BRPI1013743A2 - circuito de alimentação de um motor elétrico e orgão de comando vôo de uma aeronave - Google Patents

circuito de alimentação de um motor elétrico e orgão de comando vôo de uma aeronave

Info

Publication number
BRPI1013743A2
BRPI1013743A2 BRPI1013743A BRPI1013743A BRPI1013743A2 BR PI1013743 A2 BRPI1013743 A2 BR PI1013743A2 BR PI1013743 A BRPI1013743 A BR PI1013743A BR PI1013743 A BRPI1013743 A BR PI1013743A BR PI1013743 A2 BRPI1013743 A2 BR PI1013743A2
Authority
BR
Brazil
Prior art keywords
aircraft
electric motor
power circuit
flight control
flight
Prior art date
Application number
BRPI1013743A
Other languages
English (en)
Inventor
Roland Casimir
Tony Fourmont
Original Assignee
Sagem Defense Securite
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 Sagem Defense Securite filed Critical Sagem Defense Securite
Publication of BRPI1013743A2 publication Critical patent/BRPI1013743A2/pt
Publication of BRPI1013743B1 publication Critical patent/BRPI1013743B1/pt

Links

Classifications

    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02MAPPARATUS 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
    • H02M7/00Conversion of ac power input into dc power output; Conversion of dc power input into ac power output
    • H02M7/42Conversion of dc power input into ac power output without possibility of reversal
    • H02M7/44Conversion of dc power input into ac power output without possibility of reversal by static converters
    • H02M7/48Conversion of dc power input into ac power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode
    • H02M7/53Conversion of dc power input into ac 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
    • H02M7/537Conversion of dc power input into ac 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, e.g. single switched pulse inverters
    • H02M7/5387Conversion of dc power input into ac 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, e.g. single switched pulse inverters in a bridge configuration
    • H02M7/5388Conversion of dc power input into ac 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, e.g. single switched pulse inverters in a bridge configuration with asymmetrical configuration of switches

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Stopping Of Electric Motors (AREA)
  • Control Of Direct Current Motors (AREA)
BRPI1013743-2A 2009-04-03 2010-03-30 Circuito de alimentação de um motor elétrico e dispositivo de comando vôo de uma aeronave BRPI1013743B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0901630A FR2944166B1 (fr) 2009-04-03 2009-04-03 Circuit d'alimentation d'un moteur et organe de commande de vol equipe d'un tel circuit
FR09/01630 2009-04-03
PCT/EP2010/054225 WO2010112514A1 (fr) 2009-04-03 2010-03-30 Circuit d'alimentation d'un moteur et organe de commande de vol equipé d'un tel circuit

Publications (2)

Publication Number Publication Date
BRPI1013743A2 true BRPI1013743A2 (pt) 2016-04-05
BRPI1013743B1 BRPI1013743B1 (pt) 2019-04-24

Family

ID=41510931

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI1013743-2A BRPI1013743B1 (pt) 2009-04-03 2010-03-30 Circuito de alimentação de um motor elétrico e dispositivo de comando vôo de uma aeronave

Country Status (7)

Country Link
US (1) US8669733B2 (pt)
EP (1) EP2415149B1 (pt)
CN (1) CN102369656B (pt)
BR (1) BRPI1013743B1 (pt)
CA (1) CA2757348C (pt)
FR (1) FR2944166B1 (pt)
WO (1) WO2010112514A1 (pt)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2916032B1 (en) 2014-03-05 2019-08-14 Goodrich Actuation Systems SAS Disengageable damping assemblies for moving aerodynamic surfaces
EP2924850B1 (en) 2014-03-28 2021-05-19 Goodrich Actuation Systems SAS Motor with damping means
US9876456B2 (en) * 2016-06-01 2018-01-23 Abb Schweiz Ag Brushless electrical machine
FR3061135B1 (fr) * 2016-12-23 2019-05-24 Safran Electronics & Defense Surface mobile de vol ayant au moins un actionneur integre
US11440673B2 (en) * 2019-11-19 2022-09-13 Ge Aviation Systems Llc Aircraft propulsion system with voltage regulator
CN115313926B (zh) * 2022-08-30 2023-12-12 兰州空间技术物理研究所 一种双步进电机负载阻尼控制方法

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE69316692T2 (de) * 1992-10-02 1998-08-27 Hitachi Ltd Wechselrichter für ein elektrisches Betriebsmittel
US6058031A (en) * 1997-10-23 2000-05-02 General Electric Company Five level high power motor drive converter and control system
KR100534107B1 (ko) * 2003-02-14 2005-12-08 삼성전자주식회사 모터전원공급장치
DE102005009376A1 (de) * 2005-03-01 2006-05-04 Siemens Ag Halbleitermodul mit integrierten Dämpfungswiderständen
GB2427968A (en) * 2005-06-29 2007-01-10 Tyco Electronics A full bridge circuit
JP4798541B2 (ja) * 2005-11-14 2011-10-19 株式会社安川電機 電力変換装置
JP4830462B2 (ja) * 2005-11-18 2011-12-07 トヨタ自動車株式会社 電動車両の制御装置
JP5230068B2 (ja) * 2006-01-13 2013-07-10 オムロンオートモーティブエレクトロニクス株式会社 インバータ装置
JP4772542B2 (ja) * 2006-03-15 2011-09-14 株式会社東芝 電力変換装置
JP5109290B2 (ja) * 2006-05-30 2012-12-26 トヨタ自動車株式会社 電動機駆動制御システムおよびその制御方法

Also Published As

Publication number Publication date
EP2415149B1 (fr) 2015-05-06
EP2415149A1 (fr) 2012-02-08
WO2010112514A1 (fr) 2010-10-07
CN102369656B (zh) 2014-01-29
FR2944166B1 (fr) 2011-03-18
CA2757348A1 (fr) 2010-10-07
CA2757348C (fr) 2015-04-28
FR2944166A1 (fr) 2010-10-08
BRPI1013743B1 (pt) 2019-04-24
CN102369656A (zh) 2012-03-07
US8669733B2 (en) 2014-03-11
US20120038302A1 (en) 2012-02-16

Similar Documents

Publication Publication Date Title
BRPI0920950A2 (pt) aeronave e método de controlar a direção a direção de vôo de uma aeronave
GB201219922D0 (en) Method of controlling an aircraft electrical power generation system
PT2532081E (pt) Módulo de comutação para limitar e/ou quebrar a corrente de uma linha de energia elétrica
EP2973927A4 (en) Electric power system control with measurement of energy demand and energy efficiency using t - distributions
BRPI1013743A2 (pt) circuito de alimentação de um motor elétrico e orgão de comando vôo de uma aeronave
BR112013010666A2 (pt) método de produção de uma unidade de isolamento e unidade isolante
PL2347956T3 (pl) Pomocnicza jednostka zasilająca (APU) statku powietrznego
DE112013003232T8 (de) PTC-Heizvorrichtung ohne elektronische Leistungsregelung
DE112014005234A5 (de) Bordnetz-Leistungssteuerungsschaltung und Bordnetz
BRPI1012150A2 (pt) método de fabricar um fuselagem de aeronave e uma fuselagem de aeronave
IL224986A (en) High current regulator circuit and high voltage
PT2830178E (pt) Circuito para proteção térmica e de controlo de energia de motores elétricos
BR112012003082A2 (pt) articulação para uma unidade de sistema de distribuição de potência de aeronave e unidade de sistema de distribuição de potência para uma aeronave
BR112012004277A2 (pt) rede elétrica de um avião e método de operação da rede elétrica
EP3025899A4 (en) Detachable high-voltage isolation structure of medium-sized electric vehicle
FR2992796B1 (fr) Dispositif de ventilation et d'alimentation electrique d'un calculateur de moteur d'aeronef
BR112013023729A2 (pt) alimentação em energia elétrica de uma aeronave
BR112014016498A2 (pt) sistema de controle elétrico analógico; dispositivo de energia conectado eletricamente; e controlador opto-programado
TWI366975B (en) Control device of electric power inverter
HK1178693A1 (en) Adjustment device and an electric drive of an elevator
EP2547616A4 (en) Method and device for the startup of an electric drive of an elevator
BR112013028386A2 (pt) circuito impresso destinado a garantir a ligação de um motor elétrico e motor elétrico compreendendo o circuito impresso
GB201000149D0 (en) Aircraft power supply and method of operating the same
DE602008000551D1 (de) Elektrischer Stellantrieb zur Flugsteuerung eines Flugzeugs
DE102011003405B8 (de) Mehrkernprozessor und diesen verwendenden Bordeigene elektronische Steuereinheit

Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06A Patent application procedure suspended [chapter 6.1 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 30/03/2010, OBSERVADAS AS CONDICOES LEGAIS. (CO) 20 (VINTE) ANOS CONTADOS A PARTIR DE 30/03/2010, OBSERVADAS AS CONDICOES LEGAIS

B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time

Free format text: REFERENTE A 10A ANUIDADE.

B24J Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12)

Free format text: REFERENTE AO DESPACHO 21.6 PUBLICADO NA RPI 2560 DE 2020-01-28