CA2593953C - Active systems and methods for controlling an airfoil vortex - Google Patents
Active systems and methods for controlling an airfoil vortex Download PDFInfo
- Publication number
- CA2593953C CA2593953C CA2593953A CA2593953A CA2593953C CA 2593953 C CA2593953 C CA 2593953C CA 2593953 A CA2593953 A CA 2593953A CA 2593953 A CA2593953 A CA 2593953A CA 2593953 C CA2593953 C CA 2593953C
- Authority
- CA
- Canada
- Prior art keywords
- orifice
- fluid
- fluid flow
- flow
- airfoil
- 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
- 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 (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US84012106P | 2006-08-25 | 2006-08-25 | |
| US60/840,121 | 2006-08-25 | ||
| US11/747,112 | 2007-05-10 | ||
| US11/747,112 US8016244B2 (en) | 2004-02-20 | 2007-05-10 | Active systems and methods for controlling an airfoil vortex |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2593953A1 CA2593953A1 (en) | 2008-02-25 |
| CA2593953C true CA2593953C (en) | 2010-09-28 |
Family
ID=38581956
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA2593953A Active CA2593953C (en) | 2006-08-25 | 2007-07-17 | Active systems and methods for controlling an airfoil vortex |
Country Status (7)
| Country | Link |
|---|---|
| US (2) | US8016244B2 (https=) |
| EP (1) | EP1892184B2 (https=) |
| JP (1) | JP5231770B2 (https=) |
| CN (1) | CN101134504B (https=) |
| AT (1) | ATE461861T1 (https=) |
| CA (1) | CA2593953C (https=) |
| DE (1) | DE602007005424D1 (https=) |
Families Citing this family (31)
| 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 |
| DE05858238T1 (de) * | 2004-10-15 | 2008-03-13 | Bell Helicopter Textron, Inc., Fort Worth | 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 |
| US8894018B2 (en) * | 2009-12-10 | 2014-11-25 | University Of The Witwatersrand | Method for reducing in flight wake vortices and an aircraft wingtip arrangement used in such method |
| 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 |
| GB201719016D0 (en) * | 2017-11-17 | 2018-01-03 | Airbus Operations Gmbh | Vortex generator arrangement and control system for an aircraft |
| 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 (en) * | 2019-05-23 | 2023-07-05 | Airbus Defence and Space GmbH | Method for active flow control, flow body, and aircraft |
| 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 |
| WO2021202629A1 (en) * | 2020-04-03 | 2021-10-07 | University Of Florida Research Foundation | Blade tip vortex control |
| 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 |
| US12265766B2 (en) | 2020-08-03 | 2025-04-01 | The Boeing Company | Methods and apparatus to improve fluid flow simulations |
| CN117262209A (zh) * | 2023-08-28 | 2023-12-22 | 北京航空航天大学 | 一种旋转飞行器 |
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| US20060145027A1 (en) * | 2003-06-11 | 2006-07-06 | Clyde Warsop | Method of controlling vortex bursting |
| DE50312100D1 (de) | 2003-07-25 | 2009-12-17 | Nikolai Alekseevich Baranov | Verfahren und system zur verhinderung, dass ein fl eines wirbelerzeugers eindringt |
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| US7661629B2 (en) | 2004-02-20 | 2010-02-16 | The Boeing Company | Systems and methods for destabilizing an airfoil vortex |
| US7100875B2 (en) * | 2004-02-20 | 2006-09-05 | The Boeing Company | Apparatus and method for the control of trailing wake flows |
| 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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| 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 EP EP07075636.6A patent/EP1892184B2/en not_active Ceased
- 2007-07-25 DE DE602007005424T patent/DE602007005424D1/de active Active
- 2007-07-25 AT AT07075636T patent/ATE461861T1/de not_active IP Right Cessation
- 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 not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| JP2008049998A (ja) | 2008-03-06 |
| EP1892184B1 (en) | 2010-03-24 |
| ATE461861T1 (de) | 2010-04-15 |
| US8016244B2 (en) | 2011-09-13 |
| EP1892184A1 (en) | 2008-02-27 |
| DE602007005424D1 (de) | 2010-05-06 |
| EP1892184B2 (en) | 2013-11-20 |
| CN101134504B (zh) | 2012-05-30 |
| CN101134504A (zh) | 2008-03-05 |
| CA2593953A1 (en) | 2008-02-25 |
| US20080042013A1 (en) | 2008-02-21 |
| JP5231770B2 (ja) | 2013-07-10 |
| US8376285B1 (en) | 2013-02-19 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| H11 | Ip right ceased following rejected request for revival |
Free format text: ST27 STATUS EVENT CODE: T-6-6-H10-H11-H101 (AS PROVIDED BY THE NATIONAL OFFICE); EVENT TEXT: TIME LIMIT FOR REVERSAL EXPIRED Effective date: 20250117 |