BR112016005887A2 - sistema de distribuição de potência de aeronave e método para controlar um sistema de distribuição de potência de aeronave - Google Patents

sistema de distribuição de potência de aeronave e método para controlar um sistema de distribuição de potência de aeronave

Info

Publication number
BR112016005887A2
BR112016005887A2 BR112016005887A BR112016005887A BR112016005887A2 BR 112016005887 A2 BR112016005887 A2 BR 112016005887A2 BR 112016005887 A BR112016005887 A BR 112016005887A BR 112016005887 A BR112016005887 A BR 112016005887A BR 112016005887 A2 BR112016005887 A2 BR 112016005887A2
Authority
BR
Brazil
Prior art keywords
power distribution
distribution system
aircraft power
bus
controlling
Prior art date
Application number
BR112016005887A
Other languages
English (en)
Inventor
Vorwerk Radun Arthur
Allan Toothman Steven
Original Assignee
Ge Aviation Systems Llc
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 Aviation Systems Llc filed Critical Ge Aviation Systems Llc
Publication of BR112016005887A2 publication Critical patent/BR112016005887A2/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
    • H02J1/00—Circuit arrangements for dc mains or dc distribution networks
    • H02J1/10—Parallel operation of dc 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
    • B64D47/00—Equipment not otherwise provided for
    • 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
    • H02J1/08—Three-wire systems; Systems having more than three wires
    • H02J1/082—Plural DC voltage, e.g. DC supply voltage with at least two different DC voltage levels
    • 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
    • H02J9/061—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 for DC powered loads
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
    • H02M7/00—Conversion of ac power input into dc power output; Conversion of dc power input into ac power output
    • H02M7/02—Conversion of ac power input into dc power output without possibility of reversal
    • H02M7/04—Conversion of ac power input into dc power output without possibility of reversal by static converters
    • 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
    • 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
    • H02J9/068—Electronic means for switching from one power supply to another power supply, e.g. to avoid parallel connection

Abstract

a presente invenção refere-se a um sistema de distribuição de potência de aeronave que inclui pelo menos uma fonte de alimentação cc, um primeiro barramento de distribuição de potência cc e um segundo barramento de distribuição de potência cc, um barramento de conexão que acopla a pelo menos uma fonte de alimentação cc, o primeiro barramento de distribuição de potência cc e o segundo barramento de distribuição cc, em que o primeiro ou o segundo barramentos de distribuição cc são acoplados e desacoplados seletivamente do barramento de conexão.
BR112016005887A 2013-10-04 2013-10-04 sistema de distribuição de potência de aeronave e método para controlar um sistema de distribuição de potência de aeronave BR112016005887A2 (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US2013/063385 WO2015050555A1 (en) 2013-10-04 2013-10-04 Dc power distribution system for an aircraft

Publications (1)

Publication Number Publication Date
BR112016005887A2 true BR112016005887A2 (pt) 2017-08-01

Family

ID=49382634

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112016005887A BR112016005887A2 (pt) 2013-10-04 2013-10-04 sistema de distribuição de potência de aeronave e método para controlar um sistema de distribuição de potência de aeronave

Country Status (7)

Country Link
US (1) US20160280394A1 (pt)
EP (1) EP3053238A1 (pt)
JP (1) JP2016539609A (pt)
CN (1) CN105765816A (pt)
BR (1) BR112016005887A2 (pt)
CA (1) CA2925463A1 (pt)
WO (1) WO2015050555A1 (pt)

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EP3268753B1 (en) * 2015-07-17 2021-06-16 Hewlett Packard Enterprise Development LP Current restriction
CN106428589B (zh) * 2016-11-09 2019-01-25 北京宇航系统工程研究所 一种基于固态功率控制技术的航天飞行器供配电器
GB2558655B (en) * 2017-01-16 2020-03-25 Ge Aviat Systems Ltd Fault-tolerant solid state power controller
US10934935B2 (en) * 2017-01-30 2021-03-02 Ge Aviation Systems Llc Engine core assistance
GB2559956B (en) * 2017-02-15 2020-09-16 Ge Aviat Systems Ltd Power distribution node for a power architecture
US10137981B2 (en) * 2017-03-31 2018-11-27 General Electric Company Electric propulsion system for an aircraft
FR3067531B1 (fr) * 2017-06-13 2020-07-31 Zodiac Aero Electric Systeme de stockage d'energie electrique pour aeronef
US10381833B2 (en) * 2017-06-27 2019-08-13 Ge Aviation Systems Llc Solid state power contactor
CN107579547B (zh) * 2017-09-27 2020-05-15 湖北航天技术研究院总体设计所 基于集成固态继电器模块的飞行器电源配电系统
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
US11469611B2 (en) 2018-09-13 2022-10-11 Ls Electric Co., Ltd. Power supply system
US11008993B2 (en) * 2018-09-21 2021-05-18 Caterpillar Inc. Single solid state power supply for multiple engine systems
FR3086923B1 (fr) * 2018-10-04 2020-11-06 Safran Architecture electrique pour propulsion hybride
CN110966327A (zh) * 2019-11-25 2020-04-07 天津津航计算技术研究所 一种用于飞机刹车系统的冷却控制系统
CN111525476B (zh) * 2020-04-23 2021-11-09 新疆丝路六合电气科技有限公司 一种电气接线盒
US11845388B2 (en) 2021-05-20 2023-12-19 General Electric Company AC electrical power system for a vehicle
CN113794266A (zh) * 2021-08-16 2021-12-14 中国空间技术研究院 一种星上基于多母线配置的分布式环形配电系统架构
CN113765211B (zh) * 2021-10-09 2024-03-01 陕西航空电气有限责任公司 一种航空配电系统中直流应急汇流条不间断供电的方法
US20230378743A1 (en) * 2022-05-20 2023-11-23 Hamilton Sundstrand Corporation Direct current bus control scheme

Family Cites Families (7)

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Publication number Priority date Publication date Assignee Title
DE19617915C2 (de) * 1996-05-03 2001-11-08 Eads Airbus Gmbh Anordnung zur Energieverteilung, in einem Flugzeug
GB0031057D0 (en) * 2000-12-20 2001-01-31 Lucas Industries Ltd Power transfer system
FR2930085B1 (fr) * 2008-04-09 2012-06-08 Thales Sa Reseau electrique
DE102008043626A1 (de) * 2008-11-10 2010-05-20 Airbus Deutschland Gmbh Leistungsverteilungs-Vorrichtung zum Verteilen von Leistung und Verfahren zum Verteilen von Leistung
US8344544B2 (en) * 2010-05-19 2013-01-01 Hamilton Sundstrand Corporation Bus-tie SSPCS for DC power distribution system
US8587146B2 (en) * 2011-06-07 2013-11-19 Hamilton Sundstrand Corporation Solid state contactor assembly
US9660446B2 (en) * 2013-10-04 2017-05-23 Ge Aviation Systems Llc Power distribution system for an aircraft

Also Published As

Publication number Publication date
EP3053238A1 (en) 2016-08-10
JP2016539609A (ja) 2016-12-15
CN105765816A (zh) 2016-07-13
CA2925463A1 (en) 2015-04-09
WO2015050555A1 (en) 2015-04-09
US20160280394A1 (en) 2016-09-29

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 6A 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 2534 DE 30-07-2019 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.