ATE461861T1 - Aktive systeme und verfahren zur steuerung eines tragflächenwirbels - Google Patents
Aktive systeme und verfahren zur steuerung eines tragflächenwirbelsInfo
- Publication number
- ATE461861T1 ATE461861T1 AT07075636T AT07075636T ATE461861T1 AT E461861 T1 ATE461861 T1 AT E461861T1 AT 07075636 T AT07075636 T AT 07075636T AT 07075636 T AT07075636 T AT 07075636T AT E461861 T1 ATE461861 T1 AT E461861T1
- Authority
- AT
- Austria
- Prior art keywords
- flow
- tip
- vortex
- actuator
- vortices
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
- B64C23/065—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips
- B64C23/069—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips using one or more wing tip airfoil devices, e.g. winglets, splines, wing tip fences or raked wingtips
- B64C23/076—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips using one or more wing tip airfoil devices, e.g. winglets, splines, wing tip fences or raked wingtips the wing tip airfoil devices comprising one or more separate moveable members thereon affecting the vortices, e.g. flaps
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
- B64C23/065—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips
-
- 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
- Y02T50/10—Drag reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Medicines Containing Plant Substances (AREA)
- Acyclic And Carbocyclic Compounds In Medicinal Compositions (AREA)
- Agricultural Chemicals And Associated Chemicals (AREA)
- Jet Pumps And Other Pumps (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US84012106P | 2006-08-25 | 2006-08-25 | |
US11/747,112 US8016244B2 (en) | 2004-02-20 | 2007-05-10 | Active systems and methods for controlling an airfoil vortex |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE461861T1 true ATE461861T1 (de) | 2010-04-15 |
Family
ID=38581956
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT07075636T ATE461861T1 (de) | 2006-08-25 | 2007-07-25 | Aktive systeme und verfahren zur steuerung eines tragflächenwirbels |
Country Status (7)
Country | Link |
---|---|
US (2) | US8016244B2 (de) |
EP (1) | EP1892184B2 (de) |
JP (1) | JP5231770B2 (de) |
CN (1) | CN101134504B (de) |
AT (1) | ATE461861T1 (de) |
CA (1) | CA2593953C (de) |
DE (1) | DE602007005424D1 (de) |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7100875B2 (en) * | 2004-02-20 | 2006-09-05 | The Boeing Company | Apparatus and method for the control of trailing wake flows |
US7661629B2 (en) * | 2004-02-20 | 2010-02-16 | The Boeing Company | Systems and methods for destabilizing an airfoil vortex |
EP1828883B1 (de) * | 2004-10-15 | 2015-12-23 | Bell Helicopter Textron, Inc. | Verfahren für den entwurf eines flugzeuges |
US7686253B2 (en) * | 2006-08-10 | 2010-03-30 | The Boeing Company | Systems and methods for tracing aircraft vortices |
US8232706B2 (en) * | 2009-01-09 | 2012-07-31 | The Boeing Company | Autonomous power generation unit for auxiliary system on an airborne platform |
CN102762453B (zh) * | 2009-12-10 | 2015-03-25 | 约翰内斯堡威特沃特斯兰德大学 | 减少飞行尾迹涡流的方法和在其中使用的飞行器翼尖装置 |
US8449255B2 (en) * | 2010-03-21 | 2013-05-28 | Btpatent Llc | Wind turbine blade system with air passageway |
GB201011843D0 (en) * | 2010-07-14 | 2010-09-01 | Airbus Operations Ltd | Wing tip device |
CN101885381A (zh) * | 2010-07-15 | 2010-11-17 | 沈阳航空航天大学 | 带凹坑的机翼 |
US20170088254A1 (en) * | 2011-03-10 | 2017-03-30 | RuiQing Hong | Ultra-High-Pressure Fluid Injection Dynamic Orbit-Transfer System and Method |
US9227719B2 (en) * | 2011-03-11 | 2016-01-05 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Reactive orthotropic lattice diffuser for noise reduction |
US9132909B1 (en) * | 2011-03-11 | 2015-09-15 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Flap edge noise reduction fins |
US8632031B2 (en) | 2011-04-11 | 2014-01-21 | The Boeing Company | Systems and methods for attenuation of noise and wakes produced by aircraft |
CN102530242A (zh) * | 2011-12-01 | 2012-07-04 | 中国航天空气动力技术研究院 | 一种翼尖噪声控制方法及装置 |
US9511849B2 (en) * | 2012-10-27 | 2016-12-06 | The Boeing Company | Fluidic traverse actuator |
US9243622B2 (en) * | 2013-05-22 | 2016-01-26 | The Boeing Company | Bellows synthetic jet |
US10562613B2 (en) * | 2013-12-04 | 2020-02-18 | Tamarack Aerospace Group, Inc. | Adjustable lift modification wingtip |
GB2535488A (en) * | 2015-02-17 | 2016-08-24 | Airbus Operations Ltd | An arrangement for effecting movement of a wing tip device between a flight configuration and a ground configuration |
CN104760683B (zh) * | 2015-05-04 | 2016-04-27 | 厦门大学 | 利用零质量射流减小机翼激波阻力的方法 |
DE102015107626B4 (de) * | 2015-05-15 | 2019-11-07 | Airbus Defence and Space GmbH | Strömungssteuerungsvorrichtung, Strömungsdynamischer Profilkörper und Strömungssteuerungsverfahren mit Schallwellenerzeugung |
CN107187612B (zh) * | 2017-04-25 | 2019-06-18 | 北京航空航天大学 | 一种加快机场跑道尾涡消散的方法及其实现装置 |
GB2576929A (en) * | 2018-09-07 | 2020-03-11 | Airbus Operations Ltd | A wing tip device |
US10829204B2 (en) * | 2018-11-30 | 2020-11-10 | Textron Innovations Inc. | Electric reaction control system |
EP3741668B1 (de) * | 2019-05-23 | 2023-07-05 | Airbus Defence and Space GmbH | Verfahren zur aktiven strömungssteuerung, strömungskörper sowie flugzeug |
CN110588957A (zh) * | 2019-10-08 | 2019-12-20 | 江西洪都航空工业集团有限责任公司 | 一种机翼翼尖涡流动控制方法 |
CN111516854B (zh) * | 2020-04-03 | 2021-08-10 | 中国空气动力研究与发展中心低速空气动力研究所 | 一种促进喷流偏转的流动控制部件 |
US20200339248A1 (en) * | 2020-06-30 | 2020-10-29 | Papa Abdoulaye MBODJ | Boundary layer suction design by using wingtip vortex for a lift-generating body |
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US6963291B2 (en) * | 2002-05-17 | 2005-11-08 | The Board Of Trustees Of The Leland Stanford Junior University | Dynamic wake prediction and visualization with uncertainty analysis |
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WO2005010554A1 (fr) * | 2003-07-25 | 2005-02-03 | Zakrytoe Aktsionernoe Obschestvo Rossiyskaya Aktsionernaya Assotsiatsiya 'spetstekhnika' | Procede et systeme d'avertissement concernant l'entree possible d'un aeronef dans une zone dangereuse de sillage tourbillonnaire de generateur de tourbillons |
US7100875B2 (en) * | 2004-02-20 | 2006-09-05 | The Boeing Company | Apparatus and method for the control of trailing wake flows |
US7661629B2 (en) * | 2004-02-20 | 2010-02-16 | The Boeing Company | Systems and methods for destabilizing an airfoil vortex |
US7510149B2 (en) * | 2004-08-02 | 2009-03-31 | Lockheed Martin Corporation | System and method to control flowfield vortices with micro-jet arrays |
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US7635107B2 (en) * | 2005-08-09 | 2009-12-22 | The Boeing Company | System for aerodynamic flows and associated method |
US8033510B2 (en) * | 2005-08-09 | 2011-10-11 | The Boeing Company | Lift augmentation system and associated method |
US7104143B1 (en) | 2005-08-11 | 2006-09-12 | The Boeing Company | Oscillating vane actuator apparatus and method for active flow control |
US7686253B2 (en) * | 2006-08-10 | 2010-03-30 | The Boeing Company | Systems and methods for tracing aircraft vortices |
US20080035784A1 (en) * | 2006-08-10 | 2008-02-14 | Meserole Jere S | Aircraft wake vortex predictor and visualizer |
US7748664B2 (en) * | 2006-08-23 | 2010-07-06 | Lockheed Martin Corporation | High performance synthetic valve/pulsator |
FR2908167B1 (fr) * | 2006-11-03 | 2009-02-20 | Centre Nat Rech Scient | Dispositif pour retarder le decollement d'une couche limite |
-
2007
- 2007-05-10 US US11/747,112 patent/US8016244B2/en not_active Expired - Fee Related
- 2007-07-17 CA CA2593953A patent/CA2593953C/en active Active
- 2007-07-25 DE DE602007005424T patent/DE602007005424D1/de active Active
- 2007-07-25 AT AT07075636T patent/ATE461861T1/de not_active IP Right Cessation
- 2007-07-25 EP EP07075636.6A patent/EP1892184B2/de not_active Ceased
- 2007-08-14 JP JP2007211294A patent/JP5231770B2/ja not_active Expired - Fee Related
- 2007-08-27 CN CN2007101424383A patent/CN101134504B/zh not_active Expired - Fee Related
-
2011
- 2011-06-14 US US13/159,424 patent/US8376285B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
CA2593953A1 (en) | 2008-02-25 |
US8376285B1 (en) | 2013-02-19 |
JP2008049998A (ja) | 2008-03-06 |
EP1892184B1 (de) | 2010-03-24 |
CN101134504A (zh) | 2008-03-05 |
CA2593953C (en) | 2010-09-28 |
EP1892184B2 (de) | 2013-11-20 |
EP1892184A1 (de) | 2008-02-27 |
US20080042013A1 (en) | 2008-02-21 |
DE602007005424D1 (de) | 2010-05-06 |
JP5231770B2 (ja) | 2013-07-10 |
CN101134504B (zh) | 2012-05-30 |
US8016244B2 (en) | 2011-09-13 |
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