UA92725C2 - Система питания и управления электрооборудованием двигателя летательного аппарата или его оснащение - Google Patents
Система питания и управления электрооборудованием двигателя летательного аппарата или его оснащениеInfo
- Publication number
- UA92725C2 UA92725C2 UAA200704982A UAA200704982A UA92725C2 UA 92725 C2 UA92725 C2 UA 92725C2 UA A200704982 A UAA200704982 A UA A200704982A UA A200704982 A UAA200704982 A UA A200704982A UA 92725 C2 UA92725 C2 UA 92725C2
- Authority
- UA
- Ukraine
- Prior art keywords
- modules
- electrical equipment
- equipment
- powering
- environment
- Prior art date
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
- 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
- H02J1/00—Circuit arrangements for dc mains or dc distribution networks
- H02J1/10—Parallel operation of dc sources
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Supply And Distribution Of Alternating Current (AREA)
- Safety Devices In Control Systems (AREA)
- Stand-By Power Supply Arrangements (AREA)
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
- Direct Current Feeding And Distribution (AREA)
- Control Of Electric Motors In General (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
Abstract
Система питания и управления электрооборудованием двигателя летательного аппарата или его оборудования содержит по крайней мере одну шину питания напряжением постоянного тока, по крайней мере один блок модулей питания, при этом количество модулей превышает минимальное количество, необходимое для питания электрооборудования группы таким образом, чтобы задействовать резервный модуль, при этом каждый модуль содержит преобразователь напряжения для получения на своем выходе напряжения переменного тока из напряжения постоянного тока на шине питания, и блок коммутации, включенный между выходами блока модулей и оборудованием группы оборудования. Модули и блок коммутации управляются для питания каждого вида оборудования группы оборудования, связывая его с по крайней мере одним из модулей, и путем использования резервного модуля при выходе из строя одного из других модулей.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0651637A FR2900635B1 (fr) | 2006-05-05 | 2006-05-05 | Systeme d'alimentation et de commande d'equipements electriques d'un moteur d'aeronef ou de son environnement |
Publications (1)
Publication Number | Publication Date |
---|---|
UA92725C2 true UA92725C2 (ru) | 2010-12-10 |
Family
ID=37560847
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
UAA200704982A UA92725C2 (ru) | 2006-05-05 | 2007-05-04 | Система питания и управления электрооборудованием двигателя летательного аппарата или его оснащение |
Country Status (14)
Country | Link |
---|---|
US (1) | US7482709B2 (ru) |
EP (1) | EP1852347B1 (ru) |
JP (1) | JP5047683B2 (ru) |
CN (1) | CN101068080B (ru) |
AT (1) | ATE435152T1 (ru) |
CA (1) | CA2587068C (ru) |
DE (1) | DE602007001408D1 (ru) |
ES (1) | ES2329303T3 (ru) |
FR (1) | FR2900635B1 (ru) |
IL (1) | IL182911A (ru) |
PL (1) | PL1852347T3 (ru) |
RU (1) | RU2416871C2 (ru) |
SG (1) | SG136937A1 (ru) |
UA (1) | UA92725C2 (ru) |
Families Citing this family (46)
Publication number | Priority date | Publication date | Assignee | Title |
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US7468561B2 (en) * | 2007-03-27 | 2008-12-23 | General Electric Company | Integrated electrical power extraction for aircraft engines |
FR2920143B1 (fr) * | 2007-08-20 | 2010-01-22 | Aircelle Sa | Dispositif de commande des actionneurs de maintenance de capots d'une nacelle de turboreacteur |
US8125164B2 (en) * | 2008-07-18 | 2012-02-28 | The Boeing Company | Parallel motor controller architecture |
KR20110073517A (ko) * | 2008-09-23 | 2011-06-29 | 에어로바이론먼트 인크 | 원격 디바이스 제어 및 전원 장치 |
US8237416B2 (en) * | 2008-12-09 | 2012-08-07 | Hamilton Sundstrand Corporation | More electric engine with regulated permanent magnet machines |
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 |
FR2941107B1 (fr) * | 2009-01-09 | 2015-08-14 | Hispano Suiza Sa | Systeme electrique de demarrage des moteurs d'un aeronef |
US8949666B2 (en) | 2009-02-12 | 2015-02-03 | President And Fellows Of Harvard College | Adaptive event-guided system and method for avoiding voltage emergencies |
GB2468652B (en) | 2009-03-16 | 2011-08-31 | Ge Aviat Systems Ltd | Electrical power distribution |
FR2948337B1 (fr) * | 2009-07-24 | 2011-07-29 | Aircelle Sa | Circuit d'alimentation electrique pour nacelle de turboreacteur |
FR2951330B1 (fr) * | 2009-10-13 | 2013-03-08 | Messier Bugatti | Reseau de pilotage pour actionneurs mono ou multimoteurs, particulierement adapte a des applications aeronautiques telles que l'alimentation de moteurs de boitiers d'accrochage |
GB0919041D0 (en) * | 2009-10-30 | 2009-12-16 | Goodrich Control Sys | Power distribution apparatus |
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 |
FR2958060B1 (fr) * | 2010-03-24 | 2012-04-27 | Snecma | Procede et dispositif de detection d'une defaillance electrique affectant un systeme electrique de commande d'un actionneur hydraulique de geometries variables d'un moteur d'aeronef. |
US8446041B2 (en) * | 2010-07-12 | 2013-05-21 | Hamilton Sundstrand Corporation | No break power transfer with solid state power controls |
CN102092475A (zh) * | 2010-12-30 | 2011-06-15 | 清华大学 | 无人直升机着陆自动熄火系统 |
FR2980052B1 (fr) * | 2011-09-14 | 2013-09-06 | Hispano Suiza Sa | Stabilisation d'un reseau electrique dc |
FR2983248B1 (fr) * | 2011-11-29 | 2015-04-03 | Turbomeca | Turbomachine comportant une pompe d'alimentation en carburant a activation electrique et procede d'alimentation en carburant d'une turbomachine |
US9172272B2 (en) | 2012-02-17 | 2015-10-27 | Sikorsky Aircraft Corporation | Electrical power distribution system |
US9248907B2 (en) | 2012-03-06 | 2016-02-02 | Sikorsky Aircraft Corporation | Engine starting system for rotorcraft in flight |
FR3001443B1 (fr) * | 2013-01-30 | 2016-05-27 | Microturbo | Procede et systeme d'alimentation en energie electrique d'un aeronef |
US9771154B2 (en) | 2013-02-28 | 2017-09-26 | Bae Systems Controls Inc. | Seat power systems and methods |
US9561867B2 (en) * | 2013-10-11 | 2017-02-07 | The Boeing Company | Modular equipment center lightning threat reduction architecture |
US9488130B2 (en) | 2013-10-17 | 2016-11-08 | Honeywell International Inc. | Variable area fan nozzle systems with improved drive couplings |
US9209721B2 (en) | 2014-04-29 | 2015-12-08 | The Boeing Company | Systems and methods for the control and operation of a parallel motor controller architecture |
US9991719B2 (en) | 2014-09-30 | 2018-06-05 | The Boeing Company | Systems and methods for reducing circulating current and phase to phase imbalance in a parallel modular converter system |
US10079493B2 (en) * | 2014-09-30 | 2018-09-18 | The Boeing Company | Parallel modular converter architecture |
FR3039207B1 (fr) * | 2015-07-21 | 2019-07-26 | Safran Aircraft Engines | Carter d'echappement d'une turbomachine a duree de vie augmentee |
US10020759B2 (en) | 2015-08-04 | 2018-07-10 | The Boeing Company | Parallel modular converter architecture for efficient ground electric vehicles |
CN105429434B (zh) * | 2015-11-05 | 2018-12-07 | 浙江大华技术股份有限公司 | 电源控制装置、控制器以及供电系统 |
US9991778B2 (en) * | 2016-02-29 | 2018-06-05 | The Boeing Company | Balancing current within a modular converter system |
US10408217B2 (en) | 2016-03-15 | 2019-09-10 | General Electric Company | Controlling a compressor of a gas turbine engine |
US10454393B2 (en) | 2016-07-25 | 2019-10-22 | The Boeing Company | Balancing current within a parallel modular converter system |
US10396554B2 (en) * | 2017-02-13 | 2019-08-27 | The Boeing Company | Power distribution control within a modular converter system using efficiency calculations |
US10101749B1 (en) | 2017-03-21 | 2018-10-16 | Bell Helicopter Textron Inc. | Combined airspeed and inertial data for rotorcraft longitudinal control |
US10942527B2 (en) | 2017-05-30 | 2021-03-09 | Textron Innovations Inc. | System and method for controlling rotorcraft load priority |
CN109272785A (zh) * | 2018-11-20 | 2019-01-25 | 安徽奕甲文化传媒有限责任公司 | 远程教育系统 |
US11027719B2 (en) * | 2018-12-03 | 2021-06-08 | General Electric Company | Distributed power generation for a vehicle system |
FR3093870B1 (fr) * | 2019-03-15 | 2021-04-02 | Safran Electrical & Power | Système de commande d’un réseau électrique d’avion |
GB201913016D0 (en) * | 2019-09-10 | 2019-10-23 | Rolls Royce Plc | Elctrical systems |
GB201913017D0 (en) | 2019-09-10 | 2019-10-23 | Rolls Royce Plc | Electrical system |
GB201913015D0 (en) * | 2019-09-10 | 2019-10-23 | Rolls Royce Plc | electrical systems |
FR3116397A1 (fr) * | 2020-11-18 | 2022-05-20 | Safran Helicopter Engines | Système d’alimentation et de commande d’un actionneur |
WO2022192698A1 (en) | 2021-03-12 | 2022-09-15 | Essex Industries, Inc., | Rocker switch |
WO2022197730A1 (en) | 2021-03-15 | 2022-09-22 | Essex Industries, Inc. | Five-position switch |
US11686757B2 (en) * | 2021-09-14 | 2023-06-27 | Hamilton Sundstrand Corporation | Systems and methods for circuit failure protection |
Family Cites Families (11)
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DE2319319C3 (de) * | 1973-04-17 | 1979-12-06 | Brown, Boveri & Cie Ag, 6800 Mannheim | Stromversorgungssystem aus parallel arbeitenden Wechselstromerzeugern |
JPS6181132A (ja) * | 1984-09-25 | 1986-04-24 | 三菱重工業株式会社 | 航空機用多重電源方式 |
FI84680C (fi) * | 1988-06-01 | 1991-12-27 | Teknoware Oy | Reservkraftdriftsystem. |
JPH03265430A (ja) * | 1990-03-14 | 1991-11-26 | Hitachi Ltd | 電力供給システムおよびその制御方法 |
EP0409226A3 (en) * | 1989-07-21 | 1993-01-13 | Hitachi, Ltd. | Power supply control system |
US5233286A (en) * | 1991-07-29 | 1993-08-03 | Sundstrand Corporation | Hybrid 270 volt DC system |
DE59502398D1 (de) * | 1994-09-21 | 1998-07-09 | Inventio Ag | Verfahren und Einrichtung zur variablen Zuteilung von in Betrieb stehenden Umrichtern auf mindestens eine Last |
ATE365391T1 (de) * | 2001-01-22 | 2007-07-15 | Siemens Ag | Energiesystem für wasserfahrzeuge |
US6704625B2 (en) * | 2001-02-16 | 2004-03-09 | Hamilton Sunstrand Corporation | Aircraft architecture with a reduced bleed aircraft secondary power system |
JP4778625B2 (ja) * | 2001-03-06 | 2011-09-21 | 株式会社Nttファシリティーズ | 無停電電源システム |
FR2865864B1 (fr) * | 2004-01-30 | 2006-05-19 | Messier Bugatti | Installation de gestion de puissance dans un avion. |
-
2006
- 2006-05-05 FR FR0651637A patent/FR2900635B1/fr not_active Expired - Fee Related
-
2007
- 2007-05-01 IL IL18291107A patent/IL182911A/en active IP Right Grant
- 2007-05-02 SG SG200703165-1A patent/SG136937A1/en unknown
- 2007-05-02 JP JP2007121440A patent/JP5047683B2/ja active Active
- 2007-05-03 RU RU2007116767A patent/RU2416871C2/ru active
- 2007-05-03 ES ES07107389T patent/ES2329303T3/es active Active
- 2007-05-03 PL PL07107389T patent/PL1852347T3/pl unknown
- 2007-05-03 EP EP20070107389 patent/EP1852347B1/fr active Active
- 2007-05-03 US US11/743,936 patent/US7482709B2/en active Active
- 2007-05-03 CA CA2587068A patent/CA2587068C/fr active Active
- 2007-05-03 DE DE200760001408 patent/DE602007001408D1/de active Active
- 2007-05-03 AT AT07107389T patent/ATE435152T1/de not_active IP Right Cessation
- 2007-05-04 UA UAA200704982A patent/UA92725C2/ru unknown
- 2007-05-08 CN CN2007101017635A patent/CN101068080B/zh active Active
Also Published As
Publication number | Publication date |
---|---|
SG136937A1 (en) | 2007-11-29 |
DE602007001408D1 (de) | 2009-08-13 |
RU2007116767A (ru) | 2008-11-20 |
CA2587068C (fr) | 2014-04-08 |
ES2329303T3 (es) | 2009-11-24 |
CN101068080B (zh) | 2010-09-29 |
ATE435152T1 (de) | 2009-07-15 |
IL182911A0 (en) | 2007-08-19 |
CN101068080A (zh) | 2007-11-07 |
JP2007306786A (ja) | 2007-11-22 |
RU2416871C2 (ru) | 2011-04-20 |
IL182911A (en) | 2010-11-30 |
CA2587068A1 (fr) | 2007-11-05 |
JP5047683B2 (ja) | 2012-10-10 |
US7482709B2 (en) | 2009-01-27 |
PL1852347T3 (pl) | 2009-12-31 |
EP1852347A1 (fr) | 2007-11-07 |
FR2900635B1 (fr) | 2008-07-25 |
US20070259545A1 (en) | 2007-11-08 |
EP1852347B1 (fr) | 2009-07-01 |
FR2900635A1 (fr) | 2007-11-09 |
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