RU2603693C2 - Устройство электрического питания летательного аппарата на земле - Google Patents

Устройство электрического питания летательного аппарата на земле Download PDF

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Publication number
RU2603693C2
RU2603693C2 RU2014108158/07A RU2014108158A RU2603693C2 RU 2603693 C2 RU2603693 C2 RU 2603693C2 RU 2014108158/07 A RU2014108158/07 A RU 2014108158/07A RU 2014108158 A RU2014108158 A RU 2014108158A RU 2603693 C2 RU2603693 C2 RU 2603693C2
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RU
Russia
Prior art keywords
generator
network
aircraft
power
voltage
Prior art date
Application number
RU2014108158/07A
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English (en)
Russian (ru)
Other versions
RU2014108158A (ru
Inventor
Себастьен ВЬЕЙАР
Серж БЕРЕНЖЕР
Серж Тьерри РОК
Паскаль ДОРИАК
Original Assignee
Лабиналь Пауэр Системз
Турбомека
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Application filed by Лабиналь Пауэр Системз, Турбомека filed Critical Лабиналь Пауэр Системз
Publication of RU2014108158A publication Critical patent/RU2014108158A/ru
Application granted granted Critical
Publication of RU2603693C2 publication Critical patent/RU2603693C2/ru

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    • 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
    • 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
    • H02J4/00—Circuit arrangements for mains or distribution networks not specified as AC or DC
    • 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)
  • Supply And Distribution Of Alternating Current (AREA)
  • Direct Current Feeding And Distribution (AREA)
  • Synchronous Machinery (AREA)
  • Stand-By Power Supply Arrangements (AREA)
RU2014108158/07A 2011-08-04 2012-07-27 Устройство электрического питания летательного аппарата на земле RU2603693C2 (ru)

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 (2)

Publication Number Publication Date
RU2014108158A RU2014108158A (ru) 2015-09-10
RU2603693C2 true RU2603693C2 (ru) 2016-11-27

Family

ID=46785751

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2014108158/07A RU2603693C2 (ru) 2011-08-04 2012-07-27 Устройство электрического питания летательного аппарата на земле

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)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2629817C2 (ru) * 2012-03-30 2017-09-04 Лабиналь Пауэр Системз Устройство электрического питания летательного аппарата на земле
RU2684971C1 (ru) * 2017-12-13 2019-04-16 Эйрбас Хеликоптерс Электрическая система с двойной вторичной электросетью для запуска двигателей летательных аппаратов
RU2831133C1 (ru) * 2024-04-10 2024-12-02 Федеральное государственное бюджетное научное учреждение "Федеральный научный агроинженерный центр ВИМ" (ФГБНУ ФНАЦ ВИМ) Способ симметрирования фазных токов и напряжений, выдачи всей мощности генератора на однофазную нагрузку, повышения надёжности питания нагрузок генератора

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
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

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
RU2232109C1 (ru) * 2003-09-22 2004-07-10 ОАО "ОКБ им. А.С.Яковлева" Способ электроснабжения бортовых систем летательного аппарата
EP1897804A2 (en) * 2006-09-07 2008-03-12 The Boeing Company Systems and methods for controlling aricraft electrical power
WO2009125007A2 (fr) * 2008-04-09 2009-10-15 Thales Procede de gestion d'un reseau electrique
EP2236419A2 (en) * 2009-04-01 2010-10-06 Rolls-Royce plc An apparatus for taxiing an aircraft
FR2954283A1 (fr) * 2009-12-23 2011-06-24 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

Family Cites Families (15)

* 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
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
US7210653B2 (en) * 2002-10-22 2007-05-01 The Boeing Company Electric-based secondary power system architectures for aircraft
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
US7975960B2 (en) * 2005-08-29 2011-07-12 Borealis Technical Limited Nosewheel control apparatus
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
FR2941107B1 (fr) * 2009-01-09 2015-08-14 Hispano Suiza Sa Systeme electrique de demarrage des moteurs d'un aeronef
FR2944775B1 (fr) * 2009-04-24 2013-03-08 Messier Bugatti Procede de deplacement d'un aeronef 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.

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
RU2232109C1 (ru) * 2003-09-22 2004-07-10 ОАО "ОКБ им. А.С.Яковлева" Способ электроснабжения бортовых систем летательного аппарата
EP1897804A2 (en) * 2006-09-07 2008-03-12 The Boeing Company Systems and methods for controlling aricraft electrical power
WO2009125007A2 (fr) * 2008-04-09 2009-10-15 Thales Procede de gestion d'un reseau electrique
EP2236419A2 (en) * 2009-04-01 2010-10-06 Rolls-Royce plc An apparatus for taxiing an aircraft
FR2954283A1 (fr) * 2009-12-23 2011-06-24 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

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2629817C2 (ru) * 2012-03-30 2017-09-04 Лабиналь Пауэр Системз Устройство электрического питания летательного аппарата на земле
RU2684971C1 (ru) * 2017-12-13 2019-04-16 Эйрбас Хеликоптерс Электрическая система с двойной вторичной электросетью для запуска двигателей летательных аппаратов
RU2831133C1 (ru) * 2024-04-10 2024-12-02 Федеральное государственное бюджетное научное учреждение "Федеральный научный агроинженерный центр ВИМ" (ФГБНУ ФНАЦ ВИМ) Способ симметрирования фазных токов и напряжений, выдачи всей мощности генератора на однофазную нагрузку, повышения надёжности питания нагрузок генератора

Also Published As

Publication number Publication date
CN103703649B (zh) 2016-08-31
ES2554950T3 (es) 2015-12-28
CA2842086C (fr) 2019-05-14
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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