Ground inflation guarantee air source equipment for ground blow-turn launching of unmanned aerial vehicle

Abstract

The invention discloses ground inflation guarantee air source equipment for ground blow-turn launching of an unmanned aerial vehicle, and belongs to the technical field of configuration of power devices, the ground inflation guarantee air source equipment comprises a high-pressure air storage system, a blow-turn connection pressure control system, a pipeline and an air source trailer, and the high-pressure air storage system and the blow-turn connection pressure control system are installed in the air source trailer; the high-pressure air storage system is connected with the blow-turn connection pressure control system, the high-pressure air storage system comprises a composite gas cylinder, a gas cylinder valve, a T01 exhaust valve, an L1 filter, a T2 stop valve and an AF1 safety valve, the composite gas cylinder is connected with the gas cylinder valve through a pipeline, the gas cylinder valve is connected with the T01 exhaust valve, the L1 filter and the AF1 safety valve through pipelines, and the filter L1 is connected with the stop valve T2 through the pipeline. The output high-pressure gas drives the rotor of the unmanned aerial vehicle engine to rotate at a high speed, after the unmanned aerial vehicle engine reaches a certain initial speed, the unmanned aerial vehicle engine can secondarily increase the rotating speed through ignition of a small amount of fuel oil, and unmanned aerial vehicle launching is achieved.

Description

Technical field [0001] Technical Field The present invention belongs to the configuration of the power unit, especially for a large blow UAV powered rotation emission source, particularly, to a method for UAV ground floor turn transmitted blowing air inflatable protection device. Background technique [0002] With the development of UAV project, we have developed a multi-purpose UAV to suitable for various applications; small UAVs to use more electronically controlled engine off, but large-scale use of unmanned aircraft is fuel driven engine way for transmission, this approach will have a large UAV engine and power demanding facilities, resulting in large UAS engine fuel weight also will be greatly increased. Thus, to reduce the weight of the UAV, UAV improve and optimize performance, is urgently needed to develop a large number of power sources can be avoided using the apparatus large UAS driving fuel transferred blowing emitted. Inventive content [0003] The present invention...

AI Technical Summary

Problems solved by technology

[0002] With the development of my country's UAV project, a variety of UAVs have been developed to be suitable for applications in various fields; small UAVs mostly use electronically controlled engines to take off, but large UAVs use fuel-driven engines This method will have high requirements on the engine power and supporting facilities of large UAVs, which will greatly increase the fuel weight of the engines of large UAVs.

Images