schematic diagram of an automatic retractable wing installed on ...

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Abstract

The embodiment of the invention provides a wing capable of being automatically folded and unfolded, and relates to the technical field of flight. The wing capable of being automatically folded and unfolded comprises a wing bracket, a driving device, a lead screw and a wing sliding vane group, wherein the wing bracket comprises a top end platform and a bottom end; the bottom end is fixed on the upper surface of an aircraft; the driving device is installed on the wing bracket; the lead screw and the driving device are in axis locking; the wing sliding vane group comprises a plurality of wing sliding vanes which are vertically overlaid to cover the upper surface of the top end platform; a preset distance is formed between every two wing sliding vanes; and each wing sliding vane and the lead screw are in axis connection, and each wing sliding vane is in parallel linkage with the lead screw. The invention also provides an unmanned aerial vehicle and a control method for the unmanned aerialvehicle. By use of the above wing capable of being automatically folded and unfolded, the unmanned aerial vehicle and the control method for the unmanned aerial vehicle, the raising drag of the unmanned aerial vehicle can be reduced, and power consumption is lowered.

Description

technical field [0001] The present application relates to the field of aircraft technology, in particular to an automatic retractable wing, a drone and a control method thereof. Background technique [0002] The aircraft wings added to traditional multi-rotor aircraft are generally integrated. When placed on a multi-rotor drone that takes off and lands vertically, it is not beautiful, but also greatly increases the resistance of the rising air, and also affects The maneuverability and wind resistance of the aircraft, and the waste of energy due to the consumption of a lot of kinetic energy during the ascent. Contents of the invention [0003] The embodiment of the present application provides an automatic retractable wing, an unmanned aerial vehicle and its control method, which can pull the retractable and retractable wing slider group by a screw rod, so as to solve the problems of unsightly appearance and excessive energy consumption of the integrated wing. [0004] The...

Claims

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Application Information

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IPC IPC(8): B64C3/56B64C19/00G05D1/08
CPCG05D1/0808B64C3/56B64C19/00
Inventor 黄黎明张焱
Owner 深圳飞马机器人科技有限公司
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