- 专利标题: Gas turbine combustor
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申请号: US14772535申请日: 2013-03-13
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公开(公告)号: US10060625B2公开(公告)日: 2018-08-28
- 发明人: Kazuki Abe , Tomomi Koganezawa , Keisuke Miura
- 申请人: Mitsubishi Hitachi Power Systems, Ltd.
- 申请人地址: JP Yokohama
- 专利权人: Mitsubishi Hitachi Power Systems, Ltd.
- 当前专利权人: Mitsubishi Hitachi Power Systems, Ltd.
- 当前专利权人地址: JP Yokohama
- 代理机构: Crowell & Moring LLP
- 国际申请: PCT/JP2013/056905 WO 20130313
- 国际公布: WO2014/141397 WO 20140918
- 主分类号: F23R3/12
- IPC分类号: F23R3/12 ; F23R3/32 ; F23R3/30 ; F23R3/28 ; F23R3/34
摘要:
In a perforated coaxial jet burner implemented by a lot of air-fuel coaxial jets, a swirl plate (33) as an end face of the burner on the combustion chamber's side has a lot of air holes for supplying unburned premixed gas of fuel and air to the combustion chamber. Grooves (36) are formed downstream of the air holes of the swirl plate. Adhesion of flame to the swirl plate is inhibited by feeding part of the unburned premixed gas to the grooves. Further, the width of each remaining part (37) between adjacent grooves is set at several millimeters that is approximately equal to the flame quenching distance, by which adhesion of flame to the remaining parts is also prevented. With this configuration, both stable combustion and low NOx combustion can be achieved irrespective of the load condition.
公开/授权文献
- US20160010864A1 Gas Turbine Combustor 公开/授权日:2016-01-14
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