CA2798271C - System and method for power distribution - Google Patents

System and method for power distribution Download PDF

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Publication number
CA2798271C
CA2798271C CA2798271A CA2798271A CA2798271C CA 2798271 C CA2798271 C CA 2798271C CA 2798271 A CA2798271 A CA 2798271A CA 2798271 A CA2798271 A CA 2798271A CA 2798271 C CA2798271 C CA 2798271C
Authority
CA
Canada
Prior art keywords
power
power converter
electrical
system bus
electrical loads
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
CA2798271A
Other languages
English (en)
French (fr)
Other versions
CA2798271A1 (en
Inventor
Christof Sihler
Sebastian Pedro Rosado
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of CA2798271A1 publication Critical patent/CA2798271A1/en
Application granted granted Critical
Publication of CA2798271C publication Critical patent/CA2798271C/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02MAPPARATUS 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
    • H02M1/00Details of apparatus for conversion
    • H02M1/32Means for protecting converters other than automatic disconnection
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J1/00Circuit arrangements for DC mains or DC distribution networks
    • H02J1/08Three-wire systems; Systems having more than three wires
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D2221/00Electric power distribution systems onboard aircraft
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J2310/00The network for supplying or distributing electric power characterised by its spatial reach or by the load
    • H02J2310/40The network being an on-board power network, i.e. within a vehicle
    • H02J2310/44The network being an on-board power network, i.e. within a vehicle for aircrafts
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02MAPPARATUS 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
    • H02M1/00Details of apparatus for conversion
    • H02M1/0067Converter structures employing plural converter units, other than for parallel operation of the units on a single load
    • H02M1/0074Plural converter units whose inputs are connected in series
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02MAPPARATUS 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
    • H02M1/00Details of apparatus for conversion
    • H02M1/0067Converter structures employing plural converter units, other than for parallel operation of the units on a single load
    • H02M1/008Plural converter units for generating at two or more independent and non-parallel outputs, e.g. systems with plural point of load switching regulators

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Direct Current Feeding And Distribution (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)
CA2798271A 2011-12-15 2012-12-06 System and method for power distribution Expired - Fee Related CA2798271C (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/326,919 US9143029B2 (en) 2011-12-15 2011-12-15 System and method for power distribution
US13/326,919 2011-12-15

Publications (2)

Publication Number Publication Date
CA2798271A1 CA2798271A1 (en) 2013-06-15
CA2798271C true CA2798271C (en) 2020-01-28

Family

ID=47522292

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2798271A Expired - Fee Related CA2798271C (en) 2011-12-15 2012-12-06 System and method for power distribution

Country Status (6)

Country Link
US (1) US9143029B2 (enExample)
EP (1) EP2605386A3 (enExample)
JP (1) JP6110648B2 (enExample)
CN (1) CN103158875B (enExample)
BR (1) BR102012031851A2 (enExample)
CA (1) CA2798271C (enExample)

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HUE049822T2 (hu) * 2014-05-01 2020-10-28 Alakai Tech Corporation Tiszta üzemanyagos több rotoros (multirotor) légi jármû személyes légi szállításra pilótával ellátott és pilóta nélküli mûködéssel
DE102015207117A1 (de) * 2014-07-09 2016-01-14 Siemens Aktiengesellschaft Umrichter mit redundanter Schaltungstopologie
DE102014014122A1 (de) * 2014-09-22 2016-03-24 Liebherr-Aerospace Lindenberg Gmbh Netzwerksystem zur Stromversorgung von mindestens einem Verbraucher in einem Flugzeug
US10227137B2 (en) * 2016-03-22 2019-03-12 Ge Aviation Systems Llc Hybrid power system for an aircraft
GB2550381B (en) * 2016-05-18 2020-06-24 Ge Aviat Systems Ltd An electric distribution architecture
US10833605B2 (en) * 2016-12-16 2020-11-10 Ge Aviation Systems Llc Space vector modulation in aerospace applications
US10461542B2 (en) 2017-07-10 2019-10-29 Ge Aviation Systems Llc Power distribution network
US10797612B2 (en) 2017-08-01 2020-10-06 Ge Aviation Systems Llc Power distribution network
US10994862B2 (en) * 2017-08-02 2021-05-04 Airbus Operations Sas Modular element for an electrical power distribution network of an aircraft
EP3537552A1 (en) 2018-03-09 2019-09-11 HS Elektronik Systeme GmbH Power distribution system
FR3079210B1 (fr) * 2018-03-26 2021-04-16 Safran Systeme propulsif d'aeronef multirotor avec reseau electrique reconfigurable
CN110556814B (zh) * 2018-05-31 2023-08-25 上海航空电器有限公司 飞机电源左右正常直流配电汇流条功率输入优先级结构
CN111546998B (zh) * 2020-04-03 2022-08-02 吉利汽车研究院(宁波)有限公司 一种电源分配装置、方法和车辆
US12113458B2 (en) * 2020-05-14 2024-10-08 Eaton Intelligent Power Limited Drive system with common DC bus
CN112793795B (zh) * 2021-03-19 2022-03-29 靳晨昊 一种搭载新能源系统的小型无人机
EP3998201B1 (en) * 2021-05-19 2024-06-05 Lilium eAircraft GmbH Time variable electrical load sharing in a power distribution network of an aircraft
US11835946B2 (en) 2021-12-29 2023-12-05 Beta Air, Llc Systems and methods for redistributing electrical load in an electric aircraft
US20250087996A1 (en) * 2023-09-07 2025-03-13 B/E Aerospace, Inc. Power architecture

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US3398324A (en) 1965-01-18 1968-08-20 Ltv Aerospace Corp D-c load switching and protective circuits without mechanical contacts
US4788448A (en) 1984-12-06 1988-11-29 Ferranti Subsea Systems, Ltd. Power transfer of direct current with inductive couplings
US4766724A (en) 1987-06-10 1988-08-30 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Arcjet power supply and start circuit
US5962929A (en) * 1998-04-22 1999-10-05 Lockheed Martin Corporation Fault tolerant power distribution
CA2375125A1 (en) 1999-05-28 2000-12-07 Gunnar Kylander A wind power plant
SE518121C2 (sv) 1999-12-23 2002-08-27 Abb Ab Elkraftsystem baserat på förnyelsebara energikällor
DE20115471U1 (de) 2001-09-19 2003-02-20 Biester, Klaus, 29342 Wienhausen Universelles Energieversorgungssystem
US6664656B2 (en) * 2000-09-14 2003-12-16 The Boeing Company Aircraft electrical power distribution network
EP1387460B1 (de) * 2002-08-02 2007-09-12 Airbus Deutschland GmbH Energieversorgungsanordnung für eine Bordküche eines Verkehrsmittels, insbesondere eines Flugzeuges
CN101479909B (zh) 2006-06-28 2011-12-21 Abb技术有限公司 模块化高压直流变换器
FR2906787B1 (fr) 2006-10-10 2009-03-20 Airbus France Sa Systeme et procede d'alimentation en courant continu d'un reseau electrique a bord d'un aeronef
US7633770B2 (en) * 2006-12-08 2009-12-15 General Electric Company Collection and transmission system
US7851943B2 (en) * 2006-12-08 2010-12-14 General Electric Company Direct current power transmission and distribution system
US7550866B2 (en) * 2006-12-20 2009-06-23 The Boeing Company Vehicular power distribution system and method
US7598625B2 (en) 2007-06-08 2009-10-06 Honeywell International Inc. Network-based aircraft secondary electric power distribution system
EP2071694B1 (en) * 2007-12-11 2019-02-20 General Electric Company MVDC power transmission system for sub-sea loads
US7868621B2 (en) 2008-03-04 2011-01-11 Honeywell International Inc. Power line communication based aircraft power distribution system with real time wiring integrity monitoring capability
US8692408B2 (en) * 2008-12-03 2014-04-08 General Electric Company Modular stacked subsea power system architectures
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
GB2466871A (en) 2009-01-07 2010-07-14 Champion Aerospace Inc DC aircraft power supply having voltage modulation attenuator
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WO2011026047A1 (en) * 2009-08-28 2011-03-03 Green Plug High-and low-power power supply with standby power saving features
US8657227B1 (en) * 2009-09-11 2014-02-25 The Boeing Company Independent power generation in aircraft

Also Published As

Publication number Publication date
CN103158875A (zh) 2013-06-19
EP2605386A2 (en) 2013-06-19
JP2013124097A (ja) 2013-06-24
US20130154349A1 (en) 2013-06-20
CN103158875B (zh) 2016-09-28
JP6110648B2 (ja) 2017-04-05
BR102012031851A2 (pt) 2014-10-21
CA2798271A1 (en) 2013-06-15
US9143029B2 (en) 2015-09-22
EP2605386A3 (en) 2017-10-25

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Effective date: 20171006

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Effective date: 20201207