发明授权
- 专利标题： Gas turbine combustor, gas turbine, and jet engine
- 专利标题（中）： 燃气轮机燃烧器，燃气轮机和喷气发动机
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申请号： US10464499申请日： 2003-06-19
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公开(公告)号： US06973790B2公开(公告)日： 2005-12-13
- 发明人: Kiyoshi Suenaga , Shigemi Mandai , Masaki Ono , Katsunori Tanaka
- 申请人： Kiyoshi Suenaga , Shigemi Mandai , Masaki Ono , Katsunori Tanaka
- 申请人地址： JP Tokyo
- 专利权人： Mitsubishi Heavy Industries, Ltd.
- 当前专利权人： Mitsubishi Heavy Industries, Ltd.
- 当前专利权人地址： JP Tokyo
- 代理机构： Oblon, Spivak, McClelland, Maier & Neustadt, P.C.
- 优先权： JPP2000-371312 20001206
- 主分类号： F23M99/00
- IPC分类号： F23M99/00 ; F02C7/24
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.
公开/授权文献
- US20030233831A1 Gas turbine combustor, gas turbine, and jet engine 公开/授权日：2003-12-25
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