CN103703649B - 一种用于在地面上为航空器供电的设备 - Google Patents

一种用于在地面上为航空器供电的设备 Download PDF

Info

Publication number
CN103703649B
CN103703649B CN201280035443.3A CN201280035443A CN103703649B CN 103703649 B CN103703649 B CN 103703649B CN 201280035443 A CN201280035443 A CN 201280035443A CN 103703649 B CN103703649 B CN 103703649B
Authority
CN
China
Prior art keywords
network
electromotor
aircraft
generator
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
CN201280035443.3A
Other languages
English (en)
Chinese (zh)
Other versions
CN103703649A (zh
Inventor
塞巴斯蒂安·维拉德
瑟奇·贝伦格
瑟奇·蒂里·罗克斯
帕斯卡尔·德里亚克
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
Labinal SA
Turbomeca SA
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 Labinal SA, Turbomeca SA filed Critical Labinal SA
Publication of CN103703649A publication Critical patent/CN103703649A/zh
Application granted granted Critical
Publication of CN103703649B publication Critical patent/CN103703649B/zh
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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)
CN201280035443.3A 2011-08-04 2012-07-27 一种用于在地面上为航空器供电的设备 Active CN103703649B (zh)

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
CN103703649A CN103703649A (zh) 2014-04-02
CN103703649B true CN103703649B (zh) 2016-08-31

Family

ID=46785751

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201280035443.3A Active CN103703649B (zh) 2011-08-04 2012-07-27 一种用于在地面上为航空器供电的设备

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)

Families Citing this family (19)

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

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008062920A (ja) * 2006-09-07 2008-03-21 Boeing Co:The 航空機パワーシステムおよび航空機システムを制御するための方法
EP2236419A2 (en) * 2009-04-01 2010-10-06 Rolls-Royce plc An apparatus for taxiing an aircraft
CN102037626A (zh) * 2008-04-09 2011-04-27 塔莱斯公司 用于管理电气网络的方法

Family Cites Families (18)

* 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 (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
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
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
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.

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008062920A (ja) * 2006-09-07 2008-03-21 Boeing Co:The 航空機パワーシステムおよび航空機システムを制御するための方法
CN102037626A (zh) * 2008-04-09 2011-04-27 塔莱斯公司 用于管理电气网络的方法
EP2236419A2 (en) * 2009-04-01 2010-10-06 Rolls-Royce plc An apparatus for taxiing an aircraft

Also Published As

Publication number Publication date
ES2554950T3 (es) 2015-12-28
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

Similar Documents

Publication Publication Date Title
CN103703649B (zh) 一种用于在地面上为航空器供电的设备
CN104169168B (zh) 用于向地面上的飞机供应电功率的装置以及使用该装置的方法
US9873518B2 (en) Electrical architecture for an aircraft, an aircraft, and a method of using it
CN101529686B (zh) 飞行器上电力发生、转换、分配和起动系统
US8218341B2 (en) Integrated aircraft power conditioning unit
JP5934326B2 (ja) 航空機用電力システム
CN104471819B (zh) 用于直升机涡轮引擎的控制和功率供应系统
EP2801719B1 (en) Aircraft electrical system
US5899411A (en) Aircraft electrical system providing emergency power and electric starting of propulsion engines
CN104884349B (zh) 飞行器的电力网络的管理方法
US8238130B2 (en) Low-mass, bi-directional DC-AC interface unit
CN110626507B (zh) 飞行器电气架构、包括架构的飞行器以及架构运行方法
EP2040370B1 (en) Generator for gas turbine engine having main DC bus and accessory AC bus
EP1944858A2 (en) DC bus short circuit compliant power generation systems using induction machine
CN117597847A (zh) 用于飞行器的电气架构
Anghel A novel start system for an aircraft auxiliary power unit
US9467083B1 (en) Wound-field generator including electrically isolated engine alternator
US10472084B2 (en) Motor-generator for high efficiency auxiliary power system

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
ASS Succession or assignment of patent right

Owner name: LABINAL POWER SYSTEMS

Free format text: FORMER OWNER: HISPANO SUIZA SA

Effective date: 20150615

C41 Transfer of patent application or patent right or utility model
TA01 Transfer of patent application right

Effective date of registration: 20150615

Address after: France Blagnac

Applicant after: LABINAL

Applicant after: Turbomeca

Address before: Columbia, France

Applicant before: Hispano Suiza S. A.

Applicant before: Turbomeca

C14 Grant of patent or utility model
GR01 Patent grant