发明申请
US20120151895A1 HOT GAS PATH COMPONENT COOLING FOR HYBRID PULSE DETONATION COMBUSTION SYSTEMS
审中-公开
用于混合脉冲爆震燃烧系统的热气路径组件冷却
- 专利标题： HOT GAS PATH COMPONENT COOLING FOR HYBRID PULSE DETONATION COMBUSTION SYSTEMS
- 专利标题（中）： 用于混合脉冲爆震燃烧系统的热气路径组件冷却
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申请号： US12974031申请日： 2010-12-21
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公开(公告)号： US20120151895A1公开(公告)日： 2012-06-21
- 发明人: Venkat Eswarlu Tangirala , Narendra Digamber Joshi , Adam Rasheed , Brian Gene Brzek , Douglas Carl Hofer , Thomas Michael Lavertu , Fuhua Ma
- 申请人： Venkat Eswarlu Tangirala , Narendra Digamber Joshi , Adam Rasheed , Brian Gene Brzek , Douglas Carl Hofer , Thomas Michael Lavertu , Fuhua Ma
- 申请人地址： US NY Schenectady
- 专利权人： General Electric Company
- 当前专利权人： General Electric Company
- 当前专利权人地址： US NY Schenectady
- 主分类号： F02C5/00
- IPC分类号： F02C5/00 ; F02C7/12
摘要：
The flow through the core of a hybrid pulse detonation combustion system is passed through a compressor and then separated into a primary flow, that passes directly to the combustor, and a bypass flow, which is routed to a portion of the system to be used to cool components of the system. The bypass includes a pump that raises the pressure of the bypass flow sufficient to deliver it to downstream stations of the engine that contain combustion products that are at a higher pressure than the compressor exit.