ATE414014T1 - Automatische steuersysteme für hilfsenergieaggregate von flugzeugen und dazugehörige verfahren - Google Patents
Automatische steuersysteme für hilfsenergieaggregate von flugzeugen und dazugehörige verfahrenInfo
- Publication number
- ATE414014T1 ATE414014T1 AT05858122T AT05858122T ATE414014T1 AT E414014 T1 ATE414014 T1 AT E414014T1 AT 05858122 T AT05858122 T AT 05858122T AT 05858122 T AT05858122 T AT 05858122T AT E414014 T1 ATE414014 T1 AT E414014T1
- Authority
- AT
- Austria
- Prior art keywords
- auxiliary power
- aircraft
- power unit
- controller
- automatic control
- Prior art date
Links
Classifications
-
- 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
-
- 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
- B64D2041/002—Mounting arrangements for auxiliary power units (APU's)
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Supply And Distribution Of Alternating Current (AREA)
- Remote Monitoring And Control Of Power-Distribution Networks (AREA)
- Traffic Control Systems (AREA)
- Direct Current Feeding And Distribution (AREA)
- Feedback Control In General (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/951,185 US7364116B2 (en) | 2004-09-27 | 2004-09-27 | Automatic control systems for aircraft auxiliary power units, and associated methods |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE414014T1 true ATE414014T1 (de) | 2008-11-15 |
Family
ID=36124605
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT05858122T ATE414014T1 (de) | 2004-09-27 | 2005-09-14 | Automatische steuersysteme für hilfsenergieaggregate von flugzeugen und dazugehörige verfahren |
Country Status (7)
| Country | Link |
|---|---|
| US (3) | US7364116B2 (de) |
| EP (1) | EP1794054B1 (de) |
| JP (1) | JP5112068B2 (de) |
| AT (1) | ATE414014T1 (de) |
| CA (2) | CA2583537C (de) |
| DE (1) | DE602005011025D1 (de) |
| WO (1) | WO2007001366A2 (de) |
Families Citing this family (54)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7210653B2 (en) * | 2002-10-22 | 2007-05-01 | The Boeing Company | Electric-based secondary power system architectures for aircraft |
| US7267297B2 (en) | 2004-09-02 | 2007-09-11 | The Boeing Company | Integrated axially varying engine muffler, and associated methods and systems |
| US7364116B2 (en) * | 2004-09-27 | 2008-04-29 | The Boeing Company | Automatic control systems for aircraft auxiliary power units, and associated methods |
| US7344107B2 (en) * | 2004-10-26 | 2008-03-18 | The Boeing Company | Dual flow APU inlet and associated systems and methods |
| US7513119B2 (en) * | 2005-02-03 | 2009-04-07 | The Boeing Company | Systems and methods for starting aircraft engines |
| US7622821B2 (en) * | 2005-05-25 | 2009-11-24 | Hamilton Sundstrand Corporation | Power distribution system and load management protocol therefor |
| US7290517B2 (en) * | 2005-07-28 | 2007-11-06 | Caterpillar Inc. | Automatic start-up of an auxiliary power unit |
| US8155876B2 (en) * | 2006-09-07 | 2012-04-10 | The Boeing Company | Systems and methods for controlling aircraft electrical power |
| US7765784B2 (en) * | 2006-09-25 | 2010-08-03 | The Boeing Company | Thermally compliant APU exhaust duct arrangements and associated systems and methods |
| DE102007013345B4 (de) * | 2007-03-20 | 2022-07-07 | Airbus Operations Gmbh | Energieregelvorrichtung für ein Flugzeug |
| US8201662B2 (en) * | 2007-07-06 | 2012-06-19 | Honeywell International Inc. | Electric motor driven lubrication pump control system and method for turbomachine windmill operation |
| US8480460B2 (en) * | 2007-10-01 | 2013-07-09 | United Technologies Corporation | Cabin air supercharged aircraft internal combustion engine |
| DE102008058451B4 (de) * | 2008-11-21 | 2010-11-18 | Airbus Deutschland Gmbh | Verfahren und System zur Notbelüftung einer Flugzeugkabine im Fall eines Lecks im Bereich eines Luftmischers |
| DE102009010243A1 (de) * | 2009-02-24 | 2010-09-02 | Airbus Deutschland Gmbh | Leistungserzeugungs-Vorrichtung sowie Rumpf-Bauteil mit einer solchen Leistungserzeugungs-Vorrichtung |
| US9354618B2 (en) | 2009-05-08 | 2016-05-31 | Gas Turbine Efficiency Sweden Ab | Automated tuning of multiple fuel gas turbine combustion systems |
| US9267443B2 (en) | 2009-05-08 | 2016-02-23 | Gas Turbine Efficiency Sweden Ab | Automated tuning of gas turbine combustion systems |
| US8437941B2 (en) | 2009-05-08 | 2013-05-07 | Gas Turbine Efficiency Sweden Ab | Automated tuning of gas turbine combustion systems |
| US9671797B2 (en) | 2009-05-08 | 2017-06-06 | Gas Turbine Efficiency Sweden Ab | Optimization of gas turbine combustion systems low load performance on simple cycle and heat recovery steam generator applications |
| US8657227B1 (en) | 2009-09-11 | 2014-02-25 | The Boeing Company | Independent power generation in aircraft |
| US8310076B2 (en) * | 2009-10-15 | 2012-11-13 | Hamilton Sundstrand Corporation | Gearless turbo-generator |
| US8424800B2 (en) * | 2010-06-23 | 2013-04-23 | Hamilton Sundstrand Corporation | Multi-source emergency power optimization |
| US8307943B2 (en) | 2010-07-29 | 2012-11-13 | General Electric Company | High pressure drop muffling system |
| US8738268B2 (en) | 2011-03-10 | 2014-05-27 | The Boeing Company | Vehicle electrical power management and distribution |
| US8892265B2 (en) * | 2011-03-21 | 2014-11-18 | Hamilton Sundstrand Corporation | Automatic ram air turbine deployment |
| US9347790B2 (en) * | 2011-07-05 | 2016-05-24 | Rosemount Aerospace Inc. | Power supply system with at least a primary power source and an auxiliary power source for powering an electronic flight bag depending on an whether an aircraft is in a flight condition |
| US8594864B2 (en) * | 2011-08-24 | 2013-11-26 | Sikorsky Aircraft Corporation | Torque based power limit cueing system and method |
| US20130098051A1 (en) * | 2011-10-19 | 2013-04-25 | Jaimer Valdez | Auxiliary power unit bleed cleaning function |
| FR2983319B1 (fr) * | 2011-11-25 | 2014-02-07 | Turbomeca | Procede et systeme de regulation de puissance en cas de defaillance d'au moins un moteur d'aeronef |
| US8430202B1 (en) | 2011-12-28 | 2013-04-30 | General Electric Company | Compact high-pressure exhaust muffling devices |
| US20130204544A1 (en) * | 2012-02-03 | 2013-08-08 | Gulfstream Aerospace Corporation | Methods and systems for determining airspeed of an aircraft |
| US8511096B1 (en) | 2012-04-17 | 2013-08-20 | General Electric Company | High bleed flow muffling system |
| US9399951B2 (en) | 2012-04-17 | 2016-07-26 | General Electric Company | Modular louver system |
| US8550208B1 (en) | 2012-04-23 | 2013-10-08 | General Electric Company | High pressure muffling devices |
| WO2014005070A1 (en) | 2012-06-28 | 2014-01-03 | Alaska Airlines, Inc. | Robust systems and methods for improving passenger jet aircraft fuel economy |
| US20140032002A1 (en) * | 2012-07-30 | 2014-01-30 | The Boeing Company | Electric system stabilizing system for aircraft |
| FR2994939B1 (fr) * | 2012-09-05 | 2014-08-22 | Turbomeca | Boitier a accessoires pour la commande de volets d'un aeronef |
| CN104344946B (zh) * | 2013-07-24 | 2017-12-05 | 中国国际航空股份有限公司 | Apu涡轮叶片断裂与转轴卡阻故障的监控方法和装置 |
| US9611050B2 (en) | 2013-07-26 | 2017-04-04 | The Boeing Company | Auxiliary power unit inlet apparatus and methods |
| EP3197773A4 (de) * | 2014-09-23 | 2018-02-21 | Sikorsky Aircraft Corporation | Hybrides elektrisches antriebssystem für drehflügelflugzeug |
| US9708069B2 (en) * | 2015-04-01 | 2017-07-18 | The Boeing Company | Ram air system and methods of manufacturing the same |
| US10240521B2 (en) | 2015-08-07 | 2019-03-26 | Pratt & Whitney Canada Corp. | Auxiliary power unit with variable speed ratio |
| US10239632B2 (en) | 2017-02-20 | 2019-03-26 | Pratt & Whitney Canada Corp. | System and method for controlling an auxiliary power unit inlet door |
| US10232951B2 (en) | 2017-02-20 | 2019-03-19 | Pratt & Whitney Canada Corp. | System and method for selecting an opening angle of an auxiliary power unit inlet door |
| US10974843B2 (en) | 2017-03-21 | 2021-04-13 | Textron Innovations, Inc. | Hot-swappable hybrid APU for aircraft |
| US11034463B2 (en) * | 2019-03-26 | 2021-06-15 | The Boeing Company | Aircraft auxiliary power unit (APU) control system having variably sized air inlet |
| US11385072B2 (en) | 2019-07-15 | 2022-07-12 | Honeywell International Inc. | Engine relight visualization methods and systems |
| CA3100782C (en) | 2019-11-27 | 2026-02-03 | Bombardier Inc. | Methods and systems for operating an auxiliary power unit |
| CN112478184B (zh) * | 2020-12-01 | 2024-03-19 | 陕西航空电气有限责任公司 | 一种涡桨支线飞机rat释放控制架构 |
| WO2022192698A1 (en) | 2021-03-12 | 2022-09-15 | Essex Industries, Inc., | Rocker switch |
| US11688568B2 (en) | 2021-03-15 | 2023-06-27 | Essex Industries, Inc. | Five-position switch |
| JP7533339B2 (ja) | 2021-04-26 | 2024-08-14 | トヨタ自動車株式会社 | 飛行体 |
| US11538203B2 (en) | 2021-05-10 | 2022-12-27 | Honeywell International Inc. | Capability envelope display methods and systems |
| US20250382064A1 (en) * | 2023-04-14 | 2025-12-18 | Embraer S.A. | Autonomous Engine Shutdown and Automatic Cooldown Time |
| US12320296B2 (en) * | 2023-09-07 | 2025-06-03 | Pratt & Whitney Canada Corp. | Aircraft engine assembly for controlling engine oil flow during fire conditions and method for using same |
Family Cites Families (70)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2016253A (en) * | 1931-08-03 | 1935-10-01 | Noblitt Sparks Ind Inc | Muffler |
| US2512155A (en) * | 1949-02-19 | 1950-06-20 | Gordon C Hill | Muffler with plural perforated conical baffles |
| US2988302A (en) * | 1959-01-14 | 1961-06-13 | Gen Sound Control Inc | Silencing means for aircraft |
| US3033307A (en) * | 1959-10-06 | 1962-05-08 | Industrial Acoustics Co | Noise attenuating apparatus |
| AT254465B (de) * | 1963-12-09 | 1967-05-26 | Lothar Dr Ing Cremer | Absorptionsschalldämpfer für Gasleitungen, insbesondere Lüftungsleitungen |
| US3382671A (en) * | 1965-12-16 | 1968-05-14 | Beta Corp | Control for gas turbine emergency power system |
| US3439774A (en) * | 1966-01-21 | 1969-04-22 | Boeing Co | Sound energy absorbing apparatus |
| US3437173A (en) * | 1966-11-25 | 1969-04-08 | Gen Electric | Gas turbine engine with screech attenuating means |
| US3519843A (en) * | 1967-11-17 | 1970-07-07 | Clark Equipment Co | Electrical power supply system |
| US3648803A (en) * | 1969-10-13 | 1972-03-14 | Walker Mfg Co | Exhaust system |
| US3680660A (en) * | 1970-07-27 | 1972-08-01 | Tenneco Inc | Multi-louvered roughness silencer |
| DE2110747B2 (de) * | 1971-03-06 | 1975-06-26 | Siemens Ag, 1000 Berlin Und 8000 Muenchen | Anfahreinrichtung für einen an eine Turbine angekuppelten Generator |
| US3913702A (en) * | 1973-06-04 | 1975-10-21 | Lockheed Aircraft Corp | Cellular sound absorptive structure |
| US3920095A (en) * | 1974-02-01 | 1975-11-18 | Brunswick Corp | Free flow sound attenuating device and method of using |
| CA1027002A (en) * | 1974-08-30 | 1978-02-28 | Horst W.W. Hehmann | Phased treatment noise suppressor for acoustic duct applications |
| US4001892A (en) * | 1975-03-17 | 1977-01-04 | Xerox Corporation | Contaminant trapping in rotating disk devices |
| US4064961A (en) * | 1976-04-05 | 1977-12-27 | Rohr Industries, Incorporated | Slanted cavity resonator |
| US4137992A (en) * | 1976-12-30 | 1979-02-06 | The Boeing Company | Turbojet engine nozzle for attenuating core and turbine noise |
| US4226297A (en) * | 1979-01-12 | 1980-10-07 | United Technologies Corporation | Acoustic treated exhaust plug for turbine engine |
| US4314621A (en) * | 1979-03-07 | 1982-02-09 | Caterpillar Tractor Co. | Fluidborne noise attenuator |
| US4244441A (en) * | 1979-07-31 | 1981-01-13 | The Garrett Corporation | Broad band acoustic attenuator |
| US4370560A (en) * | 1979-10-15 | 1983-01-25 | Sundstrand Corporation | Compressor load control for an auxiliary power unit |
| JPS56143310A (en) * | 1980-03-17 | 1981-11-09 | Hiruzu Ind Ltd | Muffler and silencing method |
| US4359136A (en) * | 1980-06-09 | 1982-11-16 | Nelson Industries Inc. | Muffler construction |
| US4418879A (en) * | 1980-12-29 | 1983-12-06 | The Boeing Company | Scoop and inlet for auxiliary power units and method |
| JPS57113919A (en) | 1980-12-30 | 1982-07-15 | Futaba Sangyo Kk | Side branch type silencer |
| US4360075A (en) * | 1981-05-11 | 1982-11-23 | General Motors Corporation | Low back pressure exhaust silencer for diesel locomotives |
| US4456830A (en) * | 1982-04-22 | 1984-06-26 | Lockheed Corporation | AC Motor-starting for aircraft engines using APU free turbine driven generators |
| US4706908A (en) * | 1984-10-10 | 1987-11-17 | Duncan Aviation, Inc. | Lightweight auxiliary power and forced air supply unit |
| US4645032A (en) * | 1985-09-05 | 1987-02-24 | The Garrett Corporation | Compact muffler apparatus and associated methods |
| US4744440A (en) * | 1987-06-10 | 1988-05-17 | Tenneco, Inc., Tenneco Automotive Bldg. | Exhaust gas silencing device |
| US4979587A (en) * | 1989-08-01 | 1990-12-25 | The Boeing Company | Jet engine noise suppressor |
| US5162620A (en) * | 1989-11-28 | 1992-11-10 | Allied-Signal Inc. | Dual flow turbine engine muffler |
| FI95747B (fi) * | 1991-01-17 | 1995-11-30 | Valmet Paper Machinery Inc | Matalien taajuuksien äänenvaimennin paperitehtaiden ilmakanaviin |
| US5152141A (en) | 1991-04-08 | 1992-10-06 | Avco Corporation | Management of electrically driven engine accessories |
| JPH05163925A (ja) | 1991-12-13 | 1993-06-29 | Toyoda Gosei Co Ltd | 消音装置 |
| US5365025A (en) * | 1992-01-24 | 1994-11-15 | Tennessee Gas Pipeline Company | Low backpressure straight-through reactive and dissipative muffler |
| US5655359A (en) * | 1995-05-15 | 1997-08-12 | The Boeing Company | Passive cooling device and method for cooling an auxiliary power unit on an airplane |
| FR2736966B1 (fr) * | 1995-07-17 | 1997-10-17 | Ferri Alain | Silencieux d'echappement pour moteur a explosion, pour aeronef |
| US5734239A (en) * | 1995-07-19 | 1998-03-31 | Turner; William W. | Automatic generator start up and shut off device |
| FR2742805B1 (fr) | 1995-12-20 | 1998-01-16 | Snecma | Systeme d'aide au redemarrage des moteurs apres perte totale de motorisation |
| US5899411A (en) | 1996-01-22 | 1999-05-04 | Sundstrand Corporation | Aircraft electrical system providing emergency power and electric starting of propulsion engines |
| US5782082A (en) * | 1996-06-13 | 1998-07-21 | The Boeing Company | Aircraft engine acoustic liner |
| EP0923488B1 (de) | 1996-08-02 | 2002-04-24 | Honeywell International Inc. | Abnehmbare integrierte flugzeugheckkonus und -hilfskrafteinheit |
| US6039287A (en) * | 1996-08-02 | 2000-03-21 | Alliedsignal Inc. | Detachable integral aircraft tailcone and power assembly |
| US6018233A (en) * | 1997-06-30 | 2000-01-25 | Sundstrand Corporation | Redundant starting/generating system |
| US6092360A (en) * | 1998-07-01 | 2000-07-25 | The Boeing Company | Auxiliary power unit passive cooling system |
| US6272838B1 (en) * | 1999-02-25 | 2001-08-14 | Alliedsignal, Inc. | Method and apparatus for controlling the inlet duct leading to an auxiliary power unit |
| US6158546A (en) * | 1999-06-25 | 2000-12-12 | Tenneco Automotive Inc. | Straight through muffler with conically-ended output passage |
| US6278262B1 (en) | 1999-12-20 | 2001-08-21 | Pratt & Whitney Canada Corp. | Auxiliary power unit system and method of operating an auxiliary power unit |
| US6264137B1 (en) * | 2000-02-25 | 2001-07-24 | Honeywell International Inc. | Inlet vortex bustor and ice protector for auxiliary power units |
| JP4300682B2 (ja) * | 2000-05-30 | 2009-07-22 | 株式会社島津製作所 | 走行体 |
| DE10027426B4 (de) * | 2000-06-02 | 2006-12-14 | Dr.Ing.H.C. F. Porsche Ag | Luftzuführungseinrichtung für eine Brennkraftmaschine |
| US6695094B2 (en) * | 2001-02-02 | 2004-02-24 | The Boeing Company | Acoustic muffler for turbine engine |
| AU2002242188A1 (en) | 2001-02-16 | 2002-09-04 | United Technologies Corporation | Improved aircraft architecture with a reduced bleed aircraft secondary power system |
| US6615576B2 (en) * | 2001-03-29 | 2003-09-09 | Honeywell International Inc. | Tortuous path quiet exhaust eductor system |
| US6698180B2 (en) * | 2001-08-01 | 2004-03-02 | Rolls-Royce Corporation | Particle separator for a turbine engine |
| US6651929B2 (en) * | 2001-10-29 | 2003-11-25 | Pratt & Whitney Canada Corp. | Passive cooling system for auxiliary power unit installation |
| US6735951B2 (en) * | 2002-01-04 | 2004-05-18 | Hamilton Sundstrand Corporation | Turbocharged auxiliary power unit with controlled high speed spool |
| BR0303436A (pt) * | 2002-09-06 | 2004-09-08 | Kao Corp | Processo de regenaração de enzima imobilizada |
| US7210653B2 (en) | 2002-10-22 | 2007-05-01 | The Boeing Company | Electric-based secondary power system architectures for aircraft |
| US6777822B1 (en) * | 2003-04-01 | 2004-08-17 | Hamilton Sundstrand Corporation | Control system for an auxiliary power unit |
| JP2005016553A (ja) | 2003-06-23 | 2005-01-20 | Nsk Ltd | 直動案内軸受装置 |
| US7014144B2 (en) * | 2003-07-22 | 2006-03-21 | Honeywell International, Inc. | Dual action inlet door and method for use thereof |
| US7439634B2 (en) | 2004-08-24 | 2008-10-21 | Honeywell International Inc. | Electrical starting, generation, conversion and distribution system architecture for a more electric vehicle |
| US7267297B2 (en) * | 2004-09-02 | 2007-09-11 | The Boeing Company | Integrated axially varying engine muffler, and associated methods and systems |
| US7364116B2 (en) * | 2004-09-27 | 2008-04-29 | The Boeing Company | Automatic control systems for aircraft auxiliary power units, and associated methods |
| US7344107B2 (en) * | 2004-10-26 | 2008-03-18 | The Boeing Company | Dual flow APU inlet and associated systems and methods |
| US20060163425A1 (en) | 2005-01-27 | 2006-07-27 | Honeywell International, Inc. | Aircraft inlet assembly for reducing auxiliary power unit noise |
| US7513119B2 (en) * | 2005-02-03 | 2009-04-07 | The Boeing Company | Systems and methods for starting aircraft engines |
-
2004
- 2004-09-27 US US10/951,185 patent/US7364116B2/en not_active Expired - Lifetime
-
2005
- 2005-09-14 DE DE602005011025T patent/DE602005011025D1/de not_active Expired - Lifetime
- 2005-09-14 EP EP05858122A patent/EP1794054B1/de not_active Expired - Lifetime
- 2005-09-14 CA CA2583537A patent/CA2583537C/en not_active Expired - Lifetime
- 2005-09-14 WO PCT/US2005/032738 patent/WO2007001366A2/en not_active Ceased
- 2005-09-14 CA CA2856547A patent/CA2856547C/en not_active Expired - Lifetime
- 2005-09-14 AT AT05858122T patent/ATE414014T1/de not_active IP Right Cessation
- 2005-09-14 JP JP2007533539A patent/JP5112068B2/ja not_active Expired - Lifetime
-
2008
- 2008-03-13 US US12/047,833 patent/US7891605B2/en not_active Expired - Lifetime
-
2011
- 2011-02-04 US US13/021,422 patent/US8061650B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| US20060071123A1 (en) | 2006-04-06 |
| CA2583537C (en) | 2014-11-04 |
| US8061650B2 (en) | 2011-11-22 |
| CA2583537A1 (en) | 2007-01-04 |
| JP5112068B2 (ja) | 2013-01-09 |
| US20110127372A1 (en) | 2011-06-02 |
| US7364116B2 (en) | 2008-04-29 |
| WO2007001366A3 (en) | 2007-03-01 |
| CA2856547A1 (en) | 2007-01-04 |
| DE602005011025D1 (de) | 2008-12-24 |
| JP2008514485A (ja) | 2008-05-08 |
| CA2856547C (en) | 2016-10-18 |
| US7891605B2 (en) | 2011-02-22 |
| WO2007001366A2 (en) | 2007-01-04 |
| US20090037036A1 (en) | 2009-02-05 |
| EP1794054B1 (de) | 2008-11-12 |
| EP1794054A2 (de) | 2007-06-13 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| ATE414014T1 (de) | Automatische steuersysteme für hilfsenergieaggregate von flugzeugen und dazugehörige verfahren | |
| WO2014153151A3 (en) | Systems and methods for detecting and determiniing sources of power disturbances in connection with effective remediation | |
| WO2017074480A8 (en) | Systems and methods for disengaging a battery | |
| GB2470535A (en) | Elevator dispatching control for sway mitigation | |
| ATE548789T1 (de) | Systeme und verfahren zur verteilten serienkompensation von stromversorgungsleitungen unter verwendung passiver bauelemente | |
| MY159476A (en) | Railway signaling system with redundant controllers | |
| TWI257050B (en) | Automated power control policies based on application-specific redundancy characteristics | |
| IN2014DN10293A (de) | ||
| WO2012022345A3 (de) | Verfahren zur steuerung einzelner photovoltaik-module einer photovoltaik-anlage und steuereinrichtung | |
| DE602004032397D1 (de) | Zwischenreglersteuerung von mehreren elektrischen Stromquellen | |
| WO2013043551A3 (en) | Control and protection for parallel uninterruptible power supplies | |
| EP2289767A3 (de) | Stabile Lenkregelverfahren und -systeme | |
| WO2007130954A3 (en) | Universal ac or dc aircraft device power supply having power factor correction | |
| EP2648322A1 (de) | Überbrückungsschaltung bei Stromunterbrechung | |
| TW200612233A (en) | Controlling standby power of low power devices | |
| ATE380364T1 (de) | Elektrischer flugregler für flugzeughöhenruder | |
| WO2008033526A3 (en) | Method of controlling a load control module as part of a startup sequence | |
| WO2007128763A3 (en) | Power supply system and method | |
| WO2012006028A3 (en) | System and method for dynamically managing power in an electronic device | |
| SE0403225D0 (sv) | A vehicle including compressed air consuming devices and a method of operating the same | |
| MX390953B (es) | Dispositivo de control de carga para controlar un controlador para una carga de iluminación | |
| EP1975763A3 (de) | Betriebsmittelleistungsregler | |
| ATE472125T1 (de) | Verfahren und vorrichtung zur lastbeleuchtung auf dem tragflächensystem eines flugzeugs in rollbewegung | |
| EP2765666A3 (de) | Flugzeugkabinenumgebungssteuerung | |
| US20140354061A1 (en) | Power supply device and switch method thereof |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |