FR2492337B1 - - Google Patents

Info

Publication number
FR2492337B1
FR2492337B1 FR8022154A FR8022154A FR2492337B1 FR 2492337 B1 FR2492337 B1 FR 2492337B1 FR 8022154 A FR8022154 A FR 8022154A FR 8022154 A FR8022154 A FR 8022154A FR 2492337 B1 FR2492337 B1 FR 2492337B1
Authority
FR
France
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
FR8022154A
Other languages
French (fr)
Other versions
FR2492337A1 (fr
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 Group SAS
Original Assignee
Airbus Group SAS
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 Group SAS filed Critical Airbus Group SAS
Priority to FR8022154A priority Critical patent/FR2492337A1/fr
Priority to EP81401517A priority patent/EP0050542B1/fr
Priority to DE8181401517T priority patent/DE3169141D1/de
Priority to US06/309,233 priority patent/US4384693A/en
Priority to CA000387599A priority patent/CA1164429A/fr
Publication of FR2492337A1 publication Critical patent/FR2492337A1/fr
Application granted granted Critical
Publication of FR2492337B1 publication Critical patent/FR2492337B1/fr
Granted 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
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • 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
    • Y02T50/30—Wing lift efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Accommodation For Nursing Or Treatment Tables (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
FR8022154A 1980-10-16 1980-10-16 Aile d'aeronef pourvue d'un systeme hypersustentateur dans son bord d'attaque et aeronef comportant une telle aile Granted FR2492337A1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR8022154A FR2492337A1 (fr) 1980-10-16 1980-10-16 Aile d'aeronef pourvue d'un systeme hypersustentateur dans son bord d'attaque et aeronef comportant une telle aile
EP81401517A EP0050542B1 (fr) 1980-10-16 1981-10-01 Aile d'aéronef pourvue d'un système hypersustentateur dans son bord d'attaque et aéronef comportant une telle aile
DE8181401517T DE3169141D1 (en) 1980-10-16 1981-10-01 Aircraft wing provided with a high-lift device in the leading edge, and aircraft provided with such a wing
US06/309,233 US4384693A (en) 1980-10-16 1981-10-07 Aircraft wing provided with a high-lift system in its leading edge
CA000387599A CA1164429A (fr) 1980-10-16 1981-10-08 Aile d'aeronef pourvue d'un systeme hypersustentateur dans son bord d'attaque et aeronef comportant une telle aile

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8022154A FR2492337A1 (fr) 1980-10-16 1980-10-16 Aile d'aeronef pourvue d'un systeme hypersustentateur dans son bord d'attaque et aeronef comportant une telle aile

Publications (2)

Publication Number Publication Date
FR2492337A1 FR2492337A1 (fr) 1982-04-23
FR2492337B1 true FR2492337B1 (en:Method) 1983-10-21

Family

ID=9246970

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8022154A Granted FR2492337A1 (fr) 1980-10-16 1980-10-16 Aile d'aeronef pourvue d'un systeme hypersustentateur dans son bord d'attaque et aeronef comportant une telle aile

Country Status (5)

Country Link
US (1) US4384693A (en:Method)
EP (1) EP0050542B1 (en:Method)
CA (1) CA1164429A (en:Method)
DE (1) DE3169141D1 (en:Method)
FR (1) FR2492337A1 (en:Method)

Families Citing this family (44)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3149629C1 (de) * 1981-12-15 1983-04-21 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Einrichtung zum Abdichten eines Luftspaltes an einer Flugzeugklappe
US5056741A (en) * 1989-09-29 1991-10-15 The Boeing Company Apparatus and method for aircraft wing stall control
DE69718659T2 (de) 1996-10-22 2003-05-22 The Boeing Co., Seattle Flugzeug mit ungepfeiltem schlitzflügel für den reiseflug
DE19719922C1 (de) * 1997-05-13 1998-11-12 Daimler Benz Aerospace Airbus Einrichtung zur Beeinflussung einer Wurzelströmung
US6073889A (en) * 1997-10-16 2000-06-13 The Boeing Company Wing flap seal bump
DE19906969B4 (de) * 1999-02-19 2004-10-14 Rheinmetall W & M Gmbh Aus einem Waffenrohr verschießbares leitwerkstabilisiertes Geschoß
DE19910551C2 (de) 1999-03-10 2001-04-05 Eads Airbus Gmbh Flugzeugtragfläche mit mindestens einem kurzgekoppelten Triebwerk
US7258308B2 (en) * 2002-07-02 2007-08-21 The Boeing Company Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface
US7059563B2 (en) * 2003-06-03 2006-06-13 The Boeing Company Systems, apparatuses, and methods for moving aircraft control surfaces
US7243881B2 (en) 2003-06-03 2007-07-17 The Boeing Company Multi-function trailing edge devices and associated methods
US6935592B2 (en) * 2003-08-29 2005-08-30 Supersonic Aerospace International, Llc Aircraft lift device for low sonic boom
US6799739B1 (en) 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
US7424350B2 (en) 2004-02-02 2008-09-09 The Boeing Company Vehicle control systems and corresponding sizing methods
US7357358B2 (en) * 2004-02-27 2008-04-15 The Boeing Company Aircraft leading edge device systems and corresponding sizing methods
US6978971B1 (en) * 2004-06-15 2005-12-27 The Boeing Company Methods and apparatuses for controlling airflow proximate to engine/airfoil systems
US7270305B2 (en) 2004-06-15 2007-09-18 The Boeing Company Aircraft leading edge apparatuses and corresponding methods
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
US7322547B2 (en) 2005-01-31 2008-01-29 The Boeing Company Aerospace vehicle leading edge slat devices and corresponding methods
US7338018B2 (en) 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
US7216835B2 (en) * 2005-02-25 2007-05-15 Northrop Grumman Corporation Aircraft with extendable leading edge of fuselage and wings
US7204454B2 (en) * 2005-02-25 2007-04-17 Northrop Grumman Corporation Aircraft with articulated leading edge of fuselage and wings
US7246770B2 (en) * 2005-02-25 2007-07-24 Northrop Grumman Corporation Aircraft with rotatable leading edge of fuselage and wings
US7309043B2 (en) * 2005-04-27 2007-12-18 The Boeing Company Actuation device positioning systems and associated methods, including aircraft spoiler droop systems
US7721999B2 (en) 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7300021B2 (en) * 2005-05-20 2007-11-27 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7367530B2 (en) * 2005-06-21 2008-05-06 The Boeing Company Aerospace vehicle yaw generating systems and associated methods
US7500641B2 (en) 2005-08-10 2009-03-10 The Boeing Company Aerospace vehicle flow body systems and associated methods
US7611099B2 (en) 2005-09-07 2009-11-03 The Boeing Company Seal assemblies for use with drooped spoilers and other control surfaces on aircraft
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
GB0604026D0 (en) * 2006-02-28 2006-04-12 Airbus Uk Ltd Aircraft wing
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.
US7578484B2 (en) * 2006-06-14 2009-08-25 The Boeing Company Link mechanisms for gapped rigid krueger flaps, and associated systems and methods
BRPI0603262B1 (pt) * 2006-08-08 2021-02-23 Yaborã Indústria Aeronáutica S.A asa de aeronave incluindo um slat no bordo de ataque da asa e um fence rígido preso a uma porção estruturalmente rígida não móvel da asa
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
CA2719163C (en) * 2008-02-12 2015-10-06 Bombardier Inc. Improved slat configuration for fixed-wing aircraft
US8226048B2 (en) * 2008-12-09 2012-07-24 The Boeing Company Link mechanisms, including Stephenson II link mechanisms for multi-position flaps and associated systems and methods
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
RU2429988C1 (ru) * 2010-04-13 2011-09-27 Эдуард Дмитриевич Житников Крыло с изменяемой хордой
FR3018767B1 (fr) * 2014-03-21 2018-01-12 Airbus Operations Ensemble de support pour un systeme de volet d'aile d'un avion.
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 (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2585676A (en) * 1947-07-31 1952-02-12 Poisson-Quinton Philippe Aircraft wing and flap with boundary layer control
GB669175A (en) * 1949-01-13 1952-03-26 Jacques Jean Marie Jules Gerin Improvements in aircraft with variable-area wings
US3142457A (en) * 1962-07-16 1964-07-28 Boeing Co Stall pattern lift regulator for airplanes
US3486720A (en) * 1967-12-07 1969-12-30 Boeing Co Continuous slot forming leading edge slats for cranked wings
DE2149030A1 (de) * 1971-10-01 1973-04-05 Ver Flugtechnische Werke Tragfluegelausbildung mit geknickter fluegelvorderkante
US3910530A (en) * 1973-11-07 1975-10-07 Boeing Co Leading edge flap
US3968946A (en) * 1975-03-31 1976-07-13 The Boeing Company Extendable aerodynamic fairing
US4189121A (en) * 1978-01-23 1980-02-19 Boeing Commercial Airplane Company Variable twist leading edge flap

Also Published As

Publication number Publication date
EP0050542B1 (fr) 1985-02-27
FR2492337A1 (fr) 1982-04-23
CA1164429A (fr) 1984-03-27
DE3169141D1 (en) 1985-04-04
US4384693A (en) 1983-05-24
EP0050542A1 (fr) 1982-04-28

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Legal Events

Date Code Title Description
ST Notification of lapse