JP6316281B2 - ヘリコプタタービンエンジン用制御・電力供給システム - Google Patents
ヘリコプタタービンエンジン用制御・電力供給システム Download PDFInfo
- Publication number
- JP6316281B2 JP6316281B2 JP2015510861A JP2015510861A JP6316281B2 JP 6316281 B2 JP6316281 B2 JP 6316281B2 JP 2015510861 A JP2015510861 A JP 2015510861A JP 2015510861 A JP2015510861 A JP 2015510861A JP 6316281 B2 JP6316281 B2 JP 6316281B2
- Authority
- JP
- Japan
- Prior art keywords
- converter
- contactor
- power
- generator
- power supply
- 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
Links
- 239000011159 matrix material Substances 0.000 claims description 10
- 239000007858 starting material Substances 0.000 claims description 9
- 239000003990 capacitor Substances 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000001681 protective effect Effects 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 230000002441 reversible effect Effects 0.000 description 2
- 230000015556 catabolic process Effects 0.000 description 1
- 239000003638 chemical reducing agent Substances 0.000 description 1
- 238000006731 degradation reaction Methods 0.000 description 1
- 238000009396 hybridization Methods 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 238000005549 size reduction Methods 0.000 description 1
Images
Classifications
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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
- F02N11/0862—Circuits or control means specially adapted for starting of engines characterised by the electrical power supply means, e.g. battery
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- 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
- B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
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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
- F02N11/04—Starting of engines by means of electric motors the motors being associated with current generators
-
- 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
- F02N11/0848—Circuits or control means specially adapted for starting of engines with means for detecting successful engine start, e.g. to stop starter actuation
-
- 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
- H02J5/00—Circuit arrangements for transfer of electric power between ac networks and dc networks
-
- 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
- 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
- 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
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Power Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Eletrric Generators (AREA)
- Control Of Charge By Means Of Generators (AREA)
- Supply And Distribution Of Alternating Current (AREA)
- Control Of Ac Motors In General (AREA)
- Inverter Devices (AREA)
Description
Claims (3)
- 少なくとも1つのヘリコプタモータ発電機用の電気制御・電力供給システムであって、電気制御・電力供給システムは、電子制御回路(34)から作動される接続マトリックス(32)のコンタクタ(320、322、324、326、328、330、332)のそれぞれの位置に応じて、前記少なくとも1つのヘリコプタモータ発電機にAC電力を選択的に供給する第1のDC/ACコンバータ(30)を備え、第1のDC/ACコンバータは、APU(16)の始動発電機(18)によってコンタクタ(22)を介して供給されたAC電圧を整流する回路(36)、もしくはコンタクタ(24)を介してバッテリ(20)から電力を供給される電圧ブースタDC/DCコンバータ(38)によって形成されたDC電力供給装置によってDC電力が供給され、前記電圧ブースタDC/DCコンバータは、少なくとも1つのコンタクタ(320、322)を介して三相インダクタ(380)と第2のDC/ACコンバータ(382)とを直列接続することによって形成され、前記接続マトリックスはさらに、前記ヘリコプタモータ発電機の少なくとも1つが始動した時に、APUの前記始動発電機から追加電力を前記少なくとも1つの前記ヘリコプタモータ発電機に注入することができるように、前記第1のDC/ACコンバータを前記第2のDC/ACコンバータ(382)と並列に接続するためのコンタクタ(328)を含む、システム。
- 前記接続マトリックスは、前記第1のDC/ACコンバータを第1のモータ発電機(12C)に接続するための少なくとも1つのコンタクタ(324、330)と、前記第2のDC/ACコンバータを第2のモータ発電機(14C)に接続するための少なくとも1つのコンタクタ(322、332)とを含むことを特徴とする、請求項1に記載のシステム。
- 前記接続マトリックスはさらに、APUを前記バッテリから始動させることができるように、前記第1のDC/ACコンバータを前記始動発電機に接続するための少なくとも1つのコンタクタ(320、326)を備えることを特徴とする、請求項2に記載のシステム。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1254333A FR2990573B1 (fr) | 2012-05-11 | 2012-05-11 | Systeme de commande et d'alimentation en energie des turbomachines d'un helicoptere |
FR1254333 | 2012-05-11 | ||
PCT/FR2013/051007 WO2013167837A2 (fr) | 2012-05-11 | 2013-05-06 | Systeme de commande et d'alimentation en energie des turbomachines d'un helicoptere |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2015525551A JP2015525551A (ja) | 2015-09-03 |
JP6316281B2 true JP6316281B2 (ja) | 2018-04-25 |
Family
ID=48577113
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2015510861A Expired - Fee Related JP6316281B2 (ja) | 2012-05-11 | 2013-05-06 | ヘリコプタタービンエンジン用制御・電力供給システム |
Country Status (9)
Country | Link |
---|---|
US (1) | US9745943B2 (ja) |
EP (1) | EP2847845B1 (ja) |
JP (1) | JP6316281B2 (ja) |
CN (1) | CN104471819B (ja) |
BR (1) | BR112014027729B1 (ja) |
CA (1) | CA2872724C (ja) |
FR (1) | FR2990573B1 (ja) |
RU (1) | RU2641672C1 (ja) |
WO (1) | WO2013167837A2 (ja) |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2994386B1 (en) * | 2013-05-06 | 2020-02-19 | Sikorsky Aircraft Corporation | Supplemental power for reduction of prime mover |
FR3015571B1 (fr) * | 2013-12-23 | 2018-11-23 | Safran Helicopter Engines | Procede et systeme de demarrage fiabilise de turbomachine |
FR3017257B1 (fr) * | 2014-01-31 | 2017-11-10 | Hispano-Suiza | Systeme de distribution et de conversion electrique pour un aeronef |
FR3017258B1 (fr) | 2014-01-31 | 2016-01-15 | Hispano Suiza Sa | Systeme de distribution et de conversion electrique pour un aeronef |
FR3019214B1 (fr) * | 2014-03-27 | 2019-05-31 | Safran Helicopter Engines | Dispositif d'assistance pour une turbomachine a turbine libre d'aeronef |
FR3019218B1 (fr) * | 2014-03-27 | 2016-03-18 | Turbomeca | Architecture d'un systeme propulsif d'un helicoptere multi-moteur et helicoptere correspondant |
FR3019215B1 (fr) | 2014-03-27 | 2019-05-31 | Safran Helicopter Engines | Dispositif d'assistance pour une turbomachine a turbine libre d'un aeronef comprenant au moins deux turbomachines a turbine libre |
FR3019219B1 (fr) * | 2014-03-27 | 2016-03-18 | Turbomeca | Architecture d'un systeme propulsif d'un helicoptere multi-moteur et helicoptere correspondant |
DE102016202195A1 (de) * | 2016-02-12 | 2017-08-17 | Siemens Aktiengesellschaft | Verfahren zum Antrieb eines Luftfahrzeugs und Luftfahrzeug |
FR3054738B1 (fr) * | 2016-07-29 | 2020-10-23 | Airbus Helicopters | Architecture electrique a double reseau electrique secondaire pour le demarrage des moteurs d'un aeronef |
FR3056555B1 (fr) * | 2016-09-29 | 2018-12-07 | Safran Helicopter Engines | Systeme propulsif hybride pour aeronef a voilure tournante multirotor comprenant des moyens ameliores de conversion dc/ac |
US10934935B2 (en) * | 2017-01-30 | 2021-03-02 | Ge Aviation Systems Llc | Engine core assistance |
FR3069387B1 (fr) * | 2017-07-24 | 2019-08-30 | Safran Aircraft Engines | Harnais electrique |
US10855214B2 (en) * | 2019-04-09 | 2020-12-01 | Hamilton Sunstrand Corporation | Electrical powertrain for aircraft |
CN110395396B (zh) * | 2019-07-09 | 2021-05-25 | 西安爱生无人机技术有限公司 | 一种无人机自启动***及其控制方法 |
AT523006B1 (de) * | 2019-10-02 | 2022-05-15 | Dynell Gmbh | Bodenstromaggregat für das Bereitstellen von elektrischer Energie für Fluggeräte |
US11845388B2 (en) | 2021-05-20 | 2023-12-19 | General Electric Company | AC electrical power system for a vehicle |
US11670942B2 (en) | 2021-09-23 | 2023-06-06 | General Electric Company | Electrically driven distributed propulsion system |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3464927B2 (ja) * | 1999-01-22 | 2003-11-10 | 本田技研工業株式会社 | 発電機 |
US7210653B2 (en) * | 2002-10-22 | 2007-05-01 | The Boeing Company | Electric-based secondary power system architectures for aircraft |
US6998726B2 (en) * | 2002-12-10 | 2006-02-14 | Honeywell International Inc. | Method and system for providing single-phase excitation techniques to a start exciter in a starter/generator system |
RU2273945C1 (ru) * | 2004-10-07 | 2006-04-10 | Открытое Акционерное Общество "Агрегатное Конструкторское Бюро "Якорь" | Система электропитания |
FR2907762B1 (fr) * | 2006-10-27 | 2009-12-18 | Airbus France | Systeme de generation, conversion, distribution et demarrage electrique a bord d'un aeronef |
US7701082B2 (en) * | 2006-10-30 | 2010-04-20 | Honeywell International Inc. | Aerospace electrical power DC subsystem configuration using multi-functional DC/DC converter |
FR2930084B1 (fr) * | 2008-04-09 | 2012-06-08 | Thales Sa | Procede de gestion d'un reseau electrique |
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 |
FR2941107B1 (fr) * | 2009-01-09 | 2015-08-14 | Hispano Suiza Sa | Systeme electrique de demarrage des moteurs d'un aeronef |
FR2962404B1 (fr) * | 2010-07-08 | 2012-07-20 | Eurocopter France | Architecture electrique pour aeronef a voilure tournante a motorisation hybride |
FR2967847B1 (fr) | 2010-11-23 | 2015-06-26 | Hispano Suiza Sa | Procede et architecture de traitement de l'energie electrique regeneree d'un aeronef. |
US20140197681A1 (en) * | 2012-07-30 | 2014-07-17 | The Boeing Company | Electric system stabilizing system for aircraft |
-
2012
- 2012-05-11 FR FR1254333A patent/FR2990573B1/fr active Active
-
2013
- 2013-05-06 RU RU2014150040A patent/RU2641672C1/ru active
- 2013-05-06 US US14/400,449 patent/US9745943B2/en active Active
- 2013-05-06 EP EP13727264.7A patent/EP2847845B1/fr active Active
- 2013-05-06 CN CN201380024658.XA patent/CN104471819B/zh active Active
- 2013-05-06 WO PCT/FR2013/051007 patent/WO2013167837A2/fr active Application Filing
- 2013-05-06 JP JP2015510861A patent/JP6316281B2/ja not_active Expired - Fee Related
- 2013-05-06 BR BR112014027729-0A patent/BR112014027729B1/pt not_active IP Right Cessation
- 2013-05-06 CA CA2872724A patent/CA2872724C/fr active Active
Also Published As
Publication number | Publication date |
---|---|
CA2872724C (fr) | 2021-11-09 |
CN104471819B (zh) | 2017-11-14 |
EP2847845A2 (fr) | 2015-03-18 |
BR112014027729B1 (pt) | 2021-06-08 |
CN104471819A (zh) | 2015-03-25 |
US20150130186A1 (en) | 2015-05-14 |
US9745943B2 (en) | 2017-08-29 |
WO2013167837A2 (fr) | 2013-11-14 |
BR112014027729A2 (pt) | 2017-06-27 |
FR2990573B1 (fr) | 2015-11-20 |
JP2015525551A (ja) | 2015-09-03 |
CA2872724A1 (fr) | 2013-11-14 |
EP2847845B1 (fr) | 2018-07-04 |
RU2641672C1 (ru) | 2018-01-19 |
FR2990573A1 (fr) | 2013-11-15 |
WO2013167837A3 (fr) | 2014-02-27 |
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