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。

公开(公告)号：US09933336B2

公开(公告)日：2018-04-03

申请号：US14488686

申请日：2014-09-17

Applicant: ALSTOM Technology Ltd

Inventor： Mengbin Zhang ,  Klaus-Dieter Liedtke ,  Wenceslao Granados Gomez

IPC: F02C9/46 ,  G01M15/14 ,  F02C9/42 ,  F23N5/24 ,  F02C9/28 ,  F02C7/25 ,  F02C9/26 ,  F23N1/00 ,  F01D21/14 ,  F02C9/32 ,  F02C7/22 ,  F02C7/228

CPC classification number: G01M15/14 ,  F01D21/14 ,  F02C7/22 ,  F02C7/222 ,  F02C7/228 ,  F02C7/25 ,  F02C9/26 ,  F02C9/28 ,  F02C9/285 ,  F02C9/32 ,  F02C9/42 ,  F02C9/46 ,  F05B2260/80 ,  F05B2270/309 ,  F05B2270/335 ,  F05B2270/337 ,  F05D2260/80 ,  F05D2270/309 ,  F05D2270/335 ,  F23N1/00 ,  F23N5/24 ,  F23N5/242 ,  F23N5/245 ,  F23N5/247 ,  F23N2041/20

Abstract: The invention relates to a method for detecting a fuel leakage in the fuel distribution system between a fuel control valve and at least one burner of a gas turbine during the operation of the gas turbine. In order to detect a fuel leakage, the fuel consumption is approximated in accordance with the mechanical power of the gas turbine, the fuel amount fed to the fuel distribution system is determined, and the leakage flow is determined from the difference between the fed fuel amount and the fuel consumption. The invention further relates to a gas turbine for performing such a method.