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.

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。

公开(公告)号：US20140109586A1

公开(公告)日：2014-04-24

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: F02C7/228 ,  F02C7/12

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。