MX361552B - Sistema de autoprueba para una turbina de gas. - Google Patents
Sistema de autoprueba para una turbina de gas.Info
- Publication number
- MX361552B MX361552B MX2015010140A MX2015010140A MX361552B MX 361552 B MX361552 B MX 361552B MX 2015010140 A MX2015010140 A MX 2015010140A MX 2015010140 A MX2015010140 A MX 2015010140A MX 361552 B MX361552 B MX 361552B
- Authority
- MX
- Mexico
- Prior art keywords
- gas turbine
- turbine engine
- data
- unit
- test
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
-
- 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
- F02C9/26—Control of fuel supply
-
- 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
-
- 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
- F05D2260/00—Function
- F05D2260/12—Testing on a test bench
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M15/00—Testing of engines
- G01M15/14—Testing gas-turbine engines or jet-propulsion engines
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Testing Of Engines (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
- Testing And Monitoring For Control Systems (AREA)
Abstract
La presente invención se refiere a un sistema de turbina de gas que comprende un motor de turbina de gas (101) para generar potencia, una unidad de control (102) para controlar el motor de turbina de gas (101), un sistema de adquisición de datos (108) que comprende una unidad de modelo termodinámico (104) y una unidad de secuencia de prueba (105), un dispositivo sensor (103) que se acopla al motor de turbina de gas (101) para medir un parámetro de rendimiento (115) del motor de turbina de gas (101), y una unidad comparativa (109). La unidad de modelo termodinámico (104) genera un parámetro de rendimiento computado (113) basándose en un modelo mecánico (106) del motor de turbina de gas (101) y basándose en un modelo termodinámico (107) del motor de turbina de gas (101) La unidad de secuencia de prueba (105) genera datos de secuencia de prueba (114) que comprenden datos de funcionamiento de punto de referencia y datos de horario con los que puede operarse un ciclo de prueba del motor de turbina de gas (101) . El sistema de adquisición de datos (108) genera datos de control de prueba (112) basándose en los datos de secuencia de prueba (114), en el que el sistema de adquisición de datos (108) se acopla a la unidad de control (102) para proporcionar los datos de control de prueba (112) a la unidad de control (102), de manera que el motor de turbina de gas (101) puede controlarse basándose en los datos de control de prueba (112) . La unidad comparativa (109) se acopla al sistema de adquisición de datos (108), de manera que el parámetro de rendimiento medido (115), medido mediante el dispositivo sensor (103) puede compararse con el parámetro de rendimiento computado (113).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP13154041.1A EP2762852A1 (en) | 2013-02-05 | 2013-02-05 | Automatic Testing System for a Gas Turbine |
PCT/EP2014/051168 WO2014122013A1 (en) | 2013-02-05 | 2014-01-22 | Auto testing system for a gas turbine |
Publications (2)
Publication Number | Publication Date |
---|---|
MX2015010140A MX2015010140A (es) | 2015-12-17 |
MX361552B true MX361552B (es) | 2018-12-10 |
Family
ID=47739058
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MX2015010140A MX361552B (es) | 2013-02-05 | 2014-01-22 | Sistema de autoprueba para una turbina de gas. |
Country Status (10)
Country | Link |
---|---|
US (1) | US10067035B2 (es) |
EP (2) | EP2762852A1 (es) |
JP (1) | JP6403690B2 (es) |
KR (2) | KR20150114559A (es) |
CN (1) | CN105074413B (es) |
BR (1) | BR112015018471B1 (es) |
CA (1) | CA2898392C (es) |
MX (1) | MX361552B (es) |
RU (1) | RU2627617C2 (es) |
WO (1) | WO2014122013A1 (es) |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2762852A1 (en) | 2013-02-05 | 2014-08-06 | Siemens Aktiengesellschaft | Automatic Testing System for a Gas Turbine |
CN104168241B (zh) * | 2013-05-16 | 2017-10-17 | 华为技术有限公司 | 多输入输出正交频分复用通信系统及信号补偿方法 |
US10024187B2 (en) | 2015-03-20 | 2018-07-17 | General Electric Company | Gas turbine engine health determination |
FR3036798B1 (fr) | 2015-06-01 | 2018-06-15 | Safran Helicopter Engines | Procede de detection d'un defaut mecanique d'un generateur de gaz d'une turbomachine d'un aeronef et dispositif de mise en œuvre correspondant |
KR101860985B1 (ko) * | 2015-08-13 | 2018-07-05 | 두산중공업 주식회사 | 가스터빈 엔진의 수명평가시험장치 및 수명평가시험방법 |
EP3239684A1 (en) | 2016-04-29 | 2017-11-01 | Siemens Aktiengesellschaft | Fault diagnosis during testing of turbine unit |
CN107560864B (zh) * | 2016-06-30 | 2020-10-16 | 西门子公司 | 用于燃烧器中结垢监测和预测的方法与装置 |
FR3064680B1 (fr) * | 2017-04-03 | 2019-04-05 | Safran Helicopter Engines | Procede de verification de la puissance maximale disponible d'une turbomachine d'un aeronef equipe de deux turbomachines |
KR200489866Y1 (ko) * | 2017-11-10 | 2019-11-04 | 주식회사 이지티 | 가스 터빈 엔진 테스트 시스템 |
EP3647759B1 (en) * | 2018-11-02 | 2022-11-02 | Rolls-Royce plc | Calibrating an engine core |
GB201817933D0 (en) | 2018-11-02 | 2018-12-19 | Rolls Royce Plc | Calibrating an engine core |
CN109992880B (zh) * | 2019-03-29 | 2021-08-27 | 中国石油大学(北京) | 一种燃气轮机性能适配方法、设备以及系统 |
CN112081671A (zh) * | 2019-06-13 | 2020-12-15 | 中国科学院工程热物理研究所 | 燃气轮机燃料控制装置及基于其的仿真测试方法 |
RU198631U1 (ru) * | 2020-05-27 | 2020-07-21 | Максим Владимирович Окороков | Устройство оценки показателей безотказности технических систем по результатам наблюдений моментов отказов |
RU2758781C1 (ru) * | 2020-07-24 | 2021-11-01 | Акционерное общество "НПО Энергомаш имени академика В.П. Глушко" | Способ контроля технического состояния жидкостного ракетного двигателя на переходных режимах стендового испытания |
RU2755450C1 (ru) * | 2020-08-10 | 2021-09-16 | Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") | Способ обеспечения прочности турбины газотурбинного двигателя |
CN111963322A (zh) * | 2020-08-26 | 2020-11-20 | 四川海特亚美航空技术有限公司 | 一种涡轴发动机双通道电子控制系统数据采集系统 |
CN112611567B (zh) * | 2020-11-27 | 2022-05-27 | 中国航发四川燃气涡轮研究院 | 一种航空发动机高空模拟试车台调节阀自动选型方法 |
CN112555050B (zh) * | 2020-12-02 | 2022-03-11 | 西安航天动力试验技术研究所 | 一种分布式超音速空气流生成装置运行状态监测及急停方法 |
CN112539941B (zh) * | 2020-12-02 | 2023-01-20 | 西安航天动力研究所 | 考虑真实气体效应的液体火箭发动机热试验参数设置方法 |
KR102601898B1 (ko) * | 2020-12-21 | 2023-11-14 | 한국전력공사 | 터빈 제어 검증 시스템, 및 터빈 제어 검증 장치 |
CN112901598B (zh) * | 2021-01-29 | 2022-08-26 | 上海电气燃气轮机有限公司 | 一种燃气轮机液压执行机构测试方法、电子终端及存储介质 |
US20220300682A1 (en) * | 2021-03-18 | 2022-09-22 | Pratt & Whitney Canada Corp. | Methods and systems for assessing compliance of aircraft engines |
CN117052567B (zh) * | 2023-10-13 | 2024-06-11 | 北京星河动力装备科技有限公司 | 火箭发动机试车控制系统 |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
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US4215412A (en) | 1978-07-13 | 1980-07-29 | The Boeing Company | Real time performance monitoring of gas turbine engines |
US4389710A (en) | 1981-01-12 | 1983-06-21 | Goodyear Aerospace Corporation | Braking system test circuit |
US4821217A (en) | 1987-01-12 | 1989-04-11 | The Boeing Company | Programmable jet engine test station |
JP3024713B2 (ja) | 1991-07-31 | 2000-03-21 | 富士電機株式会社 | タービンのシミュレーション装置 |
US5521824A (en) | 1992-12-07 | 1996-05-28 | Caterpillar Inc. | Method and apparatus for controlling an engine test apparatus using lead-lag control |
US6687596B2 (en) | 2001-08-31 | 2004-02-03 | General Electric Company | Diagnostic method and system for turbine engines |
EP1293655A1 (en) * | 2001-09-13 | 2003-03-19 | Mitsubishi Heavy Industries, Ltd. | Gas turbine, driving method thereof and gas turbine combined electric power generation plant |
JP2003106525A (ja) | 2001-09-28 | 2003-04-09 | Mitsubishi Heavy Ind Ltd | 乱流反応流解析方法および装置 |
RU2340883C1 (ru) | 2007-05-18 | 2008-12-10 | Государственное образовательное учреждение высшего профессионального образования Уфимский государственный авиационный технический университет | Способ полунатурных испытаний систем автоматического управления и контроля газотурбинных двигателей и стенд для его реализации |
US20090171626A1 (en) | 2007-12-27 | 2009-07-02 | Dweik Zaineddin S | Integrated Engineering Analysis System |
JP2010019725A (ja) * | 2008-07-11 | 2010-01-28 | Denso Corp | エンジン特性パラメータの自動計測方法及び自動計測システム |
US20100089067A1 (en) * | 2008-10-10 | 2010-04-15 | General Electric Company | Adaptive performance model and methods for system maintenance |
RU2389998C1 (ru) * | 2008-11-13 | 2010-05-20 | Открытое акционерное общество "Авиадвигатель" | Способ оценки технического состояния авиационного газотурбинного двигателя |
US8381510B2 (en) * | 2009-04-30 | 2013-02-26 | General Electric Company | Method and systems for controlling engine thrust using variable trim |
US8260523B2 (en) | 2009-05-04 | 2012-09-04 | General Electric Company | Method for detecting gas turbine engine flashback |
US8712739B2 (en) | 2010-11-19 | 2014-04-29 | General Electric Company | System and method for hybrid risk modeling of turbomachinery |
US8161806B1 (en) | 2010-12-23 | 2012-04-24 | General Electric Company | Method of monitoring engine performance parameters of a gas turbine engine |
EP2762852A1 (en) | 2013-02-05 | 2014-08-06 | Siemens Aktiengesellschaft | Automatic Testing System for a Gas Turbine |
-
2013
- 2013-02-05 EP EP13154041.1A patent/EP2762852A1/en not_active Withdrawn
-
2014
- 2014-01-22 RU RU2015132521A patent/RU2627617C2/ru active
- 2014-01-22 US US14/763,765 patent/US10067035B2/en active Active
- 2014-01-22 JP JP2015556438A patent/JP6403690B2/ja active Active
- 2014-01-22 WO PCT/EP2014/051168 patent/WO2014122013A1/en active Application Filing
- 2014-01-22 CA CA2898392A patent/CA2898392C/en active Active
- 2014-01-22 MX MX2015010140A patent/MX361552B/es active IP Right Grant
- 2014-01-22 KR KR1020157023937A patent/KR20150114559A/ko not_active Application Discontinuation
- 2014-01-22 CN CN201480007448.4A patent/CN105074413B/zh active Active
- 2014-01-22 EP EP14703288.2A patent/EP2954297B1/en active Active
- 2014-01-22 KR KR1020177026306A patent/KR102072349B1/ko active IP Right Grant
- 2014-01-22 BR BR112015018471-5A patent/BR112015018471B1/pt active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
EP2954297A1 (en) | 2015-12-16 |
US20150362405A1 (en) | 2015-12-17 |
BR112015018471A2 (pt) | 2017-07-18 |
CN105074413B (zh) | 2019-10-15 |
CN105074413A (zh) | 2015-11-18 |
US10067035B2 (en) | 2018-09-04 |
WO2014122013A1 (en) | 2014-08-14 |
RU2627617C2 (ru) | 2017-08-09 |
CA2898392A1 (en) | 2014-08-14 |
KR20150114559A (ko) | 2015-10-12 |
KR102072349B1 (ko) | 2020-01-31 |
JP2016513202A (ja) | 2016-05-12 |
KR20170109087A (ko) | 2017-09-27 |
BR112015018471B1 (pt) | 2022-01-18 |
MX2015010140A (es) | 2015-12-17 |
JP6403690B2 (ja) | 2018-10-10 |
EP2762852A1 (en) | 2014-08-06 |
CA2898392C (en) | 2018-07-10 |
RU2015132521A (ru) | 2017-03-13 |
EP2954297B1 (en) | 2018-12-26 |
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Legal Events
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FG | Grant or registration |