JP2005509794A5 - - Google Patents
Download PDFInfo
- Publication number
- JP2005509794A5 JP2005509794A5 JP2003545953A JP2003545953A JP2005509794A5 JP 2005509794 A5 JP2005509794 A5 JP 2005509794A5 JP 2003545953 A JP2003545953 A JP 2003545953A JP 2003545953 A JP2003545953 A JP 2003545953A JP 2005509794 A5 JP2005509794 A5 JP 2005509794A5
- Authority
- JP
- Japan
- Prior art keywords
- engine
- surge
- temperature
- pressure compressor
- plan
- Prior art date
- Legal status (The legal status 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 status listed.)
- Granted
Links
- 239000000446 fuel Substances 0.000 claims description 47
- 230000001133 acceleration Effects 0.000 claims description 39
- 238000000034 method Methods 0.000 claims description 36
- 230000001052 transient effect Effects 0.000 claims description 34
- 239000000284 extract Substances 0.000 claims description 12
- 238000012937 correction Methods 0.000 claims description 10
- 230000008859 change Effects 0.000 claims description 7
- 239000012530 fluid Substances 0.000 claims description 5
- 230000008569 process Effects 0.000 claims description 3
- 239000007789 gas Substances 0.000 description 38
- 239000003607 modifier Substances 0.000 description 12
- 230000004044 response Effects 0.000 description 11
- 238000004891 communication Methods 0.000 description 4
- 230000007423 decrease Effects 0.000 description 4
- 230000007246 mechanism Effects 0.000 description 4
- 239000000567 combustion gas Substances 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000001514 detection method Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000006870 function Effects 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 239000002243 precursor Substances 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 230000002159 abnormal effect Effects 0.000 description 1
- 230000005856 abnormality Effects 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 230000003044 adaptive effect Effects 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 238000010420 art technique Methods 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 238000006731 degradation reaction Methods 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 239000002828 fuel tank Substances 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000013021 overheating Methods 0.000 description 1
- 238000011056 performance test Methods 0.000 description 1
- 230000010349 pulsation Effects 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 239000000779 smoke Substances 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US33538701P | 2001-11-15 | 2001-11-15 | |
| PCT/US2002/036769 WO2003044353A1 (en) | 2001-11-15 | 2002-11-15 | Method and apparatus for adaptive acceleration schedules in gas turbine engine control systems |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2005509794A JP2005509794A (ja) | 2005-04-14 |
| JP2005509794A5 true JP2005509794A5 (enExample) | 2006-01-05 |
| JP4230356B2 JP4230356B2 (ja) | 2009-02-25 |
Family
ID=23311554
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2003545953A Expired - Fee Related JP4230356B2 (ja) | 2001-11-15 | 2002-11-15 | ガスタービンエンジン制御システムに加速計画を適用するための方法および装置 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US6820429B2 (enExample) |
| EP (1) | EP1444428B1 (enExample) |
| JP (1) | JP4230356B2 (enExample) |
| DE (1) | DE60230791D1 (enExample) |
| WO (1) | WO2003044353A1 (enExample) |
Families Citing this family (34)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6935120B2 (en) * | 2002-05-09 | 2005-08-30 | General Electric Company | Approach to extending life of gas turbine engine |
| US6823675B2 (en) * | 2002-11-13 | 2004-11-30 | General Electric Company | Adaptive model-based control systems and methods for controlling a gas turbine |
| US7487029B2 (en) * | 2004-05-21 | 2009-02-03 | Pratt & Whitney Canada | Method of monitoring gas turbine engine operation |
| US7377114B1 (en) * | 2004-06-02 | 2008-05-27 | Kevin P Pearce | Turbine engine pulsed fuel injection utilizing stagger injector operation |
| US7762084B2 (en) * | 2004-11-12 | 2010-07-27 | Rolls-Royce Canada, Ltd. | System and method for controlling the working line position in a gas turbine engine compressor |
| US9273614B2 (en) * | 2005-09-12 | 2016-03-01 | Industrial Turbine Company (Uk) Limited | Determination of a signal indicative of shaft power |
| US20070214795A1 (en) * | 2006-03-15 | 2007-09-20 | Paul Cooker | Continuous real time EGT margin control |
| US7762078B2 (en) * | 2006-09-13 | 2010-07-27 | Aerojet-General Corporation | Nozzle with temperature-responsive throat diameter |
| GB0716329D0 (en) | 2007-08-21 | 2007-10-03 | Compair Uk Ltd | Improvements in compressors control |
| GB0813413D0 (en) | 2008-07-23 | 2008-08-27 | Rolls Royce Plc | A compressor variable stator vane arrangement |
| US8277208B2 (en) | 2009-06-11 | 2012-10-02 | Goodrich Pump & Engine Control Systems, Inc. | Split discharge vane pump and fluid metering system therefor |
| GB0915616D0 (en) * | 2009-09-08 | 2009-10-07 | Rolls Royce Plc | Surge margin regulation |
| US8899488B2 (en) | 2011-05-31 | 2014-12-02 | United Technologies Corporation | RFID tag system |
| FR2976622B1 (fr) * | 2011-06-16 | 2015-05-01 | Turbomeca | Architecture double corps de turbomoteur avec compresseur haute pression lie a la turbine basse pression |
| US10436208B2 (en) | 2011-06-27 | 2019-10-08 | Energy Control Technologies, Inc. | Surge estimator |
| CA2804462C (en) | 2012-07-12 | 2021-05-25 | Pratt & Whitney Canada Corp. | Aircraft power outtake management |
| US8720258B2 (en) * | 2012-09-28 | 2014-05-13 | United Technologies Corporation | Model based engine inlet condition estimation |
| US10571316B2 (en) * | 2012-11-09 | 2020-02-25 | Safran Aircraft Engines | Method and system for determining the flow rate of air collected from an aircraft engine |
| US20140130510A1 (en) * | 2012-11-09 | 2014-05-15 | Honeywell International Inc. | Systems and methods for directing cooling flow into the surge plenum of an exhaust eductor cooling system |
| US9255525B2 (en) * | 2012-11-30 | 2016-02-09 | General Electric Company | System and method for gas turbine operation |
| US9228501B2 (en) * | 2012-12-14 | 2016-01-05 | Solar Turbines Incorporated | Bleed valve override schedule on off-load transients |
| US9459671B2 (en) | 2013-02-25 | 2016-10-04 | General Electric Company | Systems and methods for use in adapting the operation of a gas turbine |
| US9605559B2 (en) | 2015-02-02 | 2017-03-28 | General Electric Company | Wash timing based on turbine operating parameters |
| US9938906B2 (en) | 2015-06-01 | 2018-04-10 | Solar Turbines Incorporated | Combustion stability logic during off-load transients |
| JP6639338B2 (ja) * | 2016-07-11 | 2020-02-05 | 三菱日立パワーシステムズ株式会社 | ガスタービン及びガスタービンの運転方法 |
| FR3059734A1 (fr) * | 2016-12-06 | 2018-06-08 | Airbus Operations Gmbh | Procede et dispositif de controle des prelevements sur une turbomachine limitant le risque de pompage par echange d'informations entre un gestionnaire d'energie et un systeme de controle de la turbomachine |
| CN110886656B (zh) * | 2018-09-11 | 2024-06-18 | 普拉特-惠特尼加拿大公司 | 用于为发动机启动设定加速度计划的方法与系统 |
| CN110886658A (zh) * | 2018-09-11 | 2020-03-17 | 普拉特 - 惠特尼加拿大公司 | 用于检测高涡轮温度操作的方法和系统 |
| CN109611217B (zh) * | 2018-11-07 | 2020-12-11 | 大连理工大学 | 一种航空发动机过渡态控制规律优化的设计方法 |
| FR3104542B1 (fr) * | 2019-12-13 | 2021-12-03 | Safran Power Units | Groupe auxiliaire de puissance comprenant un générateur de gaz à entrainement direct avec un générateur électrique et un boîtier d’accessoires |
| US12025060B2 (en) * | 2021-05-19 | 2024-07-02 | Pratt & Whitney Canada Corp. | Method and system for operating an engine to prevent high power engine surges |
| GB202201987D0 (en) * | 2022-02-15 | 2022-03-30 | Rolls Royce Plc | Engine system and method of operating the same |
| GB202201986D0 (en) | 2022-02-15 | 2022-03-30 | Rolls Royce Plc | Engine system and method of operating the same |
| US20250139318A1 (en) * | 2023-10-30 | 2025-05-01 | Honeywell International Inc. | System and Method for Turbine Engine Parameter Synthesis |
Family Cites Families (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2743578A (en) * | 1950-11-24 | 1956-05-01 | Bendix Aviat Corp | Turbojet engine control system |
| CA942408A (en) * | 1971-04-28 | 1974-02-19 | William L. Webb | Integrated control for a turbopropulsion system |
| US4117668A (en) * | 1975-11-19 | 1978-10-03 | United Technologies Corporation | Stall detector for gas turbine engine |
| US4490791A (en) | 1982-04-19 | 1984-12-25 | Chandler Evans Inc. | Adaptive gas turbine acceleration control |
| GR78259B (enExample) * | 1982-06-21 | 1984-09-26 | United Technologies Corp | |
| US4603546A (en) * | 1985-07-16 | 1986-08-05 | Rolls-Royce Limited | Control systems for gas turbine aeroengines |
| US5226287A (en) * | 1991-07-19 | 1993-07-13 | General Electric Company | Compressor stall recovery apparatus |
| US5732546A (en) * | 1996-07-19 | 1998-03-31 | General Electric Company | Transient turbine overtemperature control |
| US6141951A (en) | 1998-08-18 | 2000-11-07 | United Technologies Corporation | Control system for modulating bleed in response to engine usage |
| US6226974B1 (en) | 1999-06-25 | 2001-05-08 | General Electric Co. | Method of operation of industrial gas turbine for optimal performance |
| US6513333B2 (en) * | 2000-05-25 | 2003-02-04 | Honda Giken Kogyo Kabushiki Kaisha | Surge detection system of gas turbine aeroengine |
| JP2002138857A (ja) * | 2000-11-01 | 2002-05-17 | Honda Motor Co Ltd | ガスタービンエンジンの加減速制御装置 |
-
2002
- 2002-11-15 WO PCT/US2002/036769 patent/WO2003044353A1/en not_active Ceased
- 2002-11-15 EP EP02789692A patent/EP1444428B1/en not_active Expired - Lifetime
- 2002-11-15 DE DE60230791T patent/DE60230791D1/de not_active Expired - Lifetime
- 2002-11-15 US US10/295,571 patent/US6820429B2/en not_active Expired - Lifetime
- 2002-11-15 JP JP2003545953A patent/JP4230356B2/ja not_active Expired - Fee Related
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP4230356B2 (ja) | ガスタービンエンジン制御システムに加速計画を適用するための方法および装置 | |
| JP2005509794A5 (enExample) | ||
| CN111664009B (zh) | 机器学习在处理涡轮发动机的高频传感器信号中的应用 | |
| US7584618B2 (en) | Controlling air flow to a turbine shroud for thermal control | |
| CN104595038B (zh) | 多分管型燃烧室使用燃烧动态调谐算法的系统和方法 | |
| US8240120B2 (en) | Vibration management for gas turbine engines | |
| JP5583697B2 (ja) | ガスタービンを制御するための方法およびシステム、ならびにこのようなシステムを含むガスタービン | |
| US9458771B2 (en) | Multi-engine performance margin synchronization adaptive control system and method | |
| US10815904B2 (en) | Prognostic health management control for adaptive operability recovery for turbine engines | |
| CA2762868C (en) | Gas turbine engine with bleed air system | |
| US11761385B2 (en) | Turbine engine shaft shear detection | |
| US9200572B2 (en) | Compressor surge prevention digital system | |
| CA2336601A1 (en) | Speed modification system for gas turbine engine to allow trimming of excess thrust | |
| EP1746347A2 (en) | Method and system for operating a multi-stage combustor | |
| WO2021033559A1 (ja) | ガスタービンの燃焼制御装置、燃焼制御方法及びプログラム | |
| EP3199784B1 (en) | Fuel flow control | |
| EP3409926B1 (en) | Method and system for detecting a high temperature condition of a gas turbine | |
| KR960003682B1 (ko) | 덕트압력 손실보상기능을 갖는 가속제어장치 | |
| KR960010279B1 (ko) | 개스터빈 엔진 및 그 작동방법 | |
| RU2631974C2 (ru) | Способ управления газотурбинным двигателем с форсажной камерой сгорания и система для его осуществления | |
| EP3904660B1 (en) | System and method for detecting a shaft event on a gas turbine engine | |
| US9938906B2 (en) | Combustion stability logic during off-load transients | |
| US20240150010A1 (en) | Systems and methods for controlling propeller control unit fluid pressure | |
| EP4421574B1 (en) | Gas turbine engine control system | |
| RU2798129C1 (ru) | Способ защиты газотурбинного двигателя от помпажа |