发明名称 |
GAS TURBINE APPARATUS |
摘要 |
A gas turbine apparatus (2) has an air compressor (20) for compressing air, a combustor (21) for combusting the compressed air, a turbine (22) rotatable by a gas discharged from the combustor (21), and a recuperator (23) for exchanging heat between the air supplied from the air compressor (20) and an exhaust gas discharged from the turbine (22). The gas turbine apparatus (2) includes a fuel supply system (24) having a first fuel supply device (50) for supplying a fuel (HG) to the combustor (21), a second fuel supply device (51) for supplying a gas (LG) having a small heating value to the combustor (21), and a switching device (56) operable to switch the first fuel supply device (50) and the second fuel supply device (51) based on a temperature of the air compressed by the air compressor (20) or the exhaust gas discharged from the turbine (22). |
申请公布号 |
WO2006059749(A1) |
申请公布日期 |
2006.06.08 |
申请号 |
WO2005JP22245 |
申请日期 |
2005.11.29 |
申请人 |
EBARA CORPORATION;KATAOKA, TADASHI;HAMANO, NOBUHIKO |
发明人 |
KATAOKA, TADASHI;HAMANO, NOBUHIKO |
分类号 |
F02C7/08;F02C3/20;F02C7/22;F02C9/26;F02C9/40 |
主分类号 |
F02C7/08 |
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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