发明申请
US20120234011A1 GAS TURBINE COMBUSTOR HAVING A FUEL NOZZLE FOR FLAME ANCHORING
有权
具有用于火焰锚定的燃料喷嘴的燃气涡轮机组
- 专利标题: GAS TURBINE COMBUSTOR HAVING A FUEL NOZZLE FOR FLAME ANCHORING
- 专利标题(中): 具有用于火焰锚定的燃料喷嘴的燃气涡轮机组
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申请号: US13048564申请日: 2011-03-15
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公开(公告)号: US20120234011A1公开(公告)日: 2012-09-20
- 发明人: Predrag Popovic , Abinash Baruah , Gilbert Otto Kraemer , William Thomas Ross
- 申请人: Predrag Popovic , Abinash Baruah , Gilbert Otto Kraemer , William Thomas Ross
- 申请人地址: US NY Schnectady
- 专利权人: GENERAL ELECTRIC COMPANY
- 当前专利权人: GENERAL ELECTRIC COMPANY
- 当前专利权人地址: US NY Schnectady
- 主分类号: F02C7/22
- IPC分类号: F02C7/22
摘要:
A combustor includes an end cover having a nozzle. The nozzle has a front end face and a central axis. The nozzle includes a plurality of fuel passages and a plurality of oxidizer passages. The fuel passages are configured for fuel exiting the fuel passage. The fuel passages are positioned to direct fuel in a first direction, where the first direction is angled inwardly towards the center axis. The oxidizer passages are configured for having oxidizer exit the oxidizer passages. The oxidizer passages are positioned to direct oxidizer in a second direction, where the second direction is angled outwardly away from the center axis. The plurality of fuel passages and the plurality of oxidizer passages are positioned in relation to one another such that fuel is in a cross-flow arrangement with oxidizer to create a burning zone in the combustor.