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WO2011023678A3 - Reseau electrique d'un aeronef et procede de fonctionnement du reseau electrique - Google Patents

Reseau electrique d'un aeronef et procede de fonctionnement du reseau electrique Download PDF

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Publication number
WO2011023678A3
WO2011023678A3 PCT/EP2010/062301 EP2010062301W WO2011023678A3 WO 2011023678 A3 WO2011023678 A3 WO 2011023678A3 EP 2010062301 W EP2010062301 W EP 2010062301W WO 2011023678 A3 WO2011023678 A3 WO 2011023678A3
Authority
WO
WIPO (PCT)
Prior art keywords
current bus
grid
power grid
aircraft
generators
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.)
Ceased
Application number
PCT/EP2010/062301
Other languages
English (en)
Other versions
WO2011023678A2 (fr
Inventor
Alain Tardy
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.)
Thales SA
Original Assignee
Thales 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 Thales SA filed Critical Thales SA
Priority to EP10762879A priority Critical patent/EP2470427A2/fr
Priority to BR112012004277A priority patent/BR112012004277A2/pt
Priority to CA2772160A priority patent/CA2772160C/fr
Priority to US13/392,065 priority patent/US9425624B2/en
Publication of WO2011023678A2 publication Critical patent/WO2011023678A2/fr
Publication of WO2011023678A3 publication Critical patent/WO2011023678A3/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • 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
    • B60—VEHICLES IN GENERAL
    • B60R—VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
    • B60R16/00—Electric or fluid circuits specially adapted for vehicles and not otherwise provided for; Arrangement of elements of electric or fluid circuits specially adapted for vehicles and not otherwise provided for
    • B60R16/02—Electric or fluid circuits specially adapted for vehicles and not otherwise provided for; Arrangement of elements of electric or fluid circuits specially adapted for vehicles and not otherwise provided for electric constitutive elements
    • B60R16/03—Electric or fluid circuits specially adapted for vehicles and not otherwise provided for; Arrangement of elements of electric or fluid circuits specially adapted for vehicles and not otherwise provided for electric constitutive elements for supply of electrical power to vehicle subsystems or for
    • 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
    • B64D47/00—Equipment not otherwise provided for
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D7/00—Controlling wind motors 
    • F03D7/02—Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor
    • F03D7/026—Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor for starting-up
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D9/00—Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
    • F03D9/20—Wind motors characterised by the driven apparatus
    • F03D9/25—Wind motors characterised by the driven apparatus the apparatus being an electrical generator
    • F03D9/255—Wind motors characterised by the driven apparatus the apparatus being an electrical generator connected to electrical distribution networks; Arrangements therefor
    • 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
    • B64D2221/00—Electric power distribution systems onboard aircraft
    • 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
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/70—Wind energy
    • Y02E10/72—Wind turbines with rotation axis in wind direction

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Power Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Sustainable Development (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Eletrric Generators (AREA)
  • Supply And Distribution Of Alternating Current (AREA)
  • Rectifiers (AREA)

Abstract

L'invention concerne un réseau électrique d'un aéronef et un procédé de fonctionnement du réseau électrique. L'invention trouve une utilité particulière pour les avions commerciaux gros porteurs qui comportent de plus en plus d'équipements électriques embarqués. Le réseau comprend : • un bus alternatif (10), • un bus continu (12), • un redresseur (11) fournissant une tension continue au bus continu (12) à partir du bus alternatif, • une pluralité de convertisseurs bidirectionnels (O3 à O7) comportant deux points de raccordement, chaque convertisseur bidirectionnels (O3 à O7) étant raccordé en son premier point de raccordement au bus continu (12) et pouvant être raccordés en son second point de raccordement à une charge (13 à 17) de l'aéronef pour l'alimenter, le réseau pouvant être raccordé à au moins deux générateurs (G1, G2) susceptibles chacun de délivrer la tension alternative au bus alternatif au moyen du redresseur (11). Selon l'invention, le réseau comprend en outre au moins une liaison permettant de raccorder au moins un des générateurs (G1, G2) au second point de raccordement d'au moins un des convertisseurs bidirectionnels (O3 à O7). Le réseau permet de changer de générateur sans coupure et sans synchronisation particulière des générateurs (G1, G2).
PCT/EP2010/062301 2009-08-25 2010-08-24 Reseau electrique d'un aeronef et procede de fonctionnement du reseau electrique Ceased WO2011023678A2 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
EP10762879A EP2470427A2 (fr) 2009-08-25 2010-08-24 Reseau electrique d'un aeronef et procede de fonctionnement du reseau electrique
BR112012004277A BR112012004277A2 (pt) 2009-08-25 2010-08-24 rede elétrica de um avião e método de operação da rede elétrica
CA2772160A CA2772160C (fr) 2009-08-25 2010-08-24 Reseau electrique d'un aeronef et procede de fonctionnement du reseau electrique
US13/392,065 US9425624B2 (en) 2009-08-25 2010-08-24 Electrical network of an aircraft and method of operation of the electrical network

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0904047 2009-08-25
FR0904047A FR2949436B1 (fr) 2009-08-25 2009-08-25 Reseau electrique d'un aeronef et procede de fonctionnement du reseau electrique.

Publications (2)

Publication Number Publication Date
WO2011023678A2 WO2011023678A2 (fr) 2011-03-03
WO2011023678A3 true WO2011023678A3 (fr) 2011-10-13

Family

ID=42062467

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2010/062301 Ceased WO2011023678A2 (fr) 2009-08-25 2010-08-24 Reseau electrique d'un aeronef et procede de fonctionnement du reseau electrique

Country Status (6)

Country Link
US (1) US9425624B2 (fr)
EP (1) EP2470427A2 (fr)
BR (1) BR112012004277A2 (fr)
CA (1) CA2772160C (fr)
FR (1) FR2949436B1 (fr)
WO (1) WO2011023678A2 (fr)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8775846B2 (en) 2009-07-10 2014-07-08 Protonex Technology Corporation Portable power manager having one or more device ports for connecting with external power loads
GB2483696B (en) * 2010-09-17 2015-03-25 Ge Aviat Systems Ltd An aircraft with a power distribution system
GB2490305A (en) * 2011-04-05 2012-10-31 Rolls Royce Plc High frequency generator for isolated networks comprising a high frequency converter connected via an AC link
CN103650285B (zh) * 2011-05-24 2017-02-15 D·凯文·卡梅伦 一种整合和管理替代能源、电网功率以及负载之间需求/响应的系统和方法
US10250134B2 (en) 2013-04-01 2019-04-02 Revision Military Ltd. Power manager
EP3218985B1 (fr) 2014-11-11 2022-01-05 Galvion Soldier Power, LLC Module de commande pour réseau de puissance en courant continu
AU2016355125A1 (en) 2015-11-20 2018-07-05 David Long Power manager with reconfigurable power converting circuits
US11258366B2 (en) 2015-11-20 2022-02-22 Galvion Soldier Power, Llc Power manager with reconfigurable power converting circuits
US10848067B2 (en) 2015-11-20 2020-11-24 Galvion Soldier Power, Llc Power manager with reconfigurable power converting circuits
US12155263B2 (en) 2021-08-06 2024-11-26 Galvion Ltd. Helmet-mounted power system
USD1062615S1 (en) 2021-12-21 2025-02-18 Galvion Soldier Power, Llc Power pack
US12326707B2 (en) 2022-05-16 2025-06-10 Galvion Ltd. Method and system of providing a uniform messaging platform in a heterogeneous environment

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5013929A (en) * 1989-11-22 1991-05-07 Sundstrand Corporation Power conversion system having prime mover start capability
US5015941A (en) * 1989-10-30 1991-05-14 Sundstrand Corporation Power conversion system with bi-directional power converter having prime mover start capability
WO2007113312A1 (fr) * 2006-04-05 2007-10-11 Thales Dispositif d'alimentation d'une pluralite de charges a partir d'un reseau de fourniture d'energie electrique
US20090195074A1 (en) * 2008-01-31 2009-08-06 Buiel Edward R Power supply and storage device for improving drilling rig operating efficiency

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6018233A (en) * 1997-06-30 2000-01-25 Sundstrand Corporation Redundant starting/generating system
US7210653B2 (en) * 2002-10-22 2007-05-01 The Boeing Company Electric-based secondary power system architectures for aircraft
WO2005112219A1 (fr) * 2004-05-13 2005-11-24 Ntt Data Ex Techno Corporation Filtre actif
FR2899202B1 (fr) * 2006-04-04 2009-02-13 Airbus France Sas Dispositif et procede de generation electrique de secours a bord d'un aeronef
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
US7612514B2 (en) * 2006-11-09 2009-11-03 Honeywell International Inc. Architecture and a multiple function power converter for aircraft
GB201219925D0 (en) * 2012-11-06 2012-12-19 Rolls Royce Plc An electrical system for an aircraft
US9151272B2 (en) * 2013-12-31 2015-10-06 Google Inc. High frequency bi-directional AC power transmission

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5015941A (en) * 1989-10-30 1991-05-14 Sundstrand Corporation Power conversion system with bi-directional power converter having prime mover start capability
US5013929A (en) * 1989-11-22 1991-05-07 Sundstrand Corporation Power conversion system having prime mover start capability
WO2007113312A1 (fr) * 2006-04-05 2007-10-11 Thales Dispositif d'alimentation d'une pluralite de charges a partir d'un reseau de fourniture d'energie electrique
US20090195074A1 (en) * 2008-01-31 2009-08-06 Buiel Edward R Power supply and storage device for improving drilling rig operating efficiency

Also Published As

Publication number Publication date
CA2772160C (fr) 2018-01-02
WO2011023678A2 (fr) 2011-03-03
US20120326497A1 (en) 2012-12-27
US9425624B2 (en) 2016-08-23
FR2949436A1 (fr) 2011-03-04
BR112012004277A2 (pt) 2016-02-23
CA2772160A1 (fr) 2011-03-03
FR2949436B1 (fr) 2012-01-27
EP2470427A2 (fr) 2012-07-04

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