公开(公告)号：US09624830B2

公开(公告)日：2017-04-18

申请号：US14336174

申请日：2014-07-21

Applicant: ALSTOM Technology Ltd

Inventor： Theodoros Ferreira-Providakis ,  Ghislain Singla ,  Thiemo Meeuwissen ,  Sebastian Lipari ,  Ourania-Nektaria Margari

IPC: F02C6/00 ,  F01N3/18 ,  F02C7/22 ,  F02C7/228 ,  F02C9/20 ,  F02C9/28 ,  F23R3/34 ,  F23N1/02 ,  F23N5/02

CPC classification number: F02C6/003 ,  F01N3/18 ,  F02C7/22 ,  F02C7/228 ,  F02C9/20 ,  F02C9/28 ,  F05D2270/08 ,  F05D2270/112 ,  F05D2270/303 ,  F23N1/022 ,  F23N5/022 ,  F23N2025/08 ,  F23N2037/02 ,  F23N2041/20 ,  F23R3/346 ,  F23R2900/03341

Abstract: In a method for the low-CO emissions part load operation of a gas turbine with sequential combustion, the opening of the row of variable compressor inlet guide vanes is controlled depending on the temperatures of the operative burners of the second combustor and simultaneously the number of operative burners is kept at a minimum. This leads to low CO emissions at partial load of the gas turbine.

公开(公告)号：US09726085B2

公开(公告)日：2017-08-08

申请号：US14445627

申请日：2014-07-29

Applicant: ALSTOM Technology Ltd

Inventor： Sebastian Lipari ,  Ghislain Singla ,  Thiemo Meeuwissen ,  Theodoros Ferreira-Providakis

IPC: F02C6/00 ,  F02C9/28 ,  F02C9/34

CPC classification number: F02C9/28 ,  F02C6/003 ,  F02C9/34 ,  F05D2270/14 ,  F05D2270/303 ,  F05D2270/309

Abstract: The invention relates to a method for controlling a gas turbine group including, a first combustion chamber, a first turbine connected, a second combustion chamber, a second turbine, and a load. The method includes: measuring a temperature TAT1 at an outlet of the first turbine; determining a ratio S1R of a fuel mass flow feeding a pilot flame of the first combustion chamber to a total fuel mass flow feeding the first combustion chamber based upon the measured temperature TAT1 in accordance with a predetermined mapping table between ratio S1R and temperature TAT1; adopting the larger one between the determined ratio S1R and a predetermined booster ratio S1R to be used in the controlling fuel flow feeding the first combustion chamber of the gas turbine group. Pulsation behavior of the gas turbine group may be improved. High pulsation during fast de-loading of the gas turbine group is substantially is decreased, avoiding potential damage to the parts of the gas turbine group.

公开(公告)号：US20150040573A1

公开(公告)日：2015-02-12

申请号：US14336174

申请日：2014-07-21

Applicant: ALSTOM Technology Ltd

Inventor： Theodoros FERREIRA-PROVIDAKIS ,  Ghislain Singla ,  Thiemo Meeuwissen ,  Sebastian Lipari

IPC: F02C6/00 ,  F01N3/18 ,  F02C7/22

CPC classification number: F02C6/003 ,  F01N3/18 ,  F02C7/22 ,  F02C7/228 ,  F02C9/20 ,  F02C9/28 ,  F05D2270/08 ,  F05D2270/112 ,  F05D2270/303 ,  F23N1/022 ,  F23N5/022 ,  F23N2025/08 ,  F23N2037/02 ,  F23N2041/20 ,  F23R3/346 ,  F23R2900/03341

Abstract: In a method for the low-CO emissions part load operation of a gas turbine with sequential combustion, the opening of the row of variable compressor inlet guide vanes is controlled depending on the temperatures of the operative burners of the second combustor and simultaneously the number of operative burners is kept at a minimum. This leads to low CO emissions at partial load of the gas turbine.

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，可变压缩机入口导叶的排的开度根据第二燃烧器的操作燃烧器的温度而被控制， 操作燃烧器保持在最低限度。 这导致在燃气轮机的部分负载下的低CO排放。