发明名称 |
COMBUSTORS WITH QUENCH INSERTS |
摘要 |
A combustor is provided for a turbine engine. The combustor includes a first liner having a first hot side and a first cold side; a second liner having a second hot side and a second cold side, the second hot side and the first hot side forming a combustion chamber therebetween. The combustion chamber is configured to receive an air-fuel mixture for combustion therein. The combustor further includes an insert having a body portion extending through the first liner and terminating at a tip, the body portion configured to direct air flow into the combustion chamber. The insert further includes a cooling hole defined in the body portion and configured to direct a first portion of the air flow toward the tip as cooling air.
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申请公布号 |
US2012297778(A1) |
申请公布日期 |
2012.11.29 |
申请号 |
US201113116897 |
申请日期 |
2011.05.26 |
申请人 |
RUDRAPATNA NAGARAJA S.;FRYE LOWELL;LANDRAM WILLIAM;HONEYWELL INTERNATIONAL INC. |
发明人 |
RUDRAPATNA NAGARAJA S.;FRYE LOWELL;LANDRAM WILLIAM |
分类号 |
F23M5/08;B21D53/00;F23M5/00 |
主分类号 |
F23M5/08 |
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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