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A small fixed-wing unmanned aerial vehicle launcher

A technology of aircraft ejection frame and fixed wing, which is applied in the field of drones, can solve the problems of inconvenient carrying, difficult assembly, and bulky UAV ejection frame, etc., and achieves the effect of simple structure, high ejection reliability and light weight

Active Publication Date: 2018-08-24
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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  • A small fixed-wing unmanned aerial vehicle launcher
  • A small fixed-wing unmanned aerial vehicle launcher
  • A small fixed-wing unmanned aerial vehicle launcher

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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-sized fixed-wing unmanned aerial vehicle ejection frame, which includes a retractable tripod mechanism and an unmanned aerial vehicle support mechanism arranged on the upper end of the tripod mechanism; the unmanned aerial vehicle support mechanism includes a support seat, Support pipe, T-shaped quick release pin, T-shaped tee joint, carbon pipe and wing limit piece; two first pin connection holes are symmetrically arranged on both sides of the support seat, and two first pin connection holes are symmetrically arranged on both sides of the support seat. A second pin connection hole parallel to the first pin connection hole; one end of the support tube is pinned to the support seat at the first pin connection hole, and the T-shaped quick release pin is inserted into the second pin connection hole so that the support tube will not fall The other end of the support pipe is connected to the vertical joint of the T-shaped tee joint, and the two horizontal joints of the T-shaped tee joint are respectively connected to the carbon pipe; Between the wing limiter and the carbon tube. The invention can be assembled quickly, has small volume and is 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 Patents(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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