发明名称 |
Gas turbine and operating method of the same. |
摘要 |
<p>A gas turbine in which a centrifugal compressor (3), which is driven a high pressure turbine (5), and a variable inlet guide vane (9) located at the inlet of the centrifugal compressor are provided. An axial-flow compressor is not provided between the centrifugal compressor and the variable inlet guide vane. An operating method of a gas turbine in which the output is varied by moving a variable inlet guide vane (9) while keeping the rate of rotation at a high level. It is possible to vary the output of the gas turbine in a short period of time and the durability of engine is improved. <IMAGE></p> |
申请公布号 |
EP0515746(A1) |
申请公布日期 |
1992.12.02 |
申请号 |
EP19910304929 |
申请日期 |
1991.05.30 |
申请人 |
MITSUBISHI JUKOGYO KABUSHIKI KAISHA |
发明人 |
MORISHITA, SUSUMU;MIYAKE, YOSHIAKI;UCHIDA, SEISHI |
分类号 |
F02C3/08;F02C3/10;F02C9/20 |
主分类号 |
F02C3/08 |
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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