发明名称 |
Gas turbine combustor |
摘要 |
A gas turbine combustor includes a combustion liner in which a combustion region is formed; and a housing provided for a wall of the combustion liner in a predetermined circumferential region of the combustion liner to form a resonance space between the combustion liner and the housing. The combustion region and the resonance space are connected by a plurality of combustion liner through-holes, and a circumferential length of the housing is longer than a diameter of the combustion liner.
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申请公布号 |
US2005097890(A1) |
申请公布日期 |
2005.05.12 |
申请号 |
US20040927529 |
申请日期 |
2004.08.27 |
申请人 |
MITSUBISHI HEAVY INDUSTRIES, LTD. |
发明人 |
IKEDA KAZUFUMI;ISHIGURO TATSUO;TANAKA KATSUNORI;TANIMURA SATOSHI |
分类号 |
F23R3/16;F02C7/00;F02C7/24;F23M99/00;F23R3/00;F23R3/12;F23R3/42;(IPC1-7):F23R3/42 |
主分类号 |
F23R3/16 |
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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