发明申请
- 专利标题: Gas Turbine Combustor
- 专利标题(中): 燃气轮机燃烧器
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申请号: US13005450申请日: 2011-01-12
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公开(公告)号: US20110185703A1公开(公告)日: 2011-08-04
- 发明人: Satoshi DODO , Hiromi KOIZUMI , Hirokazu TAKAHASHI , Tomohiro ASAI , Keisuke MIURA
- 申请人: Satoshi DODO , Hiromi KOIZUMI , Hirokazu TAKAHASHI , Tomohiro ASAI , Keisuke MIURA
- 申请人地址: JP Tokyo
- 专利权人: Hitachi, Ltd.
- 当前专利权人: Hitachi, Ltd.
- 当前专利权人地址: JP Tokyo
- 优先权: JP2010-004697 20100113
- 主分类号: F23R3/28
- IPC分类号: F23R3/28 ; F02C7/228
摘要:
A gas turbine combustor includes plural multi-coaxial-injection-hole burners in which plural fuel nozzles and plural air holes provided in an air plate to correspond to the respective fuel nozzles are coaxially arranged. Each of the multi-coaxial-injection-hole burners includes a first coaxial injection burner disposed on an inner circumferential side, and a second coaxial injection burner disposed on an outer circumferential side, and a diameter of the air holes of the first coaxial injection burner is smaller than a diameter of the air holes of the second coaxial injection burner. Combustion for carrying out flame holding of a gas turbine combustor is performed by the first coaxial injection burner, and low NOx combustion of the gas turbine combustor is performed by the second coaxial injection burner.
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