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.
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
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