ATE287821T1 - Flugzeug mit flügel-rumpf-verkleidungsdichtung - Google Patents

Flugzeug mit flügel-rumpf-verkleidungsdichtung

Info

Publication number
ATE287821T1
ATE287821T1 AT02291372T AT02291372T ATE287821T1 AT E287821 T1 ATE287821 T1 AT E287821T1 AT 02291372 T AT02291372 T AT 02291372T AT 02291372 T AT02291372 T AT 02291372T AT E287821 T1 ATE287821 T1 AT E287821T1
Authority
AT
Austria
Prior art keywords
wing
fulluse
aircraft
fairing
seal
Prior art date
Application number
AT02291372T
Other languages
English (en)
Inventor
Bernard Pauly
Original Assignee
Airbus France
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 France filed Critical Airbus France
Application granted granted Critical
Publication of ATE287821T1 publication Critical patent/ATE287821T1/de

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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Gasket Seals (AREA)
  • Sealing Devices (AREA)
  • Laminated Bodies (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
  • Golf Clubs (AREA)
  • Air Bags (AREA)
AT02291372T 2001-07-06 2002-06-04 Flugzeug mit flügel-rumpf-verkleidungsdichtung ATE287821T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0108982A FR2827028B1 (fr) 2001-07-06 2001-07-06 Aeronef a carenage ventral et joint pour un tel aeronef

Publications (1)

Publication Number Publication Date
ATE287821T1 true ATE287821T1 (de) 2005-02-15

Family

ID=8865192

Family Applications (1)

Application Number Title Priority Date Filing Date
AT02291372T ATE287821T1 (de) 2001-07-06 2002-06-04 Flugzeug mit flügel-rumpf-verkleidungsdichtung

Country Status (8)

Country Link
US (1) US6581877B2 (de)
EP (1) EP1273512B1 (de)
AT (1) ATE287821T1 (de)
BR (1) BR0202753B1 (de)
CA (1) CA2389856C (de)
DE (1) DE60202716T2 (de)
ES (1) ES2234993T3 (de)
FR (1) FR2827028B1 (de)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE60203078T2 (de) * 2001-10-05 2006-05-04 Airbus France Flugzeug mit Flügel-Rumpf-Verkleidungsdichtung
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
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.
GB0800770D0 (en) * 2008-01-17 2008-02-27 Airbus Uk Ltd Aerofynamic sealing member for aircraft
FR2936489B1 (fr) * 2008-09-30 2012-07-20 Airbus France Troncon central d'aeronef avec carenage ventral travaillant
EP2338787B1 (de) * 2009-12-21 2011-12-14 Eurocopter Deutschland GmbH Abdichtung des Luftstroms zwischen einer Tragfläche und einem Rumpf
EP2361998A3 (de) * 2010-02-19 2012-03-28 Rolls-Royce plc Verfahren zur Herstellung einer selbsttragenden Form aus Beschichtungsmaterial
WO2012173542A1 (en) * 2011-06-16 2012-12-20 Saab Ab A double-curved cover for covering a gap between two structural portions of an aircraft
CN102424106A (zh) * 2011-12-14 2012-04-25 中国人民解放军总参谋部第六十研究所 海用型无人机舱段间密封和监测机构
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
EP2749493B1 (de) * 2012-12-27 2016-03-23 Airbus Operations, S.L. Flugzeug-Bauchverkleidung mit verbesserter Ladekapazität
JP6336362B2 (ja) * 2014-09-10 2018-06-06 三菱航空機株式会社 航空機
EP3179405B1 (de) * 2014-09-18 2019-07-31 Huawei Technologies Co. Ltd. Fingerabdruckidentifizierungsvorrichtung
US10077669B2 (en) 2014-11-26 2018-09-18 United Technologies Corporation Non-metallic engine case inlet compression seal for a gas turbine engine
US20190185134A1 (en) * 2017-12-19 2019-06-20 Thomas Hsueh Adjustable Fuselage Location Joint Method
DE102018127024B3 (de) * 2018-10-30 2019-10-31 Airbus Operations Gmbh Flugzeugtürdichtungssystem und Flugzeugtüranordnung
CN111003152B (zh) * 2019-12-25 2023-10-20 中国航空工业集团公司西安飞机设计研究所 一种飞机舵面前缘密封装置
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
CN113371176A (zh) * 2021-07-20 2021-09-10 中国商用飞机有限责任公司 用于飞行器增压区舱门的密封件和配备有该密封件的飞行器增压区舱门

Family Cites Families (13)

* 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
US2360220A (en) * 1943-01-16 1944-10-10 Paul R Goldman Knockdown decoy airplane and package
US2616509A (en) * 1946-11-29 1952-11-04 Thomas Wilfred Pneumatic airfoil
DE943093C (de) * 1954-10-30 1956-05-09 Canadian Patents Dev Abdichtung fuer Tueren, Kappen, Schieber od. dgl. von Druckkabinen, insbesondere von Flugzeugen
US3023860A (en) * 1957-03-18 1962-03-06 Floyd P Ellzey Body construction
US2981504A (en) * 1959-03-13 1961-04-25 Gen Dynamics Corp Fuselage blade sealing using conical surfaces
FR1523404A (fr) * 1967-03-22 1968-05-03 Sud Aviation Perfectionnement aux raccordements entre fuselage et voilure d'un aérodyne
GB1465885A (en) * 1974-05-03 1977-03-02 Neuhierl H Model aircraft
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
US4417708A (en) * 1982-05-12 1983-11-29 Grumman Aerospace Corporation Interchangeable wing aircraft
DE3538483A1 (de) * 1985-10-25 1987-04-30 Wolf Hoffmann Flugzeugbau Kg Flugzeug in kunststoffbauweise
DE4313592C2 (de) * 1993-04-26 2000-02-17 Daimler Chrysler Aerospace Großraumflugzeug
FR2789144A1 (fr) * 1999-02-03 2000-08-04 Joint Francais Joint pour panneaux et aeronef comportant un tel joint

Also Published As

Publication number Publication date
CA2389856C (fr) 2009-08-18
EP1273512B1 (de) 2005-01-26
FR2827028A1 (fr) 2003-01-10
BR0202753A (pt) 2003-05-13
DE60202716D1 (de) 2005-03-03
US6581877B2 (en) 2003-06-24
FR2827028B1 (fr) 2003-09-26
CA2389856A1 (fr) 2003-01-06
BR0202753B1 (pt) 2010-10-19
US20030006344A1 (en) 2003-01-09
EP1273512A1 (de) 2003-01-08
DE60202716T2 (de) 2006-05-11
ES2234993T3 (es) 2005-07-01

Similar Documents

Publication Publication Date Title
ATE287821T1 (de) Flugzeug mit flügel-rumpf-verkleidungsdichtung
WO2003059736A3 (en) An aircraft internal wing and design
WO2004041640A3 (en) Slotted aircraft wing
BR9806725A (pt) Conjunto de asa aeronave, aeronave, dispositivo de hipersustentação de borda dianteira, e, processo para redução do arrasto associado com uma asa de aeronave
DE50115739D1 (de) Flügelprofil mit leistungs-steigernder Hinterkante
ATE337960T1 (de) Aerodynamisches profil mit verstellbarer klappe
FR2386449A1 (fr) Dispositif hypersustentateur de bord d'attaque d'ailes d'avions
DE3875640D1 (de) Von luft oder wasser umstroemter stroemungskoerper.
FR2792285B1 (fr) Surface aerodynamique d'aeronef a deflecteur de bord de fuite
FR2891525B1 (fr) Dispositif de controle d'un sillage tourbillonnaire engendre par un element oblong sur l'extrados d'une surface portante d'un aeronef.
ATE236044T1 (de) Stromlinienverkleidungen für flugzeuge
IT1168988B (it) Perfezionamento apportati alle prese d'aria di motori a turbina a gas montati su aeromobili
DE3768092D1 (de) Vorrichtung zum beschichten einer form.
GB2138507B (en) Mounting and exhausting in turbo-propellor aircraft engines
ES8302573A1 (es) "mejoras en los aparejos de velas de ala".
FR2767111B1 (fr) Aile d'avion equipee d'un volet d'atterrissage
ATE123454T1 (de) Leichte schaufel.
SE8205103L (sv) Luftrenare vid en forbrenningsmotor
FR2735444B3 (fr) Carenage aerodynamique de la bride a conduit(s) de drainage sur pylone de suspension de reacteur d'avion
SE9802326D0 (sv) A method and device for improving the air-flow at the tip of an aircraft wing
FI952369A0 (fi) Siiveke, johon on kiinnitetty kääntösiivekkeet, laivoja varten
DE50208997D1 (de) Vorrichtung zur Entgegenwirkung von im Nabenbereich von Propellern und/oder Propellerantrieben im umgebenden Fluid erzeugten Strömungswirbeln
RU92007834A (ru) Способ формирования устойчивого вихревого потока на законцовке аэродинамических поверхностей и устройство для его осуществления
IVANOV Investigations of the intensity of oscillations of the boundary of a turbulent wake
TRIEBSTEIN et al. Determination of unsteady aerodynamic forces on engines with a view to flutter investigations(BESTIMMUNG INSTATIONAERER TRIEBWERKSLUFTKRAEFTE FUER DIE ANWENDUNG BEI FLATTERUNTERSUCHUNGEN)

Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties