BR0014682A - Dobradiça para as superfìcies móveis de controle em uma aeronave e uma peça de conexão a ser utilizada com tal dobradiça - Google Patents

Dobradiça para as superfìcies móveis de controle em uma aeronave e uma peça de conexão a ser utilizada com tal dobradiça

Info

Publication number
BR0014682A
BR0014682A BR0014682-0A BR0014682A BR0014682A BR 0014682 A BR0014682 A BR 0014682A BR 0014682 A BR0014682 A BR 0014682A BR 0014682 A BR0014682 A BR 0014682A
Authority
BR
Brazil
Prior art keywords
hinge
connecting piece
lugs
aircraft
journals
Prior art date
Application number
BR0014682-0A
Other languages
English (en)
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 filed Critical
Publication of BR0014682A publication Critical patent/BR0014682A/pt

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
    • B64C13/24—Transmitting means
    • 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
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Transmission Devices (AREA)
  • Hinges (AREA)
  • Toys (AREA)
  • Tires In General (AREA)
  • Hinge Accessories (AREA)
  • Connection Of Plates (AREA)

Abstract

"DOBRADIçA PARA AS SUPERFìCIES MóVEIS DE CONTROLE EM UMA AERONAVE E UMA PEçA DE CONEXãO A SER UTILIZADA COM TAL DOBRADIçA". A invenção se refere a uma dobradiça para superfícies de controle móveis em uma aeronave. A dobradiça compreende duas alças da dobradiça (5a, 5b) colocadas a uma distância (L) uma da outra. As alças da dobradiça (5a, 5b) incluem as alças de conexão (14a, 14b) com uma peça de conexão (15) alongada entre elas. O atuador é conectado na peça de conexão (15) transportando a força (F) por meio de alças de fixação (8a, 8b) para a dobradiça e outra para a superfície de controle. A peça de conexão (15) é girada para as alças de conexão (14a, 14b) de forma que esta possa inverter sobre seu eixo longitudinal ao mover a superfície de controle. A invenção também se refere à peça de conexão (15) pretendida para ser usada com a dobradiça como descrito acima. A peça de conexão (15) é um elemento alongado incluindo os colos de mancal (18a, 18b) em ambas as extremidades de onde a peça de conexão (15) é girada rotacionalmente sobre o seu eixo longitudinal entre as alças de conexão na dobradiça. A parte central (19) da peça de conexão (15) entre os colos de mancal (18a, 18b) é plana e afila na direção dos colos de mancal (18a, 18b).
BR0014682-0A 1999-10-12 2000-10-03 Dobradiça para as superfìcies móveis de controle em uma aeronave e uma peça de conexão a ser utilizada com tal dobradiça BR0014682A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/416,622 US6270039B1 (en) 1999-10-12 1999-10-12 Hinge for movable control surfaces in an aircraft and a connecting piece to be used with such a hinge
PCT/FI2000/000852 WO2001026965A1 (en) 1999-10-12 2000-10-03 A hinge for movable control surfaces in an aircraft and a connecting piece to be used with such a hinge

Publications (1)

Publication Number Publication Date
BR0014682A true BR0014682A (pt) 2002-08-20

Family

ID=23650675

Family Applications (1)

Application Number Title Priority Date Filing Date
BR0014682-0A BR0014682A (pt) 1999-10-12 2000-10-03 Dobradiça para as superfìcies móveis de controle em uma aeronave e uma peça de conexão a ser utilizada com tal dobradiça

Country Status (9)

Country Link
US (1) US6270039B1 (pt)
EP (1) EP1226070B1 (pt)
AT (1) ATE270216T1 (pt)
AU (1) AU7666200A (pt)
BR (1) BR0014682A (pt)
CA (1) CA2387166A1 (pt)
DE (1) DE60011923T2 (pt)
ES (1) ES2222236T3 (pt)
WO (1) WO2001026965A1 (pt)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2815933B1 (fr) * 2000-10-26 2003-01-24 Eads Airbus Sa Organe et dispositif de transmission d'efforts radiaux entre des regions centrale et d'extremite de cet organe
AT409482B (de) * 2001-01-26 2002-08-26 Fischer Adv Components Gmbh Einrichtung zum verbinden beweglicher teile mit strukturbauteilen von flugzeugen od. dgl.
US6467733B1 (en) * 2001-11-28 2002-10-22 Northrop Grumman Corporation Aerodynamic control surface system
US7229049B2 (en) * 2004-05-04 2007-06-12 Lockheed Martin Corporation Unitized rotary actuator hinge fitting
US7331548B1 (en) * 2004-12-02 2008-02-19 Hawker Beechcraft Corporation Control linkage for T-tail aircraft elevator surfaces
US7975965B2 (en) * 2008-05-13 2011-07-12 The Boeing Company Wing tip joint in airfoils
US8118260B2 (en) * 2008-10-31 2012-02-21 Airbus Operations S.L. Fitting for trimming a horizontal stabilizer of an aircraft
JP5562575B2 (ja) * 2009-04-27 2014-07-30 ナブテスコ株式会社 航空機用アクチュエータ
FR2979897B1 (fr) * 2011-09-13 2014-08-22 Airbus Operations Sas Dispositif de liaison entre une lisse et un cadre d'une structure d'un aeronef
DE102012006187B4 (de) * 2012-03-27 2020-03-12 Airbus Operations Gmbh Klappenanordnung und Flugzeug mit mindestens einer Klappenanordnung
US9914523B2 (en) 2012-10-30 2018-03-13 The Boeing Company Wing hinge assembly including hinged torque boxes
FR3022215B1 (fr) * 2014-06-13 2016-05-27 Sagem Defense Securite Actionneur pour surface de vol et ensemble de guidage d'un aeronef comprenant un tel actionneur
AT516211A1 (de) 2014-08-11 2016-03-15 Facc Ag Steuerflächenelement
CN104806872B (zh) * 2015-05-06 2017-06-13 晋西工业集团有限责任公司 尾翼支耳加工型材的使用方法
US11066148B2 (en) * 2018-08-06 2021-07-20 The Boeing Company Folding wing hinge, aircraft and method therefor

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2246116A (en) * 1937-10-28 1941-06-17 Messerschmitt Boelkow Blohm Airplane wing structure
US2779555A (en) * 1952-07-05 1957-01-29 Lockheed Aircraft Corp Wing flap actuating mechanism
US3140066A (en) * 1962-12-04 1964-07-07 North American Aviation Inc Multiple pivot mounting means
US3756089A (en) * 1971-04-15 1973-09-04 H Haladay Linkage for narrow environments
US4172575A (en) * 1975-03-24 1979-10-30 Boeing Commercial Airplane Company Airfoil flap conical extension mechanism
FR2714422A1 (fr) * 1983-01-13 1995-06-30 Snecma Tuyère convergente-divergente, en particulier pour turboréacteur.
US5098043A (en) * 1990-02-27 1992-03-24 Grumman Aerospace Corporation Integrated power hinge actuator
US5836550A (en) * 1996-11-27 1998-11-17 Boeing Company Mechanism for streamwise fowler deployment of the wing trailing or leading edge

Also Published As

Publication number Publication date
ES2222236T3 (es) 2005-02-01
DE60011923D1 (de) 2004-08-05
CA2387166A1 (en) 2001-04-19
WO2001026965A1 (en) 2001-04-19
DE60011923T2 (de) 2005-08-25
EP1226070B1 (en) 2004-06-30
AU7666200A (en) 2001-04-23
EP1226070A1 (en) 2002-07-31
ATE270216T1 (de) 2004-07-15
US6270039B1 (en) 2001-08-07

Similar Documents

Publication Publication Date Title
BR0014682A (pt) Dobradiça para as superfìcies móveis de controle em uma aeronave e uma peça de conexão a ser utilizada com tal dobradiça
KR960702788A (ko) 피봇 조인트상에 조절가능한 축방향 가로 피봇부하를 받는 반월보 없는 가위
EP1338811A4 (en) UNIAXIAL JOINT DEVICE WITH SEVERAL TORQUE GENERATION PARTS
DE69408496T2 (de) Gelenk mit Nachregulierung des Spiels für Fahrzeugsitze
IT237439Y1 (it) Cerniera per mobili e simili con braccio mobile disposto all'internodel braccio fisso
ES2163199T3 (es) Conducto multiuso para alejar humos o gases nocivos de un puesto de trabajo.
ITBO20000731A0 (it) Autovettura con superfici aereodinamiche deportanti mobili
SE9703307D0 (sv) Anordning för relativ förflyttning av två element
CA2276952A1 (en) Pivoting handle assembly
IL122062A (en) Transporting system
GB2345020A (en) Folding handle device
PL353023A1 (en) Angle bracket
ATE170376T1 (de) Kontaktgrillgerät
EP1055387A3 (en) Springless adjustable bread guard, and heating appliance including same
SE0002534D0 (sv) Anordning vid robot
FR2801833B1 (fr) Un manchon comprenant une couche de solidarisation sur un cylindre support metallique
BR0001009A (pt) Parada de porta capaz de ser desengatada para veìculos
AU3930099A (en) Scale for weighing people
DE60012325D1 (de) Schnittwinkeleinstellvorrichtung
DE9204103U1 (pt)
ATE388869T1 (de) Windschutzscheibenwischeranordnung
WO2000046000A3 (en) Hand controller
BR0111828B1 (pt) bocal para transferir um fluxo de metal lìquido em uma direção de fluxo e adaptado para uso com um regulador móvel para controlar o fluxo de metal lìquido.
Stansfield The role of design in engineering education.
EP0867339A3 (en) Hinge arrangement for warning triangle legs

Legal Events

Date Code Title Description
B11A Dismissal acc. art.33 of ipl - examination not requested within 36 months of filing
B11Y Definitive dismissal - extension of time limit for request of examination expired [chapter 11.1.1 patent gazette]