| 发明名称 |
Gas turbine combustor and operating method thereof |
| 摘要 |
A gas turbine combustor has a combustion chamber into which fuel and air are supplied, wherein the fuel and the air are supplied into said combustion chamber as a plurality of coaxial jets.
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| 申请公布号 |
US2004163393(A1) |
申请公布日期 |
2004.08.26 |
| 申请号 |
US20040784216 |
申请日期 |
2004.02.24 |
| 申请人 |
HITACHI, LTD. |
发明人 |
INOUE HIROSHI;KOGANEZAWA TOMOMI;KOBAYASHI NARIYOSHI;TAKEHARA ISAO |
| 分类号 |
F23R3/10;F23R3/28;F23R3/36;(IPC1-7):F02C7/22 |
主分类号 |
F23R3/10 |
| 代理机构 |
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代理人 |
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| 主权项 |
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