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Rapid disassembly device for rear cover of unmanned aerial vehicle

An unmanned aerial vehicle, a fast technology, applied in the field of unmanned aerial vehicles, can solve the problems of inconvenient, fast, efficient disassembly, damage to parts, complicated disassembly and assembly process, etc., to achieve the effect of easy disassembly, avoidance of damage, and simple disassembly process

Inactive Publication Date: 2019-05-21
宿迁永泰邦辰知识产权运营管理有限公司
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  • Abstract
  • Description
  • Claims
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Problems solved by technology

[0005] In view of the deficiencies in the prior art, the purpose of the present invention is to provide a quick disassembly and assembly device for the back cover of the UAV to solve the inconvenient, fast and efficient disassembly and assembly of the quick back cover of the UAV in the existing technology, and The disassembly and assembly process is complicated and easy to cause damage to parts

Method used

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  • Rapid disassembly device for rear cover of unmanned aerial vehicle
  • Rapid disassembly device for rear cover of unmanned aerial vehicle
  • Rapid disassembly device for rear cover of unmanned aerial vehicle

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Embodiment Construction

[0020] In order to make the technical means, creative features, goals and effects achieved by the present invention easy to understand, the present invention will be further described below in conjunction with specific embodiments.

[0021] see figure 1 , figure 2 and image 3 , the present invention provides a technical solution for a quick disassembly and assembly device for the back cover of an unmanned aerial vehicle: its structure includes a fixed upper cover 1, a signal indicator light 2, a flight support 3, a rotating main shaft 4, a propeller 5, a main shaft housing 6, and a landing support 7 , control button 8, heat dissipation hole 9, main engine 10, vacuum fixture 11, described flight support 3 is provided with four in total and is evenly distributed in four corners of main engine 10 and integrally formed structure, and described main shaft shell 6 upper end is provided with The circular groove of the rotating main shaft 4 is movable, the propeller 5 is mounted ...

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Abstract

The invention discloses a rapid disassembly device for a rear cover of an unmanned aerial vehicle. The device structurally includes a fixation upper cover, a signal indicating lamp, flight brackets, arotating spindle, a propeller, a spindle housing, a landing support, a control button, a heat sink hole, a main engine and a vacuum fixation device. The four flight brackets are uniformly distributedat the four corners of the main engine to form an integrally formed structure. The upper end of the spindle housing is provided with a circular groove movably mounted on the rotating spindle. The device has the advantages that the arranged vacuum fixation device achieves automatic vacuum adsorption through a spring-driven vacuum suction cup, thus the upper cover body is fixed with a main engine body, the control button controls a transmission pin to press the vacuum suction cup downwards, vacuum release thus can be achieved, the upper cover body and the main engine body can be dismantled conveniently, the dismantling process is simple, fast and efficient, and the damage of the dismantling process to parts is avoided.

Description

technical field [0001] The invention is a quick disassembly and assembly device for the back cover of an unmanned aerial vehicle, which belongs to the field of unmanned aerial vehicles. Background technique [0002] At present, small multi-rotor drones have been widely used in many fields such as aerial photography, rescue, forest fire prevention, and security. In emergency special occasions, UAVs are required to be assembled quickly to save time. The common assembly methods of the back cover and the base of the UAV include screw-fixed type, buckle type, lace-up type, and bayonet type. However, these assembly methods generally require a certain amount of time and will increase a certain amount of weight. [0003] The prior art discloses a quick disassembly and assembly device for the back cover of the drone with the application number of 201520396638.1. The lower edge of the back cover of the drone is fixedly connected with a first magnet, and there are also second magnets ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/08B64C1/14
Inventor 罗海洋
Owner 宿迁永泰邦辰知识产权运营管理有限公司
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