FR2948151B1 - Procede et systeme pour la commande d'un demarreur-generateur de moteur d'aeronef - Google Patents
Procede et systeme pour la commande d'un demarreur-generateur de moteur d'aeronefInfo
- Publication number
- FR2948151B1 FR2948151B1 FR0954983A FR0954983A FR2948151B1 FR 2948151 B1 FR2948151 B1 FR 2948151B1 FR 0954983 A FR0954983 A FR 0954983A FR 0954983 A FR0954983 A FR 0954983A FR 2948151 B1 FR2948151 B1 FR 2948151B1
- Authority
- FR
- France
- Prior art keywords
- generator
- controlling
- aircraft engine
- engine starter
- starter
- 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.)
- Active
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
- F01D15/10—Adaptations for driving, or combinations with, electric generators
-
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/26—Starting; Ignition
- F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
-
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/26—Starting; Ignition
- F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
- F02C7/275—Mechanical drives
-
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/32—Arrangement, mounting, or driving, of auxiliaries
-
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
-
- 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
- F05D2260/40—Transmission of power
-
- 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
- F05D2260/85—Starting
-
- 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)
- Control Of Eletrric Generators (AREA)
- Control Of Turbines (AREA)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0954983A FR2948151B1 (fr) | 2009-07-17 | 2009-07-17 | Procede et systeme pour la commande d'un demarreur-generateur de moteur d'aeronef |
US13/384,111 US8979705B2 (en) | 2009-07-17 | 2010-07-07 | Method and system for controlling aircraft engine starter/generator |
GB1200434.7A GB2484230B (en) | 2009-07-17 | 2010-07-07 | Method and system for controlling aircraft engine starter/generator |
PCT/FR2010/051427 WO2011007078A1 (fr) | 2009-07-17 | 2010-07-07 | Procédé et système pour la commande d'un démarreur-générateur de moteur d'aéronef |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0954983A FR2948151B1 (fr) | 2009-07-17 | 2009-07-17 | Procede et systeme pour la commande d'un demarreur-generateur de moteur d'aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2948151A1 FR2948151A1 (fr) | 2011-01-21 |
FR2948151B1 true FR2948151B1 (fr) | 2011-11-25 |
Family
ID=42035284
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0954983A Active FR2948151B1 (fr) | 2009-07-17 | 2009-07-17 | Procede et systeme pour la commande d'un demarreur-generateur de moteur d'aeronef |
Country Status (4)
Country | Link |
---|---|
US (1) | US8979705B2 (fr) |
FR (1) | FR2948151B1 (fr) |
GB (1) | GB2484230B (fr) |
WO (1) | WO2011007078A1 (fr) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20130076035A1 (en) * | 2011-09-27 | 2013-03-28 | Andreas C. Koenig | Motor-generator turbomachine starter |
CN103075255B (zh) * | 2013-01-10 | 2015-12-09 | 哈尔滨东安发动机(集团)有限公司 | 飞机发动机起动控制系统 |
CN103558561B (zh) * | 2013-10-22 | 2016-05-18 | 中国商用飞机有限责任公司 | 飞机发动机n2转速模拟装置 |
CN105083566B (zh) * | 2014-05-07 | 2017-06-06 | 哈尔滨飞机工业集团有限责任公司 | 直升机发动机起动控制电路 |
US9273610B2 (en) | 2014-05-20 | 2016-03-01 | Solar Turbines Incorporated | Starter/generator combination with all variable frequency drives |
FR3027346B1 (fr) * | 2014-10-20 | 2019-08-09 | Safran Helicopter Engines | Pack amovible de reactivation d'un turbomoteur, architecture d'un systeme propulsif d'un helicoptere multi-moteur equipe d'un tel pack et helicoptere correspondant |
FR3044044B1 (fr) * | 2015-11-19 | 2021-01-29 | Snecma | Systeme d'alimentation en fluide d'au moins un organe d'un ensemble propulsif d'aeronef |
US10598047B2 (en) * | 2016-02-29 | 2020-03-24 | United Technologies Corporation | Low-power bowed rotor prevention system |
US11473497B2 (en) | 2016-03-15 | 2022-10-18 | Hamilton Sundstrand Corporation | Engine bleed system with motorized compressor |
US10794295B2 (en) * | 2016-03-15 | 2020-10-06 | Hamilton Sunstrand Corporation | Engine bleed system with multi-tap bleed array |
US10787933B2 (en) | 2016-06-20 | 2020-09-29 | Raytheon Technologies Corporation | Low-power bowed rotor prevention and monitoring system |
FR3062424B1 (fr) * | 2017-01-30 | 2021-02-12 | Safran Aircraft Engines | Systeme d'entrainement d'une pompe a carburant d'une turbomachine |
FR3062423B1 (fr) * | 2017-01-30 | 2019-03-15 | Safran Aircraft Engines | Systeme d'entrainement d'une pompe a carburant d'une turbomachine |
GB201804128D0 (en) * | 2018-03-15 | 2018-05-02 | Rolls Royce Plc | Electrical power generator system |
US11668245B2 (en) * | 2020-01-28 | 2023-06-06 | Pratt & Whitney Canada Corp. | Gas turbine engine with clutch system between low-pressure compressor and low-pressure turbine |
BR112023016761A2 (pt) * | 2021-03-19 | 2023-10-31 | Verdego Aero Inc | Resfriamento de ar simultâneo de múltiplos elementos de um motor de alta potência híbrido |
CN113911375B (zh) * | 2021-11-03 | 2023-06-23 | 哈尔滨哈飞航空工业有限责任公司 | 一种直升机发动机手动起动控制电路 |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6895741B2 (en) * | 2003-06-23 | 2005-05-24 | Pratt & Whitney Canada Corp. | Differential geared turbine engine with torque modulation capability |
US7975465B2 (en) | 2003-10-27 | 2011-07-12 | United Technologies Corporation | Hybrid engine accessory power system |
US7481062B2 (en) * | 2005-12-30 | 2009-01-27 | Honeywell International Inc. | More electric aircraft starter-generator multi-speed transmission system |
FR2897895A1 (fr) | 2006-02-27 | 2007-08-31 | Hispano Suiza Sa | Integration d'un demarreur/generateur dans une boite de transmission d'une turbine a gaz |
DE102006039608A1 (de) * | 2006-08-24 | 2008-04-10 | Rolls-Royce Deutschland Ltd & Co Kg | Anordnung zur Energieentnahme bei einem Zwei-Wellen-Triebwerk |
WO2008082336A1 (fr) * | 2006-12-29 | 2008-07-10 | Volvo Aero Corporation | Dispositif de transmission de puissance pour une turbine à gaz, aéroplane et procédé de fonctionnement d'une turbine à gaz |
WO2008082335A1 (fr) * | 2006-12-29 | 2008-07-10 | Volvo Aero Corporation | Dispositif de transmission de puissance pour une turbine à gaz |
GB0805177D0 (en) * | 2008-03-20 | 2008-04-30 | Rolls Royce Plc | A gas turbine engine arrangement |
-
2009
- 2009-07-17 FR FR0954983A patent/FR2948151B1/fr active Active
-
2010
- 2010-07-07 WO PCT/FR2010/051427 patent/WO2011007078A1/fr active Application Filing
- 2010-07-07 US US13/384,111 patent/US8979705B2/en active Active
- 2010-07-07 GB GB1200434.7A patent/GB2484230B/en active Active
Also Published As
Publication number | Publication date |
---|---|
GB2484230A (en) | 2012-04-04 |
WO2011007078A1 (fr) | 2011-01-20 |
US8979705B2 (en) | 2015-03-17 |
US20120122631A1 (en) | 2012-05-17 |
GB201200434D0 (en) | 2012-02-22 |
GB2484230B (en) | 2016-03-30 |
FR2948151A1 (fr) | 2011-01-21 |
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Legal Events
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PLFP | Fee payment |
Year of fee payment: 8 |
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Year of fee payment: 9 |
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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170717 |
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Year of fee payment: 10 |
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PLFP | Fee payment |
Year of fee payment: 12 |
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Year of fee payment: 13 |
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