| 摘要 |
<P>PROBLEM TO BE SOLVED: To provide a gas turbine system which can achieve stably operation and high efficiency. <P>SOLUTION: The gas turbine system includes a compressor for compressing air with liquid sprayed, a combustor which is disposed in a some part of a pipe branched from a some part of a drain capture pipe connected to a discharge part of the compressor, and combusts the fuel mixed with compressed air from the compressor, and a turbine to be driven with combustion gas combusted in the combustor. The gas turbine system further includes a separator which is disposed in a some part of the drain capture pipe connected between stages and/or to a discharge part of the compressor, and separates drain from the compressor into compressed air and liquid drain. The separator has a means for intermittently discharging the liquid drain separated by the separator to a discharge system. <P>COPYRIGHT: (C)2012,JPO&INPIT |
