DE60139229D1 - Methode und Einrichtung um ein Turbinenregelsystem abzugleichen - Google Patents
Methode und Einrichtung um ein Turbinenregelsystem abzugleichenInfo
- Publication number
- DE60139229D1 DE60139229D1 DE60139229T DE60139229T DE60139229D1 DE 60139229 D1 DE60139229 D1 DE 60139229D1 DE 60139229 T DE60139229 T DE 60139229T DE 60139229 T DE60139229 T DE 60139229T DE 60139229 D1 DE60139229 D1 DE 60139229D1
- Authority
- DE
- Germany
- Prior art keywords
- adjust
- control system
- turbine control
- turbine
- control
- 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.)
- Expired - Lifetime
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
- F02C9/26—Control of fuel supply
- F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Feedback Control In General (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/629,529 US6459963B1 (en) | 2000-07-31 | 2000-07-31 | Methods and apparatus for trimming engine control systems |
Publications (1)
Publication Number | Publication Date |
---|---|
DE60139229D1 true DE60139229D1 (de) | 2009-08-27 |
Family
ID=24523381
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60139229T Expired - Lifetime DE60139229D1 (de) | 2000-07-31 | 2001-07-31 | Methode und Einrichtung um ein Turbinenregelsystem abzugleichen |
Country Status (4)
Country | Link |
---|---|
US (1) | US6459963B1 (de) |
EP (1) | EP1178196B1 (de) |
JP (1) | JP4733309B2 (de) |
DE (1) | DE60139229D1 (de) |
Families Citing this family (37)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7020595B1 (en) * | 1999-11-26 | 2006-03-28 | General Electric Company | Methods and apparatus for model based diagnostics |
US20040243284A1 (en) * | 2003-05-28 | 2004-12-02 | Caterpillar Inc. | Methods and systems for modifying flash files |
US7032388B2 (en) * | 2003-11-17 | 2006-04-25 | General Electric Company | Method and system for incorporating an emission sensor into a gas turbine controller |
US20050193739A1 (en) * | 2004-03-02 | 2005-09-08 | General Electric Company | Model-based control systems and methods for gas turbine engines |
US7603222B2 (en) * | 2005-11-18 | 2009-10-13 | General Electric Company | Sensor diagnostics using embedded model quality parameters |
US7752833B2 (en) * | 2006-01-10 | 2010-07-13 | General Electric Company | Methods and apparatus for gas turbine fuel control |
EP1837506B1 (de) * | 2006-03-24 | 2013-08-28 | Rolls-Royce plc | Verfahren zur Überwachung des Schubs eines Gasturbinentriebwerks |
US20070260424A1 (en) * | 2006-05-05 | 2007-11-08 | Harold Brown | Methods and apparatus for estimating engine thrust |
US7769503B2 (en) * | 2006-08-01 | 2010-08-03 | Hal Gerard Wick | Aircraft engine management for fuel conservation |
US7739004B2 (en) * | 2006-11-29 | 2010-06-15 | The Boeing Company | Automatic engine fuel flow monitoring and alerting fuel leak detection method |
US9074531B2 (en) | 2008-03-05 | 2015-07-07 | United Technologies Corporation | Variable area fan nozzle fan flutter management system |
US20090226303A1 (en) * | 2008-03-05 | 2009-09-10 | Grabowski Zbigniew M | Variable area fan nozzle fan flutter management system |
US8381510B2 (en) * | 2009-04-30 | 2013-02-26 | General Electric Company | Method and systems for controlling engine thrust using variable trim |
US8682562B2 (en) * | 2009-05-08 | 2014-03-25 | Rolls-Royce Corporation | Turbine engine thrust scheduling |
CA2762184A1 (en) | 2009-05-12 | 2010-11-18 | Icr Turbine Engine Corporation | Gas turbine energy storage and conversion system |
GB0912340D0 (en) * | 2009-07-16 | 2009-08-26 | Rolls Royce Plc | Aircraft power management system |
WO2011109514A1 (en) | 2010-03-02 | 2011-09-09 | Icr Turbine Engine Corporatin | Dispatchable power from a renewable energy facility |
US8862433B2 (en) | 2010-05-18 | 2014-10-14 | United Technologies Corporation | Partitioning of turbomachine faults |
US8984895B2 (en) | 2010-07-09 | 2015-03-24 | Icr Turbine Engine Corporation | Metallic ceramic spool for a gas turbine engine |
CA2813680A1 (en) | 2010-09-03 | 2012-03-08 | Icr Turbine Engine Corporation | Gas turbine engine configurations |
US9051873B2 (en) | 2011-05-20 | 2015-06-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine shaft attachment |
US8490404B1 (en) | 2012-02-28 | 2013-07-23 | General Electric Company | Sensor-based performance-seeking gas turbine engine control |
US10094288B2 (en) | 2012-07-24 | 2018-10-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine volute attachment for a gas turbine engine |
GB201219815D0 (en) * | 2012-11-05 | 2012-12-19 | Rolls Royce Plc | Engine control parameter trimming |
US10107197B2 (en) * | 2012-11-30 | 2018-10-23 | United Technologies Corporation | Lubrication system for gas turbine engines |
US9243970B2 (en) | 2012-11-30 | 2016-01-26 | Pratt & Whitney Canada Corp. | Method and system for integrating gas turbine trim balancing system into electronic engine controls |
US20140244132A1 (en) * | 2013-02-22 | 2014-08-28 | Pratt & Whitney Canada Corp. | System and method for 0n-wing engine trim verification |
EP2972620B1 (de) | 2013-03-15 | 2020-03-11 | Rolls-Royce North American Technologies, Inc. | Integrierter intaktheitsverwaltungsansatz zur begrenzung des schutzes eines antriebssteuerungssystems |
FR3029570B1 (fr) * | 2014-12-05 | 2019-08-30 | Safran Aircraft Engines | Dispositif et procede de regulation d'un moteur exploitant une mesure de poussee |
US10227933B2 (en) * | 2015-02-12 | 2019-03-12 | United Technologies Corporation | Aircraft power setting trims for life extension |
US9771878B2 (en) * | 2015-10-19 | 2017-09-26 | General Electric Company | Thrust scheduling method for variable pitch fan engines and turbo-shaft, turbo-propeller engines |
US10005561B2 (en) | 2016-06-16 | 2018-06-26 | Ge Aviation Systems Llc | Controlling aircraft using thrust differential trim |
US10604268B2 (en) * | 2017-02-22 | 2020-03-31 | Pratt & Whitney Canada Corp. | Autothrottle control for turboprop engines |
WO2019237320A1 (zh) * | 2018-06-15 | 2019-12-19 | 大连理工大学 | 一种基于模型预测的航空发动机在线优化及多变量控制设计方法 |
US11236683B2 (en) | 2018-06-20 | 2022-02-01 | Rolls-Royce Plc | Control system |
CN113969842B (zh) * | 2021-10-22 | 2022-11-18 | 清华大学 | 一种航空发动机推力高动态响应控制方法 |
US20240141839A1 (en) * | 2022-10-28 | 2024-05-02 | Pratt & Whitney Canada Corp. | System and Method for Thrust Linearization with Thrust Lever Angle |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3721120A (en) * | 1970-11-16 | 1973-03-20 | Howell Instruments | Engine performance indicator |
US3750465A (en) * | 1971-09-09 | 1973-08-07 | Howell Instruments | Engine performance indicator |
US4275557A (en) * | 1978-01-25 | 1981-06-30 | General Electric Company | Method and apparatus for controlling thrust in a gas turbine engine |
US4294069A (en) * | 1978-04-26 | 1981-10-13 | United Technologies Corporation | Exhaust nozzle control and core engine fuel control for turbofan engine |
CA1149909A (en) * | 1979-09-21 | 1983-07-12 | Robert G. Burrage | Gas turbine engine fuel control system |
GB2088961B (en) * | 1980-11-26 | 1984-06-13 | Rolls Royce | Fuel control system for a gas turbine engine |
EP0363301B1 (de) * | 1988-09-20 | 1997-07-09 | United Technologies Corporation | Steuervorrichtung für Gasturbinenanlagen |
US5274996A (en) * | 1991-10-11 | 1994-01-04 | Allied-Signal, Inc. | Closed loop fuel control system |
US5267435A (en) * | 1992-08-18 | 1993-12-07 | General Electric Company | Thrust droop compensation method and system |
US5465570A (en) | 1993-12-22 | 1995-11-14 | United Technologies Corporation | Fuel control system for a staged combustor |
US5694766A (en) | 1995-03-28 | 1997-12-09 | Mcdonnell Douglas Corporation | Method and apparatus for controlling the throat area, expansion ratio and thrust vector angle of an aircraft turbine engine exhaust nozzle using regions of locally separated flow |
JP3160757B2 (ja) * | 1996-09-13 | 2001-04-25 | 防衛庁技術研究本部長 | ガスタービンエンジン排気温度制御装置および制御方法 |
US5838588A (en) | 1996-12-13 | 1998-11-17 | Siemens Corporate Research, Inc. | Graphical user interface system for steam turbine operating conditions |
US6250877B1 (en) | 2000-07-19 | 2001-06-26 | General Electric Co. | Steam turbine controller having method and apparatus for providing variable frequency regulation |
-
2000
- 2000-07-31 US US09/629,529 patent/US6459963B1/en not_active Expired - Lifetime
-
2001
- 2001-07-30 JP JP2001228813A patent/JP4733309B2/ja not_active Expired - Fee Related
- 2001-07-31 DE DE60139229T patent/DE60139229D1/de not_active Expired - Lifetime
- 2001-07-31 EP EP01306535A patent/EP1178196B1/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JP4733309B2 (ja) | 2011-07-27 |
EP1178196B1 (de) | 2009-07-15 |
US6459963B1 (en) | 2002-10-01 |
JP2002115565A (ja) | 2002-04-19 |
EP1178196A3 (de) | 2005-08-17 |
EP1178196A2 (de) | 2002-02-06 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |