发明名称 |
Enhanced performance torroidal coolant-collection manifold |
摘要 |
A system for cooling a combustion chamber of an engine, such as a rocket engine, is provided. The system has a plurality of coolant tubes or passages surrounding the combustion chamber, a torroidal coolant-collection manifold for receiving coolant from the coolant tubes or passages and for discharging the coolant through a discharge port, and a plurality of turning vanes within the torroidal manifold for reducing pressure loss and improving pressure uniformity associated with the torroidal coolant-collection manifold.
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申请公布号 |
US7373774(B2) |
申请公布日期 |
2008.05.20 |
申请号 |
US20040777435 |
申请日期 |
2004.02.12 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
CLARK JIM A.;RICCIARDO MARK |
分类号 |
F02K99/00;F02C1/04;F02K9/64;F02K9/97 |
主分类号 |
F02K99/00 |
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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