MX2015010140A - Sistema de autoprueba para una turbina de gas. - Google Patents

Sistema de autoprueba para una turbina de gas.

Info

Publication number
MX2015010140A
MX2015010140A MX2015010140A MX2015010140A MX2015010140A MX 2015010140 A MX2015010140 A MX 2015010140A MX 2015010140 A MX2015010140 A MX 2015010140A MX 2015010140 A MX2015010140 A MX 2015010140A MX 2015010140 A MX2015010140 A MX 2015010140A
Authority
MX
Mexico
Prior art keywords
gas turbine
turbine engine
data
unit
test
Prior art date
Application number
MX2015010140A
Other languages
English (en)
Other versions
MX361552B (es
Inventor
Samuel Bowler
Michael Smith
Andrew Yarwood
Original Assignee
Siemens Ag
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 Siemens Ag filed Critical Siemens Ag
Publication of MX2015010140A publication Critical patent/MX2015010140A/es
Publication of MX361552B publication Critical patent/MX361552B/es

Links

Classifications

    • 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
    • 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

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 And Monitoring For Control Systems (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (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).
MX2015010140A 2013-02-05 2014-01-22 Sistema de autoprueba para una turbina de gas. MX361552B (es)

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 true MX2015010140A (es) 2015-12-17
MX361552B 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) KR102072349B1 (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)

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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
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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
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Also Published As

Publication number Publication date
RU2627617C2 (ru) 2017-08-09
EP2954297B1 (en) 2018-12-26
KR20170109087A (ko) 2017-09-27
CA2898392C (en) 2018-07-10
CN105074413B (zh) 2019-10-15
US10067035B2 (en) 2018-09-04
BR112015018471A2 (pt) 2017-07-18
BR112015018471B1 (pt) 2022-01-18
KR102072349B1 (ko) 2020-01-31
EP2762852A1 (en) 2014-08-06
US20150362405A1 (en) 2015-12-17
KR20150114559A (ko) 2015-10-12
JP2016513202A (ja) 2016-05-12
EP2954297A1 (en) 2015-12-16
RU2015132521A (ru) 2017-03-13
MX361552B (es) 2018-12-10
JP6403690B2 (ja) 2018-10-10
WO2014122013A1 (en) 2014-08-14
CA2898392A1 (en) 2014-08-14
CN105074413A (zh) 2015-11-18

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