公开(公告)号：US20130219904A1

公开(公告)日：2013-08-29

申请号：US13855857

申请日：2013-04-03

Applicant: Alstom Technology Ltd.

Inventor： Adnan Eroglu ,  Klaus Knapp ,  Peter Flohr ,  Hans Peter Knoepfel ,  Weiqun Geng

IPC: F02C9/26

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

Abstract: 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.

Abstract translation: 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。

公开(公告)号：US08794008B2

公开(公告)日：2014-08-05

申请号：US13855857

申请日：2013-04-03

Applicant: ALSTOM Technology Ltd.

Inventor： Adnan Eroglu ,  Klaus Knapp ,  Peter Flohr ,  Hans Peter Knoepfel ,  Weiqun Geng

IPC: F02C7/228

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

Abstract: 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.

Abstract translation: 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。

公开(公告)号：US20160018111A1

公开(公告)日：2016-01-21

申请号：US14814864

申请日：2015-07-31

Applicant: ALSTOM Technology Ltd

Inventor： Dirk THERKORN ,  Stefano BERNERO ,  Mengbin Zhang ,  Adnan Eroglu ,  Weiqun Geng

IPC: F23R3/34 ,  F02C9/22 ,  F02C6/00

CPC classification number: F23R3/346 ,  F02C6/003 ,  F02C9/22 ,  F05D2270/053 ,  F23R2900/03341

Abstract: The invention concerns a method of operating a gas turbine with staged and/or sequential combustion. The burners of a second stage or a second combustor are singularly and sequentially switched on during loading and switched off during de-loading. The total fuel mass flow and the compressor inlet guide vanes are adjusted at the same time to allow controlling gas turbine operation temperatures and engine power with respect to the required CO emission target.

Abstract translation: 本发明涉及一种操作具有分阶段和/或顺序燃烧的燃气轮机的方法。 在加载期间，第二级或第二燃烧器的燃烧器被单独且顺序地接通并且在卸载期间被关闭。 总燃料质量流量和压缩机入口引导叶片同时被调节，以允许相对于所需的CO排放目标控制燃气轮机的运行温度和发动机功率。