Launch control unmanned aerial vehicle

A technology of unmanned aerial vehicle and landing gear, applied in the field of aircraft, can solve the problems of high site requirements, inconvenient throwing and take-off, unfavorable control, etc., and achieve the effects of saving power, simple structure and long battery life

Inactive Publication Date: 2018-04-27
FOSHAN SHENHANG SCI & TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The traditional fixed-wing aircraft model needs a flat open space to take off, and has high requirements for the site. For miniature aircr

Method used

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  • Launch control unmanned aerial vehicle

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Embodiment Construction

[0011] The present invention will now be described in detail with reference to the drawings. A catapult-starting drone includes a drone body 1, a landing gear 2, a high-pressure air chamber 3, and a controller 4.

[0012] The landing gear 2 is placed under the main body of the drone. There are four landing gears, which are symmetrically distributed and have the same function. The controller 4 is placed on the drone body 1. The high-pressure air cabin 3 is placed on the drone body 1 and connected to the controller 4. The inner through hole of the landing gear 2 is connected with the high-pressure air chamber 3. The inflation and deflation of the high-pressure air chamber 3 are performed through the holes of the landing gear 2.

[0013] The working process of the ejection-start UAV: ​​Inflate the high-pressure air cabin 3 through external equipment. After the inflation is completed, use the controller 4 to open the high-pressure air cabin 3, and the gas is ejected from the through ...

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Abstract

The invention relates to a launch control unmanned aerial vehicle and belongs to the field of aircrafts. The launch control unmanned aerial vehicle comprises an unmanned aerial vehicle body, an undercarriage, a high-pressure gas cabin and a controller. The undercarriage is arranged below the unmanned aerial vehicle body. The controller is arranged on the unmanned aerial vehicle body. The high-pressure gas cabin is arranged on the unmanned aerial vehicle body and connected with the controller. An internal through hole of the undercarriage is connected with the high-pressure gas cabin. Accordingto the launch control unmanned aerial vehicle, the principle is simple, the structure is simple, launch control is achieved, the head-start effect is achieved, a power supply is saved, and the higherendurance ability is achieved.

Description

Technical field [0001] A catapult-starting UAV belongs to the field of aircraft, and particularly relates to a UAV. Background technique [0002] Traditional fixed-wing aircraft models require a flat area for take-off, which has high requirements on the field. For miniature aircraft, it can take off by throwing. However, larger aircraft models obviously cannot take off by throwing; and throwing takes off. Convenient, not conducive to manipulation. Summary of the invention [0003] The solution of the present invention is to invent a catapult-starting drone in order to overcome the shortcomings of the foregoing solution. [0004] A catapult-starting drone includes a drone body, a landing gear, a high-pressure air chamber and a controller. [0005] The landing gear is placed under the drone body. The controller is placed on the drone body. The high-pressure air chamber is placed on the drone body and connected with the controller. The inner through hole of the landing gear is conne...

Claims

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Application Information

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IPC IPC(8): B64C39/02B64C25/32B64C15/14A63H27/00A63H27/32
CPCA63H27/02B64C15/14B64C25/32B64C39/02B64U70/00
Inventor 王美航
Owner FOSHAN SHENHANG SCI & TECH CO LTD
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