发明名称 SYSTEMS AND METHODS FOR TURBINE SYSTEM OPERATION IN LOW AMBIENT TEMPERATURES
摘要 A system includes a controller communicatively coupled to a compressor (26). The controller is configured to sense an exhaust temperature of a gas turbine system (24) fluidly coupled to the compressor (26) and derive a setpoint based on the sensed exhaust temperature. The controller is also configured to actuate an inlet bleed heat valve (74) based on the derived setpoint and an ambient temperature. The inlet bleed heat valve (74) directs a compressor fluid from the compressor (26) into a fluid intake system (18) fluidly coupled to the compressor (26) upstream of the compressor (26) and configured to intake a fluid.
申请公布号 EP3064746(A1) 申请公布日期 2016.09.07
申请号 EP20160158501 申请日期 2016.03.03
申请人 GENERAL ELECTRIC COMPANY 发明人 KLOSINSKI, JOSEPH PHILIP;SCIPIO, ALSTON ILFORD;MESTRONI, JULIO ENRIQUE;MATHAI, GEORGE VARGESE;COCCA, MICHAEL ANTHONY;EKANAYAKE, SANJI
分类号 F02C9/52;F02C6/08;F02C9/28 主分类号 F02C9/52
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