| 发明名称 |
Gas turbine combustor and operating method |
| 摘要 |
A gas turbine combustor has a combustion chamber (1) into which fuel (53,54) and air (51) are supplied, wherein the fuel and the air are supplied into said combustion chamber as a plurality of coaxial jets. <IMAGE> |
| 申请公布号 |
EP1843099(A3) |
申请公布日期 |
2015.03.11 |
| 申请号 |
EP20070012941 |
申请日期 |
2002.02.28 |
| 申请人 |
MITSUBISHI HITACHI POWER SYSTEMS, LTD. |
发明人 |
INOUE, HIROSHI;KOGANEZAWA, TOMOMI;KOBAYASHI, NARIYOSHI;TAKEHARA, ISAO |
| 分类号 |
F23R3/28;F23R3/10;F23R3/36 |
主分类号 |
F23R3/28 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
|
| 地址 |
|
