WO2009156654A3 - Dispositif et procede de couplage de deux parties d'un reseau a courant continu notamment dans un aeronef - Google Patents

Dispositif et procede de couplage de deux parties d'un reseau a courant continu notamment dans un aeronef Download PDF

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Publication number
WO2009156654A3
WO2009156654A3 PCT/FR2009/051006 FR2009051006W WO2009156654A3 WO 2009156654 A3 WO2009156654 A3 WO 2009156654A3 FR 2009051006 W FR2009051006 W FR 2009051006W WO 2009156654 A3 WO2009156654 A3 WO 2009156654A3
Authority
WO
WIPO (PCT)
Prior art keywords
aircraft
portions
coupling
current network
direct current
Prior art date
Application number
PCT/FR2009/051006
Other languages
English (en)
Other versions
WO2009156654A2 (fr
Inventor
Olivier Langlois
Lucien Prisse
Marc Aiximeno
Original Assignee
Airbus Operations
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 Airbus Operations filed Critical Airbus Operations
Priority to US12/993,659 priority Critical patent/US8736099B2/en
Priority to EP09769495A priority patent/EP2289139A2/fr
Publication of WO2009156654A2 publication Critical patent/WO2009156654A2/fr
Publication of WO2009156654A3 publication Critical patent/WO2009156654A3/fr

Links

Classifications

    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
    • H02M3/00—Conversion of dc power input into dc power output
    • H02M3/02—Conversion of dc power input into dc power output without intermediate conversion into ac
    • H02M3/04—Conversion of dc power input into dc power output without intermediate conversion into ac by static converters
    • H02M3/10—Conversion of dc power input into dc power output without intermediate conversion into ac by static converters using discharge tubes with control electrode or semiconductor devices with control electrode
    • H02M3/145—Conversion of dc power input into dc power output without intermediate conversion into ac by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal
    • H02M3/155—Conversion of dc power input into dc power output without intermediate conversion into ac by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal using semiconductor devices only
    • H02M3/156—Conversion of dc power input into dc power output without intermediate conversion into ac by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal using semiconductor devices only with automatic control of output voltage or current, e.g. switching regulators
    • H02M3/158—Conversion of dc power input into dc power output without intermediate conversion into ac by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal using semiconductor devices only with automatic control of output voltage or current, e.g. switching regulators including plural semiconductor devices as final control devices for a single load
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
    • H02M3/00—Conversion of dc power input into dc power output
    • H02M3/02—Conversion of dc power input into dc power output without intermediate conversion into ac
    • H02M3/04—Conversion of dc power input into dc power output without intermediate conversion into ac by static converters
    • H02M3/10—Conversion of dc power input into dc power output without intermediate conversion into ac by static converters using discharge tubes with control electrode or semiconductor devices with control electrode
    • H02M3/145—Conversion of dc power input into dc power output without intermediate conversion into ac by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal
    • H02M3/155—Conversion of dc power input into dc power output without intermediate conversion into ac by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal using semiconductor devices only
    • H02M3/156—Conversion of dc power input into dc power output without intermediate conversion into ac by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal using semiconductor devices only with automatic control of output voltage or current, e.g. switching regulators

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Dc-Dc Converters (AREA)
  • Emergency Protection Circuit Devices (AREA)
  • Amplifiers (AREA)

Abstract

L'invention concerne un dispositif et un procédé de couplage de deux parties d'un réseau à courant continu, dans lesquelles sont respectivement installés au moins deux condensateurs (C1, C2), notamment à bord d'un aéronef. Ce dispositif comprend au moins un convertisseur statique formé par au moins un organe de couplage électronique, comprenant au moins un transistor (T) et une diode (D), associé à une inductance (L), disposés entre ces au moins deux condensateurs (C1, C2).
PCT/FR2009/051006 2008-05-29 2009-05-28 Dispositif et procede de couplage de deux parties d'un reseau a courant continu notamment dans un aeronef WO2009156654A2 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US12/993,659 US8736099B2 (en) 2008-05-29 2009-05-28 Device and method for coupling two parts of a DC network, particularly in an aircraft
EP09769495A EP2289139A2 (fr) 2008-05-29 2009-05-28 Dispositif et procede de couplage de deux parties d'un reseau a courant continu notamment dans un aeronef

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0853511 2008-05-29
FR0853511A FR2932029B1 (fr) 2008-05-29 2008-05-29 Dispositif et procede de couplage de deux parties d'un reseau a courant continu notamment dans un aeronef

Publications (2)

Publication Number Publication Date
WO2009156654A2 WO2009156654A2 (fr) 2009-12-30
WO2009156654A3 true WO2009156654A3 (fr) 2010-06-03

Family

ID=40518434

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2009/051006 WO2009156654A2 (fr) 2008-05-29 2009-05-28 Dispositif et procede de couplage de deux parties d'un reseau a courant continu notamment dans un aeronef

Country Status (4)

Country Link
US (1) US8736099B2 (fr)
EP (1) EP2289139A2 (fr)
FR (1) FR2932029B1 (fr)
WO (1) WO2009156654A2 (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2947245B1 (fr) 2009-06-29 2012-12-14 Airbus France Systeme et procede d'alimentation electrique d'un aeronef
FR2969861B1 (fr) * 2010-12-28 2014-02-28 Hispano Suiza Sa Module de conversion de tension entre un reseau electrique haute tension d'un aeronef et un element de stockage d'energie
US9484808B2 (en) * 2011-08-24 2016-11-01 Abb Schweiz Ag Bidirectional unisolated DC-DC converter based on cascaded cells
JP5250818B1 (ja) * 2012-05-22 2013-07-31 東洋システム株式会社 フルブリッジ電力変換装置
US10300791B2 (en) * 2015-12-18 2019-05-28 Ge Global Sourcing Llc Trolley interfacing device having a pre-charging unit
WO2021117213A1 (fr) * 2019-12-13 2021-06-17 三菱電機株式会社 Dispositif de conversion de puissance
EP4021149A1 (fr) 2020-12-22 2022-06-29 Textron Systems Corporation Appareil d'éclairage comprenant des del montées en parallèle et des pilotes de del

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5627459A (en) * 1993-04-19 1997-05-06 Fujitsu Limited DC/DC converter
US5982156A (en) * 1997-04-15 1999-11-09 The United States Of America As Represented By The Secretary Of The Air Force Feed-forward control of aircraft bus dc boost converter
EP1298781A1 (fr) * 2001-09-27 2003-04-02 ABB Schweiz AG Dispositif de conversion de puissance et procédé pour adapter une tension continue variable
AT413914B (de) * 2004-02-12 2006-07-15 Felix Dipl Ing Dr Himmelstoss Vorrichtung zur umwandlung einer eingangsspannung in zwei symmetrische, unipolare spannungen

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7372319B1 (en) * 2005-09-16 2008-05-13 National Semiconductor Corporation Constant boosted voltage generator circuit for feedback switches in a switched capacitor circuit
JP5250751B2 (ja) * 2006-10-11 2013-07-31 セミコンダクター・コンポーネンツ・インダストリーズ・リミテッド・ライアビリティ・カンパニー 電圧発生回路
FR2911442B1 (fr) * 2007-01-16 2015-05-15 Airbus France Systeme et procede d'alimentation en puissance pour les actionneurs a bord d'un aeronef
US8193784B2 (en) * 2007-06-15 2012-06-05 Fisher Controls International Llc Bidirectional DC to DC converter for power storage control in a power scavenging application

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5627459A (en) * 1993-04-19 1997-05-06 Fujitsu Limited DC/DC converter
US5982156A (en) * 1997-04-15 1999-11-09 The United States Of America As Represented By The Secretary Of The Air Force Feed-forward control of aircraft bus dc boost converter
EP1298781A1 (fr) * 2001-09-27 2003-04-02 ABB Schweiz AG Dispositif de conversion de puissance et procédé pour adapter une tension continue variable
AT413914B (de) * 2004-02-12 2006-07-15 Felix Dipl Ing Dr Himmelstoss Vorrichtung zur umwandlung einer eingangsspannung in zwei symmetrische, unipolare spannungen

Also Published As

Publication number Publication date
WO2009156654A2 (fr) 2009-12-30
FR2932029A1 (fr) 2009-12-04
EP2289139A2 (fr) 2011-03-02
US20110175441A1 (en) 2011-07-21
US8736099B2 (en) 2014-05-27
FR2932029B1 (fr) 2013-01-11

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