ATE351975T1 - Verfahren/system zum mapping einer brennkammer in einer gasturbine - Google Patents

Verfahren/system zum mapping einer brennkammer in einer gasturbine

Info

Publication number
ATE351975T1
ATE351975T1 AT03254810T AT03254810T ATE351975T1 AT E351975 T1 ATE351975 T1 AT E351975T1 AT 03254810 T AT03254810 T AT 03254810T AT 03254810 T AT03254810 T AT 03254810T AT E351975 T1 ATE351975 T1 AT E351975T1
Authority
AT
Austria
Prior art keywords
ring flame
limits
acoustic
mapping
flame temperature
Prior art date
Application number
AT03254810T
Other languages
German (de)
English (en)
Inventor
Richard Hook
William Lee Barrow
Eric John Kress
John Bolton
Original Assignee
Gen Electric
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Gen Electric filed Critical Gen Electric
Application granted granted Critical
Publication of ATE351975T1 publication Critical patent/ATE351975T1/de

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26Control of fuel supply
    • F02C9/28Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Regulation And Control Of Combustion (AREA)
AT03254810T 2002-08-02 2003-07-31 Verfahren/system zum mapping einer brennkammer in einer gasturbine ATE351975T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/064,646 US7302334B2 (en) 2002-08-02 2002-08-02 Automatic mapping logic for a combustor in a gas turbine engine

Publications (1)

Publication Number Publication Date
ATE351975T1 true ATE351975T1 (de) 2007-02-15

Family

ID=30113657

Family Applications (1)

Application Number Title Priority Date Filing Date
AT03254810T ATE351975T1 (de) 2002-08-02 2003-07-31 Verfahren/system zum mapping einer brennkammer in einer gasturbine

Country Status (5)

Country Link
US (1) US7302334B2 (enExample)
EP (1) EP1387062B1 (enExample)
JP (1) JP4474132B2 (enExample)
AT (1) ATE351975T1 (enExample)
DE (1) DE60311195T2 (enExample)

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US7461509B2 (en) * 2005-05-06 2008-12-09 General Electric Company Method and system for determining lean blow out condition for gas turbine combustion cans
US7818970B2 (en) 2005-09-12 2010-10-26 Rolls-Royce Power Engineering Plc Controlling a gas turbine engine with a transient load
US7739873B2 (en) * 2005-10-24 2010-06-22 General Electric Company Gas turbine engine combustor hot streak control
US7614238B2 (en) * 2005-11-22 2009-11-10 Honeywell International Inc. Method for lean blowout protection in turbine engines
GB2434437B (en) * 2006-01-19 2011-01-26 Siemens Ag Improvements in or relating to combustion apparatus
US8677761B2 (en) * 2009-02-25 2014-03-25 General Electric Company Systems and methods for engine turn down by controlling extraction air flows
US9267443B2 (en) 2009-05-08 2016-02-23 Gas Turbine Efficiency Sweden Ab Automated tuning of gas turbine combustion systems
US9671797B2 (en) 2009-05-08 2017-06-06 Gas Turbine Efficiency Sweden Ab Optimization of gas turbine combustion systems low load performance on simple cycle and heat recovery steam generator applications
US9354618B2 (en) 2009-05-08 2016-05-31 Gas Turbine Efficiency Sweden Ab Automated tuning of multiple fuel gas turbine combustion systems
US8437941B2 (en) 2009-05-08 2013-05-07 Gas Turbine Efficiency Sweden Ab Automated tuning of gas turbine combustion systems
AU2010247851B2 (en) 2009-05-12 2014-07-24 Icr Turbine Engine Corporation Gas turbine energy storage and conversion system
US9097185B2 (en) * 2009-05-26 2015-08-04 Alstom Technology Ltd Stabilizing a gas turbine engine via incremental tuning
US9890714B2 (en) 2009-05-26 2018-02-13 Ansaldo Energia Ip Uk Limited Automated extended turndown of a gas turbine engine combined with incremental tuning to maintain emissions and dynamics
CN102549342B (zh) * 2009-10-09 2015-10-21 西门子公司 燃烧设备
WO2011109514A1 (en) 2010-03-02 2011-09-09 Icr Turbine Engine Corporatin Dispatchable power from a renewable energy facility
US9086018B2 (en) 2010-04-23 2015-07-21 Hamilton Sundstrand Corporation Starting a gas turbine engine to maintain a dwelling speed after light-off
US8417433B2 (en) 2010-04-30 2013-04-09 Alstom Technology Ltd. Dynamically auto-tuning a gas turbine engine
US9927818B2 (en) 2010-05-24 2018-03-27 Ansaldo Energia Ip Uk Limited Stabilizing a gas turbine engine via incremental tuning during transients
US8984895B2 (en) 2010-07-09 2015-03-24 Icr Turbine Engine Corporation Metallic ceramic spool for a gas turbine engine
CA2813680A1 (en) 2010-09-03 2012-03-08 Icr Turbine Engine Corporation Gas turbine engine configurations
TWI429854B (zh) * 2010-12-17 2014-03-11 Grand Mate Co Ltd Detection and Compensation of Gas Safety Supply
US9051873B2 (en) 2011-05-20 2015-06-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine shaft attachment
US9297316B2 (en) * 2011-11-23 2016-03-29 General Electric Company Method and apparatus for optimizing the operation of a turbine system under flexible loads
US20140020400A1 (en) * 2012-07-18 2014-01-23 Gianni Ceccherini System and method for auto-tuning a combustion system of a gas turbine
US10094288B2 (en) 2012-07-24 2018-10-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine volute attachment for a gas turbine engine
US9447732B2 (en) 2012-11-26 2016-09-20 General Electric Company Gas turbine anti-icing system
GB201317175D0 (en) 2013-09-27 2013-11-06 Rolls Royce Plc An apparatus and a method of controlling the supply of fuel to a combustion chamber
US9599028B2 (en) * 2014-09-08 2017-03-21 General Electric Company Bulk flame temperature regulator for dry low emission engines
US9791351B2 (en) 2015-02-06 2017-10-17 General Electric Company Gas turbine combustion profile monitoring
KR20170001104A (ko) * 2015-06-25 2017-01-04 두산중공업 주식회사 진동제어를 통한 제어방법
WO2017037901A1 (ja) * 2015-09-02 2017-03-09 三菱電機株式会社 シミュレーション装置及びシミュレーションプログラム
EP3301366A1 (en) 2016-09-29 2018-04-04 Siemens Aktiengesellschaft A technique for controlling operating point of a combustion system by using pilot-air
JP6811672B2 (ja) * 2017-04-07 2021-01-13 三菱パワー株式会社 ガスタービン制御装置、ガスタービン、及びガスタービン制御方法
US11589507B2 (en) 2017-06-19 2023-02-28 Deere & Company Combine harvester control interface for operator and/or remote user
CN109579054A (zh) * 2018-11-26 2019-04-05 西安热工研究院有限公司 一种基于火焰温度控制的燃气轮机燃烧调整方法
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US5857321A (en) 1996-06-11 1999-01-12 General Electric Company Controller with neural network for estimating gas turbine internal cycle parameters
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Also Published As

Publication number Publication date
DE60311195T2 (de) 2007-10-18
US20040024516A1 (en) 2004-02-05
EP1387062A2 (en) 2004-02-04
EP1387062A3 (en) 2004-12-22
US7302334B2 (en) 2007-11-27
EP1387062B1 (en) 2007-01-17
JP2004163087A (ja) 2004-06-10
DE60311195D1 (de) 2007-03-08
JP4474132B2 (ja) 2010-06-02

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