BRPI0519176A2 - asa para aeronave - Google Patents

asa para aeronave

Info

Publication number
BRPI0519176A2
BRPI0519176A2 BRPI0519176-9A BRPI0519176A BRPI0519176A2 BR PI0519176 A2 BRPI0519176 A2 BR PI0519176A2 BR PI0519176 A BRPI0519176 A BR PI0519176A BR PI0519176 A2 BRPI0519176 A2 BR PI0519176A2
Authority
BR
Brazil
Prior art keywords
wing
panel
aircraft wing
aircraft
extend
Prior art date
Application number
BRPI0519176-9A
Other languages
English (en)
Inventor
Geoffrey Peter Mcbroom
Original Assignee
Airbus Uk Ltd
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 Airbus Uk Ltd filed Critical Airbus Uk Ltd
Publication of BRPI0519176A2 publication Critical patent/BRPI0519176A2/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/28—Leading or trailing edges attached to primary structures, e.g. forming fixed slots

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Connection Of Plates (AREA)
  • Toys (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Mobile Radio Communication Systems (AREA)

Abstract

ASA PARA AERONAVE. A invenção refere-se a um painel para asa para aeronave, por exemplo, um painel 1 superior de bordo de fuga que é ligado ao revestimen- to da asa (20) por meio de dentes (19) que se projetam e engatam com fendas (13). Preferivelmente, as fendas são fornecidas em abas (10, 11, 12) que se estendem do bordo de ataque (5) do painel e os dentes (19) são fixados a e se estendem do revestimento da asa (20).
BRPI0519176-9A 2004-12-21 2005-12-19 asa para aeronave BRPI0519176A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB0427957.6A GB0427957D0 (en) 2004-12-21 2004-12-21 An aircraft wing
PCT/GB2005/004908 WO2006067403A1 (en) 2004-12-21 2005-12-19 An aircraft wing

Publications (1)

Publication Number Publication Date
BRPI0519176A2 true BRPI0519176A2 (pt) 2008-12-30

Family

ID=34112949

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0519176-9A BRPI0519176A2 (pt) 2004-12-21 2005-12-19 asa para aeronave

Country Status (9)

Country Link
US (1) US8602355B2 (pt)
EP (1) EP1827971A1 (pt)
JP (1) JP4968537B2 (pt)
CN (1) CN101107161B (pt)
BR (1) BRPI0519176A2 (pt)
CA (1) CA2591895C (pt)
GB (1) GB0427957D0 (pt)
RU (1) RU2421375C2 (pt)
WO (1) WO2006067403A1 (pt)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0803692D0 (en) * 2008-02-29 2008-04-09 Airbus Uk Ltd Fitting for pivotally connecting aerodynamic control element to aircraft structure
GB0803689D0 (en) 2008-02-29 2008-04-09 Airbus Uk Ltd Trailing edge aircraft structure with overhaning cover
US9447690B2 (en) * 2011-09-15 2016-09-20 3 Phase Energy Systems, Inc. Wind generator hub assembly with hybrid sail blades
GB201120996D0 (en) 2011-12-07 2012-01-18 Airbus Operations Ltd Apparatus for attachment of wing panels
EP2922752A4 (en) * 2012-11-20 2017-01-25 Saab Ab An airframe leading edge
EP2899231A1 (en) 2014-01-22 2015-07-29 Solvay Specialty Polymers USA, LLC. Aerospace articles
GB2550175A (en) 2016-05-11 2017-11-15 Airbus Operations Ltd Aircraft joint
GB2563893A (en) 2017-06-29 2019-01-02 Airbus Operations Ltd Leading edge skin structure
US10773789B2 (en) * 2017-07-07 2020-09-15 The Boeing Company Skin-panel interface of an aircraft
GB201719790D0 (en) * 2017-11-28 2018-01-10 Airbus Operations Gmbh Aircraft joint with a curable composite bushing
GB2571508A (en) 2017-12-13 2019-09-04 Airbus Operations Ltd Aerofoil structures

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR555937A (fr) * 1921-09-16 1923-07-09 Metaux Et Du Bois Soc Ind Des Perfectionnements apportés aux surfaces de sustentation et de gouverne pour engins a
FR824987A (fr) * 1936-11-03 1938-02-21 Liore & Olivier Sa Des Ets Dispositif d'attache du bord d'attaque et du bord de fuite pour ailes d'aéronefs construites en plusieurs parties
US2473728A (en) * 1944-04-20 1949-06-21 Curtiss Wright Corp Structural joint
US2549110A (en) * 1949-05-31 1951-04-17 Northrop Aircraft Inc Panel hinge
US2956759A (en) * 1957-02-21 1960-10-18 English Electric Co Ltd Aircraft wings incorporating power installation for propulsion
US3004645A (en) * 1959-08-27 1961-10-17 Jr George E Moul Aerodynamic surface attaching structure
US3165280A (en) * 1962-08-27 1965-01-12 Lee Shao-Tang Amphibious convertijet aircraft
GB1022131A (en) * 1963-06-10 1966-03-09 Monte Copter Inc Sectional airfoil
US3640492A (en) * 1970-02-19 1972-02-08 Northrop Corp Modular aircraft structures
US3775238A (en) * 1971-06-24 1973-11-27 J Lyman Structural composite material
US4003533A (en) * 1973-10-01 1977-01-18 General Dynamics Corporation Combination airbrake and pitch control device
IL63240A (en) * 1980-07-11 1984-12-31 Weecan Marine Method and apparatus for manufacturing an integral shell formed body
US4574325A (en) * 1984-02-09 1986-03-04 The Boeing Company Lightning protection electrical circuit path for coupling between aircraft structures
US5086601A (en) * 1989-01-24 1992-02-11 Andersen Corporation Joint structure
US5106037A (en) * 1990-02-05 1992-04-21 Northrop Corporation Umbrella seal for aircraft
DE4340002C1 (de) * 1993-11-24 1995-05-11 Deutsche Aerospace Befestigung einer thermischen Isolationsstuktur
US5803406A (en) * 1996-04-22 1998-09-08 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Integrated thermal insulation system for spacecraft
US5836550A (en) * 1996-11-27 1998-11-17 Boeing Company Mechanism for streamwise fowler deployment of the wing trailing or leading edge
SE9900354L (sv) * 1999-02-03 1999-11-22 Saab Ericsson Space Ab Förband vid rymdfarkost
ATE284346T1 (de) * 2001-01-26 2004-12-15 Fischer Adv Components Gmbh Einrichtung zum verbinden beweglicher teile mit strukturbauteilen von flugzeugen od. dgl.
US6764047B2 (en) * 2001-01-26 2004-07-20 Todd Scott Miller Model airplane hinge construction
FR2906008B1 (fr) * 2006-09-15 2008-11-07 Airbus France Sa Eclisse de lisses et dispositif de jonction orbitale
US8128020B2 (en) * 2008-04-22 2012-03-06 The Boeing Company Active twisting of an aircraft lifting surface via modulated clamping of substructure

Also Published As

Publication number Publication date
GB0427957D0 (en) 2005-01-26
US8602355B2 (en) 2013-12-10
JP4968537B2 (ja) 2012-07-04
CA2591895A1 (en) 2006-06-29
CA2591895C (en) 2014-09-09
EP1827971A1 (en) 2007-09-05
RU2007128145A (ru) 2009-01-27
US20080156936A1 (en) 2008-07-03
CN101107161B (zh) 2012-06-20
JP2008524072A (ja) 2008-07-10
WO2006067403A1 (en) 2006-06-29
RU2421375C2 (ru) 2011-06-20
CN101107161A (zh) 2008-01-16

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Legal Events

Date Code Title Description
B25D Requested change of name of applicant approved

Owner name: AIRBUS OPERATIONS LIMITED (GB)

Free format text: NOME ALTERADO DE: AIRBUS UK LIMITED

B08F Application fees: application dismissed [chapter 8.6 patent gazette]

Free format text: REFERENTE A 11A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]