FR2518050B1 - Dispositif pour realiser l'etancheite laterale d'une fente de volet sur un avion - Google Patents

Dispositif pour realiser l'etancheite laterale d'une fente de volet sur un avion

Info

Publication number
FR2518050B1
FR2518050B1 FR8220327A FR8220327A FR2518050B1 FR 2518050 B1 FR2518050 B1 FR 2518050B1 FR 8220327 A FR8220327 A FR 8220327A FR 8220327 A FR8220327 A FR 8220327A FR 2518050 B1 FR2518050 B1 FR 2518050B1
Authority
FR
France
Prior art keywords
aircraft
realizing
side sealing
shutter slot
shutter
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
FR8220327A
Other languages
English (en)
Other versions
FR2518050A1 (fr
Inventor
Rudiger Kunz
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2518050A1 publication Critical patent/FR2518050A1/fr
Application granted granted Critical
Publication of FR2518050B1 publication Critical patent/FR2518050B1/fr
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for
FR8220327A 1981-12-15 1982-12-03 Dispositif pour realiser l'etancheite laterale d'une fente de volet sur un avion Expired FR2518050B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3149629A DE3149629C1 (de) 1981-12-15 1981-12-15 Einrichtung zum Abdichten eines Luftspaltes an einer Flugzeugklappe

Publications (2)

Publication Number Publication Date
FR2518050A1 FR2518050A1 (fr) 1983-06-17
FR2518050B1 true FR2518050B1 (fr) 1986-01-03

Family

ID=6148776

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8220327A Expired FR2518050B1 (fr) 1981-12-15 1982-12-03 Dispositif pour realiser l'etancheite laterale d'une fente de volet sur un avion

Country Status (3)

Country Link
US (1) US4471925A (fr)
DE (1) DE3149629C1 (fr)
FR (1) FR2518050B1 (fr)

Families Citing this family (42)

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US4576347A (en) * 1984-10-30 1986-03-18 The Boeing Company Flap torque tube slot seal
US5222699A (en) * 1990-04-16 1993-06-29 Ltv Aerospace And Defense Company Variable control aircraft control surface
DE9113090U1 (fr) * 1991-10-21 1992-01-16 Rochelt, Guenter, Prof., 2000 Hamburg, De
JP2606289Y2 (ja) * 1993-06-07 2000-10-10 富士重工業株式会社 航空機のナセル装置
US5794893A (en) * 1995-06-07 1998-08-18 Northrop Grumman Corporation Elastomeric transition for aircraft control surface
US5803405A (en) * 1995-06-07 1998-09-08 Northrop Grumman Corporation Expandable aircraft section
US5738298A (en) * 1995-06-08 1998-04-14 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Tip fence for reduction of lift-generated airframe noise
AU5239098A (en) 1996-10-22 1998-05-15 Boeing Company, The Airplane with unswept slotted cruise wing airfoil
DE19719922C1 (de) * 1997-05-13 1998-11-12 Daimler Benz Aerospace Airbus Einrichtung zur Beeinflussung einer Wurzelströmung
US5913494A (en) * 1997-07-25 1999-06-22 Mcdonnell Douglas Blade seal for an aircraft
US5984230A (en) * 1997-12-15 1999-11-16 Orazi; Paul Wing assemblies for aircraft
US6145791A (en) * 1998-01-09 2000-11-14 Northrop Grumman Corporation Elastomeric transition for aircraft control surface
US6244542B1 (en) * 1999-07-20 2001-06-12 Northrop Grumman Corporation Rotor driven edge
US7216833B2 (en) * 2001-07-30 2007-05-15 Iostar Corporation In orbit space transportation and recovery system
DE02761698T1 (de) * 2002-09-17 2005-11-10 Bell Helicopter Textron, Inc., Fort Worth Torsionsentkoppeltes motorhalterungssystem
US6799739B1 (en) 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
US7357358B2 (en) * 2004-02-27 2008-04-15 The Boeing Company Aircraft leading edge device systems and corresponding sizing methods
DE102004035921B4 (de) * 2004-07-23 2006-08-03 Airbus Deutschland Gmbh Klappen-Kopplungssystem für Luftfahrzeuge
US7494094B2 (en) 2004-09-08 2009-02-24 The Boeing Company Aircraft wing systems for providing differential motion to deployable lift devices
US7264206B2 (en) 2004-09-30 2007-09-04 The Boeing Company Leading edge flap apparatuses and associated methods
US7614588B2 (en) * 2004-12-23 2009-11-10 David Birkenstock Apparatus system and method for drag reduction
US7338018B2 (en) 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
US7721999B2 (en) 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
FR2892999B1 (fr) * 2005-11-08 2008-02-01 Airbus France Sas Aeronef comportant un carenage central ajusteur de pression voilure par deformations geometriques locales
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
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.
ES2301360B1 (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 del estabilizador horizontal orientable de un avion, extendido con una carena aerodinamica de sellado de la abertura existente entre el fuselaje y el estabilizador horizontal orientable.
US7954769B2 (en) 2007-12-10 2011-06-07 The Boeing Company Deployable aerodynamic devices with reduced actuator loads, and related systems and methods
US7766282B2 (en) 2007-12-11 2010-08-03 The Boeing Company Trailing edge device catchers and associated systems and methods
DE102008020390A1 (de) * 2008-04-23 2009-11-05 Airbus Deutschland Gmbh Tragflügel für ein Luftfahrzeug
ES2397802T3 (es) * 2008-05-09 2013-03-11 The Boeing Company Fuselados de carenado de unión de aeronave con porciones fijas y móviles, y sistemas y métodos asociados
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
ES2386442B1 (es) * 2009-11-27 2013-07-09 Airbus Operations S.L. Carena de timón de profundidad de aeronave.
US8342447B2 (en) * 2010-06-15 2013-01-01 The Boeing Company Morphing control surface transition
GB201018924D0 (en) * 2010-11-09 2010-12-22 Airbus Operations Ltd Seal
FR2976551B1 (fr) * 2011-06-20 2013-06-28 Snecma Pale, en particulier a calage variable, helice comprenant de telles pales, et turbomachine correspondante
DE102013012169A1 (de) * 2013-07-20 2015-01-22 Airbus Defence and Space GmbH Formvariable Spaltabdeckung zwischen Steuerflächen und angrenzenden Struktur-Bauteilen an Flugzeugen
US9623957B2 (en) * 2014-08-26 2017-04-18 The Boeing Company Torque tube door
US10000274B2 (en) * 2015-08-20 2018-06-19 The Boeing Company Mitigation of surface discontinuities between flight control surfaces and an airframe of an aircraft
US10100805B2 (en) * 2015-10-12 2018-10-16 General Electric Compant Tip extension assembly for a wind turbine rotor blade
US10800511B2 (en) 2018-05-31 2020-10-13 The Boeing Company End seal device for a high-lift device of an aircraft

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB455501A (en) * 1935-04-18 1936-10-19 Phiroze Pestonji Nazir Improvements in or relating to aeroplanes and the like
DE674434C (de) * 1937-07-10 1939-04-14 Gothaer Waggonfabrik Akt Ges Leitwerk fuer Flugzeuge
US2137047A (en) * 1937-07-26 1938-11-15 Gliwa Michael Extensible airplane wing
US2526929A (en) * 1948-05-29 1950-10-24 Curtiss Wright Corp Airplane flap extension
US3063659A (en) * 1960-12-23 1962-11-13 Szerda Frank Safety aircraft
DE1506615A1 (de) * 1967-06-12 1969-08-28 Ver Flugtechnische Werke Steuerklappenausbildung und -anordnung an einem Profil eines Flugzeuges
US3968946A (en) * 1975-03-31 1976-07-13 The Boeing Company Extendable aerodynamic fairing
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
GB1560911A (en) * 1978-02-17 1980-02-13 British Aircraft Corp Ltd Aircraft
GB2055729B (en) * 1979-08-08 1983-04-20 British Aerospace Aircraft
FR2492337A1 (fr) * 1980-10-16 1982-04-23 Aerospatiale Aile d'aeronef pourvue d'un systeme hypersustentateur dans son bord d'attaque et aeronef comportant une telle aile

Also Published As

Publication number Publication date
DE3149629C1 (de) 1983-04-21
FR2518050A1 (fr) 1983-06-17
US4471925A (en) 1984-09-18

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Legal Events

Date Code Title Description
ST Notification of lapse