WO2002083497A1 - Extremite d'aile cylindrique a fente helicoidale - Google Patents
Extremite d'aile cylindrique a fente helicoidale Download PDFInfo
- Publication number
- WO2002083497A1 WO2002083497A1 PCT/FR2002/001232 FR0201232W WO02083497A1 WO 2002083497 A1 WO2002083497 A1 WO 2002083497A1 FR 0201232 W FR0201232 W FR 0201232W WO 02083497 A1 WO02083497 A1 WO 02083497A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- wing
- helical slot
- cylindrical
- drag
- speed
- 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
-
- 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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
-
- 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
Abstract
Description
Claims
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IL15832702A IL158327A0 (en) | 2001-04-11 | 2002-04-09 | Cylindrical wing tip with helical slot |
EP02761928A EP1456081B1 (fr) | 2001-04-11 | 2002-04-09 | Extremite d'aile cylindrique a fente helicoidale |
DE60232462T DE60232462D1 (de) | 2001-04-11 | 2002-04-09 | Zylindrische flügelspitze mit schraubenförmigem schlitz |
US10/474,879 US6892988B2 (en) | 2001-04-11 | 2002-04-09 | Cylindrical wing tip with helical slot |
AT02761928T ATE432213T1 (de) | 2001-04-11 | 2002-04-09 | Zylindrische flügelspitze mit schraubenförmigem schlitz |
CA002443940A CA2443940C (fr) | 2001-04-11 | 2002-04-09 | Extremite d'aile cylindrique a fente helicoidale |
IL158327A IL158327A (en) | 2001-04-11 | 2003-10-09 | Cylindrical wing tip with helical groove |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0104998A FR2823541B1 (fr) | 2001-04-11 | 2001-04-11 | Extremite d'aile cylindrique a fente helicoidale |
FR01/04998 | 2001-04-11 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2002083497A1 true WO2002083497A1 (fr) | 2002-10-24 |
Family
ID=8862251
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/FR2002/001232 WO2002083497A1 (fr) | 2001-04-11 | 2002-04-09 | Extremite d'aile cylindrique a fente helicoidale |
Country Status (8)
Country | Link |
---|---|
US (1) | US6892988B2 (fr) |
EP (1) | EP1456081B1 (fr) |
AT (1) | ATE432213T1 (fr) |
CA (1) | CA2443940C (fr) |
DE (1) | DE60232462D1 (fr) |
FR (1) | FR2823541B1 (fr) |
IL (2) | IL158327A0 (fr) |
WO (1) | WO2002083497A1 (fr) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2883935A1 (fr) | 2005-04-01 | 2006-10-06 | Christian Hugues | Dispositif d'extremite de profil d'aile ou de gouverme a fentes helicoidales croisees pour utilisation en milieu aquatique |
US7270214B1 (en) | 2004-06-16 | 2007-09-18 | Westerngeco L.L.C. | Method and apparatus for reducing and extracting wing-tip vortex energy |
WO2009141536A1 (fr) | 2008-05-14 | 2009-11-26 | Christian Hugues | Dispositif d'extremite d'aile, de pale d'eolienne ou d' hydrolienne permettant de diminuer voire d'annuler les tourbillons marginaux dits vortex. |
US9039380B2 (en) | 2011-04-30 | 2015-05-26 | General Electric Company | Winglet for a wind turbine rotor blade |
US9103325B2 (en) | 2012-03-20 | 2015-08-11 | General Electric Company | Winglet for a wind turbine rotor blade |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AUPR982302A0 (en) * | 2002-01-03 | 2002-01-31 | Pax Fluid Systems Inc. | A fluid flow controller |
AUPR982502A0 (en) * | 2002-01-03 | 2002-01-31 | Pax Fluid Systems Inc. | A heat exchanger |
EA005545B1 (ru) * | 2002-01-03 | 2005-04-28 | Пакс Сайентифик, Инк. | Генератор вихревого кольца |
AU2003903386A0 (en) * | 2003-07-02 | 2003-07-17 | Pax Scientific, Inc | Fluid flow control device |
KR101168098B1 (ko) * | 2003-11-04 | 2012-07-24 | 팍스 싸이언티픽 인코퍼레이션 | 유체 순환 시스템 |
WO2005073560A1 (fr) * | 2004-01-30 | 2005-08-11 | Pax Scientific, Inc | Rotor a flux en vortex |
EA009581B1 (ru) * | 2004-01-30 | 2008-02-28 | Пакс Сайентифик, Инк. | Корпус для центрифугальных вентиляторов, насосов или турбин |
US20080232973A1 (en) * | 2005-07-21 | 2008-09-25 | Saint Louis University | Propeller blade |
US7644892B1 (en) * | 2006-07-06 | 2010-01-12 | Alford Jr Lionel D | Blended winglet |
WO2008042251A2 (fr) | 2006-09-29 | 2008-04-10 | Pax Streamline, Inc. | Ventilateur hélicoïdal |
US20090308472A1 (en) * | 2008-06-15 | 2009-12-17 | Jayden David Harman | Swirl Inducer |
US8651813B2 (en) * | 2009-05-29 | 2014-02-18 | Donald James Long | Fluid dynamic body having escapelet openings for reducing induced and interference drag, and energizing stagnant flow |
US8561938B2 (en) | 2010-05-31 | 2013-10-22 | Executive Access Inc. | Directional control for a helicopter |
GB201011843D0 (en) * | 2010-07-14 | 2010-09-01 | Airbus Operations Ltd | Wing tip device |
US8857761B2 (en) | 2010-10-27 | 2014-10-14 | Ata Engineering, Inc. | Variable geometry aircraft pylon structure and related operation techniques |
US9567867B2 (en) | 2011-09-14 | 2017-02-14 | Ata Engineering, Inc. | Methods and apparatus for deployable swirl vanes |
WO2013056300A1 (fr) * | 2011-10-18 | 2013-04-25 | Newcastle Innovation Limited | Générateur de tourbillons |
US9399919B2 (en) | 2012-12-31 | 2016-07-26 | General Electric Company | Extension tip sleeve for wind turbine blade |
US10318903B2 (en) | 2016-05-06 | 2019-06-11 | General Electric Company | Constrained cash computing system to optimally schedule aircraft repair capacity with closed loop dynamic physical state and asset utilization attainment control |
GB2570170B (en) * | 2018-06-15 | 2020-03-04 | James Punter Thomas | Wing-tip device |
JP2020121683A (ja) * | 2019-01-31 | 2020-08-13 | 三菱重工業株式会社 | 流体調整装置及び航空機 |
US11396367B2 (en) * | 2019-05-08 | 2022-07-26 | The Boeing Company | Vortex reduction apparatus for use with airfoils |
CN112926148B (zh) * | 2021-01-28 | 2023-02-03 | 西北工业大学 | 一种考虑三维效应影响下的螺旋桨翼型气动外形设计方法 |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR405177A (fr) | 1909-07-17 | 1909-12-22 | Georges Barbaudy | Dispositif pour sustenteur d'aviation |
US2075817A (en) | 1934-08-17 | 1937-04-06 | Arthur W Loerke | Wing vortex reducer |
US2576981A (en) * | 1949-02-08 | 1951-12-04 | Vogt Richard | Twisted wing tip fin for airplanes |
FR57646E (fr) | 1947-08-08 | 1953-03-17 | Perfectionnements apportés aux engins de navigation aérienne | |
US3596854A (en) | 1969-06-09 | 1971-08-03 | William R Haney Jr | Vortex generator for airfoil structures |
FR2294085A1 (fr) * | 1974-12-11 | 1976-07-09 | Garrett Corp | Procede et appareil de controle de tourbillon produit a une extremite d'un vehicule |
DE3127257A1 (de) | 1981-07-10 | 1983-01-27 | Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen | "verfahren zur verminderung des induzierten widestandes eines auftriebserzeugenden tragfluegels sowie vorrichtung zu seiner durchfuehrung" |
US4477042A (en) * | 1981-01-19 | 1984-10-16 | Griswold Ii Roger W | Vortex alleviating wing tip |
US5102068A (en) * | 1991-02-25 | 1992-04-07 | Gratzer Louis B | Spiroid-tipped wing |
US5297764A (en) * | 1993-03-15 | 1994-03-29 | Haney William R | Air foil providing vortex attenuation |
FR2780700A1 (fr) | 1998-07-02 | 2000-01-07 | Christian Hugues | Cavite cylindrique en spirale |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4533101A (en) * | 1984-02-02 | 1985-08-06 | The United States Of America As Represented By The Administrator Of The National Aeronautics & Space Administration | Wingtip vortex propeller |
US5332177A (en) * | 1993-09-09 | 1994-07-26 | Boyle Jr James J | Aircraft |
US6474604B1 (en) * | 1999-04-12 | 2002-11-05 | Jerry E. Carlow | Mobius-like joining structure for fluid dynamic foils |
US6371414B1 (en) * | 1999-07-16 | 2002-04-16 | Lockheed Martin Corporation | System and method for manipulating and controlling fluid flow over a surface |
US6260809B1 (en) * | 2000-04-05 | 2001-07-17 | United Technologies Corporation | Ovate loop for rotary-wing blades |
-
2001
- 2001-04-11 FR FR0104998A patent/FR2823541B1/fr not_active Expired - Fee Related
-
2002
- 2002-04-09 IL IL15832702A patent/IL158327A0/xx unknown
- 2002-04-09 CA CA002443940A patent/CA2443940C/fr not_active Expired - Lifetime
- 2002-04-09 WO PCT/FR2002/001232 patent/WO2002083497A1/fr not_active Application Discontinuation
- 2002-04-09 DE DE60232462T patent/DE60232462D1/de not_active Expired - Lifetime
- 2002-04-09 EP EP02761928A patent/EP1456081B1/fr not_active Expired - Lifetime
- 2002-04-09 AT AT02761928T patent/ATE432213T1/de not_active IP Right Cessation
- 2002-04-09 US US10/474,879 patent/US6892988B2/en not_active Expired - Fee Related
-
2003
- 2003-10-09 IL IL158327A patent/IL158327A/en not_active IP Right Cessation
Patent Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR405177A (fr) | 1909-07-17 | 1909-12-22 | Georges Barbaudy | Dispositif pour sustenteur d'aviation |
US2075817A (en) | 1934-08-17 | 1937-04-06 | Arthur W Loerke | Wing vortex reducer |
FR57646E (fr) | 1947-08-08 | 1953-03-17 | Perfectionnements apportés aux engins de navigation aérienne | |
US2576981A (en) * | 1949-02-08 | 1951-12-04 | Vogt Richard | Twisted wing tip fin for airplanes |
US3596854A (en) | 1969-06-09 | 1971-08-03 | William R Haney Jr | Vortex generator for airfoil structures |
FR2294085A1 (fr) * | 1974-12-11 | 1976-07-09 | Garrett Corp | Procede et appareil de controle de tourbillon produit a une extremite d'un vehicule |
US4477042A (en) * | 1981-01-19 | 1984-10-16 | Griswold Ii Roger W | Vortex alleviating wing tip |
DE3127257A1 (de) | 1981-07-10 | 1983-01-27 | Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen | "verfahren zur verminderung des induzierten widestandes eines auftriebserzeugenden tragfluegels sowie vorrichtung zu seiner durchfuehrung" |
US5102068A (en) * | 1991-02-25 | 1992-04-07 | Gratzer Louis B | Spiroid-tipped wing |
US5297764A (en) * | 1993-03-15 | 1994-03-29 | Haney William R | Air foil providing vortex attenuation |
FR2780700A1 (fr) | 1998-07-02 | 2000-01-07 | Christian Hugues | Cavite cylindrique en spirale |
WO2000001580A1 (fr) | 1998-07-02 | 2000-01-13 | Christian Hugues | Bout d'aile cylindrique et en spirale |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7270214B1 (en) | 2004-06-16 | 2007-09-18 | Westerngeco L.L.C. | Method and apparatus for reducing and extracting wing-tip vortex energy |
FR2883935A1 (fr) | 2005-04-01 | 2006-10-06 | Christian Hugues | Dispositif d'extremite de profil d'aile ou de gouverme a fentes helicoidales croisees pour utilisation en milieu aquatique |
WO2009141536A1 (fr) | 2008-05-14 | 2009-11-26 | Christian Hugues | Dispositif d'extremite d'aile, de pale d'eolienne ou d' hydrolienne permettant de diminuer voire d'annuler les tourbillons marginaux dits vortex. |
US8585371B2 (en) | 2008-05-14 | 2013-11-19 | Christian Hugues | Wingtip device for the tip of a wing, blade of a wind generator or marine generator for reducing or even eliminating marginal swirl |
US9039380B2 (en) | 2011-04-30 | 2015-05-26 | General Electric Company | Winglet for a wind turbine rotor blade |
US9103325B2 (en) | 2012-03-20 | 2015-08-11 | General Electric Company | Winglet for a wind turbine rotor blade |
US10047719B2 (en) | 2012-03-20 | 2018-08-14 | General Electric Company | Winglet for a wind turbine rotor blade |
Also Published As
Publication number | Publication date |
---|---|
IL158327A (en) | 2009-09-22 |
IL158327A0 (en) | 2004-05-12 |
CA2443940A1 (fr) | 2002-10-24 |
EP1456081A1 (fr) | 2004-09-15 |
FR2823541A1 (fr) | 2002-10-18 |
ATE432213T1 (de) | 2009-06-15 |
EP1456081B1 (fr) | 2009-05-27 |
FR2823541B1 (fr) | 2003-05-23 |
US6892988B2 (en) | 2005-05-17 |
US20040195461A1 (en) | 2004-10-07 |
DE60232462D1 (de) | 2009-07-09 |
CA2443940C (fr) | 2009-01-13 |
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