发明名称 |
SYSTEMS AND APPARATUS RELATING TO COMBUSTOR COOLING AND OPERATION IN GAS TURBINE ENGINES |
摘要 |
A combustor for a gas turbine engine that includes first and second combustion chambers interconnected by a throat region that includes a converging wall section, a diverging wall section, and a throat apex between the diverging wall section and the converging wall section; a plurality of cooling apertures disposed on the converging wall section; and a cooling slot disposed on the diverging wall section; wherein: the cooling apertures comprise apertures through the thickness of the converging wall section; and the cooling slot comprising a circumferentially extending slot through the length of the diverging wall section.
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申请公布号 |
US2012047895(A1) |
申请公布日期 |
2012.03.01 |
申请号 |
US20100868793 |
申请日期 |
2010.08.26 |
申请人 |
SRIDHAR KODUKULLA VENKAT;DESAI ANAND PRAFULCHANDRA;GENERAL ELECTRIC COMPANY |
发明人 |
SRIDHAR KODUKULLA VENKAT;DESAI ANAND PRAFULCHANDRA |
分类号 |
F02C1/00 |
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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