发明名称 |
Secondary Combustion System |
摘要 |
The present application provides a secondary combustion system for introducing a fuel/air mixture into a flow of combustion gases in a combustor of a gas turbine engine. The secondary combustion system may include a manifold ring and a number of injectors extending from the manifold ring. Each of the injectors may include a number of jets in communication with the manifold ring. One or more of the jets may include an angled configuration for the introduction of the fuel/air mixture into the flow of combustion gases at an angle.
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申请公布号 |
US2013298563(A1) |
申请公布日期 |
2013.11.14 |
申请号 |
US201213470577 |
申请日期 |
2012.05.14 |
申请人 |
HAYNES JOEL MEIER;JOHNSON THOMAS EDWARD;GENERAL ELECTRIC COMPANY |
发明人 |
HAYNES JOEL MEIER;JOHNSON THOMAS EDWARD |
分类号 |
F23R3/28 |
主分类号 |
F23R3/28 |
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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