Annular fuel and air co-flow premixer
    61.
    发明授权
    Annular fuel and air co-flow premixer 失效
    环形燃料和空气共流预混合器

    公开(公告)号:US08555646B2

    公开(公告)日:2013-10-15

    申请号:US12360449

    申请日:2009-01-27

    IPC分类号: F02C3/20

    CPC分类号: F23R3/286 F23D14/64 F23R3/10

    摘要: Disclosed is a premixer for a combustor including an annular outer shell and an annular inner shell. The inner shell defines an inner flow channel inside of the inner shell and is located to define an outer flow channel between the outer shell and the inner shell. A fuel discharge annulus is located between the outer flow channel and the inner flow channel and is configured to inject a fuel flow into a mixing area in a direction substantially parallel to an outer airflow through the outer flow channel and an inner flow through the inner flow channel. Further disclosed are a combustor including a plurality of premixers and a method of premixing air and fuel in a combustor.

    摘要翻译: 公开了一种用于燃烧器的预混合器,其包括环形外壳和环形内壳。 内壳在内壳内部限定内部流动通道,并且定位成在外壳和内壳之间限定外部流动通道。 燃料排出环位于外流动通道和内部流动通道之间,并且构造成将燃料流喷射到基本上平行于外部流动通道的外部气流的方向上的混合区域中,并且内部流动通过内部流动 渠道。 进一步公开的是包括多个预混合器的燃烧器和在燃烧器中预混合空气和燃料的方法。

    ANNULAR FUEL AND AIR CO-FLOW PREMIXER
    63.
    发明申请
    ANNULAR FUEL AND AIR CO-FLOW PREMIXER 失效
    ANNULAR燃油和空气流动预热器

    公开(公告)号:US20100186412A1

    公开(公告)日:2010-07-29

    申请号:US12360449

    申请日:2009-01-27

    IPC分类号: F02C7/08

    CPC分类号: F23R3/286 F23D14/64 F23R3/10

    摘要: Disclosed is a premixer for a combustor including an annular outer shell and an annular inner shell. The inner shell defines an inner flow channel inside of the inner shell and is located to define an outer flow channel between the outer shell and the inner shell. A fuel discharge annulus is located between the outer flow channel and the inner flow channel and is configured to inject a fuel flow into a mixing area in a direction substantially parallel to an outer airflow through the outer flow channel and an inner flow through the inner flow channel. Further disclosed are a combustor including a plurality of premixers and a method of premixing air and fuel in a combustor.

    摘要翻译: 公开了一种用于燃烧器的预混合器,其包括环形外壳和环形内壳。 内壳在内壳内部限定内部流动通道,并且定位成在外壳和内壳之间限定外部流动通道。 燃料排出环位于外流动通道和内部流动通道之间,并且构造成将燃料流喷射到基本上平行于外部流动通道的外部气流的方向上的混合区域中,并且内部流动通过内部流动 渠道。 进一步公开的是包括多个预混合器的燃烧器和在燃烧器中预混合空气和燃料的方法。

    Micromixer combustion head end assembly
    65.
    发明授权
    Micromixer combustion head end assembly 有权
    微混合器燃烧头端组件

    公开(公告)号:US09163839B2

    公开(公告)日:2015-10-20

    申请号:US13423894

    申请日:2012-03-19

    IPC分类号: B01F3/04 F23R3/28

    CPC分类号: F23R3/286

    摘要: Embodiments of the present application can provide systems and methods for a micromixer combustion head end assembly. The micromixer may include one or more base nozzle structures. The base nozzle structures may include coaxial tubes. The coaxial tubes may include an inner tube and an outer tube. The micromixer may also include one or more segmented mixing tube bundles at least partially supported by a respective base nozzle structure. Moreover, the micromixer may include an end cap assembly disposed about the one or more segmented mixing tube bundles.

    摘要翻译: 本申请的实施例可以提供用于微混合器燃烧头端组件的系统和方法。 微混合器可以包括一个或多个基本喷嘴结构。 基座喷嘴结构可以包括同轴管。 同轴管可包括内管和外管。 微混合器还可以包括至少部分由相应的基座喷嘴结构支撑的一个或多个分段的混合管束。 此外,微混合器可以包括围绕一个或多个分段的混合管束设置的端盖组件。

    Systems and Methods for Dampening Combustor Dynamics in a Micromixer
    66.
    发明申请
    Systems and Methods for Dampening Combustor Dynamics in a Micromixer 有权
    微混合器中阻尼燃烧器动力学的系统和方法

    公开(公告)号:US20130247581A1

    公开(公告)日:2013-09-26

    申请号:US13425950

    申请日:2012-03-21

    IPC分类号: F02C7/24

    摘要: Embodiments of the present application can provide systems and methods for dampening combustor dynamics. According to one embodiment, the system may include a micromixer. The system may also include at least one annular resonator disposed within the micromixer adjacent to a cap face plate or an impingement plate of the micromixer. The at least one annular resonator may include a first side including a number of holes forming a cold side hole pattern, a second side including a number of holes forming a hot side hole pattern, and a cavity substantially defined by the first side and the second side.

    摘要翻译: 本申请的实施例可以提供用于衰减燃烧室动力学的系统和方法。 根据一个实施例,系统可以包括微混合器。 该系统还可以包括设置在微型混合器内的至少一个环形谐振器,其邻近盖板或微型混合器的冲击板。 所述至少一个环形谐振器可以包括包括形成冷侧孔图案的多个孔的第一侧,包括形成热侧孔图案的多个孔的第二侧和基本上由第一侧和第二侧形成的空腔 侧。

    Combustor and method for supplying fuel to a combustor
    67.
    发明授权
    Combustor and method for supplying fuel to a combustor 有权
    用于向燃烧器供应燃料的燃烧器和方法

    公开(公告)号:US09341376B2

    公开(公告)日:2016-05-17

    申请号:US13400248

    申请日:2012-02-20

    IPC分类号: F23R3/28 F23D14/62 F23R3/36

    CPC分类号: F23R3/286 F23D14/62 F23R3/36

    摘要: A combustor includes an end cap having upstream and downstream surfaces and a cap shield surrounding the upstream and downstream surfaces. First and second sets of premixer tubes extend from the upstream surface through the downstream surface. A first fuel conduit supplies fuel to the first set of premixer tubes. A casing circumferentially surrounds the cap shield to define an annular passage, and a second fuel conduit supplies fuel through the annular passage to the second set of premixer tubes. A method for supplying fuel to a combustor includes flowing a working fluid through first and second sets of premixer tubes, flowing a first fuel into the first set of premixer tubes, and flowing a second fuel through an annular passage surrounding the end cap and into the second set of premixer tubes.

    摘要翻译: 燃烧器包括具有上游和下游表面的端盖和围绕上游表面和下游表面的盖罩。 第一组和第二组预混合管从上游表面延伸穿过下游表面。 第一燃料管道向第一组预混合器管供应燃料。 壳体周向地围绕盖罩以限定环形通道,并且第二燃料管道将燃料通过环形通道供应到第二组预混合器管。 用于向燃烧器供应燃料的方法包括使工作流体流过第一组和第二组预混合器管,将第一燃料流入第一组预混合器管,并使第二种燃料流过围绕端盖的环形通道并进入 第二组预混管。

    Systems and methods for dampening combustor dynamics in a micromixer
    68.
    发明授权
    Systems and methods for dampening combustor dynamics in a micromixer 有权
    用于抑制微混合器中的燃烧室动力学的系统和方法

    公开(公告)号:US09188342B2

    公开(公告)日:2015-11-17

    申请号:US13425950

    申请日:2012-03-21

    摘要: Embodiments of the present application can provide systems and methods for dampening combustor dynamics. According to one embodiment, the system may include a micromixer. The system may also include at least one annular resonator disposed within the micromixer adjacent to a cap face plate or an impingement plate of the micromixer. The at least one annular resonator may include a first side including a number of holes forming a cold side hole pattern, a second side including a number of holes forming a hot side hole pattern, and a cavity substantially defined by the first side and the second side.

    摘要翻译: 本申请的实施例可以提供用于衰减燃烧室动力学的系统和方法。 根据一个实施例,系统可以包括微混合器。 该系统还可以包括设置在微型混合器内的至少一个环形谐振器,其邻近盖板或微型混合器的冲击板。 所述至少一个环形谐振器可以包括包括形成冷侧孔图案的多个孔的第一侧,包括形成热侧孔图案的多个孔的第二侧和基本上由第一侧和第二侧形成的空腔 侧。

    COMBUSTOR AND METHOD FOR SUPPLYING FUEL TO A COMBUSTOR
    69.
    发明申请
    COMBUSTOR AND METHOD FOR SUPPLYING FUEL TO A COMBUSTOR 有权
    用于向燃烧器供应燃料的燃烧器和方法

    公开(公告)号:US20130213051A1

    公开(公告)日:2013-08-22

    申请号:US13400248

    申请日:2012-02-20

    IPC分类号: F02C7/22 F02C3/20

    CPC分类号: F23R3/286 F23D14/62 F23R3/36

    摘要: A combustor includes an end cap having upstream and downstream surfaces and a cap shield surrounding the upstream and downstream surfaces. First and second sets of premixer tubes extend from the upstream surface through the downstream surface. A first fuel conduit supplies fuel to the first set of premixer tubes. A casing circumferentially surrounds the cap shield to define an annular passage, and a second fuel conduit supplies fuel through the annular passage to the second set of premixer tubes. A method for supplying fuel to a combustor includes flowing a working fluid through first and second sets of premixer tubes, flowing a first fuel into the first set of premixer tubes, and flowing a second fuel through an annular passage surrounding the end cap and into the second set of premixer tubes.

    摘要翻译: 燃烧器包括具有上游和下游表面的端盖和围绕上游表面和下游表面的盖罩。 第一组和第二组预混合管从上游表面延伸穿过下游表面。 第一燃料管道向第一组预混合器管供应燃料。 壳体周向地围绕盖罩以限定环形通道,并且第二燃料管道将燃料通过环形通道供应到第二组预混合器管。 用于向燃烧器供应燃料的方法包括使工作流体流过第一组和第二组预混合器管,将第一燃料流入第一组预混合器管,并使第二种燃料流过围绕端盖的环形通道并进入 第二组预混管。