BRPI0704175A - sistema de alimentação de energia elétrica para uma aeronave - Google Patents

sistema de alimentação de energia elétrica para uma aeronave

Info

Publication number
BRPI0704175A
BRPI0704175A BRPI0704175-6A BRPI0704175A BRPI0704175A BR PI0704175 A BRPI0704175 A BR PI0704175A BR PI0704175 A BRPI0704175 A BR PI0704175A BR PI0704175 A BRPI0704175 A BR PI0704175A
Authority
BR
Brazil
Prior art keywords
aircraft
line
voltage
engine
mains
Prior art date
Application number
BRPI0704175-6A
Other languages
English (en)
Inventor
Serge Berenger
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 BRPI0704175A publication Critical patent/BRPI0704175A/pt

Links

Classifications

    • 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
    • H02J3/12—Circuit arrangements for ac mains or ac distribution networks for adjusting voltage in ac networks by changing a characteristic of the network load
    • 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)
  • Control Of Eletrric Generators (AREA)
  • Stand-By Power Supply Arrangements (AREA)
  • Direct Current Feeding And Distribution (AREA)

Abstract

SISTEMA DE ALIMENTAçãO DE ENERGIA ELéTRICA PARA UMA AERONAVE é descrito um gerador principal (112) que distribui uma tensão de CA a uma rede elétrica (210) a bordo do aeroplano por meio de uma linha principal (120) que tem pelo menos um contactador de linha (122) montado nela, a tensão sendo regulada por um regulador (170). Uma rede elétrica do motor (150) distribui eletricidade a várias cargas situadas na zona de um motor montado em uma aeronave e a um computador de controle do motor (130), a rede elétrica do motor (150) tendo uma primeira entrada de alimentação conectada na linha de alimentação de energia elétrica principal (120) por meio de uma linha de alimentação de energia elétrica secundária (124), a montante do contactador de linha (122), a fim de receber diretamente eletricidade derivada do gerador principal sem passar pela rede elétrica (210) a bordo da aeronave. O regulador de tensão (170) que regula a tensão distribuída pelo gerador principal pode situar-se na zona do motor e ser acionado pela rede elétrica do motor (150).
BRPI0704175-6A 2006-11-23 2007-11-23 sistema de alimentação de energia elétrica para uma aeronave BRPI0704175A (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0655072A FR2909233B1 (fr) 2006-11-23 2006-11-23 Alimentation d'un aeronef en energie electrique

Publications (1)

Publication Number Publication Date
BRPI0704175A true BRPI0704175A (pt) 2008-07-08

Family

ID=38255472

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0704175-6A BRPI0704175A (pt) 2006-11-23 2007-11-23 sistema de alimentação de energia elétrica para uma aeronave

Country Status (11)

Country Link
US (1) US20080211237A1 (pt)
EP (1) EP1926194A1 (pt)
JP (1) JP2008127013A (pt)
CN (1) CN101202454A (pt)
BR (1) BRPI0704175A (pt)
CA (1) CA2610636A1 (pt)
FR (1) FR2909233B1 (pt)
IL (1) IL187583A0 (pt)
RU (1) RU2007143382A (pt)
SG (1) SG143195A1 (pt)
ZA (1) ZA200710114B (pt)

Families Citing this family (38)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8027142B2 (en) * 2007-10-25 2011-09-27 Honeywell International Inc. Current-protected driver circuit for ignition exciter unit
US7852049B2 (en) * 2008-04-20 2010-12-14 Hamilton Sundstrand Corporation Dual channel power generation system
US8237416B2 (en) * 2008-12-09 2012-08-07 Hamilton Sundstrand Corporation More electric engine with regulated permanent magnet machines
FR2940245B1 (fr) * 2008-12-22 2011-03-18 Messier Bugatti Architecture de distribution de puissance pour distribuer la puissance a des actionneurs electromecaniques d'un aeronef
CN101710732B (zh) * 2009-11-11 2011-11-16 北京航空航天大学 具有发动机空中重起功能的无人直升机持续稳压供电系统
FR2954283B1 (fr) * 2009-12-23 2012-03-02 Hispano Suiza Sa Aeronef comportant un demarreur-generateur electrique pour le ou chaque turboreacteur et un train d'aterrissage equipe d'un moteur electrique de manoeuvre au sol
US8424416B2 (en) 2010-06-18 2013-04-23 Hamilton Sundstrand Corporation Layshaft generator
FR2962404B1 (fr) 2010-07-08 2012-07-20 Eurocopter France Architecture electrique pour aeronef a voilure tournante a motorisation hybride
CN102520621B (zh) * 2011-11-22 2014-05-21 中国商用飞机有限责任公司 飞机电源系统的模拟控制板
FR2993243B1 (fr) 2012-07-12 2014-07-11 Eurocopter France Architecture d'alimentation hybride en puissance mecanique d'un rotor, geree a partir du reseau de bord d'un giravion
CA2804462C (en) 2012-07-12 2021-05-25 Pratt & Whitney Canada Corp. Aircraft power outtake management
US20140032002A1 (en) * 2012-07-30 2014-01-30 The Boeing Company Electric system stabilizing system for aircraft
GB201219544D0 (en) * 2012-10-31 2012-12-12 Rolls Royce Deutschland Geared compressor for gas turbine engine
GB201219925D0 (en) * 2012-11-06 2012-12-19 Rolls Royce Plc An electrical system for an aircraft
US9657645B2 (en) 2013-02-25 2017-05-23 Pratt & Whitney Canada Corp. Engine architecture using electric machine
JP6152472B2 (ja) * 2013-06-06 2017-06-21 ジーイー・アビエイション・システムズ・エルエルシー ジェットエンジン組立体および電気を発生するための方法
US9413162B2 (en) * 2013-10-11 2016-08-09 The Boeing Company Modular equipment center distributed independent protections
CN103587707B (zh) * 2013-11-15 2015-08-05 中航飞机股份有限公司西安飞机分公司 一种电子飞行仪表供电系统
FR3027058B1 (fr) * 2014-10-13 2016-11-04 Turbomeca Architecture d'un systeme propulsif d'un helicoptere comprenant un turbomoteur hybride et un systeme de reactivation de ce turbomoteur hybride
FR3031635B1 (fr) * 2015-01-08 2018-05-04 Airbus Helicopters Giravion dote d'un equipement electrique regulant l'alimentation en energie electrique d'un turbomoteur en phase de demarrage
US10000296B2 (en) 2015-02-18 2018-06-19 Hamilton Sundstrand Corporation Electrical control system
CN105429127B (zh) * 2015-11-17 2018-04-13 陕西航空电气有限责任公司 一种电起动配电系统
EP3211184B1 (en) * 2016-02-29 2021-05-05 Raytheon Technologies Corporation Bowed rotor prevention system and associated method of bowed rotor prevention
US10227137B2 (en) * 2016-03-22 2019-03-12 Ge Aviation Systems Llc Hybrid power system for an aircraft
CN105978422B (zh) * 2016-06-07 2019-01-25 中国南方航空工业(集团)有限公司 直升机交流电源系统用控制装置
US10787933B2 (en) 2016-06-20 2020-09-29 Raytheon Technologies Corporation Low-power bowed rotor prevention and monitoring system
FR3062250A1 (fr) * 2017-01-24 2018-07-27 Zodiac Aero Electric Architecture de communication de puissance pour un aeronef
CN106972617A (zh) * 2017-03-29 2017-07-21 中国航空无线电电子研究所 应用于模块化航电系统的电源冗余备份装置
CN107140219B (zh) * 2017-03-31 2019-06-21 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种基于智能接触器的多电飞机分布式配电控制架构
CN108121252A (zh) * 2017-12-15 2018-06-05 石家庄飞机工业有限责任公司 一种基于全权数字电子控制系统的飞机电气控制系统
WO2019183428A1 (en) 2018-03-22 2019-09-26 Continental Motors, Inc. Engine ignition timing and power supply system
CN110556781B (zh) * 2018-05-31 2022-08-12 上海航空电器有限公司 单通道多电飞机发电机控制器的联接汇流条差动保护功能结构
KR102336316B1 (ko) * 2018-09-13 2021-12-07 엘에스일렉트릭 (주) 전원 공급 장치 및 전원 공급 시스템
US10589635B1 (en) * 2019-03-01 2020-03-17 The Boeing Company Active voltage control for hybrid electric aircraft
GB201913017D0 (en) * 2019-09-10 2019-10-23 Rolls Royce Plc Electrical system
US11005465B1 (en) * 2020-01-13 2021-05-11 Hamilton Sunstrand Corporation Zero-cross circuit with low phase delay
CN111756284A (zh) * 2020-06-17 2020-10-09 江西洪都航空工业集团有限责任公司 一种双余度设计的双通道飞机发电机控制装置
FR3126076B1 (fr) * 2021-08-09 2023-12-08 Safran Electrical & Power Réseau électrique pour aéronefs à deux points de régulation

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000077916A1 (es) * 1999-06-09 2000-12-21 Lear Automotive (Eeds) Spain, S.L. Sistema de distribucion electrica de tension dual
JP2001119860A (ja) * 1999-10-19 2001-04-27 Toshiba Corp 電力系統電圧調整方法及び装置
DE10232074A1 (de) * 2002-07-15 2004-02-05 Rwe Piller Gmbh Verfahren zur Versorgung einer entfernt angeordneten, variablen Last mit einer konstanten Wechselspannung
US6778414B2 (en) * 2002-12-20 2004-08-17 The Boeing Company Distributed system and methodology of electrical power regulation, conditioning and distribution on an aircraft

Also Published As

Publication number Publication date
CN101202454A (zh) 2008-06-18
EP1926194A1 (fr) 2008-05-28
FR2909233A1 (fr) 2008-05-30
SG143195A1 (en) 2008-06-27
JP2008127013A (ja) 2008-06-05
FR2909233B1 (fr) 2011-03-04
US20080211237A1 (en) 2008-09-04
RU2007143382A (ru) 2009-05-27
CA2610636A1 (fr) 2008-05-23
IL187583A0 (en) 2008-03-20
ZA200710114B (en) 2008-09-25

Similar Documents

Publication Publication Date Title
BRPI0704175A (pt) sistema de alimentação de energia elétrica para uma aeronave
BRPI0800221A (pt) circuito de fonte de alimentação de eletricidade em uma aeronave, e, aeronave
BR102014026540A2 (pt) sistema de potência elétrica
BR112023024233A2 (pt) Isolamento de falha elétrica em uma rede de distribuição de energia de uma aeronave
JP5932782B2 (ja) 航空機の除氷システムのための電力供給回路
GB201118313D0 (en) Thermal electrical power generation for aircraft
BR112015017917A2 (pt) arquitetura para suprir potência elétrica de emergência para uma aeronave, aeronave e método para suprir potência elétrica de emergência em uma aeronave
WO2009032368A3 (en) Power source for an aircraft engine controller
BRPI0606679A2 (pt) dispositivo compensador de energia para uma aeronave
BR112018011381A2 (pt) método para provisão de uma reserva de energia para um sistema de suprimento de energia
BR112023024214A2 (pt) Compartilhamento de carga elétrica variável no tempo em uma rede de distribuição de energia de uma aeronave
KR20160072554A (ko) 선박 제어기 테스트 시스템
BR0212663A (pt) Sistema universal de suprimento de energia
US11578579B2 (en) Wellsite adaptive power management system
US10822116B2 (en) Power distribution network
BR112022023717A2 (pt) Sistema de alimentação de energia e método para controlar sistema de alimentação de energia
CN201509159U (zh) 自供电装置以及电力柜
BR112015028984A2 (pt) dispositivo e processo de assistência para um sistema de geração de energia de uma aeronave
CN103746448A (zh) 运七飞机供电系统
ERMOLAEVA et al. ANALYSIS AND OPTIMIZATION OF OPERATING MODES OF POWER SUPPLY SYSTEMS TRANSFORMER CONNECTIONS
Nicasio Jr Design, Development, and Evaluation of a Microgrid for the Energy Management in a Small Poultry
KR20150025561A (ko) 연료전지를 이용한 고효율 비상 전원 시스템
KR20170054681A (ko) 선박의 발전 시스템
CN206471906U (zh) 一种用于小型飞行器的供电系统
Maltsev et al. Functioning of back-to-back high voltage direct current link model in Tomsk electric power system

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]
B11A Dismissal acc. art.33 of ipl - examination not requested within 36 months of filing
B11Y Definitive dismissal - extension of time limit for request of examination expired [chapter 11.1.1 patent gazette]