发明名称 |
TURBINE COMBUSTOR CONFIGURED FOR HIGH-FREQUENCY DYNAMICS MITIGATION AND RELATED METHOD |
摘要 |
A turbomachine combustor includes a combustion chamber; a plurality of micro-mixer nozzles mounted to an end cover of the combustion chamber, each including a fuel supply pipe affixed to a nozzle body located within the combustion chamber, wherein fuel from the supply pipe mixes with air in the nozzle body prior to discharge into the combustion chamber; and wherein at least some of the nozzle bodies of the plurality of micro-mixer nozzles have axial length dimensions that differ from axial length dimensions of other of the nozzle bodies. |
申请公布号 |
US2012198856(A1) |
申请公布日期 |
2012.08.09 |
申请号 |
US201113021298 |
申请日期 |
2011.02.04 |
申请人 |
UHM JONG HO;ZUO BAIFANG;YORK WILLIAM DAVID;SRINIVASAN SHIVAKUMAR;GENERAL ELECTRIC COMPANY |
发明人 |
UHM JONG HO;ZUO BAIFANG;YORK WILLIAM DAVID;SRINIVASAN SHIVAKUMAR |
分类号 |
F23R3/28;F23K5/10 |
主分类号 |
F23R3/28 |
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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