发明申请
US20140116384A1 METHOD FOR INJECTING FUEL INTO A COMBUSTION CHAMBER OF A GAS TURBINE, AND INJECTION SYSTEM FOR IMPLEMENTING SAME
有权
将燃料注入燃气轮机的燃烧室的方法和用于实施燃料的喷射系统
- 专利标题: METHOD FOR INJECTING FUEL INTO A COMBUSTION CHAMBER OF A GAS TURBINE, AND INJECTION SYSTEM FOR IMPLEMENTING SAME
- 专利标题(中): 将燃料注入燃气轮机的燃烧室的方法和用于实施燃料的喷射系统
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申请号: US14126672申请日: 2012-06-19
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公开(公告)号: US20140116384A1公开(公告)日: 2014-05-01
- 发明人: Nicolas Savary , Claude Berat , Hubert Hippolyte Vignau , Christophe Nicolas Henri Viguier
- 申请人: Nicolas Savary , Claude Berat , Hubert Hippolyte Vignau , Christophe Nicolas Henri Viguier
- 申请人地址: FR Bordes
- 专利权人: TURBOMECA
- 当前专利权人: TURBOMECA
- 当前专利权人地址: FR Bordes
- 优先权: FR1155371 20110620
- 国际申请: PCT/FR2012/051368 WO 20120619
- 主分类号: F02M7/00
- IPC分类号: F02M7/00
摘要:
An air/fuel mixer system of a combustion chamber of a gas turbine includes at least one compressed air intake swirler, the swirler having a central axis of symmetry, and a fuel injector including an injection head having an axis of symmetry. Each injector is mounted in the corresponding swirler with aid of a guide mechanism, so that the axis of symmetry of the injection head is off-center with respect to the central axis of symmetry of the swirler. The system can reduce, or even eliminate, combustion instabilities, by injecting the fuel along a particular axis which is off-center relative to the axis of the air/fuel mixer system, inducing a flow of fuel which is no longer perfectly axially symmetrical.
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