发明名称 Missile thrust system and valve with refractory piston cylinder
摘要 An improved pneumatic valve and a missile with an improved thrust directional valve. In one embodiment, a refractory material lining for a pneumatic valve enables better valve operation and better valve performance. A thin-wall cylindrical sleeve of rhenium or other suitable refractory metal is located inside a cylinder. A valve piston may then travel within the refractory sleeve with greater reliability and better operation. The refractory sleeve cylinder lining can be subject to high temperatures at a rapid rate and remain operational. Under such a hostile environmental, including corrosive/erosive environments created by the passage of hot propellant gasses, the refractory cylinder sleeve has a more reliable operational life and is lighter in weight than conventional valves made entirely of refractory metals
申请公布号 US2004025939(A1) 申请公布日期 2004.02.12
申请号 US20020216622 申请日期 2002.08.09
申请人 WOESSNER GEORGE T. 发明人 WOESSNER GEORGE T.
分类号 F02K9/56;F16L7/00;(IPC1-7):F16L7/00 主分类号 F02K9/56
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