BRPI0800221A - circuito de fonte de alimentação de eletricidade em uma aeronave, e, aeronave - Google Patents

circuito de fonte de alimentação de eletricidade em uma aeronave, e, aeronave

Info

Publication number
BRPI0800221A
BRPI0800221A BRPI0800221-5A BRPI0800221A BRPI0800221A BR PI0800221 A BRPI0800221 A BR PI0800221A BR PI0800221 A BRPI0800221 A BR PI0800221A BR PI0800221 A BRPI0800221 A BR PI0800221A
Authority
BR
Brazil
Prior art keywords
aircraft
engine
supply circuit
electricity supply
power
Prior art date
Application number
BRPI0800221-5A
Other languages
English (en)
Inventor
Rachid Boudyaf
Antoine Jean-Baptiste Stutz
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 BRPI0800221A publication Critical patent/BRPI0800221A/pt
Publication of BRPI0800221B1 publication Critical patent/BRPI0800221B1/pt

Links

Classifications

    • 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
    • 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
    • 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
    • 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; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0233—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Eletrric Generators (AREA)
  • Emergency Protection Circuit Devices (AREA)
  • Direct Current Feeding And Distribution (AREA)

Abstract

CIRCUITO DE FONTE DE ALIMENTAçãO DE ELETRICIDADE EM UMA AERONAVE, E, AERONAVE. A invenção relaciona-se a um circuito de fonte de alimentação em uma aeronave, o circuito incluindo uma rede de distribuição de eletricidade 17 a bordo da aeronave para acionar equipamento elétrico 5b situado em um motor da aeronave ou nos arredores de dito motor e um gerador de fonte de alimentação 27 integrado no motor da aeronave para acionar um circuito de degelo 5a. O equipamento elétrico inclui cargas de nacela 5b conectadas a um barramento de distribuição de tensão de CC 35, ele mesmo estando conectado a um circuito de conversor de tensão 34 acionado pela rede de distribuição 17. O circuito de degelo 5a inclui pelo menos uma resistência elétrica 61 para dissipar eletricidade possivelmente retornada ao barramento de distribuição de tensão de CC 35 por pelo menos algumas das cargas de nacela.
BRPI0800221-5A 2007-01-31 2008-01-30 Circuito de fonte de alimentação de eletricidade em uma aeronave BRPI0800221B1 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0752986 2007-01-31
FR0752986A FR2911848B1 (fr) 2007-01-31 2007-01-31 Circuit d'alimentation en energie electrique dans un aeronef pour des equipements electriques comprenant un circuit de degivrage

Publications (2)

Publication Number Publication Date
BRPI0800221A true BRPI0800221A (pt) 2008-09-16
BRPI0800221B1 BRPI0800221B1 (pt) 2020-02-11

Family

ID=38330118

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0800221-5A BRPI0800221B1 (pt) 2007-01-31 2008-01-30 Circuito de fonte de alimentação de eletricidade em uma aeronave

Country Status (17)

Country Link
US (1) US7936082B2 (pt)
EP (1) EP1953085B1 (pt)
JP (1) JP5247168B2 (pt)
CN (1) CN101234672B (pt)
AT (1) ATE467559T1 (pt)
BR (1) BRPI0800221B1 (pt)
CA (1) CA2619541C (pt)
DE (1) DE602008001166D1 (pt)
ES (1) ES2346107T3 (pt)
FR (1) FR2911848B1 (pt)
IL (1) IL189114A (pt)
MA (1) MA29728B1 (pt)
MX (1) MX2008001442A (pt)
RU (1) RU2450955C2 (pt)
SG (2) SG144890A1 (pt)
UA (1) UA94714C2 (pt)
ZA (1) ZA200801001B (pt)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2920143B1 (fr) * 2007-08-20 2010-01-22 Aircelle Sa Dispositif de commande des actionneurs de maintenance de capots d'une nacelle de turboreacteur
FR2927310B1 (fr) * 2008-02-13 2010-07-30 Aircelle Sa Systeme de commande pour nacelle de turboreacteur
US20110273010A1 (en) * 2008-04-09 2011-11-10 Thales Electrical network
KR20090127614A (ko) 2008-06-09 2009-12-14 삼성전기주식회사 광도파로, 이를 구비한 광 인쇄회로기판 및 그들의 제조방법
FR2943038B1 (fr) 2009-03-13 2012-07-27 Aircelle Sa Dispositif de degivrage,notamment pour nacelle d'aeronef
FR2948337B1 (fr) * 2009-07-24 2011-07-29 Aircelle Sa Circuit d'alimentation electrique pour nacelle de turboreacteur
GB0919041D0 (en) 2009-10-30 2009-12-16 Goodrich Control Sys Power distribution apparatus
FR2961177B1 (fr) * 2010-06-11 2013-02-15 Hispano Suiza Sa Circuit d'alimentation electrique pour un circuit de degivrage d'un aeronef
FR2962271B1 (fr) * 2010-07-02 2012-08-17 Hispano Suiza Sa Alimentation electrique des equipements portes par un support rotatif
GB2483696B (en) 2010-09-17 2015-03-25 Ge Aviat Systems Ltd An aircraft with a power distribution system
FR2967318B1 (fr) * 2010-11-10 2013-07-19 Hispano Suiza Sa Circuit d'alimentation pour un aeronef incluant une machine asynchrone
US9296483B2 (en) 2011-07-05 2016-03-29 Bell Helicopter Textron Inc. Distributed ice protection control system
FR2978878B1 (fr) * 2011-08-04 2013-08-09 Hispano Suiza Sa Dispositif d'alimentation electrique d'un aeronef au sol.
GB2495917B (en) * 2011-10-24 2014-10-22 Ge Aviat Systems Ltd Multiple source electrical power distribution in aircraft
FR2988694B1 (fr) * 2012-03-30 2014-03-28 Hispano Suiza Sa Dispositif d'alimentation electrique d'un aeronef au sol
US20140032002A1 (en) * 2012-07-30 2014-01-30 The Boeing Company Electric system stabilizing system for aircraft
BR112015010408A2 (pt) * 2012-11-08 2017-07-11 Saab Ab disposição de degelo e método para degelar um elemento estrutural
FR3000724B1 (fr) 2013-01-07 2015-01-02 Aircelle Sa Architecture degivrage electrique a haute disponibilite d'entree d'air de nacelle a etages commutes
FR3001443B1 (fr) * 2013-01-30 2016-05-27 Microturbo Procede et systeme d'alimentation en energie electrique d'un aeronef
RU2524776C1 (ru) * 2013-03-27 2014-08-10 Открытое акционерное общество "Электропривод" Способ запуска газотурбинного двигателя бесконтактным явнополюсным синхронным генератором с вращающимся выпрямителем
US9765640B2 (en) 2014-05-29 2017-09-19 Rolls-Royce Corporation System and method to manage transients for rapid power demand changes
US10377498B2 (en) * 2016-01-21 2019-08-13 The Boeing Company Aircraft and associated method for providing electrical energy to an anti-icing system
US10794295B2 (en) 2016-03-15 2020-10-06 Hamilton Sunstrand Corporation Engine bleed system with multi-tap bleed array
US11473497B2 (en) * 2016-03-15 2022-10-18 Hamilton Sundstrand Corporation Engine bleed system with motorized compressor
US20170268430A1 (en) * 2016-03-15 2017-09-21 Hamilton Sundstrand Corporation Engine bleed system with turbo-compressor
CN108082496B (zh) * 2017-11-21 2020-03-24 武汉航空仪表有限责任公司 一种谐振式结冰探测器的驱动电路
FR3079820B1 (fr) * 2018-04-09 2020-04-17 Safran Electrical & Power Systeme et procede de demarrage/generation pour turbomachine d'aeronef
EP3578464A1 (en) 2018-06-06 2019-12-11 Bombardier Inc. Electrical system for aircraft
US11465759B2 (en) * 2018-07-13 2022-10-11 The Boeing Company Multi-mode generator for ice protection on aircraft

Family Cites Families (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2566618A (en) * 1947-11-25 1951-09-04 Armstrong Siddeley Motors Ltd Turbine driving aircraft accessory
FR2281273A1 (fr) * 1974-08-05 1976-03-05 Bronzavia Sa Dispositif antigivrage d'une helice d'avion
DE3164856D1 (en) * 1980-05-08 1984-08-23 Lucas Ind Plc Switching system for sequential connection of loads to an electrical supply
US4473752A (en) * 1982-05-27 1984-09-25 Lockheed Corporation Aircraft engine starting with synchronous ac generator
JPS63245504A (ja) * 1987-01-15 1988-10-12 ザ　ビー．エフ．グッドリッチ　カンパニー 除氷方法およびその装置
US4959605A (en) * 1988-11-22 1990-09-25 Sundstrand Corporation Hybrid permanent magnet and variable reluctance generator
SU1817623A1 (ru) * 1991-04-29 1995-09-20 Авиационный научно-технический комплекс им.А.Н.Туполева Система электроснабжения летательного аппарата
RU2093426C1 (ru) * 1996-03-21 1997-10-20 Йелстаун Корпорейшн Н.В. Тепловая противообледенительная система вращаемого элемента
US5929537A (en) * 1997-06-30 1999-07-27 Sundstrand Corporation PMG main engine starter/generator system
US6249428B1 (en) * 1999-01-15 2001-06-19 Dell Usa, L.P. Method and apparatus for mounting a component and heat sink
US6130820A (en) * 1999-05-04 2000-10-10 Intel Corporation Memory card cooling device
US6269001B1 (en) * 2000-04-20 2001-07-31 International Business Machines Corporation System for enhanced cooling and latching of pluggable electronic component
US6992403B1 (en) * 2001-03-08 2006-01-31 Pacific Scientific Electric power and start system
US6769874B2 (en) * 2002-03-15 2004-08-03 Hamilton Sundstrand Permanent magnet alternator for a gas turbine engine
US6906479B2 (en) * 2002-08-06 2005-06-14 Honeywell International, Inc. Gas turbine engine starter generator with multiple windings on each exciter stator pole
US7286355B2 (en) * 2002-09-11 2007-10-23 Kioan Cheon Cooling system for electronic devices
US7210653B2 (en) * 2002-10-22 2007-05-01 The Boeing Company Electric-based secondary power system architectures for aircraft
TWI229253B (en) * 2003-01-08 2005-03-11 Ma Lab Inc Structural improvement for removable cooler
US7254465B2 (en) * 2004-06-04 2007-08-07 Honeywell International, Inc. No-break-power-transfer control system for variable frequency electrical power systems
US7439634B2 (en) * 2004-08-24 2008-10-21 Honeywell International Inc. Electrical starting, generation, conversion and distribution system architecture for a more electric vehicle
US7221569B2 (en) * 2004-09-15 2007-05-22 Comptake Technology Co., Ltd. Memory heat-dissipating device
US7448460B2 (en) * 2004-09-28 2008-11-11 Oshkosh Corporation Power takeoff for an electric vehicle
FR2882200B1 (fr) * 2005-02-17 2015-05-01 Hispano Suiza Sa Alimentation electrique d'equipements d'un moteur d'avion a turbine a gaz
ATE486779T1 (de) * 2005-06-22 2010-11-15 Airbus Operations Sas Antivereisungs- und enteisungssystem für ein flugzeugmotorengehäuse mit widerstandsmatte
US7480147B2 (en) * 2006-10-13 2009-01-20 Dell Products L.P. Heat dissipation apparatus utilizing empty component slot
US7447024B1 (en) * 2007-07-17 2008-11-04 Kuan-Yin Chou Heat sink for a memory
US20090219687A1 (en) * 2008-03-03 2009-09-03 Jui-Nan Lin Memory heat-dissipating mechanism

Also Published As

Publication number Publication date
UA94714C2 (ru) 2011-06-10
EP1953085B1 (fr) 2010-05-12
JP2008207792A (ja) 2008-09-11
JP5247168B2 (ja) 2013-07-24
US7936082B2 (en) 2011-05-03
EP1953085A1 (fr) 2008-08-06
MA29728B1 (fr) 2008-09-01
SG164372A1 (en) 2010-09-29
ZA200801001B (en) 2008-11-26
SG144890A1 (en) 2008-08-28
DE602008001166D1 (de) 2010-06-24
CN101234672B (zh) 2013-12-18
ATE467559T1 (de) 2010-05-15
MX2008001442A (es) 2009-02-24
FR2911848B1 (fr) 2009-12-25
CA2619541A1 (fr) 2008-07-31
CA2619541C (fr) 2014-08-05
US20100283319A1 (en) 2010-11-11
CN101234672A (zh) 2008-08-06
RU2008103650A (ru) 2009-08-10
FR2911848A1 (fr) 2008-08-01
ES2346107T3 (es) 2010-10-08
RU2450955C2 (ru) 2012-05-20
BRPI0800221B1 (pt) 2020-02-11
IL189114A0 (en) 2008-11-03
IL189114A (en) 2011-10-31

Similar Documents

Publication Publication Date Title
BRPI0800221A (pt) circuito de fonte de alimentação de eletricidade em uma aeronave, e, aeronave
RU2013100973A (ru) Цепь подачи мощности для противообледенительной системы летательного аппарата
UA89082C2 (ru) Устройство электрического питания и приведения в действие газотурбинного двигателя самолета
BRPI0704175A (pt) sistema de alimentação de energia elétrica para uma aeronave
BR112014001457A2 (pt) dispositivo de alimentação elétrica de uma aeronave em solo
WO2010079308A3 (fr) Systeme electrique de demarrage des moteurs d'un aeronef.
AR091747A1 (es) Procedimiento y dispositivo para alimentar energia electrica en una red de suministro electrico
ATE462216T1 (de) Systeme zur elektromechanischen energieumwandlung
AR091748A1 (es) Procedimiento para controlar un generador electrico
SG136937A1 (en) A system for powering and controlling electrical equipment of an aircraft engine or its environment
GB201118313D0 (en) Thermal electrical power generation for aircraft
EA201170523A1 (ru) Устройство аварийного электропитания
WO2014178079A3 (en) Led lighting systems using compressed air based power generation and a method thereof
ATE526721T1 (de) Vorrichtung zur einspeisung elektrischer energie in ein energieversorgungsnetz und gleichspannungswandler für eine solche vorrichtung
DK1914162T3 (da) Jævnstrømsfordelingssystem
BR112012031452A2 (pt) sistemas de distribuição de energia elétrica
SG136938A1 (en) An electrical power supply arrangement for an aircraft
BR112014027729A2 (pt) sistema para o fornecimento de energia elétrica e controle para pelo menos um motor/gerador de helicóptero
GB201113078D0 (en) An aircraft interior power converter
BR112014002892A2 (pt) disposição para fornecer uma corrente ca a uma carga para aquecimento elétrico, disposição serial, disposição de aquecimento de duto e fonte de alimentação e aquecimento elétrico direto
WO2011115419A3 (ko) 분해 조립식 태양광 및 풍력 발전장치
EP2040370A3 (en) Generator for gas turbine engine having main DC bus and accessory AC bus
GEP20156367B (en) Wind based load isolated electrical charging system
RU2009140152A (ru) Устройство и способ для подачи энергии к критичной нагрузке
MX2012012731A (es) Sistema de control de velocidad de turbina tolerante a la falla.

Legal Events

Date Code Title Description
B03A Publication of a patent application or of a certificate of addition of invention [chapter 3.1 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: 10 (DEZ) ANOS CONTADOS A PARTIR DE 11/02/2020, OBSERVADAS AS CONDICOES LEGAIS.