MX2009008076A - Metodo para detectar una falla parcial de la flama en un motor de turbina de gas y un motor de turbina de gas. - Google Patents
Metodo para detectar una falla parcial de la flama en un motor de turbina de gas y un motor de turbina de gas.Info
- Publication number
- MX2009008076A MX2009008076A MX2009008076A MX2009008076A MX2009008076A MX 2009008076 A MX2009008076 A MX 2009008076A MX 2009008076 A MX2009008076 A MX 2009008076A MX 2009008076 A MX2009008076 A MX 2009008076A MX 2009008076 A MX2009008076 A MX 2009008076A
- Authority
- MX
- Mexico
- Prior art keywords
- gas turbine
- turbine engine
- detecting
- flame failure
- partial flame
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23N—REGULATING OR CONTROLLING COMBUSTION
- F23N5/00—Systems for controlling combustion
- F23N5/02—Systems for controlling combustion using devices responsive to thermal changes or to thermal expansion of a medium
- F23N5/10—Systems for controlling combustion using devices responsive to thermal changes or to thermal expansion of a medium using thermocouples
- F23N5/102—Systems for controlling combustion using devices responsive to thermal changes or to thermal expansion of a medium using thermocouples using electronic means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/003—Arrangements for testing or measuring
-
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/26—Starting; Ignition
- F02C7/262—Restarting after flame-out
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23N—REGULATING OR CONTROLLING COMBUSTION
- F23N5/00—Systems for controlling combustion
- F23N5/24—Preventing development of abnormal or undesired conditions, i.e. safety arrangements
- F23N5/242—Preventing development of abnormal or undesired conditions, i.e. safety arrangements using electronic means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23N—REGULATING OR CONTROLLING COMBUSTION
- F23N2225/00—Measuring
- F23N2225/08—Measuring temperature
- F23N2225/16—Measuring temperature burner temperature
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23N—REGULATING OR CONTROLLING COMBUSTION
- F23N2225/00—Measuring
- F23N2225/08—Measuring temperature
- F23N2225/21—Measuring temperature outlet temperature
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23N—REGULATING OR CONTROLLING COMBUSTION
- F23N2231/00—Fail safe
- F23N2231/06—Fail safe for flame failures
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23N—REGULATING OR CONTROLLING COMBUSTION
- F23N2241/00—Applications
- F23N2241/20—Gas turbines
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Measuring Temperature Or Quantity Of Heat (AREA)
- Control Of Turbines (AREA)
Abstract
Se proporciona un método para detectar una falla parcial de la flama en turbina de gas (10) tiene un conducto de gas (34) para guiar gas de propulsión (18) y varias cámaras de combustión (24), cada una de tales cámaras de combustión (24) se llevan dentro del conducto de gas (34) y comprende un quemador (36). El método comprende las etapas de: medir una primer temperatura durante el tiempo en cada uno de por lo menos dos puntos de sondeo (32a, 32b) ubicados corriente abajo de dichas cámaras de combustión (24) en dicho conducto de gas (34), medir una segunda temperatura durante el tiempo en cada uno de por lo menos dos de dichos quemadores (36), y detectar una falla de llama parcial de dichas primeras mediciones de temperatura y dichas segundas mediciones de temperatura, para detectar una falla de llama parcial incluye la etapa de determinar un primer parámetro de detección, dicho primer parámetro de detección se determina de una tasa de cambio de una variación entre dicha primer medición de temperatura en diferentes puntos de sondeo (32a , 32b).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP07002015A EP1953454A1 (en) | 2007-01-30 | 2007-01-30 | Method of detecting a partial flame failure in a gas turbine engine and a gas turbine engine |
PCT/EP2008/050943 WO2008092822A1 (en) | 2007-01-30 | 2008-01-28 | Method of detecting a partial flame failure in a gas turbine engine and a gas turbine engine |
Publications (1)
Publication Number | Publication Date |
---|---|
MX2009008076A true MX2009008076A (es) | 2009-08-12 |
Family
ID=38116994
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MX2009008076A MX2009008076A (es) | 2007-01-30 | 2008-01-28 | Metodo para detectar una falla parcial de la flama en un motor de turbina de gas y un motor de turbina de gas. |
Country Status (6)
Country | Link |
---|---|
US (1) | US8474269B2 (es) |
EP (2) | EP1953454A1 (es) |
CN (1) | CN101595344B (es) |
MX (1) | MX2009008076A (es) |
RU (1) | RU2421662C2 (es) |
WO (1) | WO2008092822A1 (es) |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8684276B2 (en) * | 2009-08-20 | 2014-04-01 | Enerco Group, Inc. | Portable catalytic heater |
US8725448B2 (en) | 2010-09-23 | 2014-05-13 | Siemens Energy, Inc. | Self validating gas turbine engine flame detection system using duel optical verification |
EP2469041A1 (en) | 2010-12-22 | 2012-06-27 | Siemens Aktiengesellschaft | Method of detecting a predetermined condition in a gas turbine and failure detection system for a gas turbine |
EP2469167A1 (en) | 2010-12-22 | 2012-06-27 | Siemens Aktiengesellschaft | System for aerating liquid fuel with gas for a gas turbine and method for aerating liquid fuel with gas for a gas turbine |
FR2970304B1 (fr) * | 2011-01-11 | 2013-02-08 | Turbomeca | Procede de demarrage d'une turbomachine |
EP2487415A1 (en) | 2011-02-10 | 2012-08-15 | Siemens Aktiengesellschaft | An arrangement for preparation of liquid fuel for combustion and a method of preparing liquid fuel for combustion |
JP5675456B2 (ja) * | 2011-03-25 | 2015-02-25 | 三菱重工業株式会社 | 監視装置、ガスタービンプラント、及びガスタービンの監視方法 |
US20130040254A1 (en) * | 2011-08-08 | 2013-02-14 | General Electric Company | System and method for monitoring a combustor |
US20130323658A1 (en) * | 2012-05-29 | 2013-12-05 | Honeywell International Inc. | Burner flame detection and monitoring system |
US8601861B1 (en) * | 2012-08-10 | 2013-12-10 | General Electric Company | Systems and methods for detecting the flame state of a combustor of a turbine engine |
FR3022303B1 (fr) * | 2014-06-12 | 2016-07-01 | Snecma | Procede de detection d'une degradation d'une canalisation de turboreacteur |
RU2578012C1 (ru) * | 2015-03-23 | 2016-03-20 | Открытое акционерное общество "Авиадвигатель" | Способ определения погасания камеры сгорания газотурбинного двигателя |
EP3239684A1 (en) * | 2016-04-29 | 2017-11-01 | Siemens Aktiengesellschaft | Fault diagnosis during testing of turbine unit |
EP3589590B1 (fr) | 2017-02-28 | 2023-07-05 | Saint-Gobain Seva | Alliage pour assiette de fibrage |
IT201700028071A1 (it) * | 2017-03-14 | 2018-09-14 | Nuovo Pignone Tecnologie Srl | Metodi per rilevare un guasto in un bruciatore di un combustore e sistemi a turbina |
EP3531019A1 (en) * | 2018-02-27 | 2019-08-28 | Siemens Aktiengesellschaft | Analysis method for a gas turbine |
RU2696919C1 (ru) * | 2018-04-18 | 2019-08-07 | Акционерное общество "РОТЕК" (АО "РОТЕК") | Способ и система оценки технического состояния узлов газовой турбины по температурным полям |
RU2711724C1 (ru) * | 2018-10-04 | 2020-01-21 | Акционерное общество "РОТЕК" (АО "РОТЕК") | Способ оценки положения эпицентра теплового поля выхлопа газотурбинной установки |
EP4015783A1 (en) * | 2020-12-18 | 2022-06-22 | Ansaldo Energia Switzerland AG | Gas turbine engine with flame failure protection base on exhaust gas temperature and method of operating a gas turbine engine |
EP4116545A1 (en) * | 2021-07-05 | 2023-01-11 | Siemens Energy Global GmbH & Co. KG | Continuous flow engine measurement arrangement |
CN114893301B (zh) * | 2022-04-14 | 2023-09-08 | 北京动力机械研究所 | 小型涡扇发动机参控温度参数判故方法及冗余控制方法 |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4283634A (en) * | 1971-06-23 | 1981-08-11 | Westinghouse Electric Corp. | System and method for monitoring and controlling operation of industrial gas turbine apparatus and gas turbine electric power plants preferably with a digital computer control system |
US3747340A (en) * | 1971-08-12 | 1973-07-24 | Ford Motor Co | Flame sensing system for a turbine engine |
US4115998A (en) * | 1975-12-08 | 1978-09-26 | General Electric Company | Combustion monitor |
GB2282221A (en) * | 1993-09-22 | 1995-03-29 | Rolls Royce Plc | A flame detector |
JPH07189741A (ja) * | 1993-12-10 | 1995-07-28 | Solar Turbines Inc | 燃焼室1次ゾーン温度決定制御装置及び方法 |
US5551227A (en) * | 1994-12-22 | 1996-09-03 | General Electric Company | System and method of detecting partial flame out in a gas turbine engine combustor |
RU8087U1 (ru) | 1996-09-26 | 1998-10-16 | Николай Александрович Барков | Устройство контроля пламени горелки |
RU2183795C2 (ru) | 2000-05-17 | 2002-06-20 | Шутиков Владимир Антонович | Устройство для контроля наличия пламени |
US6442943B1 (en) * | 2001-05-17 | 2002-09-03 | General Electric Company | Methods and apparatus for detecting turbine engine flameout |
JP2006083730A (ja) * | 2004-09-15 | 2006-03-30 | Hitachi Ltd | ガスタービンの着火検出方法 |
RU42625U1 (ru) | 2004-09-29 | 2004-12-10 | Открытое акционерное общество "ВНИПИгаздобыча" | Горелка факельная газовая |
US7739873B2 (en) * | 2005-10-24 | 2010-06-22 | General Electric Company | Gas turbine engine combustor hot streak control |
-
2007
- 2007-01-30 EP EP07002015A patent/EP1953454A1/en not_active Withdrawn
-
2008
- 2008-01-28 EP EP08708266.5A patent/EP2108093B1/en active Active
- 2008-01-28 RU RU2009132539/06A patent/RU2421662C2/ru active
- 2008-01-28 CN CN2008800035554A patent/CN101595344B/zh active Active
- 2008-01-28 MX MX2009008076A patent/MX2009008076A/es active IP Right Grant
- 2008-01-28 US US12/524,788 patent/US8474269B2/en active Active
- 2008-01-28 WO PCT/EP2008/050943 patent/WO2008092822A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
EP2108093B1 (en) | 2017-07-19 |
RU2421662C2 (ru) | 2011-06-20 |
US8474269B2 (en) | 2013-07-02 |
EP1953454A1 (en) | 2008-08-06 |
US20100024431A1 (en) | 2010-02-04 |
WO2008092822A1 (en) | 2008-08-07 |
EP2108093A1 (en) | 2009-10-14 |
CN101595344B (zh) | 2011-11-16 |
RU2009132539A (ru) | 2011-03-10 |
CN101595344A (zh) | 2009-12-02 |
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Legal Events
Date | Code | Title | Description |
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HH | Correction or change in general | ||
FG | Grant or registration |