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    Burner system
    1.
    发明授权
    Burner system 有权

    公开(公告)号：US06572366B2

    公开(公告)日：2003-06-03

    申请号：US10145044

    申请日：2002-05-15

    申请人： Adnan Eroglu ,  Klaus Knapp ,  Bettina Paikert

    发明人： Adnan Eroglu ,  Klaus Knapp ,  Bettina Paikert

    IPC分类号： F23D1446

    CPC分类号： F23C7/002 ,  F23C2900/07002 ,  F23D11/402 ,  F23D14/70 ,  F23D17/002 ,  F23D2210/00 ,  F23R2900/03341

    摘要： What is described is a burner system with a premix burner (1), in which is provided at least one vortex generator (2), through which passes an air-containing gaseous main flow (ZL) which flows axially through the premix burner (1) and into which gaseous and/or liquid fuel is injected, downstream of the vortex generator (2), as a secondary flow for generating a fuel/air mixture, and with a combustion chamber (5) which adjoins the premix burner (1) downstream of the latter and has a combustion chamber cross section (C2) which is larger than the flow cross section (C1), delimited by the premix burner (1), directly upstream of the combustion chamber (5). The invention is distinguished in that, between the premix burner (1) and the combustion chamber (5), a flow duct (10) is provided, delimited by side walls which create a gradual transition between the flow cross section (C1) and the combustion chamber cross section (C2), and in that upstream, within and/or downstream of the flow duct (10) is provided at least one flow stall structure (11), by means of which the fuel/air mixture passing through the flow duct (10) is separated locally from the side wall of the flow duct (10).

    Flow duct with cross-sectional step
    2.
    发明授权
    Flow duct with cross-sectional step 有权
    具有横截面步骤的流道

    公开(公告)号：US06216644B1

    公开(公告)日：2001-04-17

    申请号：US09431179

    申请日：1999-11-01

    申请人： Adnan Eroglu ,  Franz Joos ,  Bettina Paikert ,  Cristian Oliver Paschereit ,  Jakob J. Keller

    发明人： Adnan Eroglu ,  Franz Joos ,  Bettina Paikert ,  Cristian Oliver Paschereit ,  Jakob J. Keller

    IPC分类号： F15D5504

    CPC分类号： F15D1/0045 ,  F15D1/06 ,  F23D2209/20 ,  F23R3/045 ,  F23R2900/00014

    摘要： In heat generators and burners, it is frequently necessary to realize discontinuous cross-sectional expansions of a flow duct. When the flow (U) passes over the step (10) formed in the wall (8) of the flow duct, coherent lateral separation vortices form which are propagated almost undamped downstream of the step and frequently represent the cause of thermo-acoustic vibrations of high amplitude. In accordance with the invention, vortex-generating elements (20) with a lateral pitch dimension (t) are arranged on a line transverse to the main flow (U) a distance (s) upstream of the step (10). Given an expedient selection of the pitch dimension (t), the lateral coherence of the separation vortex is enduringly destroyed.

    摘要翻译： 在发热体和燃烧器中，通常需要实现流路的不连续的横截面扩展。 当流动（U）通过形成在流动管道的壁（8）中的台阶（10）时，形成相干侧向分离涡流，其在步骤的下游几乎无阻尼地传播，并且经常表示热声振动的原因 高振幅。 根据本发明，具有横向间距尺寸（t）的涡流产生元件（20）在横向于主流（U）的线上布置在步骤（10）上游的距离（s）处。 考虑到桨距尺寸（t）的适当选择，分离涡流的横向相干性被持续地破坏。

    METHOD FOR REDUCING EMISSIONS FROM A COMBUSTOR
    3.
    发明申请
    METHOD FOR REDUCING EMISSIONS FROM A COMBUSTOR 有权
    减少燃烧器排放的方法

    公开(公告)号：US20090282831A1

    公开(公告)日：2009-11-19

    申请号：US12436900

    申请日：2009-05-07

    申请人： Adnan Eroglu ,  Oliver Riccius ,  Klaus Knapp ,  Peter Flohr

    发明人： Adnan Eroglu ,  Oliver Riccius ,  Klaus Knapp ,  Peter Flohr

    IPC分类号： F02C7/22

    CPC分类号： F23R3/50 ,  F23M20/005 ,  F23R3/10 ,  F23R3/286 ,  F23R2900/00014 ,  F23R2900/00016 ,  Y10T29/49231 ,  Y10T29/49233 ,  Y10T29/49323

    摘要： A modification method for reducing emissions from an annular shaped combustor of a gas turbine plant, having uniformly spaced circumferentially mounted premix burners (20), includes the steps of: removing at least one burner (20), thereby disrupting the spatial uniformity of the remaining the burners (20); and modifying the combustor air distribution system so as to compensate for the increased burner pressure drop of the remaining burners, thus enabling the modified combustor to operate at a load equivalent to the unmodified combustor. Emission reduction is enabled by the increase in the gas velocity of the burner for a given load further enabled by the flame stabilizing effect of disrupting the spatial uniformity.

    摘要翻译： 一种用于减少具有均匀间隔开的周向安装的预混燃烧器（20）的燃气轮机设备的环形燃烧器的排放的改进方法，包括以下步骤：去除至少一个燃烧器（20），从而破坏其余的空气均匀性 燃烧器（20）; 以及修改燃烧器空气分配系统，以补偿其余燃烧器的燃烧器压降的增加，从而使修改的燃烧器能够在与未改性燃烧器相当的负载下工作。 通过燃烧器对于给定负载的气体速度的增加可以实现排放减少，这进一步由于破坏空间均匀性的火焰稳定作用而实现。

    Combustor with reduced carbon monoxide emissions
    4.
    发明授权
    Combustor with reduced carbon monoxide emissions 有权
    燃烧器减少一氧化碳排放

    公开(公告)号：US07827777B2

    公开(公告)日：2010-11-09

    申请号：US12436910

    申请日：2009-05-07

    申请人： Adnan Eroglu ,  Oliver Riccius ,  Klaus Knapp ,  Peter Flohr

    发明人： Adnan Eroglu ,  Oliver Riccius ,  Klaus Knapp ,  Peter Flohr

    IPC分类号： F02C3/00

    CPC分类号： F23R3/50 ,  F23C2900/03003 ,  F23M20/005 ,  F23R3/10 ,  F23R2900/00014

    摘要： A combustor arrangement for a gas turbine engine (31) has a split line (42) and a plurality of burners (20,37) arranged in an annular ring (40). The burners (46) of the combustor on either side of the split line (42) have a separation distance of at least two times the average separation distance between burners (48) distant from the split line (42).

    摘要翻译： 一种用于燃气涡轮发动机（31）的燃烧器装置具有分开管线（42）和布置在环形环（40）中的多个燃烧器（20,37）。 分裂线（42）任一侧上的燃烧器的燃烧器（46）的间隔距离为远离分流管线（42）的燃烧器（48）之间的平均间隔距离的至少两倍。

    Gas turbine with improved part load emissions behavior
    6.
    发明授权
    Gas turbine with improved part load emissions behavior 有权
    燃气轮机具有改进的部件负荷排放行为

    公开(公告)号：US08434312B2

    公开(公告)日：2013-05-07

    申请号：US13241983

    申请日：2011-09-23

    申请人： Adnan Eroglu ,  Klaus Knapp ,  Peter Flohr ,  Hans Peter Knöpfel ,  Weiqun Geng

    发明人： Adnan Eroglu ,  Klaus Knapp ,  Peter Flohr ,  Hans Peter Knöpfel ,  Weiqun Geng

    IPC分类号： F02C7/228

    CPC分类号： F02C9/26 ,  F02C6/003 ,  F23C6/042 ,  F23N1/022 ,  F23N2037/02 ,  F23N2041/20 ,  F23R7/00 ,  F23R2900/03341 ,  Y02E20/16

    摘要： In a method for the low-CO emissions part load operation of a gas turbine with sequential combustion, the air ratio (λ) of the operative burners (9) of the second combustor (15) is kept below a maximum air ratio (λmax) at part load In order to reduce the maximum air ratio (λ), a series of modifications in the operating concept of the gas turbine are carried out individually or in combination. One modification is an opening of the row of variable compressor inlet guide vanes (14) before engaging the second combustor (15). For engaging the second combustor, the row of variable compressor inlet guide vanes (14) is quickly closed and fuel is introduced in a synchronized manner into the burner (9) of the second combustor (15). A further modification is the deactivating of individual burners (9) at part load.

    摘要翻译： 在具有顺序燃烧的燃气轮机的低CO排放部分负荷操作的方法中，第二燃烧器（15）的操作燃烧器（9）的空气比（λ）保持在最大空气比（lambdamax）以下） 在部分负载下为了降低最大空气比（lambda），对燃气轮机的操作概念进行一系列修改，可单独进行或组合进行。 一个变型是在接合第二燃烧器（15）之前的一排可变压缩机入口导叶（14）的开口。 为了接合第二燃烧器，可变压缩机入口导叶（14）的排被快速关闭，燃料以同步的方式被引入第二燃烧器（15）的燃烧器（9）。 进一步的修改是在部分负载下单个燃烧器（9）的停用。

    GAS TURBINE WITH IMPROVED PART LOAD EMISSIONS BEHAVIOR
    7.
    发明申请
    GAS TURBINE WITH IMPROVED PART LOAD EMISSIONS BEHAVIOR 有权
    具有改进的部分负荷排放的气体涡轮机行为

    公开(公告)号：US20120017601A1

    公开(公告)日：2012-01-26

    申请号：US13241983

    申请日：2011-09-23

    申请人： Adnan Eroglu ,  Klaus Knapp ,  Peter Flohr ,  Hans Peter Knöpfel ,  Weiqun Geng

    发明人： Adnan Eroglu ,  Klaus Knapp ,  Peter Flohr ,  Hans Peter Knöpfel ,  Weiqun Geng

    IPC分类号： F02C3/14 ,  F02C7/228 ,  F02C7/00

    CPC分类号： F02C9/26 ,  F02C6/003 ,  F23C6/042 ,  F23N1/022 ,  F23N2037/02 ,  F23N2041/20 ,  F23R7/00 ,  F23R2900/03341 ,  Y02E20/16

    摘要： In a method for the low-CO emissions part load operation of a gas turbine with sequential combustion, the air ratio (λ) of the operative burners (9) of the second combustor (15) is kept below a maximum air ratio (λmax) at part load In order to reduce the maximum air ratio (λ), a series of modifications in the operating concept of the gas turbine are carried out individually or in combination. One modification is an opening of the row of variable compressor inlet guide vanes (14) before engaging the second combustor (15). For engaging the second combustor, the row of variable compressor inlet guide vanes (14) is quickly closed and fuel is introduced in a synchronized manner into the burner (9) of the second combustor (15). A further modification is the deactivating of individual burners (9) at part load.

    摘要翻译： 在具有顺序燃烧的燃气轮机的低CO排放部分负荷运行的方法中，第二燃烧器（15）的操作燃烧器（9）的空气比（λ）保持在最大空气比（λmax）以下， 在部分负载下为了降低最大空气比（λ），对燃气轮机的操作概念的一系列修改单独地或组合地进行。 一个变型是在接合第二燃烧器（15）之前的一排可变压缩机入口导叶（14）的开口。 为了接合第二燃烧器，可变压缩机入口导叶（14）的排被快速关闭，燃料以同步的方式被引入第二燃烧器（15）的燃烧器（9）。 进一步的修改是在部分负载下单个燃烧器（9）的停用。

    Method for reducing emissions from a combustor
    8.
    发明授权
    Method for reducing emissions from a combustor 有权
    减少燃烧器排放的方法

    公开(公告)号：US07726019B2

    公开(公告)日：2010-06-01

    申请号：US12436900

    申请日：2009-05-07

    申请人： Adnan Eroglu ,  Oliver Riccius ,  Klaus Knapp ,  Peter Flohr

    发明人： Adnan Eroglu ,  Oliver Riccius ,  Klaus Knapp ,  Peter Flohr

    IPC分类号： B23P6/00 ,  F02C1/00

    CPC分类号： F23R3/50 ,  F23M20/005 ,  F23R3/10 ,  F23R3/286 ,  F23R2900/00014 ,  F23R2900/00016 ,  Y10T29/49231 ,  Y10T29/49233 ,  Y10T29/49323

    摘要： A modification method for reducing emissions from an annular shaped combustor of a gas turbine plant, having uniformly spaced circumferentially mounted premix burners (20), includes the steps of: removing at least one burner (20), thereby disrupting the spatial uniformity of the remaining the burners (20); and modifying the combustor air distribution system so as to compensate for the increased burner pressure drop of the remaining burners, thus enabling the modified combustor to operate at a load equivalent to the unmodified combustor. Emission reduction is enabled by the increase in the gas velocity of the burner for a given load further enabled by the flame stabilizing effect of disrupting the spatial uniformity.

    摘要翻译： 一种用于减少具有均匀间隔开的周向安装的预混燃烧器（20）的燃气轮机设备的环形燃烧器的排放的改进方法，包括以下步骤：去除至少一个燃烧器（20），从而破坏其余的空气均匀性 燃烧器（20）; 以及修改燃烧器空气分配系统，以补偿其余燃烧器的燃烧器压降的增加，从而使修改的燃烧器能够在与未改性燃烧器相当的负载下工作。 通过燃烧器对于给定负载的气体速度的增加可以实现排放减少，这进一步由于破坏空间均匀性的火焰稳定作用而实现。

    Burner arrangement with deflection elements for deflecting cooling air flow
    10.
    发明授权
    Burner arrangement with deflection elements for deflecting cooling air flow 有权
    具有用于偏转冷却空气流的偏转元件的燃烧器布置

    公开(公告)号：US09157637B2

    公开(公告)日：2015-10-13

    申请号：US13219185

    申请日：2011-08-26

    申请人： Madhavan Poyyapakkam ,  Adnan Eroglu ,  Andrea Ciani ,  Diane Lauffer ,  Uwe Ruedel

    发明人： Madhavan Poyyapakkam ,  Adnan Eroglu ,  Andrea Ciani ,  Diane Lauffer ,  Uwe Ruedel

    IPC分类号： F23R3/00 ,  F23R3/34 ,  F23R3/04

    CPC分类号： F23R3/346 ,  F23R3/002 ,  F23R3/04 ,  F23R2900/03041 ,  F23R2900/03044 ,  F23R2900/03045 ,  F23R2900/03341

    摘要： An exemplary burner arrangement and method for operating a burner arrangement are disclosed. During operation of the burner arrangement a hot combustion gas, including combustion air, flows essentially parallel to a burner wall through a mixing chamber, which is delimited by the burner wall, to a combustion chamber. In the mixing chamber the hot combustion gas is mixed with an injected fuel, where cooling air from the outside of the burner wall flows through effusion holes in the burner wall into an interior of the mixing chamber. The cooling air, on the outside of the burner wall, is deflected in a directed manner in its flow direction by means of deflection elements which are in a distributed arrangement.

    摘要翻译： 公开了用于操作燃烧器装置的示例性燃烧器布置和方法。 在燃烧器布置的操作期间，包括燃烧空气的热燃烧气体基本上平行于燃烧器壁流过燃烧器壁的混合室，燃烧器壁由燃烧室壁限定。 在混合室中，热燃烧气体与喷射的燃料混合，其中来自燃烧器壁的外部的冷却空气流过燃烧器壁中的渗出孔进入混合室的内部。 在燃烧器壁的外侧的冷却空气通过分布式布置的偏转元件在其流动方向上以有向的方式偏转。