发明名称 |
Gas turbine combustor, gas turbine, and jet engine |
摘要 |
For the purpose of reduced NOx gas emission, a gas turbine engine comprises a cylinder having a combustion region inside of the cylinder; a resonator having a cavity and provided around the surface of the cylinder and sound absorption holes formed on the cylinder and having opening ends on the cylinder.
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申请公布号 |
US6973790(B2) |
申请公布日期 |
2005.12.13 |
申请号 |
US20030464499 |
申请日期 |
2003.06.19 |
申请人 |
MITSUBISHI HEAVY INDUSTRIES, LTD. |
发明人 |
SUENAGA KIYOSHI;MANDAI SHIGEMI;ONO MASAKI;TANAKA KATSUNORI |
分类号 |
F23M99/00;(IPC1-7):F02C7/24 |
主分类号 |
F23M99/00 |
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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