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    • 23. 发明授权
    • Gas turbine combustor including a diffusion nozzle assembly with a
double cylindrical structure
    • 燃气轮机燃烧器包括具有双圆柱结构的扩散喷嘴组件
    • US5450725A
    • 1995-09-19
    • US266591
    • 1994-06-28
    • Takeshi TakaharaTadashi KobayashiMasao Itoh
    • Takeshi TakaharaTadashi KobayashiMasao Itoh
    • F23R3/32F23R3/28F23R3/34F23R3/30
    • F23R3/286F23R3/34F05D2250/231F05D2260/96F05D2270/31F23D2900/14021
    • A gas turbine combustor comprises a cylindrical outer casing having one end closed by a header plate. A combustor liner provided with an inner combustion chamber which is divided into a first-stage combustion region on a side of the header plate and a second-stage combustion region formed on a downstream side of the first-stage combustion region. A first-stage fuel supply unit mounted to the header plate for injecting a first-stage fuel to the first-stage combustion region and a second-stage fuel supply unit mounted to the header plate for injecting a second-stage fuel previously mixed in a lean fuel state. The first-stage fuel supply unit includes a first-stage fuel nozzle assembly, which supplies the first-stage fuel, formed by combining a diffusion combustion nozzle and a pre-mixture combustion nozzle. The pre-mixture combustion nozzle has, at an intermediate portion thereof, a pre-mixing portion for preliminarily mixing the first-stage fuel with an air, and the pre-mixing portion having a diameter in a downstream portion thereof smaller than that of an upstream portion thereof so as to form a pre-mixed flow into a contraction flow. The pre-mixing fuel nozzle of the first stage fuel nozzle assembly is disposed so as to surround the diffusion combustion nozzle disposed in a central portion thereof.
    • 燃气轮机燃烧器包括一个圆柱形的外壳,其一端通过集管板封闭。 一种燃烧器衬套,其具有内燃室,该内燃室被分为集管板一侧的第一级燃烧区域和形成在第一级燃烧区域的下游侧的第二级燃烧区域。 第一级燃料供给单元,安装到集管板,用于将第一级燃料喷射到第一级燃烧区域;以及第二级燃料供应单元,安装到集管板,用于将预混合在第一级燃料中的第二级燃料 贫燃状态。 第一级燃料供给单元包括:第一级燃料喷嘴组件,其供给通过组合扩散燃烧喷嘴和预混合燃烧喷嘴形成的第一级燃料。 预混合燃烧喷嘴在其中间部分具有用于预先混合第一级燃料与空气的预混合部分,并且预混合部分的下游部分中的直径小于 上游部分,以形成预混合流入收缩流。 第一级燃料喷嘴组件的预混合燃料喷嘴设置成围绕设置在其中心部分的扩散燃烧喷嘴。
    • 26. 发明授权
    • Gas turbine combustor with nozzle pressure ratio control
    • 燃气轮机燃烧器与喷嘴压力比控制
    • US5311742A
    • 1994-05-17
    • US982583
    • 1992-11-27
    • Atsuhiko IzumiMasao Itoh
    • Atsuhiko IzumiMasao Itoh
    • F02C7/228F02C9/28F02C9/34F23R3/28F23R3/34
    • F23R3/34F05D2270/31
    • A gas turbine combustor for a gas turbine power plant comprises a combustion liner connected to a turbine and provided with a main fuel nozzle assembly and a sub-fuel nozzle assembly for jetting fuel to an inside of the combustion liner through nozzle holes, a base fuel supply line, a main fuel line for supplying a fuel to the main nozzle assembly for premixing an air with the fuel jetted through the nozzle hole for carrying out a lean burning in the combustion liner, and a plurality of sub-fuel lines for supplying the fuel to the sub-fuel nozzle assembly for mixing the fuel with a combustion air for carrying out a diffusion burning in the combustion liner. The main and sub-fuel lines branch off a front end of the base fuel supply line. Distributing valves are incorporated in the main fuel line and at least one of the sub-fuel lines for distributing the fuel into the main and sub-fuel lines and degree of openings of the distributing valves are controlled by a control unit for controlling a fuel distribution ratio. The sub-fuel nozzle assembly includes a swirler provided with swirling vanes at an end portion inserted in the combustion liner for swirling the fuel therein The swirling vanes are provided with a combustion air passage to which the nozzle holes of the sub-fuel nozzle assembly are opened.
    • 用于燃气轮机发电厂的燃气轮机燃烧器包括连接到涡轮机的燃烧衬套,并且设置有主燃料喷嘴组件和用于通过喷嘴孔将燃料喷射到燃烧衬套的内部的副燃料喷嘴组件,基础燃料 供应管线,用于向主喷嘴组件供应燃料的主燃料管线,用于预先混合通过喷嘴孔喷射的燃料的空气,以在燃烧衬套中进行稀燃;以及多个副燃料管线, 燃料到副燃料喷嘴组件,用于将燃料与用于在燃烧衬套中进行扩散燃烧的燃烧空气混合。 主燃料和副燃料管线从基础燃料供应管线的前端分支。 分配阀被并入主燃料管线中,并且用于将燃料分配到主和副燃料管线中的至少一个子燃料管线和分配阀的开口程度由用于控制燃料分配的控制单元控制 比。 副燃料喷嘴组件包括在插入在燃烧衬套中的端部处设置有旋动叶片的旋流器,用于在其中旋转燃料。涡流叶片设置有燃烧空气通道,副燃料喷嘴组件的喷嘴孔 开了