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：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：US09677764B2

公开(公告)日：2017-06-13

申请号：US14189206

申请日：2014-02-25

Applicant: ALSTOM Technology Ltd

Inventor： Klaus Knapp ,  Peter Marx ,  Karl Reyser ,  Maria-Belen Gasser-Pagani

IPC: F02C9/40 ,  F23N1/00 ,  F02C7/224 ,  F02C9/00

CPC classification number: F23N1/002 ,  F02C7/224 ,  F02C9/00 ,  F02C9/40 ,  F05D2260/80 ,  Y02E20/16

Abstract: The method for adjusting a natural gas temperature for a fuel supply line of a gas turbine engine includes measuring by infrared analysis the natural gas percentage content of methane (CH4), ethane (C2H6), propane (C3H8), butane (C4H10), carbon dioxide (CO2), calculating the nitrogen (N2) percentage content as the complement to 100 of the measured percentage content of methane (CH4), ethane (C2H6), propane (C3H8), butane (C4H10), carbon dioxide (CO2), calculating an index indicative of the natural gas energy content and adjusting the natural gas temperature on the basis of the index.

公开(公告)号：US20140305128A1

公开(公告)日：2014-10-16

申请号：US14245639

申请日：2014-04-04

Applicant: ALSTOM Technology Ltd

Inventor： Madhavan Narasimhan POYYAPAKKAM ,  Khawar Syed ,  Klaus Knapp ,  Torsten Wind

IPC: F23R3/26 ,  F02C7/057

CPC classification number: F02C7/057 ,  F05D2240/35 ,  F23N1/022 ,  F23N2021/10 ,  F23R3/26 ,  F23R3/346 ,  F23R2900/03341

Abstract: A combustion chamber including a body with a fuel supply duct for supplying a fuel into the body and a carrier air supply duct for supplying air into the body. An adjusting system adjusts the carrier air mass flow supplied into the body according to the features of the fuel.

Abstract translation: 一种燃烧室，包括具有用于向主体供应燃料的燃料供应管道的主体和用于将空气供应到主体中的载体空气供应管道。 调节系统根据燃料的特征来调节供给到体内的载气质量流量。

公开(公告)号：US10544736B2

公开(公告)日：2020-01-28

申请号：US14245639

申请日：2014-04-04

Applicant: ALSTOM Technology Ltd

Inventor： Madhavan Narasimhan Poyyapakkam ,  Khawar Syed ,  Klaus Knapp ,  Torsten Wind

IPC: F02C7/057 ,  F23N1/02 ,  F23R3/26

Abstract: A combustion chamber including a body with a fuel supply duct for supplying a fuel into the body and a carrier air supply duct for supplying air into the body. An adjusting system adjusts the carrier air mass flow supplied into the body according to the features of the fuel.

公开(公告)号：US10422535B2

公开(公告)日：2019-09-24

申请号：US14260617

申请日：2014-04-24

Applicant: ALSTOM Technology Ltd

Inventor： Klaus Knapp ,  Naresh Aluri ,  Nicolas Tran ,  Ulrich Rathmann ,  Franklin Marie Genin

IPC: F23R3/28 ,  F23R3/14 ,  F23R3/34 ,  F23R3/46

Abstract: The invention relates to a can-combustor for a can-annular combustor arrangement in a gas turbine. The can combustor includes an essentially cylindrical casing with an axially upstream front panel and an axially downstream outlet end. The can combustor further includes a number of premixed burners, extending in an upstream direction from said front panel and having a burner exit, supported by this front panel, for supplying a fuel/air mixture into a combustion zone inside the casing. Up to four premixed burners are attached to the front panel in a substantially annular array. Each burner has a conical swirl generator and a mixing tube to induce a swirl flow of said fuel/air mixture.