BR112014001457A2 - dispositivo de alimentação elétrica de uma aeronave em solo - Google Patents

dispositivo de alimentação elétrica de uma aeronave em solo

Info

Publication number
BR112014001457A2
BR112014001457A2 BR112014001457-4A BR112014001457A BR112014001457A2 BR 112014001457 A2 BR112014001457 A2 BR 112014001457A2 BR 112014001457 A BR112014001457 A BR 112014001457A BR 112014001457 A2 BR112014001457 A2 BR 112014001457A2
Authority
BR
Brazil
Prior art keywords
network
aircraft
ground
electrical power
power device
Prior art date
Application number
BR112014001457-4A
Other languages
English (en)
Other versions
BR112014001457B1 (pt
Inventor
Vieillard Sébastien
Berenger Serge
Thierry Roques Serge
Dauriac Pascal
Original Assignee
Hispano-Suiza
Turbomeca
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 Hispano-Suiza, Turbomeca filed Critical Hispano-Suiza
Publication of BR112014001457A2 publication Critical patent/BR112014001457A2/pt
Publication of BR112014001457B1 publication Critical patent/BR112014001457B1/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/405—Powered wheels, e.g. for taxing
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J4/00—Circuit arrangements for mains or distribution networks not specified as ac or dc
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D41/00—Power installations for auxiliary purposes
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J9/00—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting
    • H02J9/04—Circuit 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
    • H02J9/06—Circuit 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
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J2310/00—The network for supplying or distributing electric power characterised by its spatial reach or by the load
    • H02J2310/40—The network being an on-board power network, i.e. within a vehicle
    • H02J2310/44—The network being an on-board power network, i.e. within a vehicle for aircrafts
    • 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
    • Y02T50/40—Weight reduction
    • 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
    • Y02T50/80—Energy 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)
  • Direct Current Feeding And Distribution (AREA)
  • Supply And Distribution Of Alternating Current (AREA)
  • Stand-By Power Supply Arrangements (AREA)
  • Synchronous Machinery (AREA)
BR112014001457-4A 2011-08-04 2012-07-27 dispositivo de alimentação elétrica de uma aeronave em solo BR112014001457B1 (pt)

Applications Claiming Priority (3)

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

Publications (2)

Publication Number Publication Date
BR112014001457A2 true BR112014001457A2 (pt) 2018-08-14
BR112014001457B1 BR112014001457B1 (pt) 2021-05-25

Family

ID=46785751

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112014001457-4A BR112014001457B1 (pt) 2011-08-04 2012-07-27 dispositivo de alimentação elétrica de uma aeronave em solo

Country Status (10)

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

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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***
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
US10518863B2 (en) * 2016-04-22 2019-12-31 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
CA3132288A1 (en) 2019-03-01 2020-09-17 Pratt & Whitney Canada Corp. Normal mode operation of hybrid electric propulsion systems
US11840356B2 (en) 2019-03-01 2023-12-12 Hamilton Sundstrand Corporation Indicators for hybrid electrical powerplants
EP3931097A4 (en) 2019-03-01 2022-11-16 Pratt & Whitney Canada Corp. DEGRADED MODE OF OPERATION OF HYBRID ELECTRIC PROPULSION SYSTEMS
WO2020219111A1 (en) 2019-04-25 2020-10-29 United Technologies Corporation 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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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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 (pt) * 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
US7210653B2 (en) * 2002-10-22 2007-05-01 The Boeing Company Electric-based secondary power system architectures for aircraft
RU2232109C1 (ru) * 2003-09-22 2004-07-10 ОАО "ОКБ им. А.С.Яковлева" Способ электроснабжения бортовых систем летательного аппарата
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
JP2005354861A (ja) * 2004-06-14 2005-12-22 Fuji Electric Systems Co Ltd 原動機駆動電源装置による給電装置
US7439634B2 (en) * 2004-08-24 2008-10-21 Honeywell International Inc. Electrical starting, generation, conversion and distribution system architecture for a more electric vehicle
US7445178B2 (en) * 2004-09-28 2008-11-04 The Boeing Company Powered nose aircraft wheel system
GB2444678B (en) * 2005-08-29 2010-09-22 Borealis Tech Ltd Nosewheel control apparatus
US8155876B2 (en) * 2006-09-07 2012-04-10 The Boeing Company Systems and methods for controlling aircraft electrical power
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
FR2941107B1 (fr) 2009-01-09 2015-08-14 Hispano Suiza Sa Systeme electrique de demarrage des moteurs d'un aeronef
GB0905568D0 (en) 2009-04-01 2009-05-13 Rolls Royce Plc Taxling
FR2944775B1 (fr) * 2009-04-24 2013-03-08 Messier Bugatti Procede de deplacement d'un aeronef au sol
FR2954283B1 (fr) * 2009-12-23 2012-03-02 Hispano Suiza Sa Aeronef comportant un demarreur-generateur electrique pour le ou chaque turboreacteur et un train d'aterrissage equipe d'un moteur electrique de manoeuvre au sol
FR2960520B1 (fr) * 2010-05-26 2012-06-29 Airbus Operations Sas Aeronef comprenant un moteur de train
FR2975376B1 (fr) * 2011-05-20 2018-03-30 Safran Landing Systems Procede pour alimenter des moteurs de deplacement autonome d'un aeronef.

Also Published As

Publication number Publication date
CN103703649B (zh) 2016-08-31
WO2013017789A2 (fr) 2013-02-07
JP5955960B2 (ja) 2016-07-20
US9592907B2 (en) 2017-03-14
BR112014001457B1 (pt) 2021-05-25
JP2014525873A (ja) 2014-10-02
US20140138479A1 (en) 2014-05-22
WO2013017789A3 (fr) 2013-10-24
RU2014108158A (ru) 2015-09-10
RU2603693C2 (ru) 2016-11-27
FR2978878A1 (fr) 2013-02-08
CN103703649A (zh) 2014-04-02
CA2842086A1 (fr) 2013-02-07
EP2740191B1 (fr) 2015-10-07
CA2842086C (fr) 2019-05-14
EP2740191A2 (fr) 2014-06-11
FR2978878B1 (fr) 2013-08-09
ES2554950T3 (es) 2015-12-28

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Legal Events

Date Code Title Description
B25A Requested transfer of rights approved

Owner name: TURBOMECA (FR) ; LABINAL POWER SYSTEMS (FR)

B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 27/07/2012, OBSERVADAS AS CONDICOES LEGAIS.