WO2009109714A3 - Circuit et systemes redresseurs de puissance, procède associe, aéronef comprenant de tels circuit ou systemes - Google Patents

Circuit et systemes redresseurs de puissance, procède associe, aéronef comprenant de tels circuit ou systemes Download PDF

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Publication number
WO2009109714A3
WO2009109714A3 PCT/FR2009/000063 FR2009000063W WO2009109714A3 WO 2009109714 A3 WO2009109714 A3 WO 2009109714A3 FR 2009000063 W FR2009000063 W FR 2009000063W WO 2009109714 A3 WO2009109714 A3 WO 2009109714A3
Authority
WO
WIPO (PCT)
Prior art keywords
systems
circuit
terminal
boost
assemblies
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/FR2009/000063
Other languages
English (en)
Other versions
WO2009109714A8 (fr
WO2009109714A2 (fr
Inventor
Marcelo Fernando Iturriz
Frédéric RICHARDEAU
Thierry Antoine Meynard
Hassan Helali
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
Centre National de la Recherche Scientifique CNRS
Institut National Polytechnique de Toulouse INPT
Original Assignee
Airbus Operations SAS
Centre National de la Recherche Scientifique CNRS
Institut National Polytechnique de Toulouse INPT
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, Centre National de la Recherche Scientifique CNRS, Institut National Polytechnique de Toulouse INPT filed Critical Airbus Operations SAS
Priority to CA2713369A priority Critical patent/CA2713369C/fr
Priority to JP2010544754A priority patent/JP5421292B2/ja
Priority to CN200980108162.4A priority patent/CN101965678B/zh
Priority to US12/865,575 priority patent/US8467206B2/en
Priority to EP09716653.2A priority patent/EP2245729B1/fr
Publication of WO2009109714A2 publication Critical patent/WO2009109714A2/fr
Publication of WO2009109714A3 publication Critical patent/WO2009109714A3/fr
Anticipated expiration legal-status Critical
Publication of WO2009109714A8 publication Critical patent/WO2009109714A8/fr
Ceased legal-status Critical Current

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
    • H02M7/00—Conversion of AC power input into DC power output; Conversion of DC power input into AC power output
    • H02M7/02—Conversion of AC power input into DC power output without possibility of reversal
    • H02M7/04—Conversion of AC power input into DC power output without possibility of reversal by static converters
    • H02M7/12—Conversion of AC power input into DC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode
    • H02M7/21—Conversion of AC power input into DC power output without possibility of reversal 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
    • H02M7/217—Conversion of AC power input into DC power output without possibility of reversal 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
    • H02M7/25—Conversion of AC power input into DC power output without possibility of reversal 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 arranged for operation in series, e.g. for multiplication of voltage
    • 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
    • H02M7/00—Conversion of AC power input into DC power output; Conversion of DC power input into AC power output
    • H02M7/02—Conversion of AC power input into DC power output without possibility of reversal
    • H02M7/04—Conversion of AC power input into DC power output without possibility of reversal by static converters
    • H02M7/06—Conversion of AC power input into DC power output without possibility of reversal by static converters using discharge tubes without control electrode or semiconductor devices without control electrode
    • H02M7/10—Conversion of AC power input into DC power output without possibility of reversal by static converters using discharge tubes without control electrode or semiconductor devices without control electrode arranged for operation in series, e.g. for multiplication of voltage

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Dc-Dc Converters (AREA)
  • Rectifiers (AREA)

Abstract

L'invention concerne un circuit redresseur de puissance (30) d'un signal de courant électrique fourni par une source d'alimentation alternative (12), comprenant: deux ensembles de commutation (30a, 30b) distincts agencés pour être connectés à une borne d'alimentation (31 ) de la source, au moins un ensemble de commutation comprenant une pluralité de cellules boost (310a, 310b, 320a, 320b) en cascade, chaque cellule boost comprenant une diode (312a, 312b, 322a, 322b), un moyen interrupteur (314a, 314b, 324a, 324b) et une capacité (316a, 316b, 326a, 326b), les capacités, dites capacités terminales (326a, 326b), des deux cellules boost terminales (320a, 320b) des ensembles de commutation ayant une borne en commun. Le circuit peut notamment comprendre deux ensembles composés de deux cellules boost. Application aux systèmes électriques embarqués dans des aéronefs.
PCT/FR2009/000063 2008-01-31 2009-01-21 Circuit et systemes redresseurs de puissance, procède associe, aéronef comprenant de tels circuit ou systemes Ceased WO2009109714A2 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
CA2713369A CA2713369C (fr) 2008-01-31 2009-01-21 Circuit et systemes redresseurs de puissance, procede associe, aeronef comprenant de tels circuit ou systemes
JP2010544754A JP5421292B2 (ja) 2008-01-31 2009-01-21 電力整流回路とシステム、それに関連した方法、そのような回路やシステムを有する航空機
CN200980108162.4A CN101965678B (zh) 2008-01-31 2009-01-21 功率整流器电路和系统、相关方法、包括此类电路或系统的飞行器
US12/865,575 US8467206B2 (en) 2008-01-31 2009-01-21 Power rectifier circuit and systems, associated method, and aircraft comprising such a circuit or systems
EP09716653.2A EP2245729B1 (fr) 2008-01-31 2009-01-21 Circuit et systemes redresseurs de puissance, procède associe, aéronef comprenant de tels circuit ou systemes

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0850622A FR2927201B1 (fr) 2008-01-31 2008-01-31 Circuit et systemes redresseurs de puissance, procede associe, aeronef comprenant de tels circuit ou systemes
FR0850622 2008-01-31

Publications (3)

Publication Number Publication Date
WO2009109714A2 WO2009109714A2 (fr) 2009-09-11
WO2009109714A3 true WO2009109714A3 (fr) 2009-11-26
WO2009109714A8 WO2009109714A8 (fr) 2010-08-19

Family

ID=39870427

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2009/000063 Ceased WO2009109714A2 (fr) 2008-01-31 2009-01-21 Circuit et systemes redresseurs de puissance, procède associe, aéronef comprenant de tels circuit ou systemes

Country Status (7)

Country Link
US (1) US8467206B2 (fr)
EP (1) EP2245729B1 (fr)
JP (1) JP5421292B2 (fr)
CN (1) CN101965678B (fr)
CA (1) CA2713369C (fr)
FR (1) FR2927201B1 (fr)
WO (1) WO2009109714A2 (fr)

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US20090117872A1 (en) * 2007-11-05 2009-05-07 Jorgenson Joel A Passively powered element with multiple energy harvesting and communication channels
FR2927201B1 (fr) * 2008-01-31 2010-02-12 Airbus France Circuit et systemes redresseurs de puissance, procede associe, aeronef comprenant de tels circuit ou systemes
JP4506891B2 (ja) * 2008-12-23 2010-07-21 ダイキン工業株式会社 電流形電力変換回路
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
US8711594B2 (en) * 2011-08-18 2014-04-29 Hewlett-Packard Development Company, L.P. Asymmetric switching rectifier
US9413268B2 (en) 2012-05-10 2016-08-09 Futurewei Technologies, Inc. Multilevel inverter device and method
CN102891611B (zh) * 2012-06-30 2014-10-08 华为技术有限公司 五电平功率变换器及其控制方法、控制装置
US9252670B2 (en) * 2012-12-19 2016-02-02 General Electric Company Multilevel converter
FR3001592A1 (fr) * 2013-01-29 2014-08-01 Schneider Toshiba Inverter Convertisseur de puissance multi-niveaux
CN105027376B (zh) 2013-03-15 2018-01-26 电力集成公司 具有指示器开关的整流器
CN104682736A (zh) * 2013-12-02 2015-06-03 台达电子企业管理（上海）有限公司 五电平整流器
CN103888004A (zh) * 2014-04-08 2014-06-25 青岛威控电气有限公司 一种用于铁路交直交备用电源的单相pwm整流器
US9973077B2 (en) 2014-08-27 2018-05-15 Schneider Electric It Corporation Delta conversion rectifier
US9685881B2 (en) * 2015-06-04 2017-06-20 Schneider Electric It Corporation AC-DC rectifier system
US9998116B2 (en) * 2015-08-03 2018-06-12 Rockwell Automation Technologies, Inc. Auxiliary commutated silicon-controlled rectifier circuit methods and systems
JP6551041B2 (ja) * 2015-08-19 2019-07-31 富士電機株式会社 交流−直流変換装置
US10103729B2 (en) 2016-09-28 2018-10-16 Rockwell Automation Technologies, Inc. Auxiliary commutated silicon-controlled rectifier circuit methods and systems
DE102018201925A1 (de) 2018-02-07 2019-08-08 Würth Elektronik eiSos Gmbh & Co. KG Vorrichtung zur Gewinnung elektrischer Energie und Energieerzeuger mit einer derartigen Vorrichtung
BR112021018224A2 (pt) 2019-03-19 2021-11-23 Dcbel Inc Carregador de ev com protocolo de carregamento adaptável
CN115051586A (zh) * 2022-06-27 2022-09-13 安徽建筑大学 一种具有两倍电压增益的升压型五电平逆变器
CN119813779B (zh) * 2024-11-15 2025-09-26 广州旭之源科技有限公司 一种级联电路同步整流管控制方法、控制装置及开关电源

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US5119283A (en) * 1991-06-10 1992-06-02 General Electric Company High power factor, voltage-doubler rectifier
JPH07194100A (ja) * 1993-12-28 1995-07-28 Matsushita Electric Ind Co Ltd 昇圧型ｄｃ−ｄｃコンバータの出力スイッチ装置
JPH1169786A (ja) * 1997-08-06 1999-03-09 Matsushita Electric Ind Co Ltd 昇圧型ｄｃ−ｄｃコンバータ
US6147882A (en) * 1998-12-19 2000-11-14 Delta Electronics, Inc. Single-stage input current shaping technique with voltage-doubler rectifier front-end
JP2005073440A (ja) * 2003-08-27 2005-03-17 Oki Data Corp 電源装置
JP2005117873A (ja) * 2003-10-10 2005-04-28 Nec Corp 昇圧ｄｃ−ｄｃコンバータを用いた電源装置および故障検出制御方法
JP2005328646A (ja) * 2004-05-14 2005-11-24 Fujitsu Ten Ltd 直流電源装置
FR2881896A1 (fr) * 2005-02-04 2006-08-11 Airbus France Sas Systeme de generation electrique a frequence fixe a coupleur a induction et utilisation de celui-ci dans un aeronef
FR2897731A1 (fr) * 2006-02-17 2007-08-24 Airbus France Sas Generateur de signaux alternatifs, tels que des signaux de reference, et aeronef equipe d'un tel generateur

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JPS61158698A (ja) * 1984-12-28 1986-07-18 Hitachi Medical Corp インバ−タ式ｘ線装置
JP2801621B2 (ja) * 1988-09-06 1998-09-21 株式会社東芝 Ｐｗｍ制御による電源装置
FR2679715B1 (fr) * 1991-07-25 1993-10-29 Centre Nal Recherc Scientifique Dispositif electronique de conversion d'energie electrique.
JP4369425B2 (ja) * 2003-10-17 2009-11-18 アーベーベー・リサーチ・リミテッド 多数のスイッチング電圧レベルをスイッチングするためのコンバータ回路
FR2897485B1 (fr) * 2006-02-10 2008-06-06 Artus Soc Par Actions Simplifi Convertisseur ac/dc a autotransformateur
JP4538047B2 (ja) * 2007-12-25 2010-09-08 三菱電機株式会社 電力用素子の故障検出装置
FR2927201B1 (fr) * 2008-01-31 2010-02-12 Airbus France Circuit et systemes redresseurs de puissance, procede associe, aeronef comprenant de tels circuit ou systemes
DE102008028952A1 (de) * 2008-06-18 2009-12-24 Abb Ag AC-DC-Zwischenkreis-Wandler mit sehr weitem AC-Eingangsspannungs-Bereich
KR100904299B1 (ko) * 2008-11-03 2009-06-25 주식회사 실리콘마이터스 역률 보상 회로 및 그 구동 방법
US8385091B2 (en) * 2009-08-20 2013-02-26 Electric IT Corporation 3-phase high-power UPS

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5119283A (en) * 1991-06-10 1992-06-02 General Electric Company High power factor, voltage-doubler rectifier
JPH07194100A (ja) * 1993-12-28 1995-07-28 Matsushita Electric Ind Co Ltd 昇圧型ｄｃ−ｄｃコンバータの出力スイッチ装置
JPH1169786A (ja) * 1997-08-06 1999-03-09 Matsushita Electric Ind Co Ltd 昇圧型ｄｃ−ｄｃコンバータ
US6147882A (en) * 1998-12-19 2000-11-14 Delta Electronics, Inc. Single-stage input current shaping technique with voltage-doubler rectifier front-end
JP2005073440A (ja) * 2003-08-27 2005-03-17 Oki Data Corp 電源装置
JP2005117873A (ja) * 2003-10-10 2005-04-28 Nec Corp 昇圧ｄｃ−ｄｃコンバータを用いた電源装置および故障検出制御方法
JP2005328646A (ja) * 2004-05-14 2005-11-24 Fujitsu Ten Ltd 直流電源装置
FR2881896A1 (fr) * 2005-02-04 2006-08-11 Airbus France Sas Systeme de generation electrique a frequence fixe a coupleur a induction et utilisation de celui-ci dans un aeronef
FR2897731A1 (fr) * 2006-02-17 2007-08-24 Airbus France Sas Generateur de signaux alternatifs, tels que des signaux de reference, et aeronef equipe d'un tel generateur

Also Published As

Publication number Publication date
CN101965678B (zh) 2013-07-31
CA2713369C (fr) 2016-11-29
EP2245729A2 (fr) 2010-11-03
EP2245729B1 (fr) 2014-09-10
JP2011511612A (ja) 2011-04-07
US8467206B2 (en) 2013-06-18
CA2713369A1 (fr) 2009-09-11
WO2009109714A8 (fr) 2010-08-19
JP5421292B2 (ja) 2014-02-19
CN101965678A (zh) 2011-02-02
WO2009109714A2 (fr) 2009-09-11
US20110002148A1 (en) 2011-01-06
FR2927201B1 (fr) 2010-02-12
FR2927201A1 (fr) 2009-08-07

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