发明名称 |
Combustor of a gas turbine engine |
摘要 |
A combustor has a combustion zone and a liner bounding the combustion zone. The liner has a first end portion and a second end portion spaced a defined distance from the first end portion. The combustor has a convector spaced apart from the liner. The convector has a first end portion and a second end portion spaced a defined distance of the first end portion. A plurality of passages are located between the liner and the convector. One of the passages has a length that is longer than at least one of the defined distance of the liner and the defined distance of the convector.
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申请公布号 |
US2005044857(A1) |
申请公布日期 |
2005.03.03 |
申请号 |
US20030649496 |
申请日期 |
2003.08.26 |
申请人 |
GLEZER BORIS;MOON HEE KOO |
发明人 |
GLEZER BORIS;MOON HEE KOO |
分类号 |
F23R3/42;(IPC1-7):F23R3/42 |
主分类号 |
F23R3/42 |
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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