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A small unmanned aerial vehicle ejection device and unmanned aerial vehicle take-off method

A technology of a small unmanned aerial vehicle and an ejection device, which is applied in the field of unmanned aerial vehicle take-off, can solve the problems of high price, difficult to apply to small and medium-sized unmanned aerial vehicles, and complicated structure of the ejection mechanism, and achieves a portable, light weight and simple structure. Effect

Active Publication Date: 2019-04-02
TIANXUN INNOVATION BEIJING TECH CO LTD
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  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The first object of the present invention is to provide a small unmanned aerial vehicle ejection device, and the second object of the present invention is to provide a small unmanned aerial vehicle take-off method to solve the problem that the existing ejection mechanism is complex in structure, expensive, and difficult to apply The problem with small and medium drones

Method used

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  • A small unmanned aerial vehicle ejection device and unmanned aerial vehicle take-off method
  • A small unmanned aerial vehicle ejection device and unmanned aerial vehicle take-off method
  • A small unmanned aerial vehicle ejection device and unmanned aerial vehicle take-off method

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Embodiment Construction

[0035] Hereinafter, embodiments of the ejection device for a small drone and the method for taking off the drone of the present invention will be described with reference to the accompanying drawings.

[0036] The examples described here are specific specific implementations of the present invention, and are used to illustrate the concept of the present invention. They are all explanatory and exemplary, and should not be construed as limiting the implementation of the present invention and the scope of the present invention. In addition to the embodiments described here, those skilled in the art can also adopt other obvious technical solutions based on the claims of the application and the contents disclosed in the description, and these technical solutions include adopting any obvious changes made to the embodiments described here. Replacement and modified technical solutions.

[0037] The accompanying drawings in this specification are schematic diagrams, which assist in exp...

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Abstract

The invention discloses a small unmanned aerial vehicle ejection device and an unmanned aerial vehicle take-off method. The small unmanned aerial vehicle ejection device includes: a body support assembly, and the body support assembly is used to support the unmanned aerial vehicle body and install other parts; Wing support assembly, one end of the wing support assembly is connected to the rear of the body support assembly, the wing support assembly is used to support the wings of the drone; a locking device, the locking device is installed on the The front part of the body support assembly is used to lock the ejection hook of the drone before take-off; the ejection switch is used to control the opening and closing state of the locking device; the level is installed on the The upper surface of the body support assembly. The small-sized unmanned aerial vehicle ejection device of the present invention is more convenient to carry, simple and easy to operate, so that the reliability of the unmanned aerial vehicle is higher. In addition, the functions are more diverse, it is convenient to use in small UAV systems, and it has the advantages of light weight, small size, and simple structure.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicle take-off, and in particular relates to a small-sized unmanned aerial vehicle ejection device and a method for unmanned aerial vehicle take-off realized by using the ejection device. Background technique [0002] At present, UAVs have been widely used in aerial photography, agriculture, plant protection, selfie, express delivery, disaster relief, observation of wild animals, monitoring of infectious diseases, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, etc. application. Due to the high cost of drones, users and businesses want drones to have fewer accidents. [0003] Accidents of UAVs mainly occur during the take-off phase. Using the auxiliary launch device to take off the UAV can improve the success rate of UAV launch. The ejection mechanism realizes the instantaneous acceleration of the ejection object by using the pre-...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64F1/06
CPCB64F1/06B64U70/70
Inventor 王川杨威侯家兴
Owner TIANXUN INNOVATION BEIJING TECH CO LTD
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