ES2747639T3 - Control de carga periódica de dispositivo controlable de modificación de flujo de aire - Google Patents
Control de carga periódica de dispositivo controlable de modificación de flujo de aire Download PDFInfo
- Publication number
- ES2747639T3 ES2747639T3 ES14814607T ES14814607T ES2747639T3 ES 2747639 T3 ES2747639 T3 ES 2747639T3 ES 14814607 T ES14814607 T ES 14814607T ES 14814607 T ES14814607 T ES 14814607T ES 2747639 T3 ES2747639 T3 ES 2747639T3
- Authority
- ES
- Spain
- Prior art keywords
- wing
- camd
- aircraft
- control
- extension
- 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
- 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
- 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
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/02—Mounting or supporting thereof
-
- 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
-
- 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
- Y02T50/40—Weight 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)
- Transmission Devices (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Tires In General (AREA)
- User Interface Of Digital Computer (AREA)
- Traffic Control Systems (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US201361761187P | 2013-02-05 | 2013-02-05 | |
| PCT/US2014/014956 WO2014204524A2 (en) | 2013-02-05 | 2014-02-05 | Controllable airflow modification device periodic load control |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES2747639T3 true ES2747639T3 (es) | 2020-03-11 |
Family
ID=51686139
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES14814607T Active ES2747639T3 (es) | 2013-02-05 | 2014-02-05 | Control de carga periódica de dispositivo controlable de modificación de flujo de aire |
| ES19188968T Active ES2960524T3 (es) | 2013-02-05 | 2014-02-05 | Control de carga periódica de dispositivo controlable de modificación de flujo de aire |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES19188968T Active ES2960524T3 (es) | 2013-02-05 | 2014-02-05 | Control de carga periódica de dispositivo controlable de modificación de flujo de aire |
Country Status (6)
| Country | Link |
|---|---|
| US (4) | US9567066B2 (https=) |
| EP (2) | EP3594115B1 (https=) |
| JP (1) | JP6166386B2 (https=) |
| AU (1) | AU2014281189B2 (https=) |
| ES (2) | ES2747639T3 (https=) |
| WO (1) | WO2014204524A2 (https=) |
Families Citing this family (38)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DK2303685T3 (en) | 2008-06-20 | 2016-01-18 | Aviat Partners Inc | KRUM wingtip |
| US9302766B2 (en) * | 2008-06-20 | 2016-04-05 | Aviation Partners, Inc. | Split blended winglet |
| 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 |
| CN103717490B (zh) * | 2011-06-09 | 2016-08-17 | 航空伙伴股份有限公司 | 螺旋形机翼末梢以及飞行器 |
| EP2615026B1 (en) * | 2011-06-10 | 2018-04-04 | Airbus Defence and Space GmbH | Method and apparatus for minimizing dynamic structural loads of an aircraft |
| AU2014281189B2 (en) | 2013-02-05 | 2018-02-01 | Tamarack Aerospace Group, Inc. | Controllable airflow modification device periodic load control |
| US10562613B2 (en) | 2013-12-04 | 2020-02-18 | Tamarack Aerospace Group, Inc. | Adjustable lift modification wingtip |
| US10106244B2 (en) * | 2014-11-07 | 2018-10-23 | The Boeing Company | Backup system |
| GB2532228A (en) * | 2014-11-12 | 2016-05-18 | Airbus Operations Ltd | An aircraft wing |
| CN104989760B (zh) * | 2015-06-11 | 2018-04-06 | 贵州华烽电器有限公司 | 一种凸轮载荷机构及其算法 |
| US10149631B2 (en) * | 2015-07-24 | 2018-12-11 | Embraer S.A. | Structural health monitoring sensory system integrated to a self-adapting morphing system |
| US9873502B2 (en) * | 2016-01-05 | 2018-01-23 | The Boeing Company | Controlling airloads on aircraft folding wing tips |
| US10196143B2 (en) * | 2016-06-02 | 2019-02-05 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | System and method for modular unmanned aerial system |
| EP3269635A1 (en) * | 2016-07-12 | 2018-01-17 | The Aircraft Performance Company UG | Airplane wing |
| DE102016117638B4 (de) * | 2016-09-19 | 2018-05-24 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Verminderung von an einem Luftfahrzeug auftretenden Böenlasten |
| US10189565B2 (en) * | 2016-12-02 | 2019-01-29 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Modular unmanned aerial system with multi-mode propulsion |
| 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 |
| US10507901B2 (en) * | 2017-06-07 | 2019-12-17 | The Boeing Company | Protecting and ensuring readiness of a vehicle |
| US20190057180A1 (en) * | 2017-08-18 | 2019-02-21 | International Business Machines Corporation | System and method for design optimization using augmented reality |
| US10766602B2 (en) * | 2017-11-01 | 2020-09-08 | The Boeing Company | Mechanical droop for spoiler operation |
| EP3492374A3 (en) | 2017-11-29 | 2019-09-04 | Airbus Operations Limited | Retrofit flight control surface |
| WO2019118623A1 (en) | 2017-12-12 | 2019-06-20 | American Honda Motor Co., Inc. | Flow fence for an aircraft winglet |
| ES2905192T3 (es) * | 2018-01-15 | 2022-04-07 | The Aircraft Performance Company Gmbh | Ala de avión |
| US11001371B2 (en) * | 2018-08-07 | 2021-05-11 | The Boeing Company | Hydraulic droop control for aircraft wing |
| GB2576929A (en) * | 2018-09-07 | 2020-03-11 | Airbus Operations Ltd | A wing tip device |
| USD1110923S1 (en) * | 2018-11-15 | 2026-02-03 | Textron Innovations, Inc. | Aircraft |
| US11254416B2 (en) * | 2019-05-16 | 2022-02-22 | The Boeing Company | Method and apparatus for remote angle calibration and measurement |
| GB2602113A (en) | 2020-12-18 | 2022-06-22 | Airbus Operations Ltd | Stall trigger system |
| CN112810803A (zh) * | 2021-02-22 | 2021-05-18 | 中国民用航空飞行学院 | 一种用于加快翼尖涡耗散的飞机尾流调整装置 |
| 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 |
| GB2619276A (en) | 2022-05-25 | 2023-12-06 | Airbus Operations Ltd | Wing structures for supporting wing tip devices |
| GB2628523B (en) * | 2022-11-16 | 2025-07-09 | Airbus Operations Ltd | Aircraft wing |
| US12286226B2 (en) * | 2023-05-04 | 2025-04-29 | Lockheed Martin Corporation | Unmanned aerial vehicle wing pylon system |
| WO2025015071A1 (en) | 2023-07-10 | 2025-01-16 | Archer Aviation Inc. | Systems and methods for flight control of aircraft |
| US12552550B2 (en) * | 2023-07-24 | 2026-02-17 | The Boeing Company | System and method to detect anomalous wingtip extension for a folding wing tip aircraft |
| US12522376B2 (en) | 2023-07-24 | 2026-01-13 | The Boeing Company | System and method to detect anomalous wingtip extension for a folding wing tip aircraft |
Family Cites Families (74)
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| US2074201A (en) * | 1934-01-29 | 1937-03-16 | Avions Kellner Bechereau Soc | Airfoil used in aeronautics |
| US2418301A (en) * | 1942-07-24 | 1947-04-01 | Miles Aircraft Ltd | Aircraft supporting surface |
| US2576981A (en) * | 1949-02-08 | 1951-12-04 | Vogt Richard | Twisted wing tip fin for airplanes |
| US3218005A (en) * | 1961-12-06 | 1965-11-16 | Calderon Alberto Alvarez | High lift system for high speed aircraft |
| US3734432A (en) | 1971-03-25 | 1973-05-22 | G Low | Suppression of flutter |
| US3845918A (en) * | 1972-12-07 | 1974-11-05 | Rochester Applied Science Ass | Vortex dissipator |
| US4017041A (en) * | 1976-01-12 | 1977-04-12 | Nelson Wilbur C | Airfoil tip vortex control |
| US4172574A (en) * | 1976-06-16 | 1979-10-30 | National Research Development Corporation | Fluid stream deflecting members for aircraft bodies or the like |
| US4190219A (en) * | 1977-05-17 | 1980-02-26 | Lockheed Corporation | Vortex diffuser |
| DE2756107C2 (de) * | 1977-12-16 | 1980-02-28 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Hochwirksames Seitenleitwerk mit variabler Flügelgeometrie |
| US4245804B1 (en) * | 1977-12-19 | 1993-12-14 | K. Ishimitsu Kichio | Minimum drag wing configuration for aircraft operating at transonic speeds |
| US4205810A (en) * | 1977-12-19 | 1980-06-03 | The Boeing Company | Minimum drag wing configuration for aircraft operating at transonic speeds |
| US4247063A (en) * | 1978-08-07 | 1981-01-27 | Lockheed Corporation | Flight control mechanism for airplanes |
| US4240597A (en) * | 1978-08-28 | 1980-12-23 | Gates Learjet Corporation | Wing with improved leading edge for aircraft |
| US4365773A (en) * | 1979-04-11 | 1982-12-28 | Julian Wolkovitch | Joined wing aircraft |
| US4382569A (en) * | 1979-12-26 | 1983-05-10 | Grumman Aerospace Corporation | Wing tip flow control |
| US4725020A (en) * | 1980-12-09 | 1988-02-16 | The Boeing Company | Control system incorporating structural feedback |
| FR2521520A1 (fr) * | 1982-02-15 | 1983-08-19 | Daude Martine | Ailettes marginales a angles d'attaque variables |
| US4455004A (en) * | 1982-09-07 | 1984-06-19 | Lockheed Corporation | Flight control device for airplanes |
| DE3242584A1 (de) * | 1982-11-18 | 1984-05-24 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Anordnung von zusatzflaechen an den spitzen eines tragfluegels |
| DE3310510A1 (de) * | 1983-03-23 | 1984-09-27 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Flatterbremse bei flugzeugen |
| GB8314656D0 (en) * | 1983-05-26 | 1983-06-29 | Secr Defence | Aircraft control |
| US4545552A (en) * | 1983-06-20 | 1985-10-08 | Welles Stanley W | Airframe design |
| US4674709A (en) * | 1983-06-20 | 1987-06-23 | Welles Stanley W | Airframe design |
| US4671473A (en) * | 1984-11-08 | 1987-06-09 | Goodson Kenneth W | Airfoil |
| NL8500950A (nl) * | 1985-03-29 | 1986-10-16 | Fokker Bv | Rolroer van een vliegtuigvleugel. |
| DE3634250C1 (de) * | 1986-10-08 | 1988-03-03 | Dornier Gmbh | Fluggeraetesteuerung |
| US5039032A (en) * | 1988-11-07 | 1991-08-13 | The Boeing Company | High taper wing tip extension |
| US5072894A (en) * | 1989-10-02 | 1991-12-17 | Rockwell International Corporation | Apparatus and method for increasing the angle of attack operating range of an aircraft |
| WO1992001603A1 (en) * | 1990-07-25 | 1992-02-06 | Sadleir Vtol Aircraft Co. Pty. Ltd. | Thrust unit for vtol aircraft |
| US5156358A (en) * | 1991-04-11 | 1992-10-20 | Northrop Corporation | Aircraft outboard control |
| US5348253A (en) * | 1993-02-01 | 1994-09-20 | Gratzer Louis B | Blended winglet |
| JPH07205894A (ja) * | 1994-01-27 | 1995-08-08 | Mitsubishi Heavy Ind Ltd | 航空機のフラッタ抑制装置 |
| EP0716978B1 (en) * | 1994-12-16 | 2002-03-20 | Aldo Frediani | Large dimension aircraft |
| IL119392A (en) * | 1996-10-09 | 2004-01-04 | Rafael Armament Dev Authority | Device for reducing the drag at the base of a body |
| JPH10205579A (ja) * | 1997-01-21 | 1998-08-04 | Mitsubishi Heavy Ind Ltd | フラッタ防止装置 |
| JPH10240353A (ja) * | 1997-02-25 | 1998-09-11 | Mitsubishi Heavy Ind Ltd | 振動低減装置 |
| US6095459A (en) * | 1997-06-16 | 2000-08-01 | Codina; George | Method and apparatus for countering asymmetrical aerodynamic process subjected onto multi engine aircraft |
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| DE19819341C2 (de) * | 1998-04-30 | 2000-06-15 | Daimler Chrysler Aerospace | Verfahren zur Reduktion von an einem Flugzeug auftretenden Böenlasten unterhalb der Reiseflughöhe |
| US6227487B1 (en) * | 1999-05-05 | 2001-05-08 | Northrop Grumman Corporation | Augmented wing tip drag flap |
| DE19926832B4 (de) * | 1999-06-12 | 2005-09-15 | Airbus Deutschland Gmbh | Unterschallflugzeug vorzugsweise mit gepfeilten Tragflügeln |
| DE19950403C2 (de) * | 1999-10-20 | 2002-02-07 | Deutsch Zentr Luft & Raumfahrt | Flugzeug mit Mitteln zum Reduzieren der Wirbelstärke des Flügelhauptwirbelpaars |
| US6394397B1 (en) * | 2000-12-06 | 2002-05-28 | The Boeing Company | Lifting surface with active variable tip member and method for influencing lifting surface behavior therewith |
| US6484968B2 (en) * | 2000-12-11 | 2002-11-26 | Fort F. Felker | Aircraft with elliptical winglets |
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| DE10302514B4 (de) * | 2003-01-23 | 2008-12-18 | Eads Deutschland Gmbh | Strömungsmechanisch wirksame Fläche eines sich in einem Fluid bewegenden Geräts, insbesondere eines Fluggeräts, insbesondere Tragfläche eines Fluggeräts |
| GB0326228D0 (en) * | 2003-11-10 | 2003-12-17 | Airbus Uk Ltd | Wing tip device |
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| US7744038B2 (en) * | 2007-06-15 | 2010-06-29 | The Boeing Company | Controllable winglets |
| US8083185B2 (en) * | 2007-11-07 | 2011-12-27 | The Boeing Company | Aircraft wing tip having a variable incidence angle |
| FR2929241B1 (fr) * | 2008-03-31 | 2010-06-04 | Airbus France | Procede et dispositif de reduction du tremblement d'un avion. |
| US8128035B2 (en) * | 2008-04-15 | 2012-03-06 | The Boeing Company | Winglets with recessed surfaces, and associated systems and methods |
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| US20100163669A1 (en) * | 2008-12-29 | 2010-07-01 | Im Sunstar | Super aircraft structrue |
| GB0919019D0 (en) * | 2009-10-30 | 2009-12-16 | Airbus Operations Ltd | Aerofoil |
| 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 |
| 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 |
| US8439313B2 (en) * | 2010-10-15 | 2013-05-14 | The Boeing Company | Forward swept winglet |
| US8651431B1 (en) * | 2011-08-09 | 2014-02-18 | The Boeing Company | Aircraft with movable winglets and method of control |
| EP2834146B1 (en) * | 2012-04-03 | 2023-10-11 | Tamarack Aerospace Group, Inc. | Multiple controllable airflow modification devices |
| 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 |
| US11897601B2 (en) * | 2022-02-16 | 2024-02-13 | Jetzero, Inc. | Aircraft and methods of use for aerodynamic control with winglet surfaces |
-
2014
- 2014-02-05 AU AU2014281189A patent/AU2014281189B2/en not_active Ceased
- 2014-02-05 EP EP19188968.2A patent/EP3594115B1/en active Active
- 2014-02-05 ES ES14814607T patent/ES2747639T3/es active Active
- 2014-02-05 US US14/173,746 patent/US9567066B2/en active Active
- 2014-02-05 EP EP14814607.9A patent/EP2953849B1/en active Active
- 2014-02-05 JP JP2015557039A patent/JP6166386B2/ja not_active Expired - Fee Related
- 2014-02-05 WO PCT/US2014/014956 patent/WO2014204524A2/en not_active Ceased
- 2014-02-05 ES ES19188968T patent/ES2960524T3/es active Active
-
2017
- 2017-02-13 US US15/431,719 patent/US10562610B2/en active Active
-
2020
- 2020-02-14 US US16/792,069 patent/US12017753B2/en active Active
-
2024
- 2024-06-18 US US18/747,160 patent/US20250153843A1/en active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| JP6166386B2 (ja) | 2017-07-19 |
| EP3594115B1 (en) | 2023-08-23 |
| WO2014204524A3 (en) | 2015-03-12 |
| WO2014204524A2 (en) | 2014-12-24 |
| US20250153843A1 (en) | 2025-05-15 |
| AU2014281189A1 (en) | 2015-09-24 |
| JP2016510283A (ja) | 2016-04-07 |
| US10562610B2 (en) | 2020-02-18 |
| US20200324878A1 (en) | 2020-10-15 |
| US9567066B2 (en) | 2017-02-14 |
| US20170152021A1 (en) | 2017-06-01 |
| US20140306067A1 (en) | 2014-10-16 |
| HK1219933A1 (en) | 2017-04-21 |
| US12017753B2 (en) | 2024-06-25 |
| AU2014281189B2 (en) | 2018-02-01 |
| ES2960524T3 (es) | 2024-03-05 |
| EP3594115A1 (en) | 2020-01-15 |
| EP2953849B1 (en) | 2019-08-28 |
| EP2953849A2 (en) | 2015-12-16 |
| EP2953849A4 (en) | 2016-10-05 |
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