发明名称 |
Stagnation pressure activated fuel release mechanism for hypersonic projectiles |
摘要 |
A propulsion-assisted projectile has a body, a cowl forming a combustion section and a nozzle section. The body has a fuel reservoir within a central portion of the body, and a fuel activation system located along the central axis of the body and having a portion of the fuel activation system within the fuel reservoir. The fuel activation system has a fuel release piston with a forward sealing member where the fuel release piston is adapted to be moved when the forward sealing member is impacted with an air flow, and an air-flow channel adapted to conduct ambient air during flight to the fuel release piston.
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申请公布号 |
US2002124758(A1) |
申请公布日期 |
2002.09.12 |
申请号 |
US20010799572 |
申请日期 |
2001.03.07 |
申请人 |
CARTLAND HARRY E.;HUNTER JOHN W. |
发明人 |
CARTLAND HARRY E.;HUNTER JOHN W. |
分类号 |
F02K7/10;F42B15/10;(IPC1-7):F42B15/10 |
主分类号 |
F02K7/10 |
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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