发明名称 |
Circumferentially varied quench jet arrangement for gas turbine combustors |
摘要 |
A combustor for a turbine engine is provided. The combustor includes a first liner; a second liner positioned relative to the first liner to form a combustion chamber therebetween, the combustion chamber configured to receive a fuel-air mixture; an igniter positioned relative to the combustion chamber and configured to ignite the fuel-air mixture; a first group of air admission holes positioned in the first liner and forming a regular circumferential pattern around the first liner; and a second group of air admission holes positioned in the first liner at a first circumferential position corresponding to the igniter, the second group of air admission holes departing from the regular circumferential pattern.
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申请公布号 |
US8584466(B2) |
申请公布日期 |
2013.11.19 |
申请号 |
US20100720431 |
申请日期 |
2010.03.09 |
申请人 |
BRONSON THOMAS J.;ZUPANC FRANK J.;HONEYWELL INTERNATIONAL INC. |
发明人 |
BRONSON THOMAS J.;ZUPANC FRANK J. |
分类号 |
F02C1/00;F02G3/00 |
主分类号 |
F02C1/00 |
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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