发明名称 GAS TURBINE
摘要 A compressor compresses air to produce compressed air. A mixture of fuel and the compressed air is combusted in a combustor to produce combustion gas. The combustion gas is supplied to a turbine to obtain rotational power. High-temperature gas accumulated in a space partitioned by an exhaust-side bearing portion that rotatably supports a turbine shaft and an exhaust diffuser is discharged through an exhaust gas passage. The high-temperature gas is sucked into the exhaust gas passage by exhaust gas flowing in the exhaust diffuser.
申请公布号 US2007119184(A1) 申请公布日期 2007.05.31
申请号 US20060459565 申请日期 2006.07.24
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 SATOU HIDEYUKI;TERAZAKI MASAO
分类号 F02C7/06 主分类号 F02C7/06
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