发明名称 SYSTEM AND METHOD FOR OPERATING A GAS TURBINE
摘要 A method for determining a cooling flow parameter of a cooling medium supplied through a gas turbine is disclosed. The method may generally include receiving a signal associated with a first value of a combustion product parameter at a location within a combustion zone of the gas turbine, receiving a signal associated with a second value of a combustion product parameter at a location downstream of the combustion zone, comparing the first and second values of the combustion product parameter and determining a cooling flow parameter of the cooling medium based on the comparison of the first and second values.
申请公布号 US2013174564(A1) 申请公布日期 2013.07.11
申请号 US201213345278 申请日期 2012.01.06
申请人 MORGAN REX ALLEN;GENERAL ELECTRIC COMPANY 发明人 MORGAN REX ALLEN
分类号 F02C7/12 主分类号 F02C7/12
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