发明名称 POWER GENERATION SYSTEM EXHAUST COOLING
摘要 An airflow control system for a gas turbine system according to an embodiment includes: a compressor component of a gas turbine system; a mixing area for receiving an exhaust gas stream produced by the gas turbine system; an air extraction system for extracting a supply of bypass air from an excess flow of air generated by the compressor component of the gas turbine system; an enclosure surrounding the gas turbine system and forming an air passage, the bypass air flowing through the air passage and around the gas turbine system into the mixing area to reduce a temperature of the exhaust gas stream; and an exhaust processing system for processing the reduced temperature exhaust gas stream.
申请公布号 US2016376994(A1) 申请公布日期 2016.12.29
申请号 US201514753074 申请日期 2015.06.29
申请人 General Electric Company 发明人 Kulkarni Parag Prakash;Davis, JR. Lewis Berkley;Reed Robert Joseph
分类号 F02C7/18;F01N3/20;F02C3/04;F01D15/10 主分类号 F02C7/18
代理机构 代理人
主权项 1. An airflow control system for a gas turbine system, comprising: a compressor component of a gas turbine system for generating an excess flow of air; a mixing area for receiving an exhaust gas stream produced by the gas turbine system; an air extraction system for extracting a supply of bypass air from the excess flow of air generated by the compressor component of the gas turbine system; and an enclosure surrounding the gas turbine system and forming an air passage, the bypass air flowing through the air passage and around the gas turbine system into the mixing area to reduce a temperature of the exhaust gas stream.
地址 Schenectady NY US