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.
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
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