发明名称 GAS TURBINE SYSTEM
摘要 There is provided a gas turbine system including: a compressing portion; a combustor generating a combustion operation by using first compressed air coming from the compressing portion; a turbine portion generating power by using a combustion gas coming from the combustor; a heat recoverer recovering a heat from a discharge gas of the turbine portion; and a compressed air supplier providing second compressed air to which the heat recovered by the heat recoverer is transferred, wherein at least a portion of the second compressed air to which the heat has been transferred is supplied to at least one of the combustor and the turbine portion.
申请公布号 US2016169106(A1) 申请公布日期 2016.06.16
申请号 US201414902729 申请日期 2014.06.25
申请人 HANWHA TECHWIN CO., LTD. 发明人 KIM Myeong Hyo
分类号 F02C7/10;F02C7/32;F02C3/04 主分类号 F02C7/10
代理机构 代理人
主权项 1. A gas turbine system comprising: a compressing portion; a combustor generating a combustion operation by using first compressed air coming from the compressing portion; a turbine portion generating power by using a combustion gas coming from the combustor; a heat recoverer recovering a heat from a discharge gas of the turbine portion; and a compressed air supplier providing second compressed air to which the heat recovered by the heat recoverer is transferred, wherein at least a portion of the second compressed air to which the heat has been transferred is supplied to at least one of the combustor and the turbine portion.
地址 Changwon-si KR