发明名称 |
Missile propulsion hot gas piston valve command having seat section valve sliding and second lower gas pressure closing valve when first gas supply depleted |
摘要 |
The piston valve command hot gas system has a piston valve (12) with a closing seat mechanism (25) through which gas under pressure (P2) passes. A second pressure chamber has a lower pressure (P1) initially. As the main gas supply becomes depleted, the second gas pressure closes the valve.
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申请公布号 |
FR2784444(A1) |
申请公布日期 |
2000.04.14 |
申请号 |
FR19980012959 |
申请日期 |
1998.10.13 |
申请人 |
CELERG |
发明人 |
MELLON GERARD;CHAMBAUD PHILIPPE |
分类号 |
F02K9/80;F16K31/40;(IPC1-7):F16K31/363;F42B15/01;F02K7/00 |
主分类号 |
F02K9/80 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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