MX2012006116A - Metodo de control de modo basado en temperatura de escape para turbina de gas, y turbina de gas. - Google Patents
Metodo de control de modo basado en temperatura de escape para turbina de gas, y turbina de gas.Info
- Publication number
- MX2012006116A MX2012006116A MX2012006116A MX2012006116A MX2012006116A MX 2012006116 A MX2012006116 A MX 2012006116A MX 2012006116 A MX2012006116 A MX 2012006116A MX 2012006116 A MX2012006116 A MX 2012006116A MX 2012006116 A MX2012006116 A MX 2012006116A
- Authority
- MX
- Mexico
- Prior art keywords
- sub
- gas turbine
- value
- igv
- turbine
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/16—Control of working fluid flow
- F02C9/20—Control of working fluid flow by throttling; by adjusting vanes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- F02C9/32—Control of fuel supply characterised by throttling of fuel
- F02C9/34—Joint control of separate flows to main and auxiliary burners
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/30—Control parameters, e.g. input parameters
- F05D2270/301—Pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/30—Control parameters, e.g. input parameters
- F05D2270/303—Temperature
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Control Of Turbines (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
- Control Of Positive-Displacement Air Blowers (AREA)
- Supercharger (AREA)
Abstract
Se describen una turbina de gas y un método para controlar un punto de operación de la turbina de gas que incluye un compresor, un combustor, y por lo menos una turbina. El método incluye calcular una curva de referencia de temperatura de escape de la turbina como una función de una relación de presión de turbina; determinar s la condición IGVmin + MGVI = IGVpunto de referencia = lGVmax + MGV2, y la condición ttx = ttxh + ttx3, son verdaderas; y cambiar, si ambas condiciones son verdaderas, una cantidad de combustible dividido por un segundo valor o de otra manera mantener el primer valor, el primer valor caracterizando un modo de estado estable improductivo-improductivo y el segundo valor caracterizando un modo secundario pre-mezclado de un modo pre-mezclado.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ITCO2009A000055A IT1396517B1 (it) | 2009-11-27 | 2009-11-27 | Metodo di controllo di modo basato su temperatura di scarico per turbina a gas e turbina a gas |
| PCT/EP2010/068334 WO2011064343A1 (en) | 2009-11-27 | 2010-11-26 | Exhaust temperature based mode control method for gas turbine and gas turbine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| MX2012006116A true MX2012006116A (es) | 2012-08-15 |
Family
ID=42335092
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| MX2012006116A MX2012006116A (es) | 2009-11-27 | 2010-11-26 | Metodo de control de modo basado en temperatura de escape para turbina de gas, y turbina de gas. |
Country Status (13)
| Country | Link |
|---|---|
| US (1) | US8713946B2 (es) |
| EP (1) | EP2504547B1 (es) |
| JP (1) | JP5735975B2 (es) |
| KR (1) | KR20120106780A (es) |
| CN (1) | CN102725498B (es) |
| AU (1) | AU2010323059B2 (es) |
| BR (1) | BR112012012757B8 (es) |
| CA (1) | CA2782057C (es) |
| IT (1) | IT1396517B1 (es) |
| MX (1) | MX2012006116A (es) |
| MY (1) | MY156015A (es) |
| RU (1) | RU2540210C2 (es) |
| WO (1) | WO2011064343A1 (es) |
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| 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 |
| MX354587B (es) * | 2010-07-02 | 2018-03-12 | Exxonmobil Upstream Res Company Star | Combustión estequiométrica de aire enriquecido con recirculación de gas de escape. |
| EP2588729B1 (en) * | 2010-07-02 | 2020-07-15 | Exxonmobil Upstream Research Company | Low emission triple-cycle power generation systems and methods |
| ITCO20120008A1 (it) | 2012-03-01 | 2013-09-02 | Nuovo Pignone Srl | Metodo e sistema per monitorare la condizione di un gruppo di impianti |
| US9435690B2 (en) * | 2012-06-05 | 2016-09-06 | General Electric Company | Ultra-violet flame detector with high temperature remote sensing element |
| US10392959B2 (en) | 2012-06-05 | 2019-08-27 | General Electric Company | High temperature flame sensor |
| ITCO20120067A1 (it) | 2012-12-20 | 2014-06-21 | Nuovo Pignone Srl | Misura della pressione totale e della temperatura totale in condizione di gas umido |
| KR101690444B1 (ko) * | 2013-02-26 | 2016-12-27 | 미츠비시 히타치 파워 시스템즈 가부시키가이샤 | 가스 터빈 시스템, 제어 장치 및 가스 터빈 운전 방법 |
| EP2840245A1 (en) * | 2013-08-20 | 2015-02-25 | Alstom Technology Ltd | Method for controlling a gas turbine group |
| JP6164994B2 (ja) * | 2013-09-06 | 2017-07-19 | 三菱日立パワーシステムズ株式会社 | ガスタービンプラント、その制御装置、及びガスタービンの運転方法 |
| 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 |
| EP2907990A1 (de) * | 2014-02-18 | 2015-08-19 | Siemens Aktiengesellschaft | Verfahren zum Betreiben einer Gasturbinenanlage und dieselbe |
| EP2942511A1 (de) * | 2014-05-05 | 2015-11-11 | Siemens Aktiengesellschaft | Verfahren zur Auswahl von Betriebspunkten einer Gasturbine |
| EP2952811A1 (en) | 2014-06-02 | 2015-12-09 | Siemens Aktiengesellschaft | Method and device to control a fuel split in a combustion device |
| US10669959B2 (en) * | 2014-09-02 | 2020-06-02 | Mitsubishi Hitachi Power Systems, Ltd. | Control device, system, control method, power control device, gas turbine, and power control method |
| FR3025590B1 (fr) * | 2014-09-10 | 2021-09-24 | Snecma | Repartition du debit en injection multipoints en fonction du rapport carburant/air dans la chambre de combustion |
| CN104315541B (zh) * | 2014-09-26 | 2019-01-18 | 北京华清燃气轮机与煤气化联合循环工程技术有限公司 | 燃烧室值班级喷嘴及使用该喷嘴的方法 |
| US9773584B2 (en) | 2014-11-24 | 2017-09-26 | General Electric Company | Triaxial mineral insulated cable in flame sensing applications |
| JP2018520289A (ja) | 2015-04-30 | 2018-07-26 | ヌオーヴォ・ピニォーネ・テクノロジー・ソチエタ・レスポンサビリタ・リミタータＮｕｏｖｏ Ｐｉｇｎｏｎｅ Ｔｅｃｎｏｌｏｇｉｅ Ｓ．Ｒ．Ｌ． | 機械駆動用途における超低ＮＯｘ排出ガスタービンエンジン |
| JP6033391B1 (ja) * | 2015-11-24 | 2016-11-30 | 三菱日立パワーシステムズ株式会社 | ガスタービンの運転制御方法、改装方法、及びガスタービン制御装置の設定変更方法 |
| US10036325B2 (en) * | 2016-03-30 | 2018-07-31 | General Electric Company | Variable flow compressor of a gas turbine |
| US10569759B2 (en) | 2017-06-30 | 2020-02-25 | General Electric Company | Propulsion system for an aircraft |
| US10696416B2 (en) | 2017-06-30 | 2020-06-30 | General Electric Company | Propulsion system for an aircraft |
| US10738706B2 (en) | 2017-06-30 | 2020-08-11 | General Electric Company | Propulsion system for an aircraft |
| US10953995B2 (en) | 2017-06-30 | 2021-03-23 | General Electric Company | Propulsion system for an aircraft |
| EP3456946A1 (en) | 2017-09-18 | 2019-03-20 | Siemens Aktiengesellschaft | Controller & method |
| CN111855221A (zh) * | 2020-07-28 | 2020-10-30 | 青岛中科国晟动力科技有限公司 | 一种燃气轮机燃烧状态监测方法及系统 |
| CN116245033B (zh) * | 2023-05-12 | 2023-09-15 | 南方电网数字电网研究院有限公司 | 人工智能驱动的电力系统分析方法及智能软件平台 |
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| JPH07189746A (ja) * | 1993-12-28 | 1995-07-28 | Hitachi Ltd | ガスタービン燃焼器の制御方法 |
| US6092362A (en) * | 1996-11-27 | 2000-07-25 | Hitachi, Ltd. | Gas-turbine combustor with load-responsive premix burners |
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| RU2160370C2 (ru) * | 1999-03-19 | 2000-12-10 | Акционерное общество открытого типа "Всероссийский теплотехнический научно-исследовательский институт" | Высокоэкономичная парогазовая установка малой мощности |
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| RU2237815C2 (ru) * | 2002-06-07 | 2004-10-10 | Морев Валерий Григорьевич | Способ получения полезной энергии в комбинированном цикле (его варианты) и устройство для его осуществления |
| US6779346B2 (en) * | 2002-12-09 | 2004-08-24 | General Electric Company | Control of gas turbine combustion temperature by compressor bleed air |
| US7246002B2 (en) * | 2003-11-20 | 2007-07-17 | General Electric Company | Method for controlling fuel splits to gas turbine combustor |
| RU2258147C1 (ru) * | 2003-12-29 | 2005-08-10 | Открытое Акционерное Общество "Всероссийский теплотехнический научно-исследовательский институт (ВТИ)" | Способ замещения газотурбинного топлива в энергетических циклах |
| JP4119909B2 (ja) * | 2005-09-14 | 2008-07-16 | 三菱重工業株式会社 | ガスタービンの燃焼制御装置 |
| US7549292B2 (en) * | 2005-10-03 | 2009-06-23 | General Electric Company | Method of controlling bypass air split to gas turbine combustor |
| RU2323351C2 (ru) * | 2005-12-23 | 2008-04-27 | Геннадий Павлович Барчан | Способ преобразования энергии, выделяющейся в экзотермическом процессе, в механическую работу |
| US7878004B2 (en) | 2006-04-20 | 2011-02-01 | Siemens Aktiengesellschaft | Method and device for optimizing a light-up procedure of a gas turbine engine |
| EP1860302A1 (en) | 2006-05-22 | 2007-11-28 | Siemens Aktiengesellschaft | Gas turbine engine starting method and control device |
| JP4831820B2 (ja) * | 2006-05-22 | 2011-12-07 | 三菱重工業株式会社 | ガスタービン出力学習回路及びこれを備えたガスタービンの燃焼制御装置 |
| US9043118B2 (en) | 2007-04-02 | 2015-05-26 | General Electric Company | Methods and systems for model-based control of gas turbines |
| ITMI20080164A1 (it) | 2008-02-04 | 2009-08-05 | Nuovo Pignone Spa | Metodo per l'avviamento di una turbina a gas |
| JP5490023B2 (ja) * | 2008-03-05 | 2014-05-14 | アルストム テクノロジー リミテッド | 発電所におけるガスタービンの制御方法およびその方法を実施する発電所 |
| EP2107305A1 (en) * | 2008-04-01 | 2009-10-07 | Siemens Aktiengesellschaft | Gas turbine system and method |
| UA37228U (ru) * | 2008-05-12 | 2008-11-25 | Винницкий Национальный Медицинский Университет Им. Н.И. Пирогова | Способ лечения фетоплацентарной недостаточности у беременных с гипертензивными расстройствами |
-
2009
- 2009-11-27 IT ITCO2009A000055A patent/IT1396517B1/it active
-
2010
- 2010-11-26 CN CN201080062626.5A patent/CN102725498B/zh not_active Expired - Fee Related
- 2010-11-26 BR BR112012012757A patent/BR112012012757B8/pt active IP Right Grant
- 2010-11-26 JP JP2012540444A patent/JP5735975B2/ja active Active
- 2010-11-26 AU AU2010323059A patent/AU2010323059B2/en active Active
- 2010-11-26 RU RU2012122723/06A patent/RU2540210C2/ru not_active IP Right Cessation
- 2010-11-26 MY MYPI2012002350A patent/MY156015A/en unknown
- 2010-11-26 KR KR1020127016660A patent/KR20120106780A/ko not_active Application Discontinuation
- 2010-11-26 CA CA2782057A patent/CA2782057C/en active Active
- 2010-11-26 WO PCT/EP2010/068334 patent/WO2011064343A1/en active Application Filing
- 2010-11-26 US US13/512,120 patent/US8713946B2/en active Active
- 2010-11-26 MX MX2012006116A patent/MX2012006116A/es active IP Right Grant
- 2010-11-26 EP EP10788283.9A patent/EP2504547B1/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN102725498B (zh) | 2016-03-02 |
| EP2504547A1 (en) | 2012-10-03 |
| AU2010323059A1 (en) | 2012-06-14 |
| BR112012012757B8 (pt) | 2023-03-28 |
| US20120279230A1 (en) | 2012-11-08 |
| WO2011064343A1 (en) | 2011-06-03 |
| RU2540210C2 (ru) | 2015-02-10 |
| US8713946B2 (en) | 2014-05-06 |
| EP2504547B1 (en) | 2016-02-17 |
| MY156015A (en) | 2015-12-31 |
| KR20120106780A (ko) | 2012-09-26 |
| AU2010323059B2 (en) | 2016-07-21 |
| RU2012122723A (ru) | 2014-01-10 |
| JP2013512381A (ja) | 2013-04-11 |
| IT1396517B1 (it) | 2012-12-14 |
| BR112012012757A2 (pt) | 2016-09-06 |
| CA2782057C (en) | 2017-06-13 |
| BR112012012757B1 (pt) | 2020-11-17 |
| CA2782057A1 (en) | 2011-06-03 |
| ITCO20090055A1 (it) | 2011-05-28 |
| CN102725498A (zh) | 2012-10-10 |
| JP5735975B2 (ja) | 2015-06-17 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FG | Grant or registration |