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A locking component and a multi-rotor unmanned aerial vehicle

A multi-rotor unmanned and aircraft technology, applied in the field of drones, can solve the problems of large wheelbase, large volume, inconvenient handling and storage of aircraft, and achieve the effect of reliable maintenance and reduced volume

Inactive Publication Date: 2017-06-16
无锡龙腾创新科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The rotors of the existing multi-rotor aircraft are supported by the arms, and the arms are usually fixed on the frame, so when the aircraft reaches six or even eight axes, the wheelbase of the entire aircraft will become very large and the volume will be accompanied by Larger, causing great inconvenience to handling, storage, etc.

Method used

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  • A locking component and a multi-rotor unmanned aerial vehicle
  • A locking component and a multi-rotor unmanned aerial vehicle
  • A locking component and a multi-rotor unmanned aerial vehicle

Examples

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Embodiment Construction

[0041] The specific embodiments of the present invention will be further described below in conjunction with the accompanying drawings.

[0042] Embodiments of the present invention are described in detail below, examples of which are shown in the drawings, wherein the same or similar reference numerals designate the same or similar elements or elements having the same or similar functions throughout. The accompanying drawings are used to help understand various embodiments of the present invention, and the scales of the figures in the accompanying drawings may be different. The embodiments described below by referring to the figures are exemplary only for explaining the present invention and should not be construed as limiting the present invention. On the contrary, the embodiments of the present invention include all changes, modifications and equivalents coming within the spirit and scope of the appended claims. In the description of the present invention, it should be und...

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PUM

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Abstract

The invention discloses a locking component and a multi-rotor unmanned aerial vehicle. The locking component (150) is used for locking a plurality of supporting arms (110) on a center installation base (120) when the plurality of supporting arms (110) of the multi-rotor unmanned aerial vehicle (1000) are unfolded, wherein a plurality of notch portions (122) are uniformly formed in the center installation base (120) in the circumferential direction, a plurality of bulge portions (112) are correspondingly arranged on the plurality of supporting arms (110), and the bulge portions (112) are positioned in the notch portions (122) when the plurality of supporting arms (110) are unfolded. According to the invention, the plurality of supporting arms are locked on the center installation base for one time simultaneously by the locking component when the plurality of supporting arms of the multi-rotor unmanned aerial vehicle are unfolded, and the plurality of supporting arms are reliably maintained at an unfolded state.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to a locking assembly and a multi-rotor unmanned aerial vehicle equipped with the locking assembly. Background technique [0002] Unmanned aerial vehicles have unique flight capabilities and are small in size. They have broad prospects in aerial photography, atmospheric detection, traffic monitoring, resource exploration, power inspection, forest fire prevention, agriculture, and military use. [0003] The rotors of the existing multi-rotor aircraft are supported by the arms, and the arms are usually fixed on the frame, so when the aircraft reaches six or even eight axes, the wheelbase of the entire aircraft will become very large and the volume will be accompanied by Larger, causing great inconvenience to handling, storage, etc. Contents of the invention [0004] The object of the present invention is to provide a multi-rotor unmanned aerial vehicle,...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C27/37
Inventor 王建策
Owner 无锡龙腾创新科技有限公司
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