发明名称 |
Gas turbine combustor |
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 |
US6912854(B2) |
申请公布日期 |
2005.07.05 |
申请号 |
US20030658465 |
申请日期 |
2003.09.10 |
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):F23R3/32 |
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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地址 |
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