BR0205732A - Mecanismo de flap de sustentação - Google Patents
Mecanismo de flap de sustentaçãoInfo
- Publication number
- BR0205732A BR0205732A BR0205732-8A BR0205732A BR0205732A BR 0205732 A BR0205732 A BR 0205732A BR 0205732 A BR0205732 A BR 0205732A BR 0205732 A BR0205732 A BR 0205732A
- Authority
- BR
- Brazil
- Prior art keywords
- steering lever
- joint
- flap
- lift flap
- main connection
- Prior art date
Links
Classifications
-
- 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
-
- 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
- B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
-
- 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)
- Toys (AREA)
- Forklifts And Lifting Vehicles (AREA)
- Transmission Devices (AREA)
- Steering Controls (AREA)
- Threshing Machine Elements (AREA)
- Lock And Its Accessories (AREA)
- Accommodation For Nursing Or Treatment Tables (AREA)
- Ultra Sonic Daignosis Equipment (AREA)
- Filters For Electric Vacuum Cleaners (AREA)
- Package Closures (AREA)
Abstract
"MECANISMO DE FLAP DE SUSTENTAçãO". Mecanismo de flap de sustentação para o ajuste de um flap de sustentação (2) conjugado a um suporte de flap (3) de uma asa (1) por meio de um sistema de acionamento (6), sendo que o mecanismo de flap de sustentação (4) compreende uma mecânica de conexão principal (7) e uma mecânica der conexão auxiliar (9), na forma de uma alavanca de guia (40) apoiada de modo articulado no flap de sustentação (2) e no suporte do flap (3), sendo que a mecânica de conexão principal (7) possui uma disposição de alavanca de comando (20) com pelo menos uma alavanca de comando (20a, 20b), possuindo uma primeira articulação de alavanca de comando (24) e uma segunda articulação de alavanca de comando (26), sendo que a pelo menos uma alavanca de comando (20a, 20b) está unida com o suporte do flap (3) através de um pêndulo (25) acoplado na primeira articulação de alavanca de comando (24), e a segunda articulação de alavanca de comando (26) é guiada de tal modo que com uma determinada posição de ângulo da pelo menos uma alavanca de comando (20a, 20b) são determinadas claramente as posições da articulação da conexão principal (8) e da articulação da conexão auxiliar (42).
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10133920A DE10133920B4 (de) | 2001-07-12 | 2001-07-12 | Auftriebsklappen-Mechanismus |
DE10133920.8 | 2001-07-12 | ||
PCT/EP2002/007399 WO2003008266A1 (de) | 2001-07-12 | 2002-07-04 | Auftriebsklappen-mechanismus |
Publications (2)
Publication Number | Publication Date |
---|---|
BR0205732A true BR0205732A (pt) | 2003-06-03 |
BR0205732B1 BR0205732B1 (pt) | 2011-02-08 |
Family
ID=7691549
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0205732-8A BR0205732B1 (pt) | 2001-07-12 | 2002-07-04 | mecanismo de flap de sustentação. |
Country Status (9)
Country | Link |
---|---|
US (1) | US7293744B2 (pt) |
EP (1) | EP1404573B1 (pt) |
AT (1) | ATE281346T1 (pt) |
BR (1) | BR0205732B1 (pt) |
CA (1) | CA2454145C (pt) |
DE (2) | DE10133920B4 (pt) |
RU (1) | RU2238219C2 (pt) |
UA (1) | UA73999C2 (pt) |
WO (1) | WO2003008266A1 (pt) |
Families Citing this family (38)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB0215522D0 (en) * | 2002-07-04 | 2002-08-14 | Smiths Wolverhampton Ltd | Flight surface actuator |
US6799739B1 (en) | 2003-11-24 | 2004-10-05 | The Boeing Company | Aircraft control surface drive system and associated methods |
DE102004035921B4 (de) * | 2004-07-23 | 2006-08-03 | Airbus Deutschland Gmbh | Klappen-Kopplungssystem für Luftfahrzeuge |
DE102005016639B4 (de) * | 2005-04-11 | 2010-12-02 | Eads Deutschland Gmbh | Tragflügel mit ausfahrbaren aerodynamischen Flügelklappen, insbesondere Auftriebsklappen |
DE102005016638B4 (de) * | 2005-04-11 | 2010-12-30 | Eads Deutschland Gmbh | Flügelklappen-Mechanismus zur Verstellung einer einem Tragflügel zugeordneten aerodynamischen Flügelklappe |
DE102005017307A1 (de) | 2005-04-14 | 2006-10-26 | Airbus Deutschland Gmbh | Landeklappenantriebssystem |
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 |
DE102005062919A1 (de) * | 2005-12-29 | 2007-07-12 | Airbus Deutschland Gmbh | Tragfläche für ein Flugzeug und Flugzeug |
DE102006036464B4 (de) * | 2006-08-04 | 2009-08-20 | Airbus Deutschland Gmbh | Hochauftriebssystem für ein Flugzeug |
DE102007036996A1 (de) * | 2007-08-06 | 2009-02-19 | Airbus Deutschland Gmbh | Hochauftriebssystem für ein Flugzeug |
DE102007048449A1 (de) | 2007-10-10 | 2009-04-23 | Eads Deutschland Gmbh | Auftriebsklappenträgersystem |
US7766282B2 (en) * | 2007-12-11 | 2010-08-03 | The Boeing Company | Trailing edge device catchers and associated systems and methods |
DE102007063583A1 (de) * | 2007-12-28 | 2009-07-16 | Airbus Deutschland Gmbh | Hochauftriebssystem für ein Flugzeug |
DE102008003543B4 (de) * | 2008-01-08 | 2013-01-10 | Airbus Operations Gmbh | System und Verfahren zum Verstellen von Steuerflächen für Windkanalmodelle |
GB0805599D0 (en) * | 2008-03-28 | 2008-04-30 | Airbus Uk Ltd | Slat deployment mechanism |
US8226048B2 (en) * | 2008-12-09 | 2012-07-24 | The Boeing Company | Link mechanisms, including Stephenson II link mechanisms for multi-position flaps and associated systems and methods |
US8451144B2 (en) * | 2009-02-04 | 2013-05-28 | Honeywell International Inc. | Flaps overspeed advisory system |
FR2946617B1 (fr) * | 2009-06-10 | 2012-11-16 | Sagem Defense Securite | Dispositif d'actionnement d'une gouverne d'aeronef. |
DE102009039967A1 (de) * | 2009-09-03 | 2011-03-10 | Airbus Operations Gmbh | Verstellmechanismus zur kinematischen Führung eines Verstellkörpers bei dessen Verstellung an einem tragenden Strukturteil, Verstellmechanismus zur kinematischen Verstellung eines Hochauftriebskörpers sowie Hochauftriebssystem mit einem solchen Verstellmechanismus |
US8763953B2 (en) * | 2010-07-14 | 2014-07-01 | The Boeing Company | Aircraft flap actuator assembly |
DE102011105912A1 (de) * | 2011-06-28 | 2013-01-03 | Airbus Operations Gmbh | Tragflügel mit einem Hauptflügel und einem Hochauftriebskörper sowie Verfahren zur Ausführung von Verstellbewegungen eines Hochauftriebskörpers gegenüber einem Hauptflügel |
DE102011082888B4 (de) | 2011-09-16 | 2016-01-07 | Airbus Defence and Space GmbH | Auftriebsklappenanordnung, Tragflügel sowie Flugzeug |
GB201117340D0 (en) | 2011-10-07 | 2011-11-23 | Airbus Uk Ltd | Flat support |
US8876065B2 (en) * | 2011-10-21 | 2014-11-04 | Gulfstream Aerospace Corporation | Flap roller arrangement, flap assembly, and method for removing a roller assembly from a flap fitting |
EP2808250B1 (en) * | 2013-05-28 | 2018-01-03 | Airbus Operations GmbH | Aircraft flap system with aileron functionality |
RU2627259C2 (ru) * | 2015-12-18 | 2017-08-04 | Публичное акционерное общество "Научно-производственная корпорация "Иркут" | Устройство обнаружения и предотвращения перекоса закрылка |
BR102016020505B1 (pt) * | 2016-09-05 | 2022-08-02 | Embraer S.A | Mecanismo de deflexão de painéis de flaps de aeronave |
EP3339163A1 (en) * | 2016-12-22 | 2018-06-27 | Airbus Operations GmbH | Wing for an aircraft |
EP3395678B1 (en) | 2017-04-26 | 2021-05-26 | Asco Industries NV | Guidance assembly for an airfoil leading edge high-lift device carrier track |
EP3501977B1 (en) | 2017-12-19 | 2021-08-11 | Asco Industries NV | Deployment system for an airfoil high lift leading edge device |
EP3670330B1 (en) * | 2018-12-20 | 2022-02-09 | Bombardier Inc. | Aircraft flap deployment system |
CN110294102B (zh) * | 2019-04-26 | 2023-05-23 | 庆安集团有限公司 | 一体式襟副翼的复合运动机构 |
US11312474B2 (en) * | 2019-06-14 | 2022-04-26 | The Boeing Company | Flap actuation system with support catcher link |
US11260960B2 (en) | 2019-07-09 | 2022-03-01 | The Boeing Company | Flap actuation system for aircraft |
US11260958B2 (en) * | 2019-09-04 | 2022-03-01 | The Boeing Company | Double over center crankshaft flap mechanism |
US11091248B2 (en) * | 2019-09-17 | 2021-08-17 | The Boeing Company | Flap actuator mechanism |
EP4311765A1 (en) | 2022-07-29 | 2024-01-31 | Airbus Operations GmbH | Wing assembly comprising a connecting assembly with a first and a second connecting element, wing, and aircraft |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1547902A (en) * | 1975-03-24 | 1979-06-27 | Boeing Co | Mounting mechanism for an airplane wing trailling-edge flaps |
US4434959A (en) * | 1981-09-28 | 1984-03-06 | The Boeing Company | Airfoil flap assembly with flap track member |
EP0081610B1 (en) * | 1981-12-16 | 1986-12-17 | The Boeing Company | Flap assembly aircraft wing |
US4448375A (en) * | 1982-09-29 | 1984-05-15 | The Boeing Company | Folding truss mechanism for trailing edge flaps |
US4702442A (en) * | 1984-12-06 | 1987-10-27 | The Boeing Company | Aircraft trailing edge flap apparatus |
US4669687A (en) * | 1985-03-06 | 1987-06-02 | The Boeing Company | Airfoil flap member with flap track member |
DE4107556C1 (pt) * | 1991-03-08 | 1992-05-14 | Deutsche Airbus Gmbh, 2000 Hamburg, De | |
DE19647077A1 (de) * | 1996-11-14 | 1998-05-20 | Zf Luftfahrttechnik Gmbh | Linearbewegungen übertragende Anordnung mit Kraftbegrenzung |
SE515029C2 (sv) | 1998-08-31 | 2001-05-28 | Saab Ab | Klaffmekanism |
-
2001
- 2001-07-12 DE DE10133920A patent/DE10133920B4/de not_active Expired - Fee Related
-
2002
- 2002-04-07 UA UA2003010796A patent/UA73999C2/uk unknown
- 2002-07-04 CA CA002454145A patent/CA2454145C/en not_active Expired - Lifetime
- 2002-07-04 AT AT02767171T patent/ATE281346T1/de not_active IP Right Cessation
- 2002-07-04 RU RU2003102368A patent/RU2238219C2/ru active
- 2002-07-04 EP EP02767171A patent/EP1404573B1/de not_active Expired - Lifetime
- 2002-07-04 DE DE50201480T patent/DE50201480D1/de not_active Expired - Lifetime
- 2002-07-04 US US10/483,380 patent/US7293744B2/en not_active Expired - Lifetime
- 2002-07-04 WO PCT/EP2002/007399 patent/WO2003008266A1/de not_active Application Discontinuation
- 2002-07-04 BR BRPI0205732-8A patent/BR0205732B1/pt not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
CA2454145C (en) | 2009-09-15 |
DE10133920B4 (de) | 2004-05-13 |
UA73999C2 (en) | 2005-10-17 |
US20050040294A1 (en) | 2005-02-24 |
BR0205732B1 (pt) | 2011-02-08 |
ATE281346T1 (de) | 2004-11-15 |
CA2454145A1 (en) | 2003-01-30 |
RU2238219C2 (ru) | 2004-10-20 |
EP1404573A1 (de) | 2004-04-07 |
DE50201480D1 (de) | 2004-12-09 |
DE10133920A1 (de) | 2003-01-30 |
WO2003008266A1 (de) | 2003-01-30 |
US7293744B2 (en) | 2007-11-13 |
EP1404573B1 (de) | 2004-11-03 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
B16A | Patent or certificate of addition of invention granted [chapter 16.1 patent gazette] |
Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 04/07/2002, OBSERVADAS AS CONDICOES LEGAIS. |
|
B21A | Patent or certificate of addition expired [chapter 21.1 patent gazette] |
Free format text: PATENTE EXTINTA EM 04/07/2022 |