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Small fixed wing unmanned aerial vehicle ejector rack

An aircraft ejection rack and fixed-wing technology, applied in the field of unmanned aerial vehicles, can solve the problems of inconvenient portability, difficult assembly, and heavy unmanned aerial vehicle ejection racks, etc., and achieve the effects of simple structure, high ejection reliability and light weight.

Active Publication Date: 2016-10-12
TIANXUN INNOVATION BEIJING TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to overcome the defects of bulky, inconvenient carrying and difficult assembly of the existing UAV ejection frame, and provide a small fixed-wing UAV ejection frame that is portable and easy to assemble

Method used

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  • Small fixed wing unmanned aerial vehicle ejector rack
  • Small fixed wing unmanned aerial vehicle ejector rack
  • Small fixed wing unmanned aerial vehicle ejector rack

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Embodiment Construction

[0025] In order to make the technical problems, technical solutions and beneficial effects solved by the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0026] In describing the present invention, it is to be understood that the terms "radial", "axial", "upper", "lower", "top", "bottom", "inner", "outer" etc. indicate orientation Or the positional relationship is based on the orientation or positional relationship shown in the drawings, which is only for the convenience of describing the present invention and simplifying the description, and does not indicate or imply that the referred device or element must have a specific orientation, be constructed and operated in a specific orientation , and therefore cannot be const...

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Abstract

The invention relates to the technical field of unmanned aerial vehicles, in particular to a small fixed wing unmanned aerial vehicle ejector rack. The small fixed wing unmanned aerial vehicle ejector rack comprises a telescopic tripod mechanism and an unmanned aerial vehicle supporting mechanism arranged at the upper end of the tripod mechanism, wherein the unmanned aerial vehicle supporting mechanism comprises a supporting base, a supporting pipe, a T-shaped quick release plug pin, a T-junction, carbon tubes and a wing limiting piece, two first pin joint holes are symmetrically formed in the two sides of the supporting base, and second pin joint holes parallel to the first pin joint holes are further symmetrically formed in the two sides of the supporting base; one end of the supporting pipe is in pin joint with the supporting base at the positions of the first pin joint holes, and the T-shaped quick release plug pin is inserted into the second pin joint holes to prevent the supporting pipe from falling down; the other end of the supporting pipe is connected with the vertical connector of the T-junction, and the two horizontal connectors of the T-junction are connected with the carbon tubes respectively; the wing limiting piece is of a cantilever structure and used for clamping a wing between the wing limiting piece and the carbon tubes. The small fixed wing unmanned aerial vehicle ejector rack can be quickly installed, and is small in size and convenient to carry.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a small-sized fixed-wing unmanned aerial vehicle launcher. Background technique [0002] Fixed-wing UAVs are generally used for aerial tasks such as data collection, aerial surveying and mapping, border patrol, and police investigation. It can realize multi-purpose functions such as military reconnaissance, disaster assessment, surveying and mapping aerial photography, weather detection, aerial photography, town planning, etc. It can also be used for non-military tasks such as flight test and aerial surveying and mapping. Compared with rotorcraft, fixed-wing UAVs have high efficiency, wide operating area, long flight time and can perform tasks more flexibly. Due to the take-off site requirements of fixed-wing UAVs, there are high requirements for the ejection method of the body, which is not only convenient and practical, but also reliable and efficient. [000...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/06B64C39/02
CPCB64C39/02B64F1/06B64U10/25
Inventor 王川杨威陈文涛马聪孟吉庆
Owner TIANXUN INNOVATION BEIJING TECH CO LTD
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