Gas turbine facility
申请(专利)号： US201414456233
专利号： US9562473B2 主分类号： F01K19/10
申请权利人： 8 RIVERS
CAPITAL, LLC
公开国代码： US 优先权国家： JP
摘 要：
The gas turbine facility 10 of the embodiment includes a combustor
20 combusting fuel and oxidant, a turbine 21 rotated by combustion gas, a heat exchanger
23 cooling the combustion gas, a heat exchanger 24 removing water vapor from the combustion gas
which passed through the heat exchanger 23 to regenerate dry working gas, and a compressor 25 compressing the dry working gas until it becomes supercritical fluid. Further, the gas turbine facility 10 includes a pipe 42 guiding a part of the dry working gas from the compressor
25 to the combustor 20
申请日： 2014-08-11 公开公告日： 2017-02-07
分类号： F01K19/10;
F02C6/18; F02C1/08; F02C3/34 发明设计人： MASAO ITOH;
NOBUHIRO OKIZONO;
HIDEYUKI MAEDA; YASUNORI IWAI; JEREMY ERON FETVEDT;
RODNEY JOHN ALLAM 申请国代码： US
优先权： 20130827 JP 2013-175933
摘 要 附 图：
via the heat exchanger 23, a pipe 44 exhausting a part of the dry working gas to the outside, and a pipe 45 introducing a remaining part of the dry working gas exhausted from the compressor 25 into a pipe 40 coupling an outlet of the turbine 21 and an inlet of the heat exchanger 23. 主权项：
1. A gas turbine facility, comprising: a combustor combusting fuel and oxidant; a turbine rotated by
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Gas turbine facility
