JP6441768B2 - 航空機の補足電力システム及び方法 - Google Patents

航空機の補足電力システム及び方法 Download PDF

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Publication number
JP6441768B2
JP6441768B2 JP2015159832A JP2015159832A JP6441768B2 JP 6441768 B2 JP6441768 B2 JP 6441768B2 JP 2015159832 A JP2015159832 A JP 2015159832A JP 2015159832 A JP2015159832 A JP 2015159832A JP 6441768 B2 JP6441768 B2 JP 6441768B2
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Japan
Prior art keywords
power
generator
supplemental
output
branch
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JP2015159832A
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English (en)
Japanese (ja)
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JP2016078834A (ja
JP2016078834A5 (https=
Inventor
ジェフリー・ジョセフ・ホワイト
トーマス・エフ・カリアー
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Boeing Co
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Boeing Co
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60R—VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
    • B60R16/00—Electric or fluid circuits specially adapted for vehicles and not otherwise provided for; Arrangement of elements of electric or fluid circuits specially adapted for vehicles and not otherwise provided for
    • B60R16/02—Electric or fluid circuits specially adapted for vehicles and not otherwise provided for; Arrangement of elements of electric or fluid circuits specially adapted for vehicles and not otherwise provided for electric constitutive elements
    • B60R16/03—Electric or fluid circuits specially adapted for vehicles and not otherwise provided for; Arrangement of elements of electric or fluid circuits specially adapted for vehicles and not otherwise provided for electric constitutive elements for supply of electrical power to vehicle subsystems or for
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—ELECTRIC POWER NETWORKS; 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
    • H02J3/04—Arrangements for connecting networks of the same frequency but supplied from different sources
    • H02J3/06—Controlling the transfer of power between connected networks; Controlling load sharing between connected networks
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—ELECTRIC POWER NETWORKS; 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 feeding a single network from two or more generators or sources in parallel; Arrangements for feeding already energised networks from additional generators or sources in parallel
    • 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—ELECTRIC POWER NETWORKS; CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J2105/00—Networks for supplying or distributing electric power characterised by their spatial reach or by the load
    • H02J2105/30—Networks for supplying or distributing electric power characterised by their spatial reach or by the load the load networks being external to vehicles, i.e. exchanging power with vehicles
    • H02J2105/32—Networks for supplying or distributing electric power characterised by their spatial reach or by the load the load networks being external to vehicles, i.e. exchanging power with vehicles for aircrafts

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  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Supply And Distribution Of Alternating Current (AREA)
JP2015159832A 2014-10-16 2015-08-13 航空機の補足電力システム及び方法 Active JP6441768B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US14/516,208 US10093250B2 (en) 2014-10-16 2014-10-16 Aircraft supplemental electrical power systems and methods
US14/516,208 2014-10-16

Publications (3)

Publication Number Publication Date
JP2016078834A JP2016078834A (ja) 2016-05-16
JP2016078834A5 JP2016078834A5 (https=) 2018-05-31
JP6441768B2 true JP6441768B2 (ja) 2018-12-19

Family

ID=53969212

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015159832A Active JP6441768B2 (ja) 2014-10-16 2015-08-13 航空機の補足電力システム及び方法

Country Status (4)

Country Link
US (2) US10093250B2 (https=)
EP (1) EP3010109B1 (https=)
JP (1) JP6441768B2 (https=)
CN (1) CN105523190B (https=)

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DE102015005681A1 (de) 2015-05-06 2016-11-10 Gentherm Gmbh Aufnahmevorrichtung für Getränkebehältnisse
US10443504B2 (en) * 2016-10-21 2019-10-15 Ge Aviation Systems Llc Method for allocating power in an electrical power system architecture
GB2559956B (en) * 2017-02-15 2020-09-16 Ge Aviat Systems Ltd Power distribution node for a power architecture
US10942527B2 (en) * 2017-05-30 2021-03-09 Textron Innovations Inc. System and method for controlling rotorcraft load priority
US10892635B2 (en) 2018-01-11 2021-01-12 Ford Global Technologies, Llc Redundant power supply
US10800364B2 (en) * 2018-01-11 2020-10-13 Ford Global Technologies, Llc Vehicle power supply
US10415530B2 (en) * 2018-01-16 2019-09-17 The Boeing Company System and method for operating an independent speed variable frequency generator as a starter
CN108288853B (zh) * 2018-04-04 2024-05-28 中国商用飞机有限责任公司北京民用飞机技术研究中心 飞机直流供电系统及供电方法
US10680533B1 (en) * 2019-02-01 2020-06-09 Hamilton Sunstrand Corporation Common layout rectifier or converter
US11616366B2 (en) * 2020-03-12 2023-03-28 Hamilton Sundstrand Corporation AC essential bus delta current and over current protection scheme
US11448136B2 (en) 2020-04-16 2022-09-20 Honeywell International Inc. Adaptive aircraft electrical power distribution system
WO2023091579A1 (en) * 2021-11-17 2023-05-25 Verdego Aero, Inc. Split turbocharger having independent electric turbine and electric compressor components
GB2613787A (en) * 2021-12-14 2023-06-21 Rolls Royce Plc Aircraft power and propulsion system

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US4967096A (en) 1989-01-26 1990-10-30 Sundstrand Corporation Cross-start bus configuration for a variable speed constant frequency electric power system
US4967097A (en) 1989-03-08 1990-10-30 Mehl Bryon R Hybrid power system
US5627744A (en) 1996-02-02 1997-05-06 Sundstrand Corporation Converter enhanced variable frequency power bus architecture
US5813630A (en) 1996-09-27 1998-09-29 Mcdonnell Douglas Corporation Multi-mode secondary power unit
US6037752A (en) * 1997-06-30 2000-03-14 Hamilton Sundstrand Corporation Fault tolerant starting/generating system
US6344700B1 (en) 1999-10-01 2002-02-05 Bell Helicopter Textron Inc. Redundant electrical DC power system for aircraft
US6503649B1 (en) 2000-04-03 2003-01-07 Convergence, Llc Variable fuel cell power system for generating electrical power
US6992403B1 (en) * 2001-03-08 2006-01-31 Pacific Scientific Electric power and start system
US7210653B2 (en) 2002-10-22 2007-05-01 The Boeing Company Electric-based secondary power system architectures for aircraft
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
US7254465B2 (en) 2004-06-04 2007-08-07 Honeywell International, Inc. No-break-power-transfer control system for variable frequency electrical power systems
US7116003B2 (en) * 2004-07-14 2006-10-03 Hamilton Sundstrand Corporation Aircraft starter/generator electrical system with mixed power architecture
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
FR2907762B1 (fr) * 2006-10-27 2009-12-18 Airbus France Systeme de generation, conversion, distribution et demarrage electrique a bord d'un aeronef
US7970497B2 (en) * 2007-03-02 2011-06-28 Honeywell International Inc. Smart hybrid electric and bleed architecture
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
US8738268B2 (en) 2011-03-10 2014-05-27 The Boeing Company Vehicle electrical power management and distribution
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DE102015207117A1 (de) * 2014-07-09 2016-01-14 Siemens Aktiengesellschaft Umrichter mit redundanter Schaltungstopologie

Also Published As

Publication number Publication date
US20160107588A1 (en) 2016-04-21
US10780850B2 (en) 2020-09-22
EP3010109A1 (en) 2016-04-20
US20190016280A1 (en) 2019-01-17
JP2016078834A (ja) 2016-05-16
CN105523190B (zh) 2020-01-10
CN105523190A (zh) 2016-04-27
US10093250B2 (en) 2018-10-09
EP3010109B1 (en) 2018-04-18

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