System and method for turbine combustor fuel assembly
    1.
    发明授权
    System and method for turbine combustor fuel assembly 有权
    涡轮燃烧器燃油组件的系统和方法

    公开(公告)号:US09267433B2

    公开(公告)日:2016-02-23

    申请号:US13280237

    申请日:2011-10-24

    IPC分类号: F02C3/30

    摘要: A system includes a turbine fuel supply system. The turbine fuel supply system includes a first turbine fuel mixer configured to mix a first liquid fuel and a first deaerated water to generate a first fuel mixture. The first fuel mixture is configured to combust in a combustor of a gas turbine engine. The turbine fuel supply system also includes a deaerated water flow path configured to route the first deaerated water to the first turbine fuel mixer and a liquid fuel flow path configured to route the first liquid fuel to the first turbine fuel mixer.

    摘要翻译: 一种系统包括涡轮燃料供应系统。 涡轮燃料供应系统包括构造成混合第一液体燃料和第一脱气水以产生第一燃料混合物的第一涡轮燃料混合器。 第一燃料混合物构造成在燃气涡轮发动机的燃烧器中燃烧。 涡轮燃料供应系统还包括一个脱气水流通道,其配置成将第一除气水路由第一涡轮燃料混合器和将第一液体燃料路由到第一涡轮燃料混合器的液体燃料流路。

    SYSTEM AND METHOD FOR TURBINE COMBUSTOR FUEL ASSEMBLY
    2.
    发明申请
    SYSTEM AND METHOD FOR TURBINE COMBUSTOR FUEL ASSEMBLY 有权
    用于涡轮机燃油组件的系统和方法

    公开(公告)号:US20130098056A1

    公开(公告)日:2013-04-25

    申请号:US13280237

    申请日:2011-10-24

    IPC分类号: F02C9/26 F02C3/30

    摘要: A system includes a turbine fuel supply system. The turbine fuel supply system includes a first turbine fuel mixer configured to mix a first liquid fuel and a first deaerated water to generate a first fuel mixture. The first fuel mixture is configured to combust in a combustor of a gas turbine engine. The turbine fuel supply system also includes a deaerated water flow path configured to route the first deaerated water to the first turbine fuel mixer and a liquid fuel flow path configured to route the first liquid fuel to the first turbine fuel mixer.

    摘要翻译: 一种系统包括涡轮燃料供应系统。 涡轮燃料供应系统包括构造成混合第一液体燃料和第一脱气水以产生第一燃料混合物的第一涡轮燃料混合器。 第一燃料混合物构造成在燃气涡轮发动机的燃烧器中燃烧。 涡轮燃料供应系统还包括一个脱气水流通道,其配置成将第一除气水路由第一涡轮燃料混合器和将第一液体燃料路由到第一涡轮燃料混合器的液体燃料流路。

    SYSTEM FOR TURBINE COMBUSTOR FUEL MIXING
    8.
    发明申请
    SYSTEM FOR TURBINE COMBUSTOR FUEL MIXING 有权
    涡轮机燃油混合系统

    公开(公告)号:US20130097991A1

    公开(公告)日:2013-04-25

    申请号:US13280216

    申请日:2011-10-24

    IPC分类号: F02C7/22

    摘要: A system includes a mixing assembly configured to mix a liquid fuel and a water to generate a fuel mixture. The fuel mixture is configured to combust in a combustor of a gas turbine. The mixing assembly includes a liquid fuel passage disposed in an integrated housing. The liquid fuel passage is configured to flow the liquid fuel and to exclude liquid traps. The mixing assembly also includes a water passage disposed in the integrated housing. The water passage is configured to flow the water and to exclude liquid traps. The mixing assembly also includes a mixer disposed in the integrated housing and coupled to the liquid fuel passage and the water passage. The mixer is configured to mix the liquid fuel and the water to form the fuel mixture.

    摘要翻译: 一种系统包括配置成混合液体燃料和水以产生燃料混合物的混合组件。 燃料混合物构造成在燃气轮机的燃烧器中燃烧。 混合组件包括设置在一体化壳体中的液体燃料通道。 液体燃料通道构造成流动液体燃料并排除液体捕集阱。 混合组件还包括设置在一体式壳体中的水通道。 水通道构造成流过水并排除液体捕集阱。 混合组件还包括设置在一体式壳体中并耦合到液体燃料通道和水通道的混合器。 混合器配置成混合液体燃料和水以形成燃料混合物。