Movable unmanned aerial vehicle gas-liquid power ejection system

A machine-air-liquid and mobile technology, applied in the field of UAV launch, can solve the problems of strong electromagnetic interference of electromagnetic ejection, complex structure of air-liquid ejection, and limited power, and achieve high energy efficiency, large speed-up ratio, maneuverability Good flexibility

Inactive Publication Date: 2019-11-08
BEIJING INST OF SPECIALIZED MACHINERY
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  • Summary
  • Abstract
  • Description
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  • Application Information

AI Technical Summary

Problems solved by technology

[0007] The technical problem to be solved by the present invention is: how to realize a new gas-liquid ejection system for unmanned aerial vehicles that can meet the ejection and launch requirements of large and medium-sized UAVs, so as to overcome the shortcomings of existing gas-liquid ejection structures such as complex structure and limited power , and avoid problems such as strong electromagnetic interference caused by electromagnetic ejection

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  • Movable unmanned aerial vehicle gas-liquid power ejection system
  • Movable unmanned aerial vehicle gas-liquid power ejection system

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Embodiment Construction

[0025] In order to make the purpose, content, and advantages of the present invention clearer, the specific implementation manners of the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.

[0026] The present invention provides a movable unmanned aerial vehicle gas-hydraulic power ejection system, which is an ejection device related to fluid transmission, such as figure 1 As shown, the system includes a flatbed car 1, a first swivel lug 2, a tripod 3, a release mechanism 4, a first sliding trolley 5, a second swivel lug 6, a lifting cylinder 7, a third swivel lug 8, a A guide pulley 9, a fixed pulley 10, a movable pulley 11, a second sliding trolley 12, an energy storage tank 13, a nozzle 14, a launching frame 15, a launching guide rail 16, a buffer energy-absorbing device 17, a second guide pulley 18, a steel wire rope 19, Limit block 20, acceleration guide rail 21;

[0027] The upper surface of the fla...

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Abstract

The invention relates to a movable unmanned aerial vehicle gas-liquid power ejection system, and relates to the technical field of unmanned aerial vehicle launching. According to the system, an ejection mode of an unmanned aerial vehicle is changed, reverse thrust generated from high-pressure water jetting is directly used as ejection power, an ejection speed is increased by means of pulleys, theenergy secondary conversion is avoided, the energy efficiency is high, the system structural composition is simple, the speed increasing ratio is large, the maneuvering flexibility is good, the problems of electromagnetic interference and the like are avoided, and the system can be widely applied to catapult-assisted take-off of -fixed-wing unmanned aerial vehicles of various types.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a gas-hydraulic power ejection system for a movable unmanned aerial vehicle. Background technique [0002] Catapult launch is a take-off method often used by current fixed-wing UAVs. It can significantly increase the gliding speed of the UAV under the action of external force and shorten the take-off and gliding distance. At present, the main ejection methods of UAVs include elastic ejection, electromagnetic ejection and pneumatic ejection. [0003] Among them, due to the limited energy storage of elastic ejection, the ejection power is very small; although the mechanical structure of electromagnetic ejection is simple, the electronic control device is complex, and there is still a "congenital" defect, that is, it will generate strong electromagnetic interference, which will affect electromechanical equipment and electronic control. System reliability. [0004]...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/06
CPCB64F1/06B64U70/70
Inventor 张振华李春萍吴向阳王飞申文强
Owner BEIJING INST OF SPECIALIZED MACHINERY
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