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'aeronef

Info

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
Application number
FR0954983A
Other languages
English (en)
Other versions
FR2948151A1 (fr
Inventor
Jean Pierre Galivel
Bruno Robert Gaully
Julien Ricordeau
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR0954983A priority Critical patent/FR2948151B1/fr
Priority to US13/384,111 priority patent/US8979705B2/en
Priority to GB1200434.7A priority patent/GB2484230B/en
Priority to PCT/FR2010/051427 priority patent/WO2011007078A1/fr
Publication of FR2948151A1 publication Critical patent/FR2948151A1/fr
Application granted granted Critical
Publication of FR2948151B1 publication Critical patent/FR2948151B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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)
FR0954983A 2009-07-17 2009-07-17 Procede et systeme pour la commande d'un demarreur-generateur de moteur d'aeronef Active FR2948151B1 (fr)

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)

* Cited by examiner, † Cited by third party
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***
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)

* Cited by examiner, † Cited by third party
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

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

Similar Documents

Publication Publication Date Title
FR2948151B1 (fr) Procede et systeme pour la commande d'un demarreur-generateur de moteur d'aeronef
FR2950927B1 (fr) Systeme de commande de la position angulaire d'aubes de stator et procede d'optimisation de ladite position angulaire
FR2930920B1 (fr) Systeme et procede de commande de frein d'un aeronef
FR2967479B1 (fr) Dispositif et procede pour l'allumage d'un systeme de combustion
FR2925615B1 (fr) Procede de commande pour demarreur d'un moteur a combustion et son application
FR2959725B1 (fr) Procede de commande d'un systeme de flottabilite pour aeronef et systeme de commande mettant en oeuvre ledit procede
FR2941107B1 (fr) Systeme electrique de demarrage des moteurs d'un aeronef
FR2900906B1 (fr) Systeme de fixation tolerant aux dommages pour moteur d'aeronef
FR2966879B1 (fr) Systeme et procede de diffusion d'echappement pour turbine
FR2969212B1 (fr) Procede d'arret automatique d'un moteur a combustion interne par un systeme d'arret et de redemarrage automatique
FR2913061B1 (fr) Systeme de deshuilage pour moteur d'aeronef.
FR2967972B1 (fr) Procede de commande d'un systeme de flottabilite pour aeronef et systeme de flottabilite mettant en oeuvre ledit procede, et aeronef
FR2965779B1 (fr) Procede de commande d'un demarrage d'un vehicule equipe d'un systeme de mise en veille d'un moteur
FR2937449B1 (fr) Procede et systeme d'enrichissement de mel
FR2930597B1 (fr) Procede de commande d'un moteur
FR2925595B1 (fr) Procede et systeme de caracterisation et de comptage de depassements d'un seuil par un parametre de fonctionnement d'un moteur d'aeronef
FR2979390B1 (fr) Procede et systeme de commande du fonctionnement d'un moteur de vehicule
FR2949514B1 (fr) Procede de commande d'un systeme micro-hybride
FR2941017B1 (fr) Procede et systeme de commande d'une combinaison de turbocompresseurs
FR2959486B1 (fr) Nacelle pour moteur d'aeronef
FR2938014B1 (fr) Panneau d'attenuation acoustique pour nacelle de moteur d'aeronef
FR2919343B1 (fr) Moteur a combustion et procede de commande d'un moteur a combustion.
FR2989459B1 (fr) Systeme de mesure de consommation de carburant d'un moteur et procede de commande d'un tel systeme
FR2960592B1 (fr) Procede de demarrage d'un moteur d'aeronef
FR2946016B1 (fr) Systeme pour la commande d'au moins un moteur d'aeronef et aeronef comportant un tel systeme de commande.

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 8

PLFP Fee payment

Year of fee payment: 9

CD Change of name or company name

Owner name: SAFRAN AIRCRAFT ENGINES, FR

Effective date: 20170717

PLFP Fee payment

Year of fee payment: 10

PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

Year of fee payment: 13

PLFP Fee payment

Year of fee payment: 14

PLFP Fee payment

Year of fee payment: 15