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
Application number
PCT/EP2010/062301
Other languages
English (en)
Other versions
WO2011023678A2 (fr
Inventor
Alain Tardy
Original Assignee
Thales
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 filed Critical Thales
Priority to BR112012004277A priority Critical patent/BR112012004277A2/pt
Priority to US13/392,065 priority patent/US9425624B2/en
Priority to CA2772160A priority patent/CA2772160C/fr
Priority to EP10762879A priority patent/EP2470427A2/fr
Publication of WO2011023678A2 publication Critical patent/WO2011023678A2/fr
Publication of WO2011023678A3 publication Critical patent/WO2011023678A3/fr

Links

Classifications

    • 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60RVEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
    • B60R16/00Electric 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
    • B60R16/02Electric 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
    • B60R16/03Electric 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D7/00Controlling wind motors 
    • F03D7/02Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor
    • F03D7/026Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor for starting-up
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D9/00Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
    • F03D9/20Wind motors characterised by the driven apparatus
    • F03D9/25Wind motors characterised by the driven apparatus the apparatus being an electrical generator
    • F03D9/255Wind motors characterised by the driven apparatus the apparatus being an electrical generator connected to electrical distribution networks; Arrangements therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D2221/00Electric power distribution systems onboard aircraft
    • 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
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction

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 WO2011023678A2 (fr)

Priority Applications (4)

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

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 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 (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110007491A1 (en) 2009-07-10 2011-01-13 Protonex Technology Corporation Portable power manager enclosure
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
WO2012162570A1 (fr) * 2011-05-24 2012-11-29 Cameron D Kevin Système et procédé pour intégrer et gérer une demande/réponse entre des sources d'énergie alternative, un réseau électrique et des charges
CA2908309C (fr) 2013-04-01 2020-05-05 Protonex Technology Corporation Gestionnaire d'alimentation
WO2016077216A1 (fr) 2014-11-11 2016-05-19 Protonex Technology Corporation Module de commande pour réseau de puissance en courant continu
US10848067B2 (en) 2015-11-20 2020-11-24 Galvion Soldier Power, Llc Power manager with reconfigurable power converting circuits
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

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

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