AU2010326260B2 - Active winglet - Google Patents
Active winglet Download PDFInfo
- Publication number
- AU2010326260B2 AU2010326260B2 AU2010326260A AU2010326260A AU2010326260B2 AU 2010326260 B2 AU2010326260 B2 AU 2010326260B2 AU 2010326260 A AU2010326260 A AU 2010326260A AU 2010326260 A AU2010326260 A AU 2010326260A AU 2010326260 B2 AU2010326260 B2 AU 2010326260B2
- Authority
- AU
- Australia
- Prior art keywords
- aircraft
- winglet
- wing
- modification device
- airflow modification
- 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.)
- Ceased
Links
- 230000004048 modification Effects 0.000 claims abstract description 47
- 238000012986 modification Methods 0.000 claims abstract description 47
- 238000000034 method Methods 0.000 claims description 11
- 238000005452 bending Methods 0.000 claims description 5
- 230000004044 response Effects 0.000 abstract description 2
- 230000008878 coupling Effects 0.000 description 10
- 238000010168 coupling process Methods 0.000 description 10
- 238000005859 coupling reaction Methods 0.000 description 10
- 238000013461 design Methods 0.000 description 10
- 230000008859 change Effects 0.000 description 5
- 230000008901 benefit Effects 0.000 description 4
- 230000000694 effects Effects 0.000 description 2
- 230000000670 limiting effect Effects 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000002803 fossil fuel Substances 0.000 description 1
- 230000006870 function Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000000135 prohibitive effect Effects 0.000 description 1
- 230000002829 reductive effect Effects 0.000 description 1
- 230000002441 reversible effect Effects 0.000 description 1
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
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
-
- 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)
- Automation & Control Theory (AREA)
- Toys (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Mechanical Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AU2013200686A AU2013200686B2 (en) | 2009-12-01 | 2013-02-08 | Active winglet |
Applications Claiming Priority (7)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US26553409P | 2009-12-01 | 2009-12-01 | |
| US61/265,534 | 2009-12-01 | ||
| US12/797,742 | 2010-06-10 | ||
| US12/797,742 US20110127383A1 (en) | 2009-12-01 | 2010-06-10 | Active winglet |
| US12/890,557 | 2010-09-24 | ||
| US12/890,557 US7900877B1 (en) | 2009-12-01 | 2010-09-24 | Active winglet |
| PCT/US2010/056586 WO2011068659A2 (en) | 2009-12-01 | 2010-11-12 | Active winglet |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AU2013200686A Division AU2013200686B2 (en) | 2009-12-01 | 2013-02-08 | Active winglet |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| AU2010326260A1 AU2010326260A1 (en) | 2012-06-14 |
| AU2010326260B2 true AU2010326260B2 (en) | 2012-11-08 |
Family
ID=43639207
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AU2010326260A Ceased AU2010326260B2 (en) | 2009-12-01 | 2010-11-12 | Active winglet |
Country Status (6)
| Country | Link |
|---|---|
| US (7) | US20110127383A1 (enExample) |
| EP (1) | EP2346734B1 (enExample) |
| JP (3) | JP5542955B2 (enExample) |
| AU (1) | AU2010326260B2 (enExample) |
| ES (1) | ES2533402T3 (enExample) |
| WO (1) | WO2011068659A2 (enExample) |
Families Citing this family (43)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8544800B2 (en) * | 2005-07-21 | 2013-10-01 | The Boeing Company | Integrated wingtip extensions for jet transport aircraft and other types of aircraft |
| US9302766B2 (en) | 2008-06-20 | 2016-04-05 | Aviation Partners, Inc. | Split blended winglet |
| WO2009155584A1 (en) | 2008-06-20 | 2009-12-23 | Aviation Partners, Inc. | Curved wing tip |
| DE102009019542A1 (de) * | 2009-04-30 | 2010-11-11 | Airbus Deutschland Gmbh | Nicht-planares Flügelendstück für Tragflügel von Flugzeugen sowie Tragflügel mit einem solchen Flügelendstück |
| US20110127383A1 (en) | 2009-12-01 | 2011-06-02 | Guida Associates Consulting, Inc. | Active winglet |
| US9162755B2 (en) * | 2009-12-01 | 2015-10-20 | Tamarack Aerospace Group, Inc. | Multiple controllable airflow modification devices |
| GB201011843D0 (en) | 2010-07-14 | 2010-09-01 | Airbus Operations Ltd | Wing tip device |
| FR2970699B1 (fr) * | 2011-01-25 | 2014-11-28 | Lisa Airplanes | Avion motorise a structure mixte hydrodynamique et aerodynamique pour le decollage et l'atterrissage sur l'eau, le sol ou la neige |
| ES2856270T3 (es) | 2011-06-09 | 2021-09-27 | Aviation Partners Inc | El winglet integrado doble |
| EP2551737B1 (en) * | 2011-07-28 | 2015-04-29 | Airbus Defence and Space GmbH | Method and apparatus for minimizing dynamic structural loads of an aircraft |
| DE102011116841B4 (de) * | 2011-10-25 | 2017-10-26 | Airbus Defence and Space GmbH | Höhenluftfahrzeug, Luftfahrzeugverband und Verfahren zum Betreiben eines Luftfahrzeugverbands |
| GB201120862D0 (en) * | 2011-12-05 | 2012-01-18 | Airbus Operations Ltd | A wingtip fin of an aircraft |
| ES2964283T3 (es) | 2012-04-03 | 2024-04-05 | Tamarack Aerospace Group Inc | Dispositivos múltiples de modificación de flujo de aire controlables |
| US8788122B1 (en) | 2012-08-24 | 2014-07-22 | The Boeing Company | Wing load alleviation methods and apparatus |
| AU2014281189B2 (en) * | 2013-02-05 | 2018-02-01 | Tamarack Aerospace Group, Inc. | Controllable airflow modification device periodic load control |
| US9845159B2 (en) * | 2013-03-07 | 2017-12-19 | United Technologies Corporation | Conjoined reverse core flow engine arrangement |
| WO2015050617A2 (en) * | 2013-07-15 | 2015-04-09 | Design Intelligence Incorporated, LLC | Unmanned aerial vehicle (uav) with inter-connecting wing sections |
| US10562613B2 (en) * | 2013-12-04 | 2020-02-18 | Tamarack Aerospace Group, Inc. | Adjustable lift modification wingtip |
| JP6758183B2 (ja) * | 2013-12-05 | 2020-09-23 | タマラック エアロスペース グループ インコーポレイテッド | ウィングチップデバイス |
| USD732657S1 (en) * | 2014-02-27 | 2015-06-23 | Delta T Corporation | Winglet |
| 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 |
| DE102015008974A1 (de) * | 2015-07-10 | 2017-01-12 | Liebherr-Aerospace Lindenberg Gmbh | Winglet mit steuerbarem Luftwiderstandselement |
| CN106802205B (zh) * | 2015-11-26 | 2019-08-02 | 中国飞行试验研究院 | 一种消除剖面内载荷影响的飞行载荷测量方法 |
| GB2551554B (en) * | 2016-06-22 | 2018-08-15 | Airbus Operations Ltd | Methods of configuring a wing tip device on an aircraft |
| EP3269635A1 (en) * | 2016-07-12 | 2018-01-17 | The Aircraft Performance Company UG | Airplane wing |
| US10710702B2 (en) * | 2016-08-12 | 2020-07-14 | Aviation Partners, Inc. | Shape adaptive airfoil |
| RU2637149C1 (ru) * | 2016-11-02 | 2017-11-30 | Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") | Спироидный винглет |
| US10745107B1 (en) * | 2017-05-08 | 2020-08-18 | Government Of The United States, As Represented By The Secretary Of The Air Force | Rapid flap deflection for high lift transients |
| USD858421S1 (en) * | 2017-09-28 | 2019-09-03 | Tesla, Inc. | Winglet |
| EP3492374A3 (en) | 2017-11-29 | 2019-09-04 | Airbus Operations Limited | Retrofit flight control surface |
| GB201719806D0 (en) * | 2017-11-29 | 2018-01-10 | Airbus Operations Ltd | Retrofit flight control surface |
| ES2905192T3 (es) * | 2018-01-15 | 2022-04-07 | The Aircraft Performance Company Gmbh | Ala de avión |
| GB2576929A (en) * | 2018-09-07 | 2020-03-11 | Airbus Operations Ltd | A wing tip device |
| GB2580930A (en) * | 2019-01-30 | 2020-08-05 | Airbus Operations Ltd | Fairing for folding wing tip |
| WO2022087607A1 (en) * | 2020-10-20 | 2022-04-28 | Roland Industries, Inc. | Mono-winged drone |
| CN113665787B (zh) * | 2021-09-24 | 2023-11-24 | 肇庆市海特复合材料技术研究院 | 一种复合材料无人机机翼结构 |
| GB2615311A (en) * | 2022-01-31 | 2023-08-09 | Airbus Operations Ltd | Aircraft wing with movable wing tip device |
| GB2616252A (en) * | 2022-01-31 | 2023-09-06 | Airbus Operations Ltd | Aircraft with movable wing tip device |
| US11897601B2 (en) | 2022-02-16 | 2024-02-13 | Jetzero, Inc. | Aircraft and methods of use for aerodynamic control with winglet surfaces |
| GB2628523B (en) * | 2022-11-16 | 2025-07-09 | Airbus Operations Ltd | Aircraft wing |
| US12428138B2 (en) | 2023-09-08 | 2025-09-30 | Textron Innovations Inc. | Blended falx winglet |
| USD1073579S1 (en) | 2023-09-08 | 2025-05-06 | Textron Innovations, Inc. | Blended falx winglet |
| CN117208195A (zh) * | 2023-10-31 | 2023-12-12 | 南京航空航天大学 | 飞行器尾翼伸缩机构、单体飞行器和组合式飞行器 |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5988563A (en) * | 1997-12-30 | 1999-11-23 | Mcdonnell Douglas Corporation | Articulating winglets |
| US7275722B2 (en) * | 2003-11-10 | 2007-10-02 | Airbus Uk Limited | Wing tip device |
| US20090200431A1 (en) * | 2007-11-07 | 2009-08-13 | Konings Christopher A | Aircraft wing tip having a variable incidence angle |
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| US20100163669A1 (en) * | 2008-12-29 | 2010-07-01 | Im Sunstar | Super aircraft structrue |
| US9162755B2 (en) * | 2009-12-01 | 2015-10-20 | Tamarack Aerospace Group, Inc. | Multiple controllable airflow modification devices |
| US20110127383A1 (en) * | 2009-12-01 | 2011-06-02 | Guida Associates Consulting, Inc. | Active winglet |
| US8651431B1 (en) | 2011-08-09 | 2014-02-18 | The Boeing Company | Aircraft with movable winglets and method of control |
| ES2964283T3 (es) | 2012-04-03 | 2024-04-05 | Tamarack Aerospace Group Inc | Dispositivos múltiples de modificación de flujo de aire controlables |
| AU2014281189B2 (en) * | 2013-02-05 | 2018-02-01 | Tamarack Aerospace Group, Inc. | Controllable airflow modification device periodic load control |
| US9469391B1 (en) * | 2013-04-26 | 2016-10-18 | The Boeing Company | Adaptive wing for an aircraft |
| US10562613B2 (en) * | 2013-12-04 | 2020-02-18 | Tamarack Aerospace Group, Inc. | Adjustable lift modification wingtip |
| US10710702B2 (en) * | 2016-08-12 | 2020-07-14 | Aviation Partners, Inc. | Shape adaptive airfoil |
-
2010
- 2010-06-10 US US12/797,742 patent/US20110127383A1/en not_active Abandoned
- 2010-09-24 US US12/890,557 patent/US7900877B1/en active Active
- 2010-11-12 EP EP10821429.7A patent/EP2346734B1/en active Active
- 2010-11-12 WO PCT/US2010/056586 patent/WO2011068659A2/en not_active Ceased
- 2010-11-12 AU AU2010326260A patent/AU2010326260B2/en not_active Ceased
- 2010-11-12 JP JP2012542043A patent/JP5542955B2/ja not_active Expired - Fee Related
- 2010-11-12 ES ES10821429.7T patent/ES2533402T3/es active Active
-
2011
- 2011-03-30 US US13/075,934 patent/US8684315B2/en active Active
-
2014
- 2014-03-21 US US14/222,437 patent/US9764825B2/en active Active
- 2014-05-07 JP JP2014096151A patent/JP2014193717A/ja active Pending
-
2017
- 2017-02-27 JP JP2017035382A patent/JP6854667B2/ja not_active Expired - Fee Related
- 2017-09-18 US US15/707,991 patent/US10486797B2/en active Active
-
2019
- 2019-11-25 US US16/694,875 patent/US11884383B2/en active Active
-
2024
- 2024-01-24 US US18/421,610 patent/US20240409204A1/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5988563A (en) * | 1997-12-30 | 1999-11-23 | Mcdonnell Douglas Corporation | Articulating winglets |
| US7275722B2 (en) * | 2003-11-10 | 2007-10-02 | Airbus Uk Limited | Wing tip device |
| US20090200431A1 (en) * | 2007-11-07 | 2009-08-13 | Konings Christopher A | Aircraft wing tip having a variable incidence angle |
Also Published As
| Publication number | Publication date |
|---|---|
| US7900877B1 (en) | 2011-03-08 |
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| US20240409204A1 (en) | 2024-12-12 |
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| ES2533402T3 (es) | 2015-04-09 |
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| EP2346734B1 (en) | 2015-01-07 |
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| US10486797B2 (en) | 2019-11-26 |
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