ES8204963A1 - Perfeccionamientos en sistemas de gobierno para motores de avion. - Google Patents
Perfeccionamientos en sistemas de gobierno para motores de avion.Info
- Publication number
- ES8204963A1 ES8204963A1 ES81504841A ES504841A ES8204963A1 ES 8204963 A1 ES8204963 A1 ES 8204963A1 ES 81504841 A ES81504841 A ES 81504841A ES 504841 A ES504841 A ES 504841A ES 8204963 A1 ES8204963 A1 ES 8204963A1
- Authority
- ES
- Spain
- Prior art keywords
- metering devices
- management system
- motor
- engine management
- parameters
- 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
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
-
- 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)
- Combined Controls Of Internal Combustion Engines (AREA)
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
Abstract
SISTEMA DE CONTROL DE COMBUSTIBLE PARA MOTORES DE AVION. PRESENTA UN SISTEMA DE GOBIERNO DE MOTORES (28) QUE VERIFICA PARAMETROS DE LOS MOTORES (12) POR MEDIO DE UNOS CONDUCTORES (30), ASI COMO PARAMETROS EXTERNOS A TRAVES DE OTRO CONDUCTOR (32), TODO ELLO CON EL OBJETO DE PROPORCIONAR UN AJUSTE DE FACULTAD LIMITADA PRA EL FUNCIONAMIENTO DE LOS DISPOSITIVOS DOSIFICADORES DE COMBUSTIBLE (26). UNAS PALANCAS INTERMEDIAS (34) ACTUAN SOBRE LOS DISPOSITIVOS DOSIFICADORES, EN FUNCION DE LOS CAMBIOS DE POSICION DE LOS ACELERADORES (18) Y DE UNA SEÑAL DE ENTRADA QUE PROVIENE DEL SISTEMA DE GOBIERNO DE MOTORES (28). SE PRETENDE CON ELLO DISMINUIR EL TRABAJO DE LA TRIOPULACION NECESARIO PARA OPTIMIZAR EL EMPUJE EN EL DESPEGUE.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/US1980/001065 WO1982000687A1 (en) | 1980-08-21 | 1980-08-21 | Engine management system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| ES504841A0 ES504841A0 (es) | 1982-05-16 |
| ES8204963A1 true ES8204963A1 (es) | 1982-05-16 |
Family
ID=22154493
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES81504841A Expired ES8204963A1 (es) | 1980-08-21 | 1981-08-20 | Perfeccionamientos en sistemas de gobierno para motores de avion. |
Country Status (12)
| Country | Link |
|---|---|
| US (1) | US4551972A (es) |
| EP (1) | EP0058158B1 (es) |
| JP (1) | JPS611613B2 (es) |
| AU (1) | AU7223781A (es) |
| BR (1) | BR8009103A (es) |
| CA (1) | CA1176952A (es) |
| DE (1) | DE3050534A1 (es) |
| ES (1) | ES8204963A1 (es) |
| GB (1) | GB2094405B (es) |
| IL (1) | IL63566A0 (es) |
| IT (1) | IT1171447B (es) |
| WO (1) | WO1982000687A1 (es) |
Families Citing this family (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2580034B1 (es) * | 1985-04-03 | 1987-05-29 | Aerospatiale | |
| US4918629A (en) * | 1988-04-07 | 1990-04-17 | The Boeing Company | Engine trim tachometer unit and calibration method |
| US5136841A (en) * | 1989-02-27 | 1992-08-11 | Zimmerman Ward H | Aircraft propulsion control system |
| US5044155A (en) * | 1989-02-27 | 1991-09-03 | The Boeing Company | Aircraft propulsion control system |
| FR2680386B1 (fr) * | 1991-08-12 | 1993-11-05 | Aerospatiale Ste Nationale Indle | Dispositif pour la commande du regime des moteurs d'un aeronef. |
| US5315819A (en) * | 1991-09-17 | 1994-05-31 | Allied-Signal Inc. | Power management system for turbine engines |
| GB2272783B (en) * | 1992-11-20 | 1996-05-22 | Rolls Royce Plc | Aircraft engine control system |
| US5339636A (en) * | 1992-12-04 | 1994-08-23 | United Technologies Corporation | Fuel splitter valve assembly for gas turbine |
| US5517819A (en) * | 1994-12-19 | 1996-05-21 | General Electric Company | Engine full authority digital engine control automatic mach hold |
| US6186447B1 (en) * | 1997-11-10 | 2001-02-13 | The Boeing Company | Autothrottle retard rate control system |
| US6715278B2 (en) * | 2001-10-02 | 2004-04-06 | Dennis G. Demers | Fail fixed fuel metering device for providing bumpless transfer to backup |
| US6688097B2 (en) | 2001-12-19 | 2004-02-10 | Honeywell International Inc. | Multivariant set point using N1 and N2 for engine control |
| FR2858658B1 (fr) * | 2003-08-06 | 2005-09-30 | Airbus France | Procede et dispositif pour l'alimentation des turboreacteurs d'un aeronef en vol automatique |
| US7107131B2 (en) * | 2004-03-05 | 2006-09-12 | Honeywell International, Inc. | Cross-engine aircraft communication system |
| US20090145105A1 (en) * | 2004-12-01 | 2009-06-11 | Suciu Gabriel L | Remote engine fuel control and electronic engine control for turbine engine |
| GB0504272D0 (en) * | 2005-03-02 | 2005-04-06 | Rolls Royce Plc | A turbine engine and a method of operating a turbine engine |
| US7739004B2 (en) * | 2006-11-29 | 2010-06-15 | The Boeing Company | Automatic engine fuel flow monitoring and alerting fuel leak detection method |
| EP2356327B1 (en) * | 2008-11-13 | 2014-12-31 | Sikorsky Aircraft Corporation | Adaptive fail-fixed system for fadec controlled gas turbine engines |
| US8290683B2 (en) * | 2010-02-16 | 2012-10-16 | Telectro-Mek, Inc. | Apparatus and method for reducing aircraft fuel consumption |
| FR2998618B1 (fr) * | 2012-11-27 | 2015-01-16 | Motorisations Aeronautiques | Dispositif de positionnement d'un organe de commande d'une pompe d'injection |
| WO2016123613A1 (en) * | 2015-01-30 | 2016-08-04 | General Electric Technology Gmbh | Automated extended turndown of a gas turbine engine combined with incremental tuning to maintain emissions and dynamics |
| US10801361B2 (en) | 2016-09-09 | 2020-10-13 | General Electric Company | System and method for HPT disk over speed prevention |
| US11377223B2 (en) * | 2018-10-29 | 2022-07-05 | Pratt & Whitney Canada Corp. | Autothrottle control system on turbopropeller-powered aircraft |
| US20200271018A1 (en) * | 2019-02-21 | 2020-08-27 | Pratt & Whitney Canada Corp. | System and method for managing power to an engine controller |
Family Cites Families (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2781856A (en) * | 1952-06-06 | 1957-02-19 | Rotol Ltd | Control system for variable pitch screw propellers |
| US2935136A (en) * | 1954-02-04 | 1960-05-03 | Rotol Ltd | Control systems for power plants |
| US3174284A (en) * | 1963-02-19 | 1965-03-23 | United Aircraft Corp | Power management fuel control for plural gas turbine engines |
| US3261405A (en) * | 1965-02-09 | 1966-07-19 | Fairchild Hiller Corp | Aircraft power control apparatus |
| GB1311841A (en) * | 1968-12-23 | 1973-03-28 | Secr Defence | Control system |
| GB1331984A (en) * | 1970-04-25 | 1973-09-26 | Lucas Industries Ltd | Fuel control system for gas turbine engine |
| US3875390A (en) * | 1970-07-09 | 1975-04-01 | Secr Defence Brit | On-line computer control system |
| GB1369653A (en) * | 1971-01-06 | 1974-10-09 | Lucas Industries Ltd | Fuel control system for gas turbine engine |
| US3832846A (en) * | 1972-04-27 | 1974-09-03 | Woodward Governor Co | Speed governor with fuel rate control |
| US3839860A (en) * | 1972-07-21 | 1974-10-08 | United Aircraft Corp | Automatic engine pressure ratio equalization system |
| US3852956A (en) * | 1972-07-21 | 1974-12-10 | United Aircraft Corp | Aircraft engine pressure ratio autotrim system |
| US3813063A (en) * | 1972-07-21 | 1974-05-28 | United Aircraft Corp | Automatic aircraft engine pressure ratio control system |
| US3854287A (en) * | 1973-12-26 | 1974-12-17 | United Aircraft Corp | Self-trimming control for turbofan engines |
| US3963372A (en) * | 1975-01-17 | 1976-06-15 | General Motors Corporation | Helicopter power plant control |
| US4134257A (en) * | 1976-11-03 | 1979-01-16 | The Garrett Corporation | Gas turbine fuel delivery and control system |
| GB2005790B (en) * | 1977-10-04 | 1982-02-10 | Rolls Royce | Control mechanisms |
| US4197699A (en) * | 1977-12-22 | 1980-04-15 | The Garrett Corporation | Free turbine type gas turbine engine with variable free turbine guide vane control system |
| US4275558A (en) * | 1977-12-22 | 1981-06-30 | The Garrett Corporation | Gas turbine engine fuel governor |
| US4258545A (en) * | 1978-06-15 | 1981-03-31 | General Electric Company | Optimal control for a gas turbine engine |
| US4248042A (en) * | 1978-11-03 | 1981-02-03 | The Boeing Company | Engine thrust control system |
| US4259838A (en) * | 1979-06-26 | 1981-04-07 | Rockwell International Corporation | Throttle tracking in multiengine aircraft |
| EP0047582B1 (en) * | 1980-08-21 | 1984-12-05 | The Garrett Corporation | Engine fuel control systems |
-
1980
- 1980-08-21 US US06/664,949 patent/US4551972A/en not_active Expired - Lifetime
- 1980-08-21 DE DE803050534A patent/DE3050534A1/de not_active Ceased
- 1980-08-21 JP JP56501892A patent/JPS611613B2/ja not_active Expired
- 1980-08-21 AU AU72237/81A patent/AU7223781A/en not_active Withdrawn
- 1980-08-21 BR BR8009103A patent/BR8009103A/pt not_active IP Right Cessation
- 1980-08-21 EP EP81901389A patent/EP0058158B1/en not_active Expired
- 1980-08-21 WO PCT/US1980/001065 patent/WO1982000687A1/en not_active Ceased
- 1980-08-21 GB GB8208801A patent/GB2094405B/en not_active Expired
-
1981
- 1981-08-06 IT IT49061/81A patent/IT1171447B/it active
- 1981-08-07 CA CA000383448A patent/CA1176952A/en not_active Expired
- 1981-08-13 IL IL63566A patent/IL63566A0/xx not_active IP Right Cessation
- 1981-08-20 ES ES81504841A patent/ES8204963A1/es not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| US4551972A (en) | 1985-11-12 |
| IT8149061A0 (it) | 1981-08-06 |
| JPS57501391A (es) | 1982-08-05 |
| EP0058158A1 (en) | 1982-08-25 |
| IL63566A0 (en) | 1981-12-31 |
| IT8149061A1 (it) | 1983-02-06 |
| IT1171447B (it) | 1987-06-10 |
| ES504841A0 (es) | 1982-05-16 |
| DE3050534A1 (en) | 1982-09-23 |
| EP0058158B1 (en) | 1987-03-25 |
| CA1176952A (en) | 1984-10-30 |
| JPS611613B2 (es) | 1986-01-18 |
| BR8009103A (pt) | 1982-06-22 |
| EP0058158A4 (en) | 1982-12-27 |
| GB2094405A (en) | 1982-09-15 |
| WO1982000687A1 (en) | 1982-03-04 |
| AU7223781A (en) | 1982-03-17 |
| GB2094405B (en) | 1984-05-31 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FD1A | Patent lapsed |
Effective date: 19970203 |