发明名称 Gas turbine engine
摘要 A method of operating a gas turbine engine having a compressor, a combustor between a waste fluid compressor and a power turbine, a counter-rotating compressor turbine installed downstream of the power turbine, and a heat exchanger having two circuits, in which a heated fluid is prepared by burning fuel with combustion air in a mixture with a waste fluid obtained downstream of a compressor turbine that which is cooled, compressed and heated before mixing with combustion air while keeping the temperature of the waste fluid downstream of the compressor turbine constant and removing a partial flow of the waste fluid into the atmosphere before heating the waste fluid prior to supplying the waste fluid for mixing with the combustion air.
申请公布号 US6363708(B1) 申请公布日期 2002.04.02
申请号 US20000632734 申请日期 2000.08.04
申请人 ALM DEVELOPMENT, INC. 发明人 RAKHMAILOV ANATOLY
分类号 F02C3/067;F02C3/10;F02C3/34;(IPC1-7):F02C3/34;F02C9/50 主分类号 F02C3/067
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