发明名称 GAS TURBINE INTAKE CONTROL SYSTEM AND METHOD
摘要 PROBLEM TO BE SOLVED: To provide a system capable of both increasing warm day output and maintaining compressor operating margin across the ambient and load range of a gas turbine combined cycle installation. SOLUTION: The proposed solution takes advantage of a fact that both goals can be satisfied by manipulation of compressor intake air temperature. Specifically, the system is designed to heat intake air as may be required to maintain safe compressor operating margin at low ambient air temperature or when burning dilute fuels. In an alternative, the system is designed to cool intake air on warm days. COPYRIGHT: (C)2008,JPO&INPIT
申请公布号 JP2007285298(A) 申请公布日期 2007.11.01
申请号 JP20070103588 申请日期 2007.04.11
申请人 GENERAL ELECTRIC CO <GE> 发明人 SMITH RAUB WARFIELD;GULEN SEYFETTIN C;GARDINER BARRETT D
分类号 F02C7/08;F01K17/02;F01K23/10;F02C7/143 主分类号 F02C7/08
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