| 发明名称 |
GAS TURBINE COMBUSTOR, GAS TURBINE, AND JET ENGINE |
| 摘要 |
16 For the purpose of reduced NO x 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). |
| 申请公布号 |
CA2364377(C) |
申请公布日期 |
2007.03.27 |
| 申请号 |
CA20012364377 |
申请日期 |
2001.12.05 |
| 申请人 |
MITSUBISHI HEAVY INDUSTRIES, LTD. |
发明人 |
MANDAI, SHIGEMI;ONO, MASAKI;SUENAGA, KIYOSHI;TANAKA, KATSUNORI |
| 分类号 |
F23R3/42;F02C7/18;F02K1/82;F23M99/00;F23R3/18 |
主分类号 |
F23R3/42 |
| 代理机构 |
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