FR2948628B1 - Avion a controle en lacet par trainee differentielle - Google Patents
Avion a controle en lacet par trainee differentielleInfo
- Publication number
- FR2948628B1 FR2948628B1 FR0955454A FR0955454A FR2948628B1 FR 2948628 B1 FR2948628 B1 FR 2948628B1 FR 0955454 A FR0955454 A FR 0955454A FR 0955454 A FR0955454 A FR 0955454A FR 2948628 B1 FR2948628 B1 FR 2948628B1
- Authority
- FR
- France
- Prior art keywords
- lacet
- airplane
- control
- differential training
- training
- 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
-
- 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)
- Details Of Aerials (AREA)
- Mechanical Control Devices (AREA)
- Braking Arrangements (AREA)
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0955454A FR2948628B1 (fr) | 2009-08-03 | 2009-08-03 | Avion a controle en lacet par trainee differentielle |
| US12/847,108 US8876044B2 (en) | 2009-08-03 | 2010-07-30 | Aircraft with yaw control by differential drag |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0955454A FR2948628B1 (fr) | 2009-08-03 | 2009-08-03 | Avion a controle en lacet par trainee differentielle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2948628A1 FR2948628A1 (fr) | 2011-02-04 |
| FR2948628B1 true FR2948628B1 (fr) | 2012-02-03 |
Family
ID=42079188
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR0955454A Active FR2948628B1 (fr) | 2009-08-03 | 2009-08-03 | Avion a controle en lacet par trainee differentielle |
Country Status (2)
| Country | Link |
|---|---|
| US (1) | US8876044B2 (fr) |
| FR (1) | FR2948628B1 (fr) |
Families Citing this family (38)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ES3040742T3 (en) | 2008-06-20 | 2025-11-04 | Aviation Partners Inc | Curved wing tip |
| US9302766B2 (en) * | 2008-06-20 | 2016-04-05 | Aviation Partners, Inc. | Split blended winglet |
| FR2941915B1 (fr) * | 2009-02-12 | 2013-05-10 | Airbus France | Aeronef presentant deux paires d'ailes |
| GB201011843D0 (en) * | 2010-07-14 | 2010-09-01 | Airbus Operations Ltd | Wing tip device |
| US9004411B2 (en) * | 2010-11-15 | 2015-04-14 | Michael Lam | Mechanical control mixer and method therefor |
| EP2718183B1 (fr) * | 2011-06-09 | 2018-02-28 | Aviation Partners, Inc. | Spiroïde divisé |
| DE102011107251A1 (de) | 2011-07-14 | 2013-01-17 | Airbus Operations Gmbh | Flügelendstück eines Tragflügels sowie ein Tragflügel mit einem solchen Flügelendstück |
| US8936219B2 (en) * | 2012-03-30 | 2015-01-20 | The Boeing Company | Performance-enhancing winglet system and method |
| FR2992072B1 (fr) * | 2012-06-15 | 2016-07-22 | Thales Sa | Procede de pilotage automatique de l'axe de lacet pour aeronef a commandes de vol mecaniques |
| WO2015065551A1 (fr) * | 2013-07-25 | 2015-05-07 | Lam Aviation, Inc. | Structure d'aile d'avion et système de commande |
| US10239606B2 (en) * | 2013-12-04 | 2019-03-26 | Tamarack Aerospace Group, Inc. | Airflow interrupting devices |
| US10562613B2 (en) * | 2013-12-04 | 2020-02-18 | Tamarack Aerospace Group, Inc. | Adjustable lift modification wingtip |
| DK2998571T3 (en) * | 2014-09-19 | 2017-12-18 | Siemens Ag | Buoyancy actuator for a rotor blade of a wind turbine |
| DE102015008974A1 (de) * | 2015-07-10 | 2017-01-12 | Liebherr-Aerospace Lindenberg Gmbh | Winglet mit steuerbarem Luftwiderstandselement |
| US9587933B2 (en) | 2015-08-07 | 2017-03-07 | General Electric Company | System and method for inspecting an object |
| FR3042777B1 (fr) * | 2015-10-22 | 2018-07-20 | Danielson Aircraft Systems | Aeronef a voilure fixe et a stabilite statique accrue |
| US20170253322A1 (en) * | 2016-03-02 | 2017-09-07 | Google Inc. | Split Winglet Lateral Control |
| RU167454U1 (ru) * | 2016-05-04 | 2017-01-10 | Общество с ограниченной ответственностью "Ижмаш" - Беспилотные системы" | Устройство отклонения элерона |
| EP3269635A1 (fr) * | 2016-07-12 | 2018-01-17 | The Aircraft Performance Company UG | Aile d'avion |
| FR3053956B1 (fr) * | 2016-07-18 | 2019-06-28 | Airbus Operations | Gouverne crocodile pour aeronef |
| ES2905192T3 (es) * | 2018-01-15 | 2022-04-07 | The Aircraft Performance Company Gmbh | Ala de avión |
| GB2578472A (en) * | 2018-10-29 | 2020-05-13 | Airbus Operations Ltd | Apparatus, aircraft and method for moving a wing tip device away from a load-alleviating configuration |
| CN109703744A (zh) * | 2019-02-20 | 2019-05-03 | 西安爱生技术集团公司 | 一种无人机副翼舵面快速拆装机构及拆装方法 |
| US11873078B2 (en) * | 2019-05-20 | 2024-01-16 | The Boeing Company | Aircraft nacelles having adjustable chines |
| US11613345B2 (en) | 2019-05-20 | 2023-03-28 | The Boeing Company | Aircraft nacelles having adjustable chines |
| US11745860B2 (en) | 2019-05-20 | 2023-09-05 | The Boeing Company | Aircraft nacelles having adjustable chines |
| US11591097B2 (en) | 2019-05-20 | 2023-02-28 | The Boeing Company | Aircraft nacelles having adjustable chines |
| FR3105172B1 (fr) * | 2019-12-18 | 2023-11-24 | Safran | Ailerette d’aile d’aeronef |
| CN111017191A (zh) * | 2019-12-19 | 2020-04-17 | 中国航空工业集团公司西安飞机设计研究所 | 一种翼梢小翼 |
| USD930549S1 (en) * | 2019-12-30 | 2021-09-14 | Bombardier Inc. | Aircraft winglet |
| IL298177A (en) * | 2020-05-14 | 2023-01-01 | Pterodynamics Inc | Control of aircraft with vertical take-off and landing capabilities |
| WO2022087607A1 (fr) * | 2020-10-20 | 2022-04-28 | Roland Industries, Inc. | Drone mono-ailette |
| USD1066119S1 (en) | 2022-01-06 | 2025-03-11 | REGENT Craft Inc. | Winged vehicle, toy, and/or replica model thereof |
| 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 |
| CN115783240B (zh) * | 2022-11-17 | 2025-10-24 | 中国直升机设计研究所 | 一种直升机复合构型垂直安定面 |
Family Cites Families (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2279615A (en) * | 1938-05-06 | 1942-04-14 | Bugatti Ettore | Aircraft |
| US2434341A (en) * | 1943-09-02 | 1948-01-13 | Electrolux Corp | Wing flap actuating mechanism |
| US2557829A (en) * | 1947-11-07 | 1951-06-19 | Thomas B Lavelle | Aircraft control means |
| US2612329A (en) * | 1948-11-13 | 1952-09-30 | Northrop Aircraft Inc | Aileron, flap, and dive brake |
| US2697568A (en) * | 1949-02-02 | 1954-12-21 | Cons Vultee Aircraft Corp | Aircraft rudder control |
| FR1496152A (fr) * | 1966-06-20 | 1967-09-29 | Giravions Dorand | Tuyère pour aile d'avion ou pale d'hélicoptère soufflée |
| US3575363A (en) * | 1969-08-28 | 1971-04-20 | Mc Donnell Douglas Corp | Horizontal tail for aircraft |
| US4003533A (en) * | 1973-10-01 | 1977-01-18 | General Dynamics Corporation | Combination airbrake and pitch control device |
| IT1192641B (it) * | 1978-03-25 | 1988-04-27 | Messerschmitt Boelkow Blohm | Timone per la generazione aerodinamica di momenti su aeroplani |
| US4566657A (en) * | 1979-05-21 | 1986-01-28 | Grow Harlow B | Span loaded flying wing control |
| US4455004A (en) * | 1982-09-07 | 1984-06-19 | Lockheed Corporation | Flight control device for airplanes |
| DE3415976A1 (de) * | 1984-04-28 | 1985-10-31 | Hellmuth Dipl.-Ing. 7000 Stuttgart Binder | Klappenanordnung an den endscheiben von tragfluegeln |
| US5570859A (en) * | 1995-01-09 | 1996-11-05 | Quandt; Gene A. | Aerodynamic braking device |
| ES2137092B1 (es) * | 1996-11-14 | 2000-08-16 | Munoz Saiz Manuel | Flap automatico. |
| US6079672A (en) * | 1997-12-18 | 2000-06-27 | Lam; Lawrence Y. | Aileron for fixed wing aircraft |
| US5988563A (en) * | 1997-12-30 | 1999-11-23 | Mcdonnell Douglas Corporation | Articulating winglets |
| US6491261B1 (en) * | 2000-04-17 | 2002-12-10 | The United States Of America As Represented By The Secretary Of The Air Force | Wing mounted aircraft yaw control device |
| DE20107102U1 (de) * | 2001-04-25 | 2001-12-13 | Breuer, Hartmut, 89188 Merklingen | Seitenleitwerk für Luft- und Raumfahrzeuge |
| GB0115130D0 (en) * | 2001-06-21 | 2001-08-15 | Bae Systems Plc | A winglet |
| DE10160315A1 (de) * | 2001-12-07 | 2003-11-13 | Airbus Gmbh | Einrichtung zur Landeanflug-Steuerung eines Flugszeuges |
| US20050116116A1 (en) * | 2003-11-11 | 2005-06-02 | Supersonic Aerospace International, Llc | Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance |
| US7744038B2 (en) * | 2007-06-15 | 2010-06-29 | The Boeing Company | Controllable winglets |
-
2009
- 2009-08-03 FR FR0955454A patent/FR2948628B1/fr active Active
-
2010
- 2010-07-30 US US12/847,108 patent/US8876044B2/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| US8876044B2 (en) | 2014-11-04 |
| US20110024556A1 (en) | 2011-02-03 |
| FR2948628A1 (fr) | 2011-02-04 |
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Legal Events
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| PLFP | Fee payment |
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