BR0203556B1 - aeronave com carenagem ventral e junta para esta. - Google Patents

aeronave com carenagem ventral e junta para esta.

Info

Publication number
BR0203556B1
BR0203556B1 BRPI0203556-1A BR0203556A BR0203556B1 BR 0203556 B1 BR0203556 B1 BR 0203556B1 BR 0203556 A BR0203556 A BR 0203556A BR 0203556 B1 BR0203556 B1 BR 0203556B1
Authority
BR
Brazil
Prior art keywords
aircraft
joint
ventral fairing
fairing
ventral
Prior art date
Application number
BRPI0203556-1A
Other languages
English (en)
Other versions
BR0203556A (pt
Inventor
Jean-Pierre Maury
Alain Milhau
Bernard Pauly
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
Priority claimed from FR0112829A external-priority patent/FR2827029B1/fr
Application filed filed Critical
Publication of BR0203556A publication Critical patent/BR0203556A/pt
Publication of BR0203556B1 publication Critical patent/BR0203556B1/pt

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16J—PISTONS; CYLINDERS; SEALINGS
    • F16J15/00—Sealings
    • F16J15/02—Sealings between relatively-stationary surfaces
    • F16J15/021—Sealings between relatively-stationary surfaces with elastic packing
    • F16J15/022—Sealings between relatively-stationary surfaces with elastic packing characterised by structure or material
    • F16J15/024—Sealings between relatively-stationary surfaces with elastic packing characterised by structure or material the packing being locally weakened in order to increase elasticity
    • F16J15/027—Sealings between relatively-stationary surfaces with elastic packing characterised by structure or material the packing being locally weakened in order to increase elasticity and with a hollow profile

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Gasket Seals (AREA)
  • Laminated Bodies (AREA)
  • Seal Device For Vehicle (AREA)
BRPI0203556-1A 2001-10-05 2002-08-30 aeronave com carenagem ventral e junta para esta. BR0203556B1 (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0112829A FR2827029B1 (fr) 2001-07-06 2001-10-05 Aeronef a carenage ventral et joint pour un tel aeronef

Publications (2)

Publication Number Publication Date
BR0203556A BR0203556A (pt) 2004-05-25
BR0203556B1 true BR0203556B1 (pt) 2010-11-16

Family

ID=8867964

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0203556-1A BR0203556B1 (pt) 2001-10-05 2002-08-30 aeronave com carenagem ventral e junta para esta.

Country Status (6)

Country Link
US (1) US6655635B2 (pt)
EP (1) EP1300335B1 (pt)
BR (1) BR0203556B1 (pt)
CA (1) CA2397190C (pt)
DE (1) DE60203078T2 (pt)
ES (1) ES2237655T3 (pt)

Families Citing this family (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6814331B2 (en) * 2002-05-10 2004-11-09 Goodrich Hella Aerospace Lighting Systems Gmbh Device for removably fastening a first part to a second part mountable in an aircraft
US7784799B2 (en) * 2003-12-31 2010-08-31 The Boeing Company Apparatus and method for sealing surfaces
FR2869872B1 (fr) * 2004-05-04 2007-07-20 Airbus France Sas Cale de transition entre un moyen de fixation d'une aile sur un fuselage d'un aeronef et ladite aile, et aeronef comportant une telle cale.
FR2871436B1 (fr) * 2004-06-11 2007-09-07 Airbus France Sas Aeronef muni d'un carenage ventral, et carenage ventral.
FR2892999B1 (fr) * 2005-11-08 2008-02-01 Airbus France Sas Aeronef comportant un carenage central ajusteur de pression voilure par deformations geometriques locales
DE102005062190B3 (de) * 2005-12-23 2007-06-14 Airbus Deutschland Gmbh Verfahren zum Herstellen einer lösbaren Dichtung mit einer Dichtmasse sowie Verwendung von Klebestreifen zur Durchführung des Verfahrens
ES2300184B1 (es) * 2006-04-28 2009-05-01 Airbus España, S.L. Disposicion para acoplar un pivote de acoplamiento para un estabilizador horizontal trimable al fuselaje de cola de una aeronave.
ES2301359B1 (es) * 2006-05-16 2009-05-01 Airbus España, S.L. Sistema de sellado del hueco existente entre el fuselaje y el timon de altura de un avion con estabilizador horizontal orientable.
ES2317762B1 (es) * 2006-10-31 2010-02-10 Airbus España, S.L. Carena ventral para un avion.
US20090078820A1 (en) * 2007-09-26 2009-03-26 The Boeing Company Wing-to-body fairing
GB0800770D0 (en) * 2008-01-17 2008-02-27 Airbus Uk Ltd Aerofynamic sealing member for aircraft
US9045216B2 (en) 2008-01-18 2015-06-02 The Boeing Company Flight vehicle fairing having vibration-damping blankets
GB0815778D0 (en) * 2008-09-01 2008-10-08 Airbus Uk Ltd Seal
US9027883B2 (en) * 2008-11-05 2015-05-12 Airbus Operations Limited Aircraft fairing
ES2343879B1 (es) * 2008-11-28 2011-08-02 Airbus Operations, S.L. Perfil de sellado y uso del mismo.
US8714488B2 (en) * 2009-01-08 2014-05-06 The Boeing Company Elastic aircraft joint fairing
ES2386136B1 (es) * 2009-03-30 2013-07-25 Airbus Operations, S.L. Estructura para el acoplamiento de la carena de una aeronave
EP2239195A1 (en) * 2009-04-06 2010-10-13 Airbus Deutschland GmbH Center fuselage bellows
ATE537059T1 (de) * 2009-12-21 2011-12-15 Eurocopter Deutschland Abdichtung des luftstroms zwischen einer tragfläche und einem rumpf
EP2361998A3 (en) * 2010-02-19 2012-03-28 Rolls-Royce plc Method of producing a self supporting form from a coating material
FR2966425B1 (fr) * 2010-10-26 2013-08-16 Eurocopter France Aeronef muni d'un empennage comprenant un moyen de lutte contre le flottement aeroelastique.
DE102011111864A1 (de) * 2011-08-31 2013-02-28 Airbus Operations Gmbh Abdecksystem für einen Innenraum eines Fahrzeugs, Verfahren zum Abdecken eines Bereichs eines Innenraums eines Fahrzeugs und Fahrzeug mit einem Innenraum, der zumindest bereichsweise durch das Abdecksystem abgedeckt ist
US10501166B2 (en) 2012-09-20 2019-12-10 The Boeing Company Methods and apparatus to control a gap between movable aircraft wing components
US9688384B1 (en) * 2012-09-20 2017-06-27 The Boeing Company Methods and apparatus to control a gap between movable aircraft wing components
US9415853B2 (en) 2013-01-30 2016-08-16 The Boeing Company Surface sealing system
US9618118B2 (en) * 2013-05-23 2017-04-11 Alaska Airlines, Inc. Air seal assembly for aircraft flap seal
US9452819B2 (en) * 2014-03-24 2016-09-27 The Boeing Company Flight control surface seal
US10077669B2 (en) * 2014-11-26 2018-09-18 United Technologies Corporation Non-metallic engine case inlet compression seal for a gas turbine engine
US10017239B2 (en) 2015-12-18 2018-07-10 Northrop Grumman Systems Corporation Dynamic conformal aerodynamic seal (CAS) for aircraft control surfaces
DE202016106250U1 (de) * 2016-11-09 2016-11-22 WP Systems GmbH Dichtungsanordnung
US10773788B2 (en) 2017-08-15 2020-09-15 The Boeing Company Fairing assembly and method therefor
FR3072908B1 (fr) * 2017-10-26 2021-02-26 Safran Nacelles Ensemble propulsif pour aeronef
DE102018127024B3 (de) * 2018-10-30 2019-10-31 Airbus Operations Gmbh Flugzeugtürdichtungssystem und Flugzeugtüranordnung
FR3089561B1 (fr) * 2018-12-05 2022-04-01 Safran Aircraft Engines Dispositif ameliore d’etancheite a l’air destine a etre interpose entre un element de carter de turbomachine d’aeronef a double flux, et un element de nacelle
FR3106569B1 (fr) * 2020-01-23 2022-02-11 Airbus Operations Sas Assemblage pour aéronef comprenant un système d’étanchéité à l’air amélioré entre un carénage ventral et une aile
CN111361723B (zh) * 2020-03-31 2022-02-22 中国商用飞机有限责任公司 连接于民用飞机机身下方的整流罩组件
CN111717366B (zh) * 2020-06-29 2022-02-08 中国商用飞机有限责任公司 密封堵件以及包括该密封堵件的密封组件

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE694021C (de) * 1939-07-02 1940-07-24 Messerschmitt A G Spaltverkleidung fuer Flugzeuge
US2616509A (en) * 1946-11-29 1952-11-04 Thomas Wilfred Pneumatic airfoil
US3023860A (en) * 1957-03-18 1962-03-06 Floyd P Ellzey Body construction
FR1523404A (fr) * 1967-03-22 1968-05-03 Sud Aviation Perfectionnement aux raccordements entre fuselage et voilure d'un aérodyne
US3756529A (en) * 1972-05-01 1973-09-04 Mc Donnell Douglas Corp Fuselage seal
US4034939A (en) * 1975-11-05 1977-07-12 The Boeing Company Assembly for sealing the mounting opening for a flying horizontal stabilizer on a vertical stabilizer
US4399998A (en) * 1981-12-28 1983-08-23 The Timken Company Self-venting seal lip
DE3430649A1 (de) * 1984-08-21 1986-03-06 Süddeutsche Kühlerfabrik Julius Fr. Behr GmbH & Co KG, 7000 Stuttgart Dichtungsprofil fuer zwei mit parallelen raendern aneinander anschliessende gehaeuseteile
US5114162A (en) * 1986-11-13 1992-05-19 A-Lok Products, Inc. Gasket for use in manhole bases and the like
DE4443525C1 (de) * 1994-12-07 1996-02-15 Daimler Benz Ag Dachanordnung zum Verschließen eines Dachausschnitts eines Kraftfahrzeugs
DE29713153U1 (de) * 1997-07-24 1997-09-18 Lehnen, Hans Günter, Dipl.-Ing., 66687 Wadern Anpress- und Fugendichtungen für Wandmodulbausysteme
FR2789144A1 (fr) * 1999-02-03 2000-08-04 Joint Francais Joint pour panneaux et aeronef comportant un tel joint
FR2793538A1 (fr) * 1999-05-11 2000-11-17 Joint Francais Joint d'etancheite deformable
FR2827028B1 (fr) * 2001-07-06 2003-09-26 Airbus France Aeronef a carenage ventral et joint pour un tel aeronef

Also Published As

Publication number Publication date
ES2237655T3 (es) 2005-08-01
CA2397190A1 (fr) 2003-04-05
CA2397190C (fr) 2009-07-28
BR0203556A (pt) 2004-05-25
US6655635B2 (en) 2003-12-02
EP1300335B1 (fr) 2005-03-02
EP1300335A1 (fr) 2003-04-09
DE60203078T2 (de) 2006-05-04
US20030066933A1 (en) 2003-04-10
DE60203078D1 (de) 2005-04-07

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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

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 30/08/2002, OBSERVADAS AS CONDICOES LEGAIS.

B25A Requested transfer of rights approved

Free format text: TRANSFERIDO POR INCORPORACAO DE: AIRBUS FRANCE

B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time
B24J Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12)

Free format text: EM VIRTUDE DA EXTINCAO PUBLICADA NA RPI 2477 DE 26-06-2018 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDA A EXTINCAO DA PATENTE E SEUS CERTIFICADOS, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.