Satellite-used bilateral shearing-type normally-closed titanium alloy gunpowder fuel gas actuated valve

A titanium alloy and double-sided technology is applied in the field of double-sided cut-off titanium alloy propellant gas actuated valves for satellites. It can solve the problems of high quality, poor sealing and stability, and achieve light weight, improved reliability, and The effect of mitigating product quality

Inactive Publication Date: 2013-04-10
NO 11 INST OF NO 6 ACADEMY OF CHINA AEROSPACE SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In order to solve the technical problems of large mass, poor sealing performance and low stability of the existing propellant and gas actuated valve, the present invention provides a double-sided cut-off normally closed titanium allo

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  • Satellite-used bilateral shearing-type normally-closed titanium alloy gunpowder fuel gas actuated valve
  • Satellite-used bilateral shearing-type normally-closed titanium alloy gunpowder fuel gas actuated valve

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Embodiment Construction

[0024] Such as figure 1 As shown, the double-sided cut-off type normally closed titanium alloy gunpowder gas actuated valve for satellites of the present invention mainly includes a base body 1, a blind pipe assembly 2, a cutter 3, an anti-burning ring 4, a sealing ring 5, a screw plug 6, a sealing Sheet 7, plug 8, welding sheet 9, the cutter is set in the inner cavity of the base body and sealed with the base body through the sealing assembly, the inner cavity of the base body forms a high-pressure and high-temperature gas chamber 10, a cutter channel 11 and a chip chamber 13 in turn, and a blind pipe Component 2 is fixed on the substrate and runs through the substrate and the cutter channel,

[0025] Wherein the blind pipe assembly 2 comprises a connector 21, a first channel 22 and a second channel 23, one end of the connector 21 is connected to the first channel 22, the other end of the connector 21 is connected to the second channel 23, and the center of the connector 21 ...

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Abstract

The invention relates to a satellite-used bilateral shearing-type normally-closed titanium alloy gunpowder fuel gas actuated valve, which mainly comprises a matrix, a blind pipe component, a cutter, a burning resisting ring, a seal ring, a choke plug, a sealing fin, a plug and a soldering flake, wherein the cutter is arranged in an inner chamber of the matrix and is in matching seal with the matrix through a seal component; a high-pressure high-temperature fuel gas chamber, a cutter channel and a cuttings chamber are formed in the inner chamber of the matrix in sequence; and the blind pipe component is fixed on the matrix and runs through the matrix and the cutter channel. Conical surface wedge tightness seal is formed by the cutter and the matrix after the cutter acts, so that the seal reliability and resistance to pressure of the valve are improved after the valve acts, thereby being beneficial for long-term storage of a medium.

Description

technical field [0001] The invention relates to a double-sided cut-off type normally closed titanium alloy gunpowder gas actuated valve for satellites, which is used in different parts of satellite propulsion subsystems to control the opening of helium and propellants. Background technique [0002] The gunpowder gas actuated valve is one of the important automatic components in various systems of aerospace models, and plays a role in fluid control in the system. The gunpowder gas actuated valve is actuated by the high-pressure gas generated by the combustion of gunpowder. It has the characteristics of good sealing, small size, light weight, fast response, and it can actuate high-voltage energy with only a small pulse power supply. Therefore, Widely used in liquid rocket engines. At present, in various aerospace model systems in our country, the gunpowder gas actuated valve is mostly used in the workplace where the working medium is isolated and closed. However, the existin...

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Application Information

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IPC IPC(8): F16K3/02F16K3/314F16K3/30F16K27/10
Inventor 陶正陈炜段增斌孙彦堂袁洪滨黄清伟李海王运卯谭屏刘立创王胜强赵文华吴晓东
Owner NO 11 INST OF NO 6 ACADEMY OF CHINA AEROSPACE SCI & TECH
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