BR0205732A - Mecanismo de flap de sustentação - Google Patents

Mecanismo de flap de sustentação

Info

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
Application number
BR0205732-8A
Other languages
English (en)
Other versions
BR0205732B1 (pt
Inventor
Juan Perez-Sanchez
Claudia Bechheim
Martin Voglsinger
Original Assignee
Eads Deutschland Gmbh
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Eads Deutschland Gmbh filed Critical Eads Deutschland Gmbh
Publication of BR0205732A publication Critical patent/BR0205732A/pt
Publication of BR0205732B1 publication Critical patent/BR0205732B1/pt

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).
BRPI0205732-8A 2001-07-12 2002-07-04 mecanismo de flap de sustentação. BR0205732B1 (pt)

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)

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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

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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

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