DE602005011025D1 - Automatische steuersysteme für hilfsenergieaggregate von flugzeugen und dazugehörige verfahren - Google Patents
Automatische steuersysteme für hilfsenergieaggregate von flugzeugen und dazugehörige verfahrenInfo
- Publication number
- DE602005011025D1 DE602005011025D1 DE602005011025T DE602005011025T DE602005011025D1 DE 602005011025 D1 DE602005011025 D1 DE 602005011025D1 DE 602005011025 T DE602005011025 T DE 602005011025T DE 602005011025 T DE602005011025 T DE 602005011025T DE 602005011025 D1 DE602005011025 D1 DE 602005011025D1
- Authority
- DE
- Germany
- Prior art keywords
- power unit
- auxiliary power
- aircraft
- automatic control
- control systems
- 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.)
- Active
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)
- Feedback Control In General (AREA)
- Direct Current Feeding And Distribution (AREA)
- Traffic Control Systems (AREA)
Applications Claiming Priority (2)
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 |
PCT/US2005/032738 WO2007001366A2 (en) | 2004-09-27 | 2005-09-14 | Automatic control systems for aircraft auxilliary power units, and associated methods |
Publications (1)
Publication Number | Publication Date |
---|---|
DE602005011025D1 true DE602005011025D1 (de) | 2008-12-24 |
Family
ID=36124605
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602005011025T Active DE602005011025D1 (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 (50)
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 |
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 |
US9267443B2 (en) | 2009-05-08 | 2016-02-23 | Gas Turbine Efficiency Sweden Ab | Automated tuning of gas turbine combustion systems |
US9354618B2 (en) | 2009-05-08 | 2016-05-31 | Gas Turbine Efficiency Sweden Ab | Automated tuning of multiple fuel gas turbine combustion systems |
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 |
US9399951B2 (en) | 2012-04-17 | 2016-07-26 | General Electric Company | Modular louver system |
US8511096B1 (en) | 2012-04-17 | 2013-08-20 | General Electric Company | High bleed flow muffling 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 |
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 |
US11014684B2 (en) | 2017-03-21 | 2021-05-25 | Textron Innovations, Inc. | Expedited preflight readiness system 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 |
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 |
EP4305653A1 (de) | 2021-03-12 | 2024-01-17 | Essex Industries, Inc. | Wippschalter |
US11688568B2 (en) | 2021-03-15 | 2023-06-27 | Essex Industries, Inc. | Five-position switch |
JP2022168713A (ja) | 2021-04-26 | 2022-11-08 | 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 |
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US2016253A (en) * | 1931-08-03 | 1935-10-01 | Noblitt Sparks Ind Inc | Muffler |
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AT254465B (de) * | 1963-12-09 | 1967-05-26 | Lothar Dr Ing Cremer | Absorptionsschalldämpfer für Gasleitungen, insbesondere Lüftungsleitungen |
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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 |
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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 |
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US6704625B2 (en) | 2001-02-16 | 2004-03-09 | Hamilton Sunstrand Corporation | Aircraft architecture with a reduced bleed aircraft secondary power system |
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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 active Active
-
2005
- 2005-09-14 DE DE602005011025T patent/DE602005011025D1/de active Active
- 2005-09-14 CA CA2583537A patent/CA2583537C/en active Active
- 2005-09-14 EP EP05858122A patent/EP1794054B1/de active Active
- 2005-09-14 AT AT05858122T patent/ATE414014T1/de not_active IP Right Cessation
- 2005-09-14 CA CA2856547A patent/CA2856547C/en active Active
- 2005-09-14 JP JP2007533539A patent/JP5112068B2/ja active Active
- 2005-09-14 WO PCT/US2005/032738 patent/WO2007001366A2/en active Application Filing
-
2008
- 2008-03-13 US US12/047,833 patent/US7891605B2/en active Active
-
2011
- 2011-02-04 US US13/021,422 patent/US8061650B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
CA2583537A1 (en) | 2007-01-04 |
EP1794054A2 (de) | 2007-06-13 |
ATE414014T1 (de) | 2008-11-15 |
CA2583537C (en) | 2014-11-04 |
US20110127372A1 (en) | 2011-06-02 |
CA2856547C (en) | 2016-10-18 |
EP1794054B1 (de) | 2008-11-12 |
WO2007001366A3 (en) | 2007-03-01 |
JP5112068B2 (ja) | 2013-01-09 |
WO2007001366A2 (en) | 2007-01-04 |
US7891605B2 (en) | 2011-02-22 |
US20090037036A1 (en) | 2009-02-05 |
US8061650B2 (en) | 2011-11-22 |
CA2856547A1 (en) | 2007-01-04 |
US20060071123A1 (en) | 2006-04-06 |
US7364116B2 (en) | 2008-04-29 |
JP2008514485A (ja) | 2008-05-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |