发明名称 |
Combustor for gas turbine |
摘要 |
A combustor for a gas turbine capable of performing stable combustion even by using high temperature air, comprising a first burner (5) jetting fuel and air into a combustion chamber (2) and a second burner (8) causing the circulating jet of the fuel and air installed at a position corresponding to the tip part of a flame caused by the first burner (5). |
申请公布号 |
AU2003289368(A1) |
申请公布日期 |
2005.07.05 |
申请号 |
AU20030289368 |
申请日期 |
2003.12.16 |
申请人 |
HITACHI, LTD. |
发明人 |
SATOSHI DODO;SUSUMU NAKANO;KUNIYOSHI TSUBOUCHI;SHOUHEI YOSHIDA;YOSHITAKA HIRATA |
分类号 |
F23R3/14;F23R3/34;F23R3/44 |
主分类号 |
F23R3/14 |
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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