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    BURNER FOR A CAN COMBUSTOR
    1.
    发明申请
    BURNER FOR A CAN COMBUSTOR 审中-公开
    燃烧器为燃烧器

    公开(公告)号：US20140109588A1

    公开(公告)日：2014-04-24

    申请号：US14060931

    申请日：2013-10-23

    Applicant: ALSTOM Technology Ltd

    Inventor： Andrea Ciani ,  John Philip Wood ,  Douglas Anthony Pennell ,  Ewald Freitag ,  Urs Benz ,  Andre Theuer

    IPC: F23R3/28

    CPC classification number: F23R3/16 ,  F02C6/003 ,  F02C9/26 ,  F02C9/32 ,  F02C9/34 ,  F05B2260/222 ,  F23R3/20 ,  F23R3/286 ,  F23R3/34 ,  F23R3/346 ,  F23R3/36 ,  F23R3/46 ,  F23R2900/03341

    Abstract: The present invention relation to a burner for a combustion chamber of a gas turbine with a mixing and injection device. The mixing and injection device includes a limiting wall that defines a gas-flow channel and at least two streamlined bodies, each extending in a first transverse direction into the gas-flow channel. Each streamlined body has two lateral surfaces that are arranged essentially parallel to the main-flow direction, the lateral surfaces being joined to one another at their upstream side to form a leading edge of the body and joined at their downstream side to form a trailing edge of the body. Each streamlined body has a cross-section perpendicular to the first transverse direction that is shaped as a streamlined profile. At least one of the streamlined bodies is provided with a mixing structure and with at least one fuel nozzle located at its trailing edge for introducing at least one fuel essentially parallel to the main-flow direction into the flow channel, wherein at least two of the streamlined bodies have different lengths along the first transverse direction such that they may be used for a can combustor. The invention also relates to a method of using said burner in a gas turbine.

    Abstract translation: 本发明涉及一种具有混合和注射装置的燃气轮机燃烧室的燃烧器。 混合和注入装置包括界定气流通道的限制壁和至少两个流线型的主体，每个流体线体在第一横向方向上延伸到气体流动通道中。 每个流线型体具有基本上平行于主流动方向布置的两个侧表面，侧表面在其上游侧彼此连接以形成主体的前缘并在其下游侧接合以形成后缘 的身体。 每个流线型本体具有垂直于第一横向方向的横截面，其形状为流线型轮廓。 流线型主体中的至少一个设置有混合结构，并且具有位于其后缘处的至少一个燃料喷嘴，用于将基本上平行于主流动方向的至少一个燃料引入流动通道中，其中至少两个 流线型主体沿着第一横向方向具有不同的长度，使得它们可以用于罐式燃烧器。 本发明还涉及在燃气轮机中使用所述燃烧器的方法。

    Method for operating a gas turbine with sequential combustion and gas turbine for conducting said method
    3.
    发明授权
    Method for operating a gas turbine with sequential combustion and gas turbine for conducting said method 有权
    用于操作具有顺序燃烧和燃气轮机的燃气轮机进行所述方法的方法

    公开(公告)号：US09518511B2

    公开(公告)日：2016-12-13

    申请号：US14060065

    申请日：2013-10-22

    Applicant: ALSTOM Technology Ltd

    Inventor： Andrea Ciani ,  Adnan Eroglu ,  Douglas Anthony Pennell ,  Nicolas Tran ,  Ewald Freitag

    IPC: F02C7/141 ,  F02C7/12 ,  F02C7/228 ,  F02C9/28

    CPC classification number: F02C7/12 ,  F02C7/141 ,  F02C7/228 ,  F02C9/28 ,  F05D2270/08 ,  Y02E20/16

    Abstract: The invention discloses a method for operating a gas turbine with sequential combustion, which gas turbine includes a compressor, a first combustor with a first combustion chamber and first burners, which receives compressed air from the compressor, a second combustor with a second combustion chamber and second burners, which receives hot gas from the first combustor with a predetermined second combustor inlet temperature, and a turbine, which receives hot gas from the second combustor. The CO emission for part-load operation is reduced by reducing the second combustor inlet temperature for base-load operation of the gas turbine, and increasing the second combustor inlet temperature when decreasing the gas turbine load (RLGT) from base-load to part-load.

    Abstract translation: 本发明公开了一种用于操作具有顺序燃烧的燃气轮机的方法，该燃气轮机包括压缩机，具有第一燃烧室的第一燃烧器和从压缩机接收压缩空气的第一燃烧器，具有第二燃烧室的第二燃烧器， 第二燃烧器，其以预定的第二燃烧器入口温度从第一燃烧器接收热气体;以及涡轮机，其接收来自第二燃烧器的热气体。 通过降低燃气轮机的基本负载运行的第二燃烧器入口温度，并且当将燃气轮机负载（RLGT）从基本负载降低到部分负载时，增加第二燃烧器入口温度， 加载。

    COMBUSTION DEVICE
    4.
    发明申请
    COMBUSTION DEVICE 有权
    燃烧装置

    公开(公告)号：US20150007547A1

    公开(公告)日：2015-01-08

    申请号：US14491082

    申请日：2014-09-19

    Applicant: ALSTOM Technology Ltd

    Inventor： Michael DUESING ,  Andrea Ciani ,  Adnan Eroglu

    IPC: F23R3/34 ,  F02C6/00 ,  F02C7/228

    CPC classification number: F23R3/34 ,  F02C6/003 ,  F02C7/228 ,  F23C3/002 ,  F23R3/18 ,  F23R3/28 ,  F23R2900/03341

    Abstract: The combustion device includes a burner, a combustion chamber downstream of the burner, a lance projecting into the burner for fuel and air injection, and a plenum that at least partly houses the burner. The plenum is connected to the inside of the lance to supply an oxidiser to it.

    Abstract translation: 燃烧装置包括燃烧器，在燃烧器下游的燃烧室，突出到燃烧器中的喷枪用于燃料和空气喷射，以及至少部分地容纳燃烧器的增压室。 增压室连接到喷枪内部以向其供应氧化剂。

    OPERATING METHOD FOR HYDROGEN/NATURAL GAS BLENDS WITHIN A REHEAT GAS TURBINE
    6.
    发明申请
    OPERATING METHOD FOR HYDROGEN/NATURAL GAS BLENDS WITHIN A REHEAT GAS TURBINE 审中-公开
    氢气/天然气混合燃气涡轮机运行方法

    公开(公告)号：US20130091852A1

    公开(公告)日：2013-04-18

    申请号：US13649502

    申请日：2012-10-11

    Applicant: ALSTOM TECHNOLOGY LTD

    Inventor： John Philip Wood ,  Madhavan Poyyapakkam ,  Andrea Ciani ,  Khawar Syed ,  Thierry Lachaux ,  Franklin Marie Genin ,  Adnan Eroglu

    IPC: F02C9/40

    CPC classification number: F01D19/00 ,  F02C3/20 ,  F02C9/34 ,  F02C9/40

    Abstract: A gas turbine is operated using a varying blend of a first fuel, preferably natural gas, and a second fuel that is hydrogen. The hydrogen concentration is varied depending on operating conditions in order to reduce emissions of CO and NOx, and/or to mitigate LBO. The fuel mixture is varied using a controller based on a combination of factors in a modular operation concept to address different issues according to relevant load limitations. A method of operating a gas turbine according to this modular operational concept is also provided.

    Abstract translation: 燃气轮机使用第一燃料，优选天然气和作为氢的​​第二燃料的变化混合来操作。 氢浓度根据操作条件而变化，以减少CO和NOx的排放，和/或减轻LBO。 使用基于模块化操作概念的因素的组合的控制器来改变燃料混合物，以根据相关的负载限制来解决不同的问题。 还提供了一种根据该模块化操作概念来操作燃气轮机的方法。

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