FR2932029B1 - 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

Info

Publication number
FR2932029B1
FR2932029B1 FR0853511A FR0853511A FR2932029B1 FR 2932029 B1 FR2932029 B1 FR 2932029B1 FR 0853511 A FR0853511 A FR 0853511A FR 0853511 A FR0853511 A FR 0853511A FR 2932029 B1 FR2932029 B1 FR 2932029B1
Authority
FR
France
Prior art keywords
aircraft
coupling
parts
current network
continuous current
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.)
Expired - Fee Related
Application number
FR0853511A
Other languages
English (en)
Other versions
FR2932029A1 (fr
Inventor
Olivier Langlois
Lucien Prisse
Larc Aiximeno
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
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 SAS filed Critical Airbus Operations SAS
Priority to FR0853511A priority Critical patent/FR2932029B1/fr
Priority to EP09769495A priority patent/EP2289139A2/fr
Priority to US12/993,659 priority patent/US8736099B2/en
Priority to PCT/FR2009/051006 priority patent/WO2009156654A2/fr
Publication of FR2932029A1 publication Critical patent/FR2932029A1/fr
Application granted granted Critical
Publication of FR2932029B1 publication Critical patent/FR2932029B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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)
FR0853511A 2008-05-29 2008-05-29 Dispositif et procede de couplage de deux parties d'un reseau a courant continu notamment dans un aeronef Expired - Fee Related FR2932029B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
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
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
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
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

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
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
FR2932029A1 FR2932029A1 (fr) 2009-12-04
FR2932029B1 true FR2932029B1 (fr) 2013-01-11

Family

ID=40518434

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0853511A Expired - Fee Related 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

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
EP2748917B1 (fr) * 2011-08-24 2018-05-30 ABB Schweiz AG Convertisseur cc-cc bidirectionnel non-isolé avec des cellules en cascade
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
EP4075657A4 (fr) * 2019-12-13 2022-12-07 Mitsubishi Electric Corporation 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

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06311736A (ja) * 1993-04-19 1994-11-04 Fujitsu Ltd Ｄｃ／ｄｃコンバータ
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
EP1298781B1 (fr) * 2001-09-27 2009-11-04 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
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

Also Published As

Publication number Publication date
US20110175441A1 (en) 2011-07-21
FR2932029A1 (fr) 2009-12-04
WO2009156654A2 (fr) 2009-12-30
WO2009156654A3 (fr) 2010-06-03
US8736099B2 (en) 2014-05-27
EP2289139A2 (fr) 2011-03-02

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Legal Events

Date Code Title Description
CA Change of address

Effective date: 20110916

CD Change of name or company name

Owner name: AIRBUS HOLDING, FR

Effective date: 20110916

CJ Change in legal form

Effective date: 20110916

TP Transmission of property

Owner name: AIRBUS HOLDING, FR

Effective date: 20110913

PLFP Fee payment

Year of fee payment: 9

PLFP Fee payment

Year of fee payment: 10

PLFP Fee payment

Year of fee payment: 11

ST Notification of lapse

Effective date: 20200108