发明名称 |
Systems and methods for bulk temperature variation reduction of a gas turbine through can-to-can fuel temperature modulation |
摘要 |
<p>A gas turbine (10) includes a plurality of combustion chambers (14); at least one fuel nozzle (16, 18, 20) for each of the combustion chambers; at least one fuel line (34, 36, 38) for each fuel nozzle in each of the combustion chambers; at least one heat exchanger (28, 30, 32) for each fuel line configured to adjust a temperature of a fuel flow to each fuel nozzle; and a controller (50) configured to control each of the heat exchangers to reduce temperature variations amongst the combustion chambers.</p> |
申请公布号 |
EP2546575(A2) |
申请公布日期 |
2013.01.16 |
申请号 |
EP20120176010 |
申请日期 |
2012.07.11 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
ROMIG, BRYAN WESLEY;ZIMINSKY, WILLY STEVE;SIMONS, DERRICK WALTER |
分类号 |
F23R3/46;F02C7/224;F23K5/20;F23R3/28 |
主分类号 |
F23R3/46 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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