发明名称 |
Gas turbine having a cooling air system and a spray air system |
摘要 |
A gas turbine has a cooling air system supplying air for cooling a high temperature part of the gas turbine and a spray air system supplying air for spraying fuel into a combustor and is formed so that a part of high-pressure air compressed by a gas turbine compressor is used as air of the cooling air system and spray air system, wherein a heat exchanger and a boost compressor are arranged downstream of the outlet of compressed air of the gas turbine compressor, and the boost compressor is composed of a parallel connection of a compressor driven by the turbine shaft and ae compressor driven by a driven source other than the turbine shaft, and pressurized air from the boost compressor is used as air for the cooling air system and the spray air system.
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申请公布号 |
US2002095940(A1) |
申请公布日期 |
2002.07.25 |
申请号 |
US20020107400 |
申请日期 |
2002.03.28 |
申请人 |
YAMANAKA KAZUNORI;KONDOU SATOSHI;NODA MASAMI |
发明人 |
YAMANAKA KAZUNORI;KONDOU SATOSHI;NODA MASAMI |
分类号 |
F02C3/10;F02C3/30;F02C7/14;F02C7/143;F02C7/18;F02C7/236;(IPC1-7):F02C7/18 |
主分类号 |
F02C3/10 |
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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