发明名称 INLET BLEED HEAT SYSTEM THERMAL LAG MITIGATION USING COMPRESSOR INTERSTAGE BLEED
摘要 PROBLEM TO BE SOLVED: To provide a system 10 to mitigate thermal lag of start-up operations of a gas turbine 20. SOLUTION: The system includes: a housing 60 which is disposed upstream from and which is fluidly coupled to a compressor 30 of the gas turbine 20; a first system 70 coupled to an aft portion 33 of the compressor 30 and to the housing 60 which, when activated, receives a first air supply from the compressor 30 and delivers the first air supply to the housing 60; and a second system 80, coupled to the first system 70, which removes a second air supply from an intermediate portion 32 of the compressor 30 and delivers the second air supply to the first system 70 prior to the activation of the first system 70. COPYRIGHT: (C)2010,JPO&INPIT
申请公布号 JP2010164050(A) 申请公布日期 2010.07.29
申请号 JP20100002464 申请日期 2010.01.08
申请人 GENERAL ELECTRIC CO 发明人 TILLERY STEVEN WILLIAM
分类号 F02C6/08;F02C7/05;F02C9/18 主分类号 F02C6/08
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