发明名称 |
Cooling scheme for scramjet variable geometry hardware |
摘要 |
A cooling system for use in an engine having an element to be cooled includes at least one cooling channel on a first side of the element, at least one cooling channel on a second side of the element, and the at least one cooling channel on the first side communicating with the at least one channel on the second side in a nose region of the element so as to form a cooling circuit. The cooling system has particular utility in cooling interior and exterior surfaces of a movable cowl inlet flap used in a scramjet engine.
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申请公布号 |
US2005235629(A1) |
申请公布日期 |
2005.10.27 |
申请号 |
US20040829890 |
申请日期 |
2004.04.22 |
申请人 |
CUVA WILLIAM J;PAULUS DONALD E |
发明人 |
CUVA WILLIAM J.;PAULUS DONALD E. |
分类号 |
F02K1/00;F02K7/10;F02K7/14;(IPC1-7):F02K1/00 |
主分类号 |
F02K1/00 |
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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