发明名称 |
GAS TURBINE SYSTEM AND METHOD OF OPERATION |
摘要 |
<p>A gas turbine system (10) is provided. The gas turbine system (10) includes a compressor assembly (14) configured to compress ambient air and a combustor (16) in flow communication with the compressor assembly (14), the combustor (16) being configured to receive compressed air from the compressor assembly (14) and to combust a first fuel stream to generate a combustor exit gas stream. The gas turbine system (10) includes a first turbine (18) located downstream of the combustor (16) and configured to partially expand the combustor exit gas stream and a reheating device (12) in flow communication with the first turbine (18). The reheating device (12) is configured to introduce a second fuel stream in a transverse direction to a working gas stream from the first turbine (18) for combusting the fuel in presence of the working gas stream. The gas turbine system (10) also includes a second turbine (20) configured to expand an exit gas stream from the reheating device (12).</p> |
申请公布号 |
SG130102(A1) |
申请公布日期 |
2007.03.20 |
申请号 |
SG20060049720 |
申请日期 |
2006.07.24 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
GOLDMEER, JEFFREY SCOTT;HAYNES, JOEL MEIER |
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