发明名称 POWER GENERATION SYSTEM HAVING COMPRESSOR CREATING EXCESS AIR FLOW AND TURBO-EXPANDER USING SAME
摘要 A power generation system may include a generator, and a gas turbine system for powering the generator, the gas turbine system including a turbine component, an integral compressor and a combustor to which air from the integral compressor and fuel are supplied, the combustor arranged to supply hot combustion gases to the turbine component, and the integral compressor having a flow capacity greater than an intake capacity of at least one of the combustor and the turbine component, creating an excess air flow. A turbo-expander may also power the generator. A first control valve control flow of the excess air flow along an excess air flow path to an inlet of the turbo-expander. An educator may be positioned in the excess air flow path for using the excess air flow as a motive force to augment the excess air flow with additional air. A discharge of the turbo-expander is supplied to an exhaust of the turbine component for an HRSG.
申请公布号 US2016273403(A1) 申请公布日期 2016.09.22
申请号 US201514662847 申请日期 2015.03.19
申请人 General Electric Company 发明人 Ekanayake Sanji;Kim Kihyung;Rehg Timothy Joseph;Scipio Alston Ilford;Tong Leslie Yung Min
分类号 F01K23/10;F02C3/32;F02C6/08;F02C3/04 主分类号 F01K23/10
代理机构 代理人
主权项 1. A power generation system, comprising: a generator; a gas turbine system for powering the generator, the gas turbine system including a turbine component, an integral compressor and a combustor to which air from the integral compressor and fuel are supplied, the combustor arranged to supply hot combustion gases to the turbine component, and the integral compressor having a flow capacity greater than an intake capacity of at least one of the combustor and the turbine component, creating an excess air flow; a turbo-expander for powering the generator; and a first control valve controlling flow of the excess air flow along an excess air flow path to an inlet of the turbo-expander, wherein a discharge of the turbo-expander is supplied to an exhaust of the turbine component.
地址 Schenectady NY US