Unmanned flying robot launched based on compressed gas cold booster

A flying robot and compressed gas technology, applied in the field of unmanned aerial robots and flying robots, can solve the problems of the aircraft's effective flight time not being well utilized, increasing the time to reach the mission area, being shot down, damaged, and consumed by the opponent.

Active Publication Date: 2021-05-14
北京理工伺服科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

It can be seen that the existing unmanned aerial vehicles cannot combine the hovering advantage of helicopters with the fast flight of winged aircraft. When there are disaster relief and battlefield flight missions, the flight speed is relatively slow, which increases the time to reach the mission area and is shot down or damaged by the opponent. chance of
Moreover, a large amount of energy and fuel carried by the aircraft are consumed during the lift-off stage of the aircraft, which cannot make good use of the effective flight time of the aircraft.

Method used

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  • Unmanned flying robot launched based on compressed gas cold booster
  • Unmanned flying robot launched based on compressed gas cold booster
  • Unmanned flying robot launched based on compressed gas cold booster

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Embodiment Construction

[0025] The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0026] The present invention provides a kind of unmanned aerial robot based on compressed gas cold-assisted launch, unmanned aerial robot 17 utilizes the compressed air of compressed gas cold-assisted launching mechanism compressed air as auxiliary power to carry out ejection and take-off, and unmanned aerial robot 17 takes off with its own The main thrust of the turbojet realizes the horizontal flight of the unmanned flying robot 17, and the flight direction change and vertical lift of the unmanned flying robot 17 are realized with the auxiliary electric drive as the auxiliary power.

[0027] as attached figure 1 and 2 As shown, the unmanned aerial robot 17 includes a robot housing 1, an auxiliary electric turbofan 2, a swing motor 3, a transmission mechanism 4, a frame-type mission cabin 5, a mission load 6, a gyroscope 7, a control module 8, a power ba...

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Abstract

The invention discloses an unmanned flying robot based on compressed gas cold-assisted launch, and belongs to the technical field of unmanned aerial vehicles and compressed air-assisted cold launch. The invention belongs to the technical field of unmanned aerial vehicle and compressed air assisting cold launch. The unmanned flying robot uses compressed air as the auxiliary power for ejection and take-off. After the unmanned flying robot is lifted into the air, the power generated by the turbojet engine is used as the main thrust to realize the horizontal attitude flight of the unmanned flying robot, and the auxiliary electric drive is used as the auxiliary power to realize unmanned flying. The flight state of the human flying robot changes and vertical lift, and the payload cabin inside the unmanned flying robot releases the payload to the air and the ground by folding the mechanical arm, or grabs or recovers ground items by folding the mechanical arm. The invention can realize free switching flight of two kinds of speeds and two kinds of flying postures, and greatly improves the diversity of disaster relief missions of unmanned flying robots and the stealth and survival rate of battlefields.

Description

technical field [0001] The invention relates to a flying robot, in particular to an unmanned flying robot for cold-assisted launch, and belongs to the technical field of unmanned aerial vehicles and compressed air-assisted cold launch. Background technique [0002] At present, the existing military and civilian rotor UAVs are all single-rotor, and the multi-rotor UAV and its winged UAV are developed according to the technical solution of manned aircraft, or simplified manual operation, or Some intelligent operation. It can be seen that the existing unmanned aerial vehicles cannot combine the hovering advantage of helicopters with the fast flight of winged aircraft. When there are disaster relief and battlefield flight missions, the flight speed is relatively slow, which increases the time to reach the mission area and is shot down or damaged by the opponent. probability. Moreover, the energy and fuel carried by a large amount of aircraft are consumed during the lift-off st...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C39/02B64F1/06
CPCB64C39/02B64F1/06B64U50/12B64U70/70B64U2101/00
Inventor 姚晓先周莉焦让万吉王因翰
Owner 北京理工伺服科技有限公司
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