BR112015028984A2 - dispositivo e processo de assistência para um sistema de geração de energia de uma aeronave - Google Patents

dispositivo e processo de assistência para um sistema de geração de energia de uma aeronave

Info

Publication number
BR112015028984A2
BR112015028984A2 BR112015028984A BR112015028984A BR112015028984A2 BR 112015028984 A2 BR112015028984 A2 BR 112015028984A2 BR 112015028984 A BR112015028984 A BR 112015028984A BR 112015028984 A BR112015028984 A BR 112015028984A BR 112015028984 A2 BR112015028984 A2 BR 112015028984A2
Authority
BR
Brazil
Prior art keywords
power generation
generation system
contactor
regulator
generator
Prior art date
Application number
BR112015028984A
Other languages
English (en)
Other versions
BR112015028984B1 (pt
Inventor
Chapotin Bruno
Carre Nicolas
Henrard Pierre
Original Assignee
Labinal Power Systems
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 Labinal Power Systems filed Critical Labinal Power Systems
Publication of BR112015028984A2 publication Critical patent/BR112015028984A2/pt
Publication of BR112015028984B1 publication Critical patent/BR112015028984B1/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60R—VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
    • B60R16/00—Electric 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
    • B60R16/02—Electric 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
    • B60R16/03—Electric 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00—Equipment not otherwise provided for
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01H—ELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H47/00—Circuit arrangements not adapted to a particular application of the relay and designed to obtain desired operating characteristics or to provide energising current
    • H01H47/02—Circuit arrangements not adapted to a particular application of the relay and designed to obtain desired operating characteristics or to provide energising current for modifying the operation of the relay
    • H01H47/04—Circuit arrangements not adapted to a particular application of the relay and designed to obtain desired operating characteristics or to provide energising current for modifying the operation of the relay for holding armature in attracted position, e.g. when initial energising circuit is interrupted; for maintaining armature in attracted position, e.g. with reduced energising current
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02H—EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS
    • H02H7/00—Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions
    • H02H7/06—Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions for dynamo-electric generators; for synchronous capacitors
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J3/00—Circuit arrangements for ac mains or ac distribution networks
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J4/00—Circuit arrangements for mains or distribution networks not specified as ac or dc
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D2221/00—Electric power distribution systems onboard aircraft
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01H—ELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H47/00—Circuit arrangements not adapted to a particular application of the relay and designed to obtain desired operating characteristics or to provide energising current
    • H01H47/22—Circuit arrangements not adapted to a particular application of the relay and designed to obtain desired operating characteristics or to provide energising current for supplying energising current for relay coil
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J2310/00—The network for supplying or distributing electric power characterised by its spatial reach or by the load
    • H02J2310/40—The network being an on-board power network, i.e. within a vehicle
    • H02J2310/44—The network being an on-board power network, i.e. within a vehicle for aircrafts

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Eletrric Generators (AREA)
  • Rehabilitation Tools (AREA)

Abstract

1/1 resumo “dispositivo e processo de assistência para um sistema de geração de energia de uma aeronave” a invenção diz respeito a um dispositivo de assistência (17) para um sistema de geração de energia elétrica (11) de uma aeronave, o sistema (11) compreendendo um gerador (13), um regulador (14) e um contator (15) compreendendo contatos e um controle para abrir/fechar os contatos, controlado pelo regulador (14) e arranjado entre o gerador (13) e uma arquitetura de distribuição (12), o dispositivo de assistência sendo caracterizado pelo fato de ser conectado em pelo menos uma fonte de alimentação (18) separada do gerador (13) e do regulador (14), e em que compreende dispositivos para fechar o contator capazes de conectar a fonte de alimentação (18) no controle do contator (15) a fim de fornecer a corrente necessária para fechar o contator (15).
BR112015028984-3A 2013-06-10 2014-06-06 Dispositivo e processo de assistência para um sistema de geração de energia de uma aeronave BR112015028984B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1355347 2013-06-10
FR1355347A FR3006817B1 (fr) 2013-06-10 2013-06-10 Dispositif et procede d'assistance d'un systeme de generation electrique d'un aeronef
PCT/FR2014/051371 WO2014199056A1 (fr) 2013-06-10 2014-06-06 Dispositif et procédé d'assistance d'un système de génération électrique d'un aéronef

Publications (2)

Publication Number Publication Date
BR112015028984A2 true BR112015028984A2 (pt) 2017-07-25
BR112015028984B1 BR112015028984B1 (pt) 2021-10-26

Family

ID=49054778

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015028984-3A BR112015028984B1 (pt) 2013-06-10 2014-06-06 Dispositivo e processo de assistência para um sistema de geração de energia de uma aeronave

Country Status (9)

Country Link
US (1) US9969341B2 (pt)
EP (1) EP3008745B1 (pt)
CN (1) CN105308711B (pt)
BR (1) BR112015028984B1 (pt)
CA (1) CA2912229C (pt)
ES (1) ES2623763T3 (pt)
FR (1) FR3006817B1 (pt)
RU (1) RU2658336C2 (pt)
WO (1) WO2014199056A1 (pt)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10462073B2 (en) * 2015-01-06 2019-10-29 The Boeing Company Aircraft control domain communication framework
FR3093870B1 (fr) * 2019-03-15 2021-04-02 Safran Electrical & Power Système de commande d’un réseau électrique d’avion
CN114228825A (zh) * 2021-12-27 2022-03-25 天津德科智控股份有限公司 一种电动助力转向控制系统以及方法

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4024496A1 (de) * 1990-08-02 1992-02-06 Bosch Gmbh Robert Schaltungsanordnung zum betrieb von elektromagnetischen verbrauchern
EP1220409B1 (en) * 2000-12-28 2012-04-11 ABB Technology AG An improved medium voltage switching device
RU2208258C1 (ru) * 2002-02-06 2003-07-10 Пухов Игорь Константинович Дифференциальное реле
CN2694588Y (zh) * 2004-03-26 2005-04-20 佛山市创电电源设备有限公司 不间断电源双路输入自动切换装置
CN201274407Y (zh) * 2009-01-16 2009-07-15 迪克斯汽车电器(上海)有限公司 用于汽车发电机的过电压保护器
RU95435U1 (ru) * 2009-12-30 2010-06-27 Николай Сергеевич Говоров Комплекс электропитания антенного поста зенитно-ракетного комплекса
CN102754176B (zh) * 2010-02-08 2015-12-02 西门子公司 用于电磁开关设备的装置
JP4978721B2 (ja) * 2010-08-23 2012-07-18 株式会社デンソー 運転支援装置
EP2643842B1 (en) * 2010-11-26 2014-11-19 Renault Trucks Method for piloting a relay on-board an automotive vehicle
US8855952B2 (en) * 2011-01-05 2014-10-07 Hamilton Sundstrand Corporation Ram air turbine with flux regulated permanent magnet generator and testing method
US8232778B1 (en) * 2011-01-28 2012-07-31 Hamilton Sundstrand Corporation Independent, redundant overvoltage protection for a generator
US8615982B2 (en) * 2011-07-05 2013-12-31 Hamilton Sundstrand Corporation Integrated electric variable area fan nozzle thrust reversal actuation system
RU2479908C1 (ru) * 2011-12-28 2013-04-20 Общество с ограниченной ответственностью "Электросистемы" Способ управления одной или несколькими электрогенераторными установками

Also Published As

Publication number Publication date
FR3006817A1 (fr) 2014-12-12
ES2623763T3 (es) 2017-07-12
EP3008745A1 (fr) 2016-04-20
EP3008745B1 (fr) 2017-04-05
WO2014199056A1 (fr) 2014-12-18
RU2015152025A3 (pt) 2018-04-25
RU2658336C2 (ru) 2018-06-20
CA2912229C (fr) 2021-06-22
CN105308711B (zh) 2017-11-07
RU2015152025A (ru) 2017-07-14
US20160129862A1 (en) 2016-05-12
CA2912229A1 (fr) 2014-12-18
CN105308711A (zh) 2016-02-03
FR3006817B1 (fr) 2016-11-18
US9969341B2 (en) 2018-05-15
BR112015028984B1 (pt) 2021-10-26

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B350 Update of information on the portal [chapter 15.35 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 06/06/2014, 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 9A ANUIDADE.

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

Free format text: EM VIRTUDE DA EXTINCAO PUBLICADA NA RPI 2726 DE 04-04-2023 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDA A EXTINCAO DA PATENTE E SEUS CERTIFICADOS, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.