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：US09394808B2

公开(公告)日：2016-07-19

申请号：US13847171

申请日：2013-03-19

Applicant: ALSTOM Technology Ltd

Inventor： Andrea Brighenti ,  Darrel Shayne Lilley ,  Karsten Franitza ,  Anton Nemet

IPC: F01K27/00 ,  F01K21/00 ,  F01K23/10 ,  F02C6/18

CPC classification number: F01K21/00 ,  F01K23/101 ,  F02C6/18 ,  F05D2270/083 ,  F05D2270/0831 ,  F05D2270/303 ,  Y02E20/14 ,  Y02E20/16

Abstract: Disclosed is a method for operating a gas turbine (11) comprising a compressor (14), which is equipped with variable inlet guide vanes (13) and receives at its inlet an inlet air flow, which has passed a temperature-affecting air inlet system (12a), a combustor (15, 15′) and a turbine (16, 16′). In a closed loop control scheme, a control variable indicative of the turbine outlet temperature (TAT2) is generated, and the air inlet system (12a) and/or the variable inlet guide vanes (13) are controlled in accordance with said control variable such that the turbine outlet temperature (TAT2) is kept at or above a desired setting value (TAT2min).

Abstract translation: 公开了一种用于操作燃气涡轮机（11）的方法，该燃气涡轮机（11）包括压缩机（14），其配备有可变入口导向叶片（13），并在其入口处接收入口空气流，该入口空气流已通过温度影响的进气系统 （12a），燃烧器（15,15'）和涡轮机（16,16'）。 在闭环控制方案中，产生指示涡轮出口温度（TAT2）的控制变量，并且根据所述控制变量控制进气系统（12a）和/或可变入口导流叶片（13） 涡轮出口温度（TAT2）保持在或高于所需设定值（TAT2min）。