发明名称 GAS TURBINE FACILITY
摘要 A gas turbine facility 10 of an embodiment has a combustor 20 combusting fuel and oxidant, a turbine 28 rotated by combustion gas exhausted from the combustor 20, a heat exchanger 25 cooling the combustion gas from the turbine 28, a pipe 46 guiding a part of the combustion gas to the combustor 20 via the heat exchanger 25, and a pipe 45 exhausting a remaining part of the combustion gas to an outside. Further, the facility has a pipe 40 supplying fuel to the combustor 20, a pipe 41 supplying oxidant to the combustor 20 via the heat exchanger 25, and a pipe 42 branched from the pipe 41, bypassing the heat exchanger 25, and coupled to the pipe 41, so as to introduce the oxidant into the pipe 41.
申请公布号 US2015027099(A1) 申请公布日期 2015.01.29
申请号 US201414331599 申请日期 2014.07.15
申请人 KABUSHIKI KAISHA TOSHIBA 发明人 IWAI Yasunori;ITOH Masao;SUZUKI Shinju
分类号 F02C7/057;F02C7/08;F02C3/34 主分类号 F02C7/057
代理机构 代理人
主权项 1. A gas turbine facility, comprising: a combustor combusting fuel and oxidant; a turbine rotated by combustion gas exhausted from the combustor; a heat exchanger cooling the combustion gas exhausted from the turbine; a working fluid supply pipe guiding a part of the combustion gas as working fluid to the combustor via the heat exchanger; an exhaust pipe exhausting a remaining part of the combustion gas to an outside; a fuel supply pipe supplying fuel to the combustor; an oxidant supply pipe supplying the oxidant to the combustor via the heat exchanger; and an oxidant bypass supply pipe branched from the oxidant supply pipe, bypassing the heat exchanger, and coupled to the oxidant supply pipe at a position between the heat exchanger and the combustor, so as to introduce the oxidant into the oxidant supply pipe.
地址 Minato-ku JP