ES2554950T3 - Dispositivo de alimentación eléctrica de una aeronave en el suelo - Google Patents

Dispositivo de alimentación eléctrica de una aeronave en el suelo Download PDF

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Publication number
ES2554950T3
ES2554950T3 ES12753762.9T ES12753762T ES2554950T3 ES 2554950 T3 ES2554950 T3 ES 2554950T3 ES 12753762 T ES12753762 T ES 12753762T ES 2554950 T3 ES2554950 T3 ES 2554950T3
Authority
ES
Spain
Prior art keywords
generator
network
aircraft
ground
power
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
ES12753762.9T
Other languages
English (en)
Spanish (es)
Inventor
Sébastien VIEILLARD
Serge Berenger
Serge Thierry Roques
Pascal Dauriac
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 Helicopter Engines SAS
Safran Electrical and Power SAS
Original Assignee
Turbomeca SA
Labinal Power Systems 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 Turbomeca SA, Labinal Power Systems SAS filed Critical Turbomeca SA
Application granted granted Critical
Publication of ES2554950T3 publication Critical patent/ES2554950T3/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/405Powered wheels, e.g. for taxing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D41/00Power installations for auxiliary purposes
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J4/00Circuit arrangements for mains or distribution networks not specified as AC or DC
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J9/00Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting
    • H02J9/04Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source
    • H02J9/06Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source with automatic change-over, e.g. UPS systems
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J2310/00The network for supplying or distributing electric power characterised by its spatial reach or by the load
    • H02J2310/40The network being an on-board power network, i.e. within a vehicle
    • H02J2310/44The network being an on-board power network, i.e. within a vehicle for aircrafts
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/80Energy efficient operational measures, e.g. ground operations or mission management

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Power Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Control Of Eletrric Generators (AREA)
  • Supply And Distribution Of Alternating Current (AREA)
  • Direct Current Feeding And Distribution (AREA)
  • Synchronous Machinery (AREA)
  • Stand-By Power Supply Arrangements (AREA)
ES12753762.9T 2011-08-04 2012-07-27 Dispositivo de alimentación eléctrica de una aeronave en el suelo Active ES2554950T3 (es)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1157169 2011-08-04
FR1157169A FR2978878B1 (fr) 2011-08-04 2011-08-04 Dispositif d'alimentation electrique d'un aeronef au sol.
PCT/FR2012/051790 WO2013017789A2 (fr) 2011-08-04 2012-07-27 Dispositif d'alimentation électrique d'un aéronef au sol

Publications (1)

Publication Number Publication Date
ES2554950T3 true ES2554950T3 (es) 2015-12-28

Family

ID=46785751

Family Applications (1)

Application Number Title Priority Date Filing Date
ES12753762.9T Active ES2554950T3 (es) 2011-08-04 2012-07-27 Dispositivo de alimentación eléctrica de una aeronave en el suelo

Country Status (10)

Country Link
US (1) US9592907B2 (enExample)
EP (1) EP2740191B1 (enExample)
JP (1) JP5955960B2 (enExample)
CN (1) CN103703649B (enExample)
BR (1) BR112014001457B1 (enExample)
CA (1) CA2842086C (enExample)
ES (1) ES2554950T3 (enExample)
FR (1) FR2978878B1 (enExample)
RU (1) RU2603693C2 (enExample)
WO (1) WO2013017789A2 (enExample)

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FR2988694B1 (fr) * 2012-03-30 2014-03-28 Hispano Suiza Sa Dispositif d'alimentation electrique d'un aeronef au sol
CN103746448A (zh) * 2013-12-04 2014-04-23 中国飞行试验研究院 运七飞机供电系统
EP2886387A3 (en) * 2013-12-23 2015-12-23 Rolls-Royce Corporation Dual redundant motor/generator for an engine
US20150283908A1 (en) * 2014-04-02 2015-10-08 Hamilton Sundstrand Corporation Systems utilizing a controllable voltage ac generator system
EP3095988A1 (en) * 2015-05-18 2016-11-23 Airbus Operations, S.L. Auxiliary power unit starting system for an aircraft
GB201511033D0 (en) * 2015-05-19 2015-08-05 Rolls Royce Plc Aircraft electrical network
US9771149B2 (en) * 2015-10-30 2017-09-26 Honeywell International Inc. Gate departure system for aircraft
EP3235723B1 (en) * 2016-04-22 2019-11-27 Rolls-Royce plc Aircraft electrical network
FR3054738B1 (fr) * 2016-07-29 2020-10-23 Airbus Helicopters Architecture electrique a double reseau electrique secondaire pour le demarrage des moteurs d'un aeronef
GB201715598D0 (en) 2017-09-27 2017-11-08 Rolls Royce Plc Electrical interconnect system
RU2684971C1 (ru) * 2017-12-13 2019-04-16 Эйрбас Хеликоптерс Электрическая система с двойной вторичной электросетью для запуска двигателей летательных аппаратов
FR3079820B1 (fr) 2018-04-09 2020-04-17 Safran Electrical & Power Systeme et procede de demarrage/generation pour turbomachine d'aeronef
FR3087960B1 (fr) * 2018-10-31 2021-06-04 Safran Systeme de conversion et de transport d'energie electrique pour l'hybridation interne d'un aeronef a turboreacteurs
US11840356B2 (en) 2019-03-01 2023-12-12 Hamilton Sundstrand Corporation Indicators for hybrid electrical powerplants
US11999495B2 (en) 2019-03-01 2024-06-04 Pratt & Whitney Canada Corp. Degraded mode operation of hybrid electric propulsion systems
WO2020185274A2 (en) 2019-03-01 2020-09-17 United Technologies Advanced Projects, Inc. Normal mode operation of hybrid electric propulsion systems
EP3927620B1 (en) 2019-04-25 2024-08-28 Pratt & Whitney Canada Corp. Control systems for hybrid electric powerplants
US11958622B2 (en) 2020-05-15 2024-04-16 Pratt & Whitney Canada Corp. Protection functions
US11794917B2 (en) 2020-05-15 2023-10-24 Pratt & Whitney Canada Corp. Parallel control loops for hybrid electric aircraft

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FR1059612A (fr) 1952-07-09 1954-03-26 Andre Mathieu Freres Perfectionnement au montage des plaquettes nasales de lunettes
SU868926A1 (ru) * 1980-01-03 1981-09-30 Предприятие П/Я М-6374 Устройство дл автоматического переключени потребителей с одного канала питани посто нного тока на другой
JPH0214415U (enExample) * 1988-07-13 1990-01-30
US5899411A (en) * 1996-01-22 1999-05-04 Sundstrand Corporation Aircraft electrical system providing emergency power and electric starting of propulsion engines
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JP4725010B2 (ja) * 2003-10-31 2011-07-13 シンフォニアテクノロジー株式会社 2系統相互バックアップ式電源装置
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FR2907762B1 (fr) * 2006-10-27 2009-12-18 Airbus France Systeme de generation, conversion, distribution et demarrage electrique a bord d'un aeronef
FR2911848B1 (fr) * 2007-01-31 2009-12-25 Hispano Suiza Sa Circuit d'alimentation en energie electrique dans un aeronef pour des equipements electriques comprenant un circuit de degivrage
FR2930084B1 (fr) * 2008-04-09 2012-06-08 Thales Sa Procede de gestion d'un reseau electrique
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Also Published As

Publication number Publication date
CN103703649B (zh) 2016-08-31
CA2842086C (fr) 2019-05-14
RU2603693C2 (ru) 2016-11-27
JP5955960B2 (ja) 2016-07-20
WO2013017789A2 (fr) 2013-02-07
EP2740191B1 (fr) 2015-10-07
FR2978878A1 (fr) 2013-02-08
RU2014108158A (ru) 2015-09-10
EP2740191A2 (fr) 2014-06-11
JP2014525873A (ja) 2014-10-02
BR112014001457B1 (pt) 2021-05-25
CA2842086A1 (fr) 2013-02-07
US20140138479A1 (en) 2014-05-22
FR2978878B1 (fr) 2013-08-09
US9592907B2 (en) 2017-03-14
CN103703649A (zh) 2014-04-02
BR112014001457A2 (pt) 2018-08-14
WO2013017789A3 (fr) 2013-10-24

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