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    • 11. 发明专利
    • Gas turbine combustor and its fuel-supply method
    • 燃气轮机及其燃料供应方法
    • JP2005009414A
    • 2005-01-13
    • JP2003175030
    • 2003-06-19
    • Hitachi Ltd株式会社日立製作所
    • YOSHIDA SHOHEIHIRATA YOSHITAKAITO KAZUYUKIMUROTA TOMOYAINOUE HIROSHIASAI TOMOHIRO
    • F02C7/04F02C7/22F23R3/28F23R3/34F23R3/42
    • F23R3/286F23R3/343
    • PROBLEM TO BE SOLVED: To provide a gas turbine combustor and its fuel-supply method in which backfire is prevented from occurring while reducing the amount of NO
      x generation.
      SOLUTION: In the combustor 2, fuel is mixed with combustion air let in from a compressor 1, and the mixture is burned. Generated combustion gas is supplied to the gas turbine 3. A liquid-fuel nozzle 13 injecting the fuel is installed in the center of a mixing chamber wall 5 having a mixing chamber 4 in the inside. The wall 5 is of a hollow conical shape flared in the direction of injection. In the mixing chamber wall 5, a plurality of air-conduction holes 14, 15, 16 are made so that while passing the combustion air in the mixing chamber 4, the angle for passing the air is deviated at least to the peripheral direction of the wall 5. Gaseous-fuel nozzles 17 are provided on the outside periphery of the wall 5 so as to respectively oppose to the air-conduction holes 14, 15, 16. The nozzles 17 inject the fuel nearly coaxially with the axes of L1, L2, L3 of the air-conduction holes 14, 15, 16.
      COPYRIGHT: (C)2005,JPO&NCIPI
    • 要解决的问题:提供一种燃气轮机燃烧器及其燃料供给方法,其中在减少NO x 产生量的同时防止发生回火。 解决方案:在燃烧器2中,燃料与从压缩机1引入的燃烧空气混合,混合物燃烧。 产生的燃烧气体被供给到燃气轮机3.喷射燃料的液体燃料喷嘴13安装在混合室壁5的中部,混合室壁5的内部具有混合室4。 壁5是在注射方向上张开的中空圆锥形状。 在混合室壁5中,形成多个通气孔14,15,16,使得在混合室4内的燃烧空气通过时,使空气通过的角度至少偏离 气体燃料喷嘴17设置在壁5的外周上,以分别与通气孔14,15,16相对。喷嘴17将燃料与L1,L2的轴线几乎同轴地注入 ,空气导通孔14,15,16的L3。版权所有(C)2005,JPO&NCIPI