|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F01K-019/10 F02C-006/18 F02C-001/08 F02C-003/34|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 139|
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 via the...
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 water vapor remover removing water vapor from the combustion gas which passed through the heat exchanger to regenerate dry working gas therefrom; a compressor compressing the dry working gas until it becomes supercritical fluid; a combustor introduction pipe guiding a part of the supercritical fluid exhausted from the compressor to the co...