公开(公告)号：US20150176842A1

公开(公告)日：2015-06-25

申请号：US14574978

申请日：2014-12-18

Applicant: ALSTOM Technology Ltd

Inventor： Klaus DOEBBELING ,  Ewald FREITAG

IPC: F23R3/36 ,  F23R3/02 ,  F23R3/28 ,  F23R3/42 ,  F23R3/34

CPC classification number: F23R3/36 ,  F02C6/003 ,  F23R3/02 ,  F23R3/16 ,  F23R3/18 ,  F23R3/20 ,  F23R3/286 ,  F23R3/34 ,  F23R3/346 ,  F23R3/42 ,  F23R2900/00015 ,  F23R2900/03341

Abstract: The invention provides a new path of combustion technology for gas turbine operation with multifuel capability, low emissions of NO and CO and high thermal efficiency. Further to the present invention providing a method for operating a combustor for a gas turbine and a combustor for a gas turbine are disclosed. The combustor includes a first combustion chamber with a wide operating range, a subsequent deflection unit for deflecting the hot gas flow of the first combustion chamber at least in circumferential direction and components for injecting and mixing additional air and/or fuel, and a sequential combustion chamber with a short residence time, where the temperature of the hot gases reaches its maximum.

Abstract translation: 本发明为具有多种能力的燃气轮机操作提供了燃烧技术的新途径，NO和CO的排放量低，热效率高。 本发明还提供了一种操作燃气轮机燃烧器和燃气轮机燃烧器的方法。 燃烧器包括具有宽工作范围的第一燃烧室，用于至少沿圆周方向偏转第一燃烧室的热气流的后续偏转单元和用于喷射和混合附加空气和/或燃料的部件以及顺序燃烧 室内停留时间短，其中热气体的温度达到最大值。

公开(公告)号：US20150089955A1

公开(公告)日：2015-04-02

申请号：US14501465

申请日：2014-09-30

Applicant: ALSTOM Technology Ltd.

Inventor： Klaus KNAPP ,  Klaus DOEBBELING

IPC: F02C9/18 ,  F02C7/143

CPC classification number: F02C9/18 ,  F02C6/08 ,  F02C7/143 ,  F02C7/18 ,  F02C9/52

Abstract: A gas turbine and method for operating a gas turbine, includes a compressor, a combustor, a turbine and a cooling air cooling system having at least a first cooling air line going from a first bleed of the compressor to the turbine, and at least one second cooling air line at a downstream position of the compressor relative to the first cooling air line. A heat exchanger is arranged in the second cooling air line for cooling the extracted air of higher pressure. The heat exchanger is connected with an air inlet side of the compressor such that heat is transferred in order to heat up the inlet air of the compressor.

Abstract translation: 一种用于操作燃气轮机的燃气轮机和方法，包括压缩机，燃烧器，涡轮机和冷却空气冷却系统，其具有至少第一冷却空气管线从压缩机的第一次泄放到涡轮机，以及至少一个 第二冷却空气管线在压缩机的下游位置相对于第一冷却空气管路。 在第二冷却空气管路中布置有热交换器，用于冷却抽出的较高压力的空气。 热交换器与压缩机的空气入口侧连接，以便传递热量以加热压缩机的入口空气。

公开(公告)号：US20150204247A1

公开(公告)日：2015-07-23

申请号：US14600599

申请日：2015-01-20

Applicant: ALSTOM Technology Ltd.

Inventor： Klaus DOEBBELING ,  Anton Nemet ,  Martin Zajadatz ,  Rene Waelchli

IPC: F02C9/18 ,  F02C3/13 ,  F01D25/30 ,  F01K23/10

CPC classification number: F02C9/18 ,  F01D9/065 ,  F01D25/30 ,  F01D25/305 ,  F01K23/10 ,  F02C3/13 ,  F02C6/08 ,  F02C6/18 ,  F05D2220/32 ,  F05D2220/72 ,  F05D2270/08 ,  Y02E20/16

Abstract: The invention relates to a method of operating a gas turbine assembly, which includes a compressor, a combustor and a gas turbine. The method includes operating the gas turbine assembly at a partial load with respect to a base load of the gas turbine assembly; bypassing a portion of blow-off air from the compressor; and introducing the portion of blow-off air into an exhaust gas duct after the gas turbine. The gas turbine assembly, when operating at partial load, can maintain the air-to-fuel ratio approximately constant and hence to control the combustion flame temperature at a level where emissions are kept below the permission limit.

Abstract translation: 本发明涉及一种操作燃气轮机组件的方法，其包括压缩机，燃烧器和燃气轮机。 该方法包括以相对于燃气轮机组件的基本负载的部分负载操作燃气轮机组件; 绕过来自压缩机的一部分吹出空气; 并且在燃气轮机之后将排出空气的一部分引入排气管道。 当部分负荷运行时，燃气轮机组件能够将空燃比保持在大致恒定范围，从而将燃烧火焰温度控制在允许限度以下的排放水平。

公开(公告)号：US20150098792A1

公开(公告)日：2015-04-09

申请号：US14496856

申请日：2014-09-25

Applicant: ALSTOM Technology Ltd

Inventor： Klaus DOEBBELING ,  Christopher Michael Robson ,  Massimo Giusti

IPC: F01D21/14 ,  F02C9/48 ,  F01D21/00

CPC classification number: F01D21/14 ,  F01D19/00 ,  F01D21/00 ,  F01D21/003 ,  F01D21/006 ,  F01D21/02 ,  F02C9/48 ,  F05B2260/85 ,  F05B2260/90 ,  F05B2270/304

Abstract: The present invention relates to a method of decelerating a turbine rotor of a turbine engine. At least one electric motor is engaged with the turbine rotor. A braking system, preferably the starting system, is engaged with the at least one electric motor, preferably the generator of the turbine engine, so as to use the at least one electric motor to apply a negative (braking) torque on the turbine rotor. The method includes after flame off, the braking system being used for dissipating kinetic energy available in the turbine engine after flame off by means of the at least one electric motor.

Abstract translation: 本发明涉及一种减速涡轮发动机的涡轮转子的方法。 至少一个电动机与涡轮机转子接合。 优选地，起动系统的制动系统与至少一个电动机（优选地是涡轮发动机的发电机）接合，以便使用至少一个电动机来对涡轮转子施加负（制动）转矩。 该方法包括在火焰熄灭之后，制动系统用于通过至少一个电动机消除涡轮发动机可用的动能。