ES2179440T3 - Dispositivo de arranque para una turbina de gas en una aeronave. - Google Patents

Dispositivo de arranque para una turbina de gas en una aeronave.

Info

Publication number
ES2179440T3
ES2179440T3 ES98402549T ES98402549T ES2179440T3 ES 2179440 T3 ES2179440 T3 ES 2179440T3 ES 98402549 T ES98402549 T ES 98402549T ES 98402549 T ES98402549 T ES 98402549T ES 2179440 T3 ES2179440 T3 ES 2179440T3
Authority
ES
Spain
Prior art keywords
turbine
starting device
aircraft
gas turbine
electric drive
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
Application number
ES98402549T
Other languages
English (en)
Inventor
Serge Boyer
Regine Sutra-Orus
Stephane Tregine-Regent
Alain Tardy
Claude Barbier
Philippe Buron
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.)
Airbus Operations SAS
Artus SAS
Original Assignee
Airbus Operations SAS
Artus 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 Airbus Operations SAS, Artus SAS filed Critical Airbus Operations SAS
Application granted granted Critical
Publication of ES2179440T3 publication Critical patent/ES2179440T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02N—STARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
    • F02N11/00—Starting of engines by means of electric motors
    • F02N11/08—Circuits specially adapted for starting of engines
    • F02N11/0859—Circuits specially adapted for starting of engines specially adapted to the type of the starter motor or integrated into it
    • 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
    • F02N—STARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
    • F02N11/00—Starting of engines by means of electric motors
    • F02N11/08—Circuits specially adapted for starting of engines
    • F02N11/0862—Circuits specially adapted for starting of engines characterised by the electrical power supply means, e.g. battery
    • F02N11/0866—Circuits specially adapted for starting of engines characterised by the electrical power supply means, e.g. battery comprising several power sources, e.g. battery and capacitor or two batteries
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02N—STARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
    • F02N11/00—Starting of engines by means of electric motors
    • F02N11/08—Circuits specially adapted for starting of engines
    • F02N2011/0881—Components of the circuit not provided for by previous groups
    • F02N2011/0896—Inverters for electric machines, e.g. starter-generators
    • 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
    • F05D2220/00—Application
    • F05D2220/50—Application for auxiliary power units (APU's)
    • 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)
  • Inverter Devices (AREA)
  • Control Of Ac Motors In General (AREA)
  • Control Of Eletrric Generators (AREA)
  • Control Of Turbines (AREA)
  • Motor And Converter Starters (AREA)

Abstract

ESTE DISPOSITIVO DE ARRANQUE ES DEL TIPO QUE INCLUYE MEDIOS DE ALIMENTACION DE ENERGIA ELECTRICA (13) QUE GENERA UNA CORRIENTE CONTINUA, Y UN MOTOR ELECTRICO DE ARRASTRE (14), QUE GRACIAS A ESTOS MEDIOS DE ALIMENTACION (13), ES INDEPENDIENTE DE LA TURBINA (10) QUE HAY QUE ARRANCAR, Y CUYO EJE DE SALIDA (5) ES SUSCEPTIBLE DE ESTAR MECANICAMENTE ACOPLADO EN ROTACION A SU EJE DE ENTRADA (17). SEGUN LA INVENCION, EL MOTOR ELECTRICO DE ARRASTRE (14) ES UN MOTOR SINCRONO ALIMENTADO CON CORRIENTE ALTERNA TRIFASICA Y CONTROLADO POR UN DISPOSITIVO ONDULADOR (18) CONECTADO A LOS MEDIOS DE ALIMENTACION (13). APLICACION, CONCRETAMENTE EN EL CASO DE QUE LA TURBINA QUE HAY QUE ARRASTRAR SEA UNA TURBINA DE GRAN POTENCIA.
ES98402549T 1997-10-20 1998-10-14 Dispositivo de arranque para una turbina de gas en una aeronave. Expired - Lifetime ES2179440T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9713107A FR2769952A1 (fr) 1997-10-20 1997-10-20 Dispositif de demarrage pour turbine a gaz dans un aeronef

Publications (1)

Publication Number Publication Date
ES2179440T3 true ES2179440T3 (es) 2003-01-16

Family

ID=9512420

Family Applications (1)

Application Number Title Priority Date Filing Date
ES98402549T Expired - Lifetime ES2179440T3 (es) 1997-10-20 1998-10-14 Dispositivo de arranque para una turbina de gas en una aeronave.

Country Status (5)

Country Link
US (1) US6351090B1 (es)
EP (1) EP0911515B1 (es)
DE (1) DE69807169T2 (es)
ES (1) ES2179440T3 (es)
FR (1) FR2769952A1 (es)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6256977B1 (en) * 1999-09-07 2001-07-10 Alliedsignal, Inc. Start circuit for electric starting of engines
US6838778B1 (en) * 2002-05-24 2005-01-04 Hamilton Sundstrand Corporation Integrated starter generator drive having selective torque converter and constant speed transmission for aircraft having a constant frequency electrical system
US6838779B1 (en) * 2002-06-24 2005-01-04 Hamilton Sundstrand Corporation Aircraft starter generator for variable frequency (vf) electrical system
US6831442B2 (en) * 2002-07-03 2004-12-14 General Motors Corporation Utilizing zero-sequence switchings for reversible converters
US7227271B2 (en) * 2004-09-21 2007-06-05 Honeywell International Inc. Method and apparatus for controlling an engine start system
CN101036329B (zh) * 2004-10-07 2011-06-08 汤姆逊许可公司 音频/视频路由器
US7242105B2 (en) * 2005-08-17 2007-07-10 Hamilton Sundstrand Corporation Electric engine start with two motors and single motor drive
US7508086B2 (en) * 2006-03-24 2009-03-24 General Electric Company Aircraft engine starter/generator and controller
US7687928B2 (en) * 2006-06-14 2010-03-30 Smiths Aerospace, Llc Dual-structured aircraft engine starter/generator
US7997085B2 (en) * 2006-09-27 2011-08-16 General Electric Company Gas turbine engine assembly and method of assembling same
FR2907761B1 (fr) * 2006-10-27 2009-07-03 Airbus France Sas Dispositif de generation electrique d'un aeronef et de demarrage electrique d'un reacteur a bord d'un aeronef
US8695321B2 (en) * 2007-12-27 2014-04-15 Mitsubishi Heavy Industries, Ltd. Gas turbine control apparatus and control method for generating an electric motor torque instruction based on the detected exhaust gas temperature
US7586204B2 (en) * 2008-01-22 2009-09-08 Hamilton Sundstrand Corporation Permanent magnet alternator speed detection circuit with feedback at lower speeds
US20120032633A1 (en) * 2009-04-09 2012-02-09 Ralf Cordes Transmission of power bidirectionally and without contact to charge electric vehicles
US8148834B2 (en) * 2009-05-19 2012-04-03 General Electric Company Aircraft engine starting/generating system and method of control
FR2951330B1 (fr) * 2009-10-13 2013-03-08 Messier Bugatti Reseau de pilotage pour actionneurs mono ou multimoteurs, particulierement adapte a des applications aeronautiques telles que l'alimentation de moteurs de boitiers d'accrochage
US8232702B2 (en) 2010-07-30 2012-07-31 Ge Aviation Systems, Llc Apparatus for a high speed sleeveless rotor
US9840997B2 (en) * 2013-03-14 2017-12-12 Pratt & Whitney Canada Corp. Engine starting system using stored energy
FR3022949B1 (fr) * 2014-06-26 2016-07-15 Snecma Procedes de determination de caracteristiques d'ouvertures ou de fermetures d'une vanne de demarrage de turbomoteur
FR3023989B1 (fr) 2014-07-17 2016-08-26 Airbus Helicopters Architecture electrique d'un aeronef, aeronef et procede mis en oeuvre
CN104883107B (zh) * 2015-04-28 2017-05-10 西北工业大学 一种三级电励磁式同步电机动态起动控制方法
FR3036798B1 (fr) * 2015-06-01 2018-06-15 Safran Helicopter Engines Procede de detection d'un defaut mecanique d'un generateur de gaz d'une turbomachine d'un aeronef et dispositif de mise en œuvre correspondant
DE102016202195A1 (de) * 2016-02-12 2017-08-17 Siemens Aktiengesellschaft Verfahren zum Antrieb eines Luftfahrzeugs und Luftfahrzeug
WO2019183428A1 (en) 2018-03-22 2019-09-26 Continental Motors, Inc. Engine ignition timing and power supply system
US12445079B2 (en) 2023-10-16 2025-10-14 Honeywell International, Inc. Motor control system for energizing a low-voltage motor from a high-voltage source
FR3156170B1 (fr) 2023-12-05 2025-10-24 Airbus Helicopters Installation motrice munie d’un turbomoteur et d’un circuit de démarrage adaptatif et procédé de démarrage adaptatif d’un turbomoteur

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4456830A (en) * 1982-04-22 1984-06-26 Lockheed Corporation AC Motor-starting for aircraft engines using APU free turbine driven generators
US5175439A (en) * 1987-12-21 1992-12-29 Robert Bosch Gmbh Power supply circuit for motor vehicles
US5172543A (en) * 1990-12-26 1992-12-22 Sundstrand Corporation Starting system for a gas turbine and method of starting a gas turbine
JPH07119594A (ja) * 1993-09-02 1995-05-09 Nippondenso Co Ltd 車両用内燃機関始動装置
US5512811A (en) * 1994-01-21 1996-04-30 Sundstrand Corporation Starter/generator system having multivoltage generation capability
US5493201A (en) * 1994-11-15 1996-02-20 Sundstrand Corporation Starter/generator system and method utilizing a low voltage source
US5899411A (en) * 1996-01-22 1999-05-04 Sundstrand Corporation Aircraft electrical system providing emergency power and electric starting of propulsion engines
US5966925A (en) * 1996-04-26 1999-10-19 Kabushiki Kaisha Toshiba Gas turbine power plant control for starting and stopping

Also Published As

Publication number Publication date
FR2769952A1 (fr) 1999-04-23
US6351090B1 (en) 2002-02-26
DE69807169T2 (de) 2003-05-08
EP0911515B1 (fr) 2002-08-14
EP0911515A1 (fr) 1999-04-28
DE69807169D1 (de) 2002-09-19

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