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Reverse detonation driven generator for high speed loading

A generator and detonation technology, applied in the field of ultra-high-speed impact loading test, can solve the problems of poor effect, the complexity of the applicability acceleration equipment, etc., and achieve the effect of simple structure, wide application range and good reliability

Active Publication Date: 2018-06-01
BEIJING INSTITUTE OF TECHNOLOGYGY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Based on the above background, light gas cannon and other high-speed launch technologies, such as explosive detonation launch technology, electromagnetic propulsion technology, directional concentrated energy accelerator technology, laser-driven flyer technology, electrostatic accelerator technology, plasma acceleration technology, etc., have emerged as the times require. They have shown great interest in ultra-high-speed launch technology, and have achieved certain research results. At present, some research results have been applied to experimental research, but some technologies have a series of problems such as applicability and acceleration equipment complexity. making them less effective in practical applications

Method used

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  • Reverse detonation driven generator for high speed loading
  • Reverse detonation driven generator for high speed loading
  • Reverse detonation driven generator for high speed loading

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Embodiment Construction

[0015] The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0016] See attached figure 1 , a combustible gas detonation-driven generator for high-speed loading, which includes: a combustion chamber 1, an ignition head 2, a diaphragm 3 and a launch tube 5;

[0017] The combustion chamber 1 is a cylindrical structure with one end closed and one end open; the ignition head 2 is installed on the side wall near the opening end of the combustion chamber 1; an air injection hole 6 is opened on the side wall of the combustion chamber 1;

[0018] The launch tube 5 is a tubular structure with openings at both ends, one end of which is docked with the open end of the combustion chamber 1, and a diaphragm 3 is provided at the joint; the joint between the launch tube 5 and the combustion chamber 1 is fixed by a fastening screw barrel 7;

[0019] The projectile 4 is located in the launch tube 5 close to the diaphragm 3; before ...

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Abstract

The invention belongs to the technical field of super-high-speed collision loading tests, and particularly relates to a reverse detonation drive generator. According to the technical scheme, the reverse detonation drive generator used for high-speed loading comprises a combustion chamber, an ignition head, a membrane and an emission pipe; the ignition head is mounted on the side wall close to the opening end of the combustion chamber; before the test, hydrogen and oxygen are injected into the combustion chamber through an injection hole successively, after the set time, the ignition head is externally connected with a direct-current power source to generate electric sparks, combustible gas on the opening portion of the combustion chamber carries out detonation and is gradually spread to the tail of the combustion chamber, that is, the detonation wave spreading direction is from the back to the front, and when the pressure of the opening portion of the combustion chamber reaches the critical value, the membrane is broken, and high-temperature and high-pressure gas drives a shot; compared with a tail ignition manner, the reverse detonation drive generator has the beneficial effects that the effect of the detonation pressure on the shot loading time is improved, and the emission of the shot at the higher speed is achieved.

Description

technical field [0001] The invention belongs to the technical field of ultra-high-speed impact loading test, in particular to a reverse detonation drive generator. Background technique [0002] With the continuous development of aerospace technology, human activities in space are becoming more and more frequent. At the same time, the debris generated by space spacecraft is also increasing, which has brought long-term hidden dangers to the safety of spacecraft currently operating in low orbit. , have an extremely serious impact on the aerospace industry. The average speed of space debris hitting the spacecraft is about 10km / s, and the maximum speed is even above 20km / s. Therefore, the ground simulation experiment of space debris plays an indispensable role in the spacecraft protection design and effectiveness verification. In the ground simulation experiment of space debris, the ultra-high-speed projectile launched by the ultra-high-speed launch technology device is often us...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F41B11/70F41B11/80
CPCF41B11/70F41B11/80
Inventor 张庆明陆阳予龙仁荣施尚春薛一江陈利
Owner BEIJING INSTITUTE OF TECHNOLOGYGY
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