BR112012031489A2 - circuito de fonte de alimentação para um sistema de degelo de aeronave - Google Patents

circuito de fonte de alimentação para um sistema de degelo de aeronave

Info

Publication number
BR112012031489A2
BR112012031489A2 BR112012031489A BR112012031489A BR112012031489A2 BR 112012031489 A2 BR112012031489 A2 BR 112012031489A2 BR 112012031489 A BR112012031489 A BR 112012031489A BR 112012031489 A BR112012031489 A BR 112012031489A BR 112012031489 A2 BR112012031489 A2 BR 112012031489A2
Authority
BR
Brazil
Prior art keywords
aircraft
power supply
supply circuit
defrost system
defrost
Prior art date
Application number
BR112012031489A
Other languages
English (en)
Other versions
BR112012031489B1 (pt
Inventor
Alexis Patouillard
Nicolas Alain Bader
Rachid Boudyaf
Sébastien Daniel Pierron
Original Assignee
Hispano Suiza Sa
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 Hispano Suiza Sa filed Critical Hispano Suiza Sa
Publication of BR112012031489A2 publication Critical patent/BR112012031489A2/pt
Publication of BR112012031489B1 publication Critical patent/BR112012031489B1/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D41/00—Power installations for auxiliary purposes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • 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
    • H02J1/00—Circuit arrangements for dc mains or dc distribution networks
    • H02J1/10—Parallel operation of dc sources
    • 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
    • H02J3/00—Circuit arrangements for ac mains or ac distribution networks
    • H02J3/007—Arrangements for selectively connecting the load or loads to one or several among a plurality of power lines or power sources
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D2221/00—Electric power distribution systems onboard aircraft
    • 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

Abstract

circuito de fonte de alimentação para um sistema de degelo de aeronave. a invenção refere-se a um circuito de abastecimento elétrico de aeronave que inclui: uma rede de distribuição de potência (17), a bordo da aeronave, para dispositivos elétricos (5b) localizados em um motor da aeronave ou próximos ao dito motor; e um gerador de fonte de alimentação (27) construído no interior do motor da aeronave de modo a fornecer tensão de ca potência a um sistema de degelo ou anti-congelamento (5a). o dito circuito de fonte de alimentação de aeronave é caracterizado pelo fato de que o gerador de fonte de alimentação (27) está conectado a um acionador eletromecânico reversor de empuxo (5c) por meio de um retificador (1) para fornecer potência de tensão de cc ao dito acionador.
BR112012031489-0A 2010-06-11 2011-06-06 circuito de fonte de alimentação para um sistema de degelo de aeronave BR112012031489B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1054627A FR2961177B1 (fr) 2010-06-11 2010-06-11 Circuit d'alimentation electrique pour un circuit de degivrage d'un aeronef
FR1054627 2010-06-11
PCT/FR2011/051270 WO2011154645A1 (fr) 2010-06-11 2011-06-06 Circuit d'alimentation electrique pour un circuit de degivrage d'un aeronef.

Publications (2)

Publication Number Publication Date
BR112012031489A2 true BR112012031489A2 (pt) 2016-11-01
BR112012031489B1 BR112012031489B1 (pt) 2021-04-20

Family

ID=43502613

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112012031489-0A BR112012031489B1 (pt) 2010-06-11 2011-06-06 circuito de fonte de alimentação para um sistema de degelo de aeronave

Country Status (10)

Country Link
US (1) US9233759B2 (pt)
EP (1) EP2580122B1 (pt)
JP (1) JP5932782B2 (pt)
CN (1) CN102947183B (pt)
BR (1) BR112012031489B1 (pt)
CA (1) CA2802159C (pt)
ES (1) ES2575659T3 (pt)
FR (1) FR2961177B1 (pt)
RU (1) RU2523303C1 (pt)
WO (1) WO2011154645A1 (pt)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ITRM20120014A1 (it) * 2012-01-17 2013-07-18 Pavel Miodushevsky Convertiplano da plurimpiego.
DE102012201269A1 (de) * 2012-01-30 2013-08-01 Siemens Aktiengesellschaft Wahlweise Steuerung eines Wechselstrommotors oder Gleichstrommotors
CN102590664A (zh) * 2012-02-08 2012-07-18 湖南省电力公司科学研究院 直流融冰装置低压大电流试验平台
FR3017857B1 (fr) * 2014-02-26 2016-04-29 Airbus Helicopters Procede et systeme de traitement du givre pour un parebrise d'un aeronef
US9638044B2 (en) 2014-03-11 2017-05-02 Hamilton Sundstrand Corporation Resistive-inductive propeller blade de-icing system including contactless power supply
FR3056839B1 (fr) * 2016-09-27 2018-10-05 Liebherr-Aerospace Toulouse Sas Reseau electrique et procede de distribution d'energie electrique a alimentation partagee a bord d'un aeronef
FR3058278B1 (fr) * 2016-10-27 2020-02-28 Safran Electrical & Power Systeme pour l'alimentation d'actionneurs electriques embarques dans un aeronef
US10934935B2 (en) * 2017-01-30 2021-03-02 Ge Aviation Systems Llc Engine core assistance
US11465759B2 (en) * 2018-07-13 2022-10-11 The Boeing Company Multi-mode generator for ice protection on aircraft
US10975768B2 (en) * 2018-08-20 2021-04-13 Hamilton Sunstrand Corporation Using aircraft electric icing protection system for electrical power system quality
CN109733615B (zh) * 2018-12-07 2022-07-05 武汉航空仪表有限责任公司 一种飞机电加热除冰控制电路
FR3117550A1 (fr) * 2020-12-11 2022-06-17 Safran Nacelles Dispositif de pilotage d’un système de commande électrique d’inverseur de poussée pour aéronef
US11845388B2 (en) 2021-05-20 2023-12-19 General Electric Company AC electrical power system for a vehicle

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3657514A (en) * 1970-06-03 1972-04-18 Goodrich Co B F Electrical deicer for aircraft propeller
US5899411A (en) * 1996-01-22 1999-05-04 Sundstrand Corporation Aircraft electrical system providing emergency power and electric starting of propulsion engines
US6992403B1 (en) * 2001-03-08 2006-01-31 Pacific Scientific Electric power and start system
US7210653B2 (en) * 2002-10-22 2007-05-01 The Boeing Company Electric-based secondary power system architectures for aircraft
FR2900636B1 (fr) * 2006-05-05 2009-03-06 Hispano Suiza Sa Circuit d'alimentation en energie electrique pour des equipements electriques d'un moteur d'aeronef ou de son environnement
FR2911848B1 (fr) 2007-01-31 2009-12-25 Hispano Suiza Sa Circuit d'alimentation en energie electrique dans un aeronef pour des equipements electriques comprenant un circuit de degivrage
FR2911847B1 (fr) * 2007-01-31 2009-10-23 Hispano Suiza Sa Circuit d'alimentation en energie electrique pour des equipements electriques d'un moteur d'aeronef

Also Published As

Publication number Publication date
FR2961177A1 (fr) 2011-12-16
CN102947183A (zh) 2013-02-27
JP5932782B2 (ja) 2016-06-08
JP2013529567A (ja) 2013-07-22
EP2580122B1 (fr) 2016-04-06
RU2523303C1 (ru) 2014-07-20
CA2802159A1 (fr) 2011-12-15
FR2961177B1 (fr) 2013-02-15
CA2802159C (fr) 2017-08-15
WO2011154645A1 (fr) 2011-12-15
US9233759B2 (en) 2016-01-12
BR112012031489B1 (pt) 2021-04-20
US20130206902A1 (en) 2013-08-15
ES2575659T3 (es) 2016-06-30
RU2013100973A (ru) 2014-07-20
CN102947183B (zh) 2015-09-16
EP2580122A1 (fr) 2013-04-17

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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]
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 06/06/2011, OBSERVADAS AS CONDICOES LEGAIS.