JP6148324B2 - 地上の航空機に電力を供給するための装置 - Google Patents
地上の航空機に電力を供給するための装置 Download PDFInfo
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- JP6148324B2 JP6148324B2 JP2015502402A JP2015502402A JP6148324B2 JP 6148324 B2 JP6148324 B2 JP 6148324B2 JP 2015502402 A JP2015502402 A JP 2015502402A JP 2015502402 A JP2015502402 A JP 2015502402A JP 6148324 B2 JP6148324 B2 JP 6148324B2
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- generator
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- aircraft
- power
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- 239000007858 starting material Substances 0.000 claims description 19
- 238000000034 method Methods 0.000 claims description 10
- 230000005284 excitation Effects 0.000 claims description 9
- 230000001360 synchronised effect Effects 0.000 claims description 6
- 238000004804 winding Methods 0.000 claims description 6
- 230000007257 malfunction Effects 0.000 claims 1
- 230000001276 controlling effect Effects 0.000 description 6
- 230000008901 benefit Effects 0.000 description 3
- 230000002950 deficient Effects 0.000 description 3
- 230000001052 transient effect Effects 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000005672 electromagnetic field Effects 0.000 description 1
- 239000003350 kerosene Substances 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 238000010200 validation analysis Methods 0.000 description 1
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Classifications
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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
- B60R16/0307—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 using generators driven by a machine different from the vehicle motor
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/405—Powered wheels, e.g. for taxing
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- 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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02N—STARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
- F02N11/00—Starting of engines by means of electric motors
- F02N11/08—Circuits or control means specially adapted for starting of engines
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- 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
- 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
-
- 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
- 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
-
- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
-
- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/80—Energy efficient operational measures, e.g. ground operations or mission management
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Power Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Control Of Eletrric Generators (AREA)
- Supply And Distribution Of Alternating Current (AREA)
- Control Of Charge By Means Of Generators (AREA)
Description
Claims (10)
- 補助動力装置(220)によって駆動される2つの発電機(216、218)を備える、地上の航空機に電力を供給するための装置(210)にして、第1の発電機が、航空機の車輪を駆動するための電気モータ(226)を備える電気タキシングネットワーク(214)に給電することを目的としており、第2の発電機が、電気航空機ネットワーク(212)に給電することを目的としている装置であって、第1の発電機は、選択的な接続/切断手段(232)によって航空機およびタキシングネットワークに接続され、これが航空機ネットワークに接続されると第1のAC電圧Vac2を航空機ネットワークに、または、これがタキシングネットワークに接続されると第1のAC電圧Vac2より高いAC電圧Vac1またはタキシングネットワークを駆動するのに十分な電力Pを供給することができ、第2の発電機は、選択的な接続/切断手段(232)によって航空機およびタキシングネットワークに接続され、第1のAC電圧Vac2をこれが接続されるネットワークに供給することができることを特徴とする、装置。
- 発電機(216、218)のうちの1つが、補助動力装置(220)を始動させることができる始動機/発電機であることを特徴とする、請求項1に記載の装置。
- 補助動力装置(220)の始動を制御するための始動機/発電機(216、218)に接続されるモータ制御ユニット(228、270、272)を備えることを特徴とする、請求項2に記載の装置。
- 第1の発電機(218)が、巻線型回転子励磁の3段同期発電機であることを特徴とする、請求項1から3のいずれか一項に記載の装置。
- 第1の発電機(218)が、航空機ネットワークに接続される場合には400Hzで115Vacの電圧(Vac2)、および90kVAの電力を供給することを特徴とする、請求項1から4のいずれか一項に記載の装置。
- 第1の発電機(218)が、タキシングネットワークに接続される場合には150kWの電力を供給することを特徴とする、請求項1から5のいずれか一項に記載の装置。
- 第2の発電機(216)が、地上の航空機に電荷を供給するための電力と、400Hzで115Vacの電圧Vac2とを供給することを特徴とする、請求項1から6のいずれか一項に記載の装置。
- 請求項1から7のいずれか一項に記載の装置(210)を使って地上の航空機に電力を供給する方法であって、第1の発電機(218)によってタキシングネットワーク(214)に、かつ第2の発電機(216)を使って航空機ネットワーク(212)に給電することにあるステップと、タキシング機能が使用されない場合に第1の発電機(218)を使って航空機ネットワーク(212)に給電するステップであり、この場合第2の発電機(216)が運転停止中であることにあるステップとを含むことを特徴とする、方法。
- 第1の発電機(218)が、巻線型回転子励磁の3段同期発電機であり、この発電機の励磁が、電圧発生器Vac1から電圧発生器Vac2に、または電力Pの発生器から電圧発生器Vac2に切り換えるためにモータ制御ユニット(232)によって制御されることを特徴とする、請求項8に記載の方法。
- 第1の発電機(218)に不具合がある場合に、第2の発電機(216)によってタキシングネットワーク(214)に給電することにあるステップを含むことを特徴とする、請求項8または9に記載の方法。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1252957A FR2988694B1 (fr) | 2012-03-30 | 2012-03-30 | Dispositif d'alimentation electrique d'un aeronef au sol |
FR1252957 | 2012-03-30 | ||
PCT/FR2013/050527 WO2013144479A1 (fr) | 2012-03-30 | 2013-03-14 | Dispositif d'alimentation électrique d'un aéronef au sol |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2015514036A JP2015514036A (ja) | 2015-05-18 |
JP6148324B2 true JP6148324B2 (ja) | 2017-06-14 |
Family
ID=48083494
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2015502402A Active JP6148324B2 (ja) | 2012-03-30 | 2013-03-14 | 地上の航空機に電力を供給するための装置 |
Country Status (10)
Country | Link |
---|---|
US (1) | US9849849B2 (ja) |
EP (1) | EP2830938B1 (ja) |
JP (1) | JP6148324B2 (ja) |
CN (1) | CN104169168B (ja) |
BR (1) | BR112014022553B1 (ja) |
CA (1) | CA2867545C (ja) |
ES (1) | ES2568642T3 (ja) |
FR (1) | FR2988694B1 (ja) |
RU (1) | RU2629817C2 (ja) |
WO (1) | WO2013144479A1 (ja) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2520024B (en) | 2013-11-06 | 2016-02-03 | Ge Aviat Systems Ltd | Electrical power system for an aircraft |
GB201511033D0 (en) * | 2015-05-19 | 2015-08-05 | Rolls Royce Plc | Aircraft electrical network |
US20170107910A1 (en) * | 2015-10-15 | 2017-04-20 | Ge Aviation Systems Llc | Method and apparatus for starting an aircraft engine and operating a power architecture for an aircraft |
US9771149B2 (en) * | 2015-10-30 | 2017-09-26 | Honeywell International Inc. | Gate departure system for aircraft |
EP3235723B1 (en) * | 2016-04-22 | 2019-11-27 | Rolls-Royce plc | Aircraft electrical network |
WO2020180381A1 (en) | 2019-03-01 | 2020-09-10 | United Technologies Advanced Projects, Inc. | Indicators for hybrid electrical powerplants |
WO2020185274A2 (en) | 2019-03-01 | 2020-09-17 | United Technologies Advanced Projects, Inc. | Normal mode operation of hybrid electric propulsion systems |
WO2020180372A2 (en) | 2019-03-01 | 2020-09-10 | United Technologies Advanced Projects, Inc. | Degraded mode operation of hybrid electric propulsion systems |
EP3927620A4 (en) | 2019-04-25 | 2022-11-16 | Pratt & Whitney Canada Corp. | CONTROL SYSTEMS FOR HYBRID POWER PLANTS |
US11794917B2 (en) | 2020-05-15 | 2023-10-24 | Pratt & Whitney Canada Corp. | Parallel control loops for hybrid electric aircraft |
US11958622B2 (en) | 2020-05-15 | 2024-04-16 | Pratt & Whitney Canada Corp. | Protection functions |
EP4305653A1 (en) | 2021-03-12 | 2024-01-17 | Essex Industries, Inc. | Rocker switch |
US11688568B2 (en) | 2021-03-15 | 2023-06-27 | Essex Industries, Inc. | Five-position switch |
EP4385902A1 (en) * | 2022-12-13 | 2024-06-19 | Airbus Operations, S.L.U. | Auxiliary power system |
Family Cites Families (23)
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FR1059612A (fr) | 1952-07-09 | 1954-03-26 | Andre Mathieu Freres | Perfectionnement au montage des plaquettes nasales de lunettes |
SU868926A1 (ru) * | 1980-01-03 | 1981-09-30 | Предприятие П/Я М-6374 | Устройство дл автоматического переключени потребителей с одного канала питани посто нного тока на другой |
US5422517A (en) * | 1993-05-26 | 1995-06-06 | United Technologies Corporation | Control of electric loads during generator failure in a multi-generator 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 |
RU2232109C1 (ru) * | 2003-09-22 | 2004-07-10 | ОАО "ОКБ им. А.С.Яковлева" | Способ электроснабжения бортовых систем летательного аппарата |
US7445178B2 (en) * | 2004-09-28 | 2008-11-04 | The Boeing Company | Powered nose aircraft wheel system |
JP2007015423A (ja) * | 2005-07-05 | 2007-01-25 | Shin Meiwa Ind Co Ltd | 航空機の電源システム |
GB2444678B (en) * | 2005-08-29 | 2010-09-22 | Borealis Tech Ltd | Nosewheel control apparatus |
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 |
US8155876B2 (en) * | 2006-09-07 | 2012-04-10 | The Boeing Company | Systems and methods for controlling aircraft electrical power |
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 |
US7980509B2 (en) * | 2007-03-08 | 2011-07-19 | The Ashman Group, Llc | Aircraft taxiing systems |
US7800245B2 (en) * | 2007-07-09 | 2010-09-21 | Honeywell International Inc. | Method and architecture for reduction in vehicle wiring |
FR2930084B1 (fr) * | 2008-04-09 | 2012-06-08 | Thales Sa | Procede de gestion d'un reseau electrique |
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 |
GB0905568D0 (en) * | 2009-04-01 | 2009-05-13 | Rolls Royce Plc | Taxling |
FR2944775B1 (fr) * | 2009-04-24 | 2013-03-08 | Messier Bugatti | Procede de deplacement d'un aeronef au sol |
US8148834B2 (en) * | 2009-05-19 | 2012-04-03 | General Electric Company | Aircraft engine starting/generating system and method of control |
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 |
FR2960520B1 (fr) * | 2010-05-26 | 2012-06-29 | Airbus Operations Sas | Aeronef comprenant un moteur de train |
FR2978878B1 (fr) | 2011-08-04 | 2013-08-09 | Hispano Suiza Sa | Dispositif d'alimentation electrique d'un aeronef au sol. |
-
2012
- 2012-03-30 FR FR1252957A patent/FR2988694B1/fr not_active Expired - Fee Related
-
2013
- 2013-03-14 CN CN201380016065.9A patent/CN104169168B/zh active Active
- 2013-03-14 BR BR112014022553-2A patent/BR112014022553B1/pt active IP Right Grant
- 2013-03-14 US US14/385,622 patent/US9849849B2/en active Active
- 2013-03-14 ES ES13715315.1T patent/ES2568642T3/es active Active
- 2013-03-14 RU RU2014143541A patent/RU2629817C2/ru active
- 2013-03-14 WO PCT/FR2013/050527 patent/WO2013144479A1/fr active Application Filing
- 2013-03-14 EP EP13715315.1A patent/EP2830938B1/fr active Active
- 2013-03-14 CA CA2867545A patent/CA2867545C/fr active Active
- 2013-03-14 JP JP2015502402A patent/JP6148324B2/ja active Active
Also Published As
Publication number | Publication date |
---|---|
FR2988694A1 (fr) | 2013-10-04 |
WO2013144479A1 (fr) | 2013-10-03 |
BR112014022553A2 (pt) | 2017-06-20 |
CN104169168A (zh) | 2014-11-26 |
EP2830938A1 (fr) | 2015-02-04 |
CA2867545A1 (fr) | 2013-10-03 |
US20150042155A1 (en) | 2015-02-12 |
RU2014143541A (ru) | 2016-05-27 |
ES2568642T3 (es) | 2016-05-03 |
FR2988694B1 (fr) | 2014-03-28 |
BR112014022553B1 (pt) | 2021-08-17 |
RU2629817C2 (ru) | 2017-09-04 |
CN104169168B (zh) | 2016-02-10 |
EP2830938B1 (fr) | 2016-03-09 |
JP2015514036A (ja) | 2015-05-18 |
US9849849B2 (en) | 2017-12-26 |
CA2867545C (fr) | 2019-11-19 |
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