DE69020537T2 - Klappe- und querrudersystem eines flügels für ein verwandlungsflugzeug. - Google Patents
Klappe- und querrudersystem eines flügels für ein verwandlungsflugzeug.Info
- Publication number
- DE69020537T2 DE69020537T2 DE69020537T DE69020537T DE69020537T2 DE 69020537 T2 DE69020537 T2 DE 69020537T2 DE 69020537 T DE69020537 T DE 69020537T DE 69020537 T DE69020537 T DE 69020537T DE 69020537 T2 DE69020537 T2 DE 69020537T2
- Authority
- DE
- Germany
- Prior art keywords
- flap
- wing
- convertible aircraft
- aileron system
- aileron
- 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.)
- Expired - Lifetime
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/04—Adjustable control surfaces or members, e.g. rudders with compound dependent movements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/44—Varying camber
- B64C3/50—Varying camber by leading or trailing edge flaps
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
- B64C9/18—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single 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
-
- 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
- Y02T50/30—Wing lift efficiency
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/417,811 US5094412A (en) | 1989-10-13 | 1989-10-13 | Flaperon system for tilt rotor wings |
PCT/US1990/005353 WO1991005699A1 (en) | 1989-10-13 | 1990-09-25 | Flaperon system for tilt rotor wings |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69020537D1 DE69020537D1 (de) | 1995-08-03 |
DE69020537T2 true DE69020537T2 (de) | 1995-11-02 |
Family
ID=23655483
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69020537T Expired - Lifetime DE69020537T2 (de) | 1989-10-13 | 1990-09-25 | Klappe- und querrudersystem eines flügels für ein verwandlungsflugzeug. |
Country Status (7)
Country | Link |
---|---|
US (1) | US5094412A (de) |
EP (1) | EP0448695B1 (de) |
JP (1) | JP3213752B2 (de) |
AU (1) | AU6617590A (de) |
DE (1) | DE69020537T2 (de) |
IL (1) | IL95885A0 (de) |
WO (1) | WO1991005699A1 (de) |
Families Citing this family (61)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6048581A (en) | 1996-09-24 | 2000-04-11 | Mcdonnell Douglas Corporation | Elastic ground plane and method |
US6293497B1 (en) | 1996-10-22 | 2001-09-25 | The Boeing Company | Airplane with unswept slotted cruise wing airfoil |
CN1184056A (zh) * | 1996-11-29 | 1998-06-10 | 三星航空产业株式会社 | 飞机的机翼 |
US7455264B2 (en) | 1997-08-26 | 2008-11-25 | Mcdonnell Douglas Corporation | Reconfiguration control system for an aircraft wing |
US6209824B1 (en) * | 1997-09-17 | 2001-04-03 | The Boeing Company | Control surface for an aircraft |
FR2791634B1 (fr) * | 1999-03-30 | 2001-06-15 | Eurocopter France | Perfectionnements aux aeronefs convertibles a rotors basculants |
FR2798359B1 (fr) | 1999-09-14 | 2001-11-09 | Eurocopter France | Perfectionnements aux aeronefs convertibles a rotors basculants |
EP1328438A4 (de) * | 2000-09-22 | 2009-04-01 | Diversified Technologies Inc | Läuferschaufel mit variabler kante |
US6481667B1 (en) | 2001-03-05 | 2002-11-19 | Northrop Grumman Corporation | System and method for deflecting an aerodynamic control surface |
US7258308B2 (en) * | 2002-07-02 | 2007-08-21 | The Boeing Company | Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface |
US6796534B2 (en) * | 2002-09-10 | 2004-09-28 | The Boeing Company | Method and apparatus for controlling airflow with a leading edge device having a flexible flow surface |
US7059563B2 (en) * | 2003-06-03 | 2006-06-13 | The Boeing Company | Systems, apparatuses, and methods for moving aircraft control surfaces |
US6799739B1 (en) * | 2003-11-24 | 2004-10-05 | The Boeing Company | Aircraft control surface drive system and associated methods |
US7424350B2 (en) * | 2004-02-02 | 2008-09-09 | The Boeing Company | Vehicle control systems and corresponding sizing methods |
DE102004006940B4 (de) * | 2004-02-12 | 2009-02-26 | Airbus Deutschland Gmbh | Landeklappenführung für Luftfahrzeuge |
US6978971B1 (en) * | 2004-06-15 | 2005-12-27 | The Boeing Company | Methods and apparatuses for controlling airflow proximate to engine/airfoil systems |
US7270305B2 (en) * | 2004-06-15 | 2007-09-18 | The Boeing Company | Aircraft leading edge apparatuses and corresponding methods |
US7494094B2 (en) * | 2004-09-08 | 2009-02-24 | The Boeing Company | Aircraft wing systems for providing differential motion to deployable lift devices |
GB2417937B (en) * | 2004-09-10 | 2009-08-12 | Ultra Electronics Ltd | An aircraft wing coupling arrangement |
US7264206B2 (en) * | 2004-09-30 | 2007-09-04 | The Boeing Company | Leading edge flap apparatuses and associated methods |
DE102004049504A1 (de) * | 2004-10-11 | 2006-04-13 | Airbus Deutschland Gmbh | Flugzeugflügel, Verfahren zum Betreiben eines Flugzeugflügels und Verwendung einer schwenkbaren Hinterkante an einem Hauptflügel eines Flugzeugflügels zum Justieren der Form und Breite eines Luftspalts |
US7322547B2 (en) * | 2005-01-31 | 2008-01-29 | The Boeing Company | Aerospace vehicle leading edge slat devices and corresponding methods |
US7338018B2 (en) * | 2005-02-04 | 2008-03-04 | The Boeing Company | Systems and methods for controlling aircraft flaps and spoilers |
US7309043B2 (en) * | 2005-04-27 | 2007-12-18 | The Boeing Company | Actuation device positioning systems and associated methods, including aircraft spoiler droop systems |
US7721999B2 (en) * | 2005-05-20 | 2010-05-25 | The Boeing Company | Aerospace vehicle fairing systems and associated methods |
US7300021B2 (en) * | 2005-05-20 | 2007-11-27 | The Boeing Company | Aerospace vehicle fairing systems and associated methods |
US7367530B2 (en) * | 2005-06-21 | 2008-05-06 | The Boeing Company | Aerospace vehicle yaw generating systems and associated methods |
WO2007005687A1 (en) * | 2005-06-30 | 2007-01-11 | Bell Helicopter Textron Inc. | Retractable vortex generator |
US7500641B2 (en) * | 2005-08-10 | 2009-03-10 | The Boeing Company | Aerospace vehicle flow body systems and associated methods |
US7611099B2 (en) * | 2005-09-07 | 2009-11-03 | The Boeing Company | Seal assemblies for use with drooped spoilers and other control surfaces on aircraft |
DE102005045759A1 (de) | 2005-09-23 | 2007-04-12 | Airbus Deutschland Gmbh | Fortschrittlicheflügelhinterkante am Flügel eines Flugzeugs |
WO2007120199A2 (en) * | 2005-11-09 | 2007-10-25 | Morgan Aircraft, Llc | Aircraft attitude control configuration |
US7708231B2 (en) | 2005-11-21 | 2010-05-04 | The Boeing Company | Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods |
US7475854B2 (en) | 2005-11-21 | 2009-01-13 | The Boeing Company | Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods |
US7578484B2 (en) * | 2006-06-14 | 2009-08-25 | The Boeing Company | Link mechanisms for gapped rigid krueger flaps, and associated systems and methods |
GB0722425D0 (en) * | 2007-11-15 | 2007-12-27 | Airbus Uk Ltd | Slat support funk plate |
US7954769B2 (en) | 2007-12-10 | 2011-06-07 | The Boeing Company | Deployable aerodynamic devices with reduced actuator loads, and related systems and methods |
US7766282B2 (en) | 2007-12-11 | 2010-08-03 | The Boeing Company | Trailing edge device catchers and associated systems and methods |
GB0814610D0 (en) * | 2008-08-11 | 2008-09-17 | Airbus Uk Ltd | A bi-directional flight control surface mechanism |
DE102008056655A1 (de) * | 2008-11-10 | 2010-05-27 | Airbus Deutschland Gmbh | Flügel mit einer Stellklappe und einer Spaltabdeckungs-Vorrichtung und Verstellmechanismus für eine Spaltabdeckungs-Vorrichtung |
US8393799B2 (en) * | 2009-01-28 | 2013-03-12 | The Boeing Company | Spring track roller assembly |
US8382045B2 (en) | 2009-07-21 | 2013-02-26 | The Boeing Company | Shape-changing control surface |
WO2011034531A1 (en) * | 2009-09-17 | 2011-03-24 | Bell Helicopter Textron Inc. | Removable horizontal stabilizer for helicopter |
US20140076419A1 (en) * | 2012-02-27 | 2014-03-20 | Sinhatech | Self adjusting deturbulator enhanced flap and wind deflector |
US9108715B2 (en) * | 2012-05-29 | 2015-08-18 | The Boeing Company | Rotary actuated high lift gapped aileron |
EP2886451A1 (de) * | 2013-12-18 | 2015-06-24 | Airbus Operations GmbH | Hinterkantenklappensystem für einen Flügel eines Flugzeugs und Flugzeug mit einem Flügel und mindestens einem solche Hinterkantenklappensystem |
US9038943B1 (en) * | 2014-04-11 | 2015-05-26 | Ralph F. Morris | Safety aileron system |
JP2016078584A (ja) * | 2014-10-15 | 2016-05-16 | 三菱航空機株式会社 | 航空機 |
US9550567B1 (en) | 2014-10-27 | 2017-01-24 | Amazon Technologies, Inc. | In-flight reconfigurable hybrid unmanned aerial vehicle |
CN105620723A (zh) * | 2014-10-31 | 2016-06-01 | 中国航空工业集团公司西安飞机设计研究所 | 一种襟副翼 |
US10633092B2 (en) | 2015-12-07 | 2020-04-28 | Aai Corporation | UAV with wing-plate assemblies providing efficient vertical takeoff and landing capability |
US10252798B2 (en) | 2017-04-27 | 2019-04-09 | Pterodynamics | Vertical takeoff and landing airframe |
US11014652B1 (en) * | 2018-05-03 | 2021-05-25 | Ardura, Inc. | Active lift control device and method |
EP3584153A1 (de) * | 2018-06-20 | 2019-12-25 | Bombardier Inc. | System mit variabler wölbung |
US11046421B2 (en) * | 2018-10-18 | 2021-06-29 | Textron Innovations Inc. | Slotted flaperon seal mechanism for aircraft devices |
EP3674211B1 (de) | 2018-12-28 | 2021-02-17 | LEONARDO S.p.A. | Wandelbares flugzeug und zugehöriges steuerungsverfahren |
EP3674202B1 (de) * | 2018-12-28 | 2021-03-17 | LEONARDO S.p.A. | Flugzeugflügel |
US11091248B2 (en) | 2019-09-17 | 2021-08-17 | The Boeing Company | Flap actuator mechanism |
US11733715B2 (en) * | 2019-10-08 | 2023-08-22 | California Institute Of Technology | Airflow sensing based adaptive nonlinear flight control of a flying car or fixed-wing VTOL |
PL439361A1 (pl) | 2021-10-29 | 2023-05-02 | Stowarzyszenie B-4 | Skrzydło bezzałogowego aparatu latającego z klapą szczelinową, zwłaszcza gyrodyny |
CN115384757B (zh) * | 2022-10-31 | 2023-01-24 | 北京启时智航科技有限公司 | 襟副翼作动机构及机翼结构 |
Family Cites Families (32)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3126173A (en) * | 1964-03-24 | Alvarez-calderdn | ||
US1785620A (en) * | 1927-10-26 | 1930-12-16 | Bristol Aeroplane Co Ltd | Control surface for aircraft, submersibles, and the like |
US2407401A (en) * | 1941-09-08 | 1946-09-10 | Douglas Aircraft Co Inc | Lateral control arrangement |
US2772058A (en) * | 1951-05-10 | 1956-11-27 | Charles H Grant | Aircraft wing with means to increase lift through control of air flow |
US2908454A (en) * | 1954-02-17 | 1959-10-13 | Konink Nl Vliegtuigenfabriek F | Aircraft wing |
US2928626A (en) * | 1956-01-17 | 1960-03-15 | Tino Ovid | Sustaining airfoil with retractable cylindrical rotor |
US2920844A (en) * | 1957-04-12 | 1960-01-12 | North American Aviation Inc | Aircraft boundary-layer control system |
US3092354A (en) * | 1960-08-08 | 1963-06-04 | Alvarez-Calderon Alberto | Aerodynamic system and apparatus |
US3129907A (en) * | 1960-08-18 | 1964-04-21 | Dornier Werke Gmbh | Airplane wing flap |
US3112089A (en) * | 1960-10-12 | 1963-11-26 | Dornier Werke Gmbh | Airplane wing flaps |
US3203647A (en) * | 1961-12-06 | 1965-08-31 | Alvarez-Calderon Alberto | High lift fdaps for aircraft wings |
US3121544A (en) * | 1962-01-08 | 1964-02-18 | Alvarez-Calderon Alberto | Safety and high lift system and apparatus for aircraft |
US3145950A (en) * | 1962-01-22 | 1964-08-25 | Boeing Co | Wing lift increasing device |
US3195836A (en) * | 1962-04-16 | 1965-07-20 | Alvarez-Calderon Alberto | High lift slotted flap |
US3167273A (en) * | 1962-04-20 | 1965-01-26 | Calderon Alberto Alvarez | Stability and control system and apparatus for ducted fan aircraft |
US3179354A (en) * | 1962-04-24 | 1965-04-20 | Alvarez-Calderon Alberto | Convertiplane and apparatus thereof |
US3223356A (en) * | 1963-03-06 | 1965-12-14 | Alvarez-Calderon Alberto | Deflected slipstream system for aircraft |
US3371888A (en) * | 1965-07-12 | 1968-03-05 | Alberto Alvarez Calderon | Inverting flap system |
US3430894A (en) * | 1967-04-17 | 1969-03-04 | Air Vehicle Corp | Vtol aircraft having free-floating wings and independently tilting propellers |
US3481561A (en) * | 1967-08-21 | 1969-12-02 | Alvarez Calderon Alberto | Inverting flap shapes and mechanisms |
US3524610A (en) * | 1968-02-05 | 1970-08-18 | Alvarez Calderon Alberto | Leading edge flap of variable camber and thickness |
DE1943680C2 (de) * | 1969-08-28 | 1982-06-24 | Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen | Steuerklappenanordnung |
US3977630A (en) * | 1973-03-09 | 1976-08-31 | The Boeing Company | STOL aircraft |
US3917192A (en) * | 1973-07-09 | 1975-11-04 | Alvarez Calderon Alberto | Flap mechanisms and apparatus |
US3874617A (en) * | 1974-07-17 | 1975-04-01 | Mc Donnell Douglas Corp | Stol flaps |
US4248395A (en) * | 1975-03-24 | 1981-02-03 | The Boeing Company | Airplane wing trailing-edge flap-mounting mechanism |
US4149688A (en) * | 1976-10-01 | 1979-04-17 | Aereon Corporation | Lifting body aircraft for V/STOL service |
US4566657A (en) * | 1979-05-21 | 1986-01-28 | Grow Harlow B | Span loaded flying wing control |
US4360176A (en) * | 1979-11-05 | 1982-11-23 | The Boeing Company | Wing leading edge slat |
US4498646A (en) * | 1981-07-01 | 1985-02-12 | Dornier Gmbh | Wing for short take-off and landing aircraft |
US4471927A (en) * | 1981-09-29 | 1984-09-18 | The Boeing Company | Trailing edge flap assembly |
US4605187A (en) * | 1984-03-09 | 1986-08-12 | The Boeing Company | Wing flap mechanism |
-
1989
- 1989-10-13 US US07/417,811 patent/US5094412A/en not_active Expired - Lifetime
-
1990
- 1990-09-25 JP JP51495490A patent/JP3213752B2/ja not_active Expired - Lifetime
- 1990-09-25 AU AU66175/90A patent/AU6617590A/en not_active Abandoned
- 1990-09-25 WO PCT/US1990/005353 patent/WO1991005699A1/en active IP Right Grant
- 1990-09-25 EP EP90916106A patent/EP0448695B1/de not_active Expired - Lifetime
- 1990-09-25 DE DE69020537T patent/DE69020537T2/de not_active Expired - Lifetime
- 1990-10-03 IL IL95885A patent/IL95885A0/xx unknown
Also Published As
Publication number | Publication date |
---|---|
JP3213752B2 (ja) | 2001-10-02 |
US5094412A (en) | 1992-03-10 |
EP0448695B1 (de) | 1995-06-28 |
AU6617590A (en) | 1991-05-16 |
DE69020537D1 (de) | 1995-08-03 |
EP0448695A1 (de) | 1991-10-02 |
EP0448695A4 (en) | 1993-03-31 |
WO1991005699A1 (en) | 1991-05-02 |
IL95885A0 (en) | 1991-07-18 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE69020537D1 (de) | Klappe- und querrudersystem eines flügels für ein verwandlungsflugzeug. | |
DE3762027D1 (de) | Fluegelklappensteuersystem eines flugzeuges. | |
DE68917365D1 (de) | Klappenventil für ein Luftfahrzeug. | |
GB2010761B (en) | Tapered variable camber leading edge flap for aircraft wing | |
DE3568317D1 (en) | Aircraft trailing edge flap apparatus | |
DE69107235D1 (de) | Schwebeflug-Positionshaltesystem für Drehflügelflugzeuge. | |
DE3462865D1 (en) | Aircraft swept wing provided with high-lift devices and an engine pylon, and engine pylon for such a wing | |
DE69213041T2 (de) | Integriertes Flug- und Anflug-Leitsystem für Luftfahrzeuge | |
ES531594A0 (es) | Un ala de avion | |
GB2204538B (en) | Wing leading edge arrangements for aircraft | |
GB2200330B (en) | A system for coupling two flaps of an aircraft wing, and an aircraft wing equipped with such a system | |
NO874474L (no) | Vinge for supersonisk vifte eller kompressor. | |
GB2186849B (en) | Variable camber leading edge arrangements for aircraft wings | |
DE68907330T2 (de) | Aerodynamische Geräuschunterdrückung für Tragflächenklappen. | |
DE69002048T2 (de) | Stromlinienverkleidungen für Flugzeug. | |
DE69707277D1 (de) | Segmentierte tragflächenklappe mit änderbarer wölbung für luftfahrzeuge | |
DE3860476D1 (de) | Landungssystem eines flugzeuges. | |
DE68928110D1 (de) | Steuerungssystem für den Antrieb eines Luftfahrzeugs | |
EP0303458A3 (en) | Trailing edge flaps for aircraft wings | |
GB2172861B (en) | Aileron for an airplane wing | |
EP0322172A3 (en) | Wing leading edge arrangements for aircraft | |
FR2585326B3 (fr) | Configuration d'arriere de fuselage d'avion | |
GB2100684B (en) | Flap arrangement for the leading edge of an aircraft wing | |
DE69326695T2 (de) | Flugemulations-Prüfsystem für ein Flugzeug | |
EP0272396A3 (en) | Aerodynamic aircraft wing flap system, in particular for slot flaps |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |