BR102012026464A2 - Método para fornecer energia elétrica para uma aeronave e sistema de distribuição de energia elétrica para uma aeronave - Google Patents

Método para fornecer energia elétrica para uma aeronave e sistema de distribuição de energia elétrica para uma aeronave

Info

Publication number
BR102012026464A2
BR102012026464A2 BRBR102012026464-1A BR102012026464A BR102012026464A2 BR 102012026464 A2 BR102012026464 A2 BR 102012026464A2 BR 102012026464 A BR102012026464 A BR 102012026464A BR 102012026464 A2 BR102012026464 A2 BR 102012026464A2
Authority
BR
Brazil
Prior art keywords
aircraft
electric power
distribution system
power
power distribution
Prior art date
Application number
BRBR102012026464-1A
Other languages
English (en)
Inventor
Adrian Shipley
Simon Jeremy Linacre
Victor Bernard Bonneau
Original Assignee
Ge Aviat Systems Ltd
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 Ge Aviat Systems Ltd filed Critical Ge Aviat Systems Ltd
Publication of BR102012026464A2 publication Critical patent/BR102012026464A2/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
    • H02J9/00—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting
    • H02J9/04—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source
    • H02J9/06—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source with automatic change-over, e.g. UPS systems
    • 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
    • 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
    • H02J3/38—Arrangements for parallely feeding a single network by two or more generators, converters or transformers
    • 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
    • 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
    • H02J9/00—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting
    • H02J9/04—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source
    • 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
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J2300/00—Systems for supplying or distributing electric power characterised by decentralized, dispersed, or local generation
    • H02J2300/30—The power source being a fuel cell
    • 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
    • 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
    • Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
    • Y02B90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02B90/10—Applications of fuel cells in buildings

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Supply And Distribution Of Alternating Current (AREA)
  • Stand-By Power Supply Arrangements (AREA)
  • Fuel Cell (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)

Abstract

MÉTODO PARA FORNECER ENERGIA ELÉTRICA PARA UMA AERONAVE E SISTEMA DE DISTRIBUIÇÃO DE ENERGIA ELÉTRICA PARA UMA AERONAVE Trata-se de um método que compreende fornecer energia elétrica para uma aeronave, que compreende abastecer energia seletivamente a partir de uma pluralidade de fontes de energia, em que as fontes de energia incluem um ou mais geradores (2, 3, 4, 5) acionados por um motor, e pelo menos outra fonte de energia selecionada do grupo que compreende um ou mais meios de armazenamento elétrico (23, 26), uma ou mais células de combustível (24, 25) e uma ou mais fontes de energia termoelétrica (22, 27). Um sistema de distribuição de energia correspondente é revelado no presente documento.
BRBR102012026464-1A 2011-10-24 2012-10-16 Método para fornecer energia elétrica para uma aeronave e sistema de distribuição de energia elétrica para uma aeronave BR102012026464A2 (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1118314.2A GB2495917B (en) 2011-10-24 2011-10-24 Multiple source electrical power distribution in aircraft

Publications (1)

Publication Number Publication Date
BR102012026464A2 true BR102012026464A2 (pt) 2014-06-24

Family

ID=45373307

Family Applications (1)

Application Number Title Priority Date Filing Date
BRBR102012026464-1A BR102012026464A2 (pt) 2011-10-24 2012-10-16 Método para fornecer energia elétrica para uma aeronave e sistema de distribuição de energia elétrica para uma aeronave

Country Status (8)

Country Link
US (1) US20130099560A1 (pt)
JP (1) JP6159073B2 (pt)
CN (1) CN103057716B (pt)
BR (1) BR102012026464A2 (pt)
CA (1) CA2792595A1 (pt)
DE (1) DE102012109990A1 (pt)
FR (1) FR2981808A1 (pt)
GB (1) GB2495917B (pt)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10128662B2 (en) 2013-09-09 2018-11-13 Ge Aviation Systems Llc Power system for an aircraft with dual hybrid energy sources
GB2520024B (en) 2013-11-06 2016-02-03 Ge Aviat Systems Ltd Electrical power system for an aircraft
CN104659900B (zh) * 2013-11-25 2017-03-15 中国直升机设计研究所 无人直升机电源系统
CN103847970B (zh) * 2014-03-28 2015-12-09 北京理工大学 一种基于功率跟随的混合动力无人机能源控制方法
US20160211673A1 (en) * 2015-01-16 2016-07-21 Hamilton Sundstrand Corporation Localized source selection and power conversion power distribution system
US10090676B2 (en) 2015-06-03 2018-10-02 Northrop Grumman Systems Corporation Aircraft DC power distribution systems and methods
US10899466B2 (en) 2015-09-02 2021-01-26 Bae Systems Plc Electrical power supply on a vehicle
WO2017037434A1 (en) 2015-09-02 2017-03-09 Bae Systems Plc A vehicle comprising an engine restart system
CN107922055B (zh) * 2015-09-11 2021-10-08 庞巴迪公司 在可用功率有限的条件下在航空器上分配电功率的装置和方法
US10214417B2 (en) 2016-02-25 2019-02-26 Ge Aviation Systems Llc Solid hydrogen reaction system and method of liberation of hydrogen gas
GB2557292B (en) * 2016-12-05 2020-09-02 Ge Aviat Systems Ltd Method and apparatus for operating a power system architecture
GB2559956B (en) * 2017-02-15 2020-09-16 Ge Aviat Systems Ltd Power distribution node for a power architecture
US11970062B2 (en) 2017-04-05 2024-04-30 Ge Aviation Systems Llc Systems and methods of power allocation for hybrid electric architecture
US10530153B2 (en) * 2017-05-23 2020-01-07 Ge Aviation Systems Llc Method and apparatus for operating a power system architecture
CN109747848B (zh) * 2017-11-03 2021-04-02 海鹰航空通用装备有限责任公司 无人机电源组件管理系统、管理方法及无人机
EP3814861B1 (en) 2018-06-29 2022-10-19 BAE SYSTEMS plc Load controller
US11198515B2 (en) 2018-09-11 2021-12-14 Embraer S.A. Method and system for distributed electrical loads connected to shared power sources
US11008993B2 (en) * 2018-09-21 2021-05-18 Caterpillar Inc. Single solid state power supply for multiple engine systems
CN111186317A (zh) * 2018-11-14 2020-05-22 长城汽车股份有限公司 选择能量供应路径的方法、系统及燃料电池车辆
US11498691B2 (en) * 2019-04-04 2022-11-15 Hamilton Sundstrand Corporation Redundant systems for vehicle critical systems
FR3127980A1 (fr) * 2021-10-07 2023-04-14 Safran Electrical & Power Système de distribution d’énergie électrique générée par une turbomachine
US11794912B2 (en) 2022-01-04 2023-10-24 General Electric Company Systems and methods for reducing emissions with a fuel cell
US11719441B2 (en) 2022-01-04 2023-08-08 General Electric Company Systems and methods for providing output products to a combustion chamber of a gas turbine engine
US11933216B2 (en) 2022-01-04 2024-03-19 General Electric Company Systems and methods for providing output products to a combustion chamber of a gas turbine engine
US11970282B2 (en) 2022-01-05 2024-04-30 General Electric Company Aircraft thrust management with a fuel cell
US11804607B2 (en) 2022-01-21 2023-10-31 General Electric Company Cooling of a fuel cell assembly
US11967743B2 (en) 2022-02-21 2024-04-23 General Electric Company Modular fuel cell assembly
US11817700B1 (en) 2022-07-20 2023-11-14 General Electric Company Decentralized electrical power allocation system
US11923586B1 (en) 2022-11-10 2024-03-05 General Electric Company Gas turbine combustion section having an integrated fuel cell assembly
US11859820B1 (en) 2022-11-10 2024-01-02 General Electric Company Gas turbine combustion section having an integrated fuel cell assembly

Family Cites Families (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5442905A (en) * 1994-04-08 1995-08-22 Alliedsignal Inc. Integrated power and cooling environmental control system
GB9412261D0 (en) * 1994-06-18 1994-08-10 Smiths Industries Plc Electrical systems
AU2001239730A1 (en) * 2000-02-18 2001-08-27 Motorola, Inc. Thermoelectric power generator for an aircraft
US7210653B2 (en) * 2002-10-22 2007-05-01 The Boeing Company Electric-based secondary power system architectures for aircraft
KR20060004806A (ko) * 2004-07-08 2006-01-16 한국항공우주산업 주식회사 항공기의 보조 및 비상 동력 시스템
DE102005010399B4 (de) * 2005-03-07 2010-08-05 Airbus Deutschland Gmbh Luftfahrzeug mit einem Brennstoffzellen-Notsystem und Verfahren zur außenluftunabhängigen Energie-Notversorgung
JP2007015423A (ja) * 2005-07-05 2007-01-25 Shin Meiwa Ind Co Ltd 航空機の電源システム
DE102006002470A1 (de) * 2005-09-08 2007-03-15 Airbus Deutschland Gmbh Brennstoffzellensystem zur Versorgung mit Trinkwasser und Sauerstoff
KR100658684B1 (ko) * 2005-09-28 2006-12-15 삼성에스디아이 주식회사 연료개질용 촉매 및 이를 포함하는 연료전지 시스템
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
US7966830B2 (en) * 2006-06-29 2011-06-28 The Boeing Company Fuel cell/combustor systems and methods for aircraft and other applications
FR2907762B1 (fr) * 2006-10-27 2009-12-18 Airbus France Systeme de generation, conversion, distribution et demarrage electrique a bord d'un aeronef
US7550866B2 (en) * 2006-12-20 2009-06-23 The Boeing Company Vehicular power distribution system and method
DE102007017820A1 (de) * 2007-01-16 2008-08-07 Liebherr-Aerospace Lindenberg Gmbh Energieversorgungssystem eines Luftfahrzeuges
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
DE102007013345B4 (de) * 2007-03-20 2022-07-07 Airbus Operations Gmbh Energieregelvorrichtung für ein Flugzeug
WO2009025307A1 (ja) * 2007-08-22 2009-02-26 Gs Yuasa Corporation 航空機、及び航空機の使用法
US8119294B2 (en) * 2007-11-19 2012-02-21 Clearedge Power, Inc. System and method for operating a high temperature fuel cell as a back-up power supply with reduced performance decay
US9018512B2 (en) * 2007-12-21 2015-04-28 The Boeing Company Thermoelectric generation system
DE102008007469A1 (de) * 2008-02-04 2009-08-06 Airbus Deutschland Gmbh Verlängerungsteil für eine Einlaufklappe, Einlaufklappe mit einem solchen Verlängerungsteil und Triebwerk mit einer Einlaufklappe
US8019522B2 (en) * 2008-09-30 2011-09-13 General Electric Company Method and system for providing cooling and power
US7872368B2 (en) * 2008-10-24 2011-01-18 The Boeing Company Intelligent energy management architecture
DE102009005270A1 (de) * 2008-10-29 2010-05-12 Diehl Aerospace Gmbh Elektrisches Energieversorgungssystem, insbesondere in einem Luftfahrzeug
DE102008043626A1 (de) * 2008-11-10 2010-05-20 Airbus Deutschland Gmbh Leistungsverteilungs-Vorrichtung zum Verteilen von Leistung und Verfahren zum Verteilen von Leistung
US8128019B2 (en) * 2008-12-12 2012-03-06 Honeywell International Inc. Hybrid power for ducted fan unmanned aerial systems
FR2941107B1 (fr) * 2009-01-09 2015-08-14 Hispano Suiza Sa Systeme electrique de demarrage des moteurs d'un aeronef
GB2468652B (en) * 2009-03-16 2011-08-31 Ge Aviat Systems Ltd Electrical power distribution
US8657227B1 (en) * 2009-09-11 2014-02-25 The Boeing Company Independent power generation in aircraft
WO2011072366A1 (en) * 2009-12-15 2011-06-23 Messier-Dowty Inc. Electric accumulator utilizing an ultra-capacitor array
DE102010001333A1 (de) * 2010-01-28 2011-08-18 Airbus Operations GmbH, 21129 Verfahren und Vorrichtung zum Bereitstellen einer Bordnetz-Wechselspannung bei einem Flugzeug

Also Published As

Publication number Publication date
JP2013091488A (ja) 2013-05-16
FR2981808A1 (fr) 2013-04-26
DE102012109990A1 (de) 2013-04-25
CN103057716B (zh) 2017-05-24
JP6159073B2 (ja) 2017-07-05
US20130099560A1 (en) 2013-04-25
GB2495917A (en) 2013-05-01
GB201118314D0 (en) 2011-12-07
CA2792595A1 (en) 2013-04-24
CN103057716A (zh) 2013-04-24
GB2495917B (en) 2014-10-22

Similar Documents

Publication Publication Date Title
BR102012026464A2 (pt) Método para fornecer energia elétrica para uma aeronave e sistema de distribuição de energia elétrica para uma aeronave
BR112012018551A2 (pt) aeronave conduzida eletricamente
EP2557034A3 (en) Hybrid power system architecture for an aircraft
BR112015011248A2 (pt) micrograde baseada em sistema de trigeração híbrido combinada com resfriamento, aquecimento e fornecimento de energia de aquecimento, resfriamento, geração de energia elétrica e armazenamento de energia usando um sistema de automação integrado para monitoramento, análise e controle.
CL2013003763A1 (es) Recinto que contiene: un compartimiento de control, un compartimiento de transformador y un compartimiento de celdas de energia para recibir una pluralidad de celdas de energia, suministro de energia y sistema de distribucion de energia electrica.
BR112018012379A2 (pt) sistema integrado e método para produzir produto de metanol
CL2014002438A1 (es) Procedimiento para controlar una disposición para introducir energia electrica en una red de suministro electrico, que presenta una intalacion de energia eolica, donde el metodo comprende generar energia electrica con la instalación a partir del viento, introducir una primera potencia generada en la red de suministro, suministrar una segunda potencia a un consumidor que reduce parte o parcialmente la potencia conducida al consumidor y se añade a la primera parte; y dicha disposicion
CL2011002715A1 (es) Aparato de generacion de energia electrica a partir de flujos de agua, que se compone de al menos dos conjuntos de aspas que se disponen coaxialmente con un generador aumentando la eficiencia del aparato.
AR103532A1 (es) Procedimiento para operar un parque eólico
BR112013019340A2 (pt) sistema de suprimento de energia para um acionamento elétrico de uma embarcação marítima
MX2014015109A (es) Integracion fotovoltaica de red electrica utilizando almacenamiento y gestion de energia distribuida.
AR092391A1 (es) Parque eolico
BR112012029288B8 (pt) Sistema de carga para veículos elétricos e método para operação da matriz de interruptores em um sistema de carga
CL2011002868A1 (es) Un metodo y sistema para suministrar energia electrica desde una fuente de energia electrica a al menos una excavadora minera, en donde cada excavadora minera comprende al menos un motor electrico y un gasto ciclico de energia desde al menos la fuente de energia electrica.
EP2727839A3 (en) Method of Controlling an Aircraft Electrical Power Generation System
BR112013023255A2 (pt) sistema de abastecimento de energia auto-contido híbrido para aparelhos elétricos e uma unidade e um método para gerenciar o sistema
BR112013019259A2 (pt) sistema de acionamento, sistema de acionamento para veículo ferroviário, e veículo ferroviário e trem multicarros montado com o mesmo
CL2014000715A1 (es) Sistema de energia para equipos pesados que tiene un actuador para operar una herramienta que comprende un bus para proveer de electricidad al actuador, un motor para proveer de una salida de potencia, un generador acomplado de motor, un dispositivo de almacenamiento de energia, un controlador configurado para cambair la salida de potencia del motor; metodo para controlar un sistema de energia.
EP2614981A3 (en) Electric power supply system and controller of vehicle that can supply electric power to outside
BR112018068367A2 (pt) veículo subaquático não tripulado, sistema e método para a manutenção e inspeção de instalações subaquáticas
BR112015015613A2 (pt) sistema de potência elétrica para uma aeronave e método para produzir potência elétrica em uma aeronave
AR100961A1 (es) Procedimiento para la alimentación de energía eléctrica por medio de una instalación de energía eólica
GB201118313D0 (en) Thermal electrical power generation for aircraft
BR112015005648A2 (pt) dispositivo e processo de fornecimento de potência não propulsora para uma aeronave
AR089432A1 (es) Aparato y metodo para monitorear la calidad de un suministro de hidrogeno en celulas de combustible

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]
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 7A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2536 DE 13-08-2019 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.