| 发明名称 |
Gas turbine combustor, gas turbine, and jet engine |
| 摘要 |
<p>For the purpose of reduced NOx gas emission, a gas turbine engine comprises a cylinder (2) having a combustion region (11) inside of the cylinder (2); a resonator (16) having a cavity (15) and provided around the surface of the cylinder (2) and sound absorption holes (14) formed on the cylinder (2) and having opening ends on the cylinder (2). <IMAGE></p> |
| 申请公布号 |
EP1213539(B1) |
申请公布日期 |
2004.09.15 |
| 申请号 |
EP20010128924 |
申请日期 |
2001.12.05 |
| 申请人 |
MITSUBISHI HEAVY INDUSTRIES, LTD. |
发明人 |
SUENAGA, KIYOSHI;MANDAI, SHIGEMI;ONO, MASAKI;TANAKA, KATSUNORI |
| 分类号 |
F23R3/42;F02C7/18;F02K1/82;F23M99/00;F23R3/18;(IPC1-7):F23M13/00 |
主分类号 |
F23R3/42 |
| 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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