Reusable multi-connected-pipe air pressure emitter structure and using method thereof

Abstract

The invention discloses a reusable multi-connected-pipe air pressure emitter structure and a using method of the reusable multi-connected-pipe air pressure emitter structure. The launcher structure comprises a high-pressure tank, a low-pressure tank, a control gas collecting pipe and a launching cylinder; the high-pressure tank is communicated with the low-pressure tank, the low-pressure tank is communicated with the launching cylinder, and the control gas collecting pipe is also communicated with the high-pressure tank; and the control gas collecting pipe is a closed pipeline for storing control gas for controlling opening and closing of the emission valve. Compressed air provided by the compressor serves as a launching power source, and the device has the advantages of being capable of being conveniently and repeatedly used, high in safety, high in reliability, free of light, heat and other signals during launching and good in concealment. And the inflation time is greatly shortened by adopting a high-pressure tank mode and a low-pressure tank mode.

Description

technical field [0001] The invention belongs to the field of aerodynamic launch of unmanned aerial vehicles, in particular to a structure of a reusable multi-tube pneumatic launcher and a method for using the same. Background technique [0002] Cruise missiles, also known as suicide drones, are the result of a fusion of advanced small drone technology and precision-guided munitions technology. It can quickly reach the target area, and can perform single or multi-task precision guided weapons in the target area, such as roving flight, battlefield reconnaissance and surveillance, target position guidance, damage effect assessment, aerial wireless relay and precision strike targets, and traditional weapons. In comparison, loitering missiles have many obvious advantages. [0003] Due to the limitation of detection ability, weapon load, endurance time and other factors, a single UAV has low carrying capacity, maneuverability, and protection ability, making it difficult to comple...

AI Technical Summary

Problems solved by technology

[0008] The purpose of the present invention is to avoid the problem of poor concealment of the gunpowder-type gas-generating agent / rocket booster; to avoid cumbersome steps such as replacing the gas-generating agent and cleaning the gunpowder residue in the system when the gas-generating agent is used repeatedly; to avoid the long response time of the hydraulic method , the problem of high system failure rate; avoid the long interval between the launch of multiple cruise missiles in the existing air pressure launch method, which is easy to expose the location of the launch position, and the safety of soldiers and the difficulty of task execution are difficult to guarantee.

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