FR2695905B1 - Bec kruger rigide, pour bord d'attaque de voilure d'aéronef. - Google Patents

Bec kruger rigide, pour bord d'attaque de voilure d'aéronef.

Info

Publication number
FR2695905B1
FR2695905B1 FR9211405A FR9211405A FR2695905B1 FR 2695905 B1 FR2695905 B1 FR 2695905B1 FR 9211405 A FR9211405 A FR 9211405A FR 9211405 A FR9211405 A FR 9211405A FR 2695905 B1 FR2695905 B1 FR 2695905B1
Authority
FR
France
Prior art keywords
kruger
spout
rigid
leading edge
aircraft wings
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 - Fee Related
Application number
FR9211405A
Other languages
English (en)
Other versions
FR2695905A1 (fr
Inventor
Patrick Capbern
Jerome Charieras
Pascal Chaumel
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 FR9211405A priority Critical patent/FR2695905B1/fr
Priority to US08/126,708 priority patent/US5474265A/en
Publication of FR2695905A1 publication Critical patent/FR2695905A1/fr
Application granted granted Critical
Publication of FR2695905B1 publication Critical patent/FR2695905B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • B64C9/24—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by single flap
FR9211405A 1992-09-24 1992-09-24 Bec kruger rigide, pour bord d'attaque de voilure d'aéronef. Expired - Fee Related FR2695905B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR9211405A FR2695905B1 (fr) 1992-09-24 1992-09-24 Bec kruger rigide, pour bord d'attaque de voilure d'aéronef.
US08/126,708 US5474265A (en) 1992-09-24 1993-09-24 Rigid kruger nose for the leading edge of an aircraft wing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9211405A FR2695905B1 (fr) 1992-09-24 1992-09-24 Bec kruger rigide, pour bord d'attaque de voilure d'aéronef.

Publications (2)

Publication Number Publication Date
FR2695905A1 FR2695905A1 (fr) 1994-03-25
FR2695905B1 true FR2695905B1 (fr) 1994-12-16

Family

ID=9433854

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9211405A Expired - Fee Related FR2695905B1 (fr) 1992-09-24 1992-09-24 Bec kruger rigide, pour bord d'attaque de voilure d'aéronef.

Country Status (2)

Country Link
US (1) US5474265A (fr)
FR (1) FR2695905B1 (fr)

Families Citing this family (30)

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Publication number Priority date Publication date Assignee Title
US6293497B1 (en) 1996-10-22 2001-09-25 The Boeing Company Airplane with unswept slotted cruise wing airfoil
DE19719922C1 (de) * 1997-05-13 1998-11-12 Daimler Benz Aerospace Airbus Einrichtung zur Beeinflussung einer Wurzelströmung
DE19743907C1 (de) * 1997-10-04 1998-12-10 Daimler Benz Aerospace Airbus Tragfläche mit kurzgekoppeltem Triebwerk
DE19910551C2 (de) 1999-03-10 2001-04-05 Eads Airbus Gmbh Flugzeugtragfläche mit mindestens einem kurzgekoppelten Triebwerk
GB0114634D0 (en) * 2001-06-15 2001-08-08 Broadbent Michael C Contiguous variable camber device
EP1338506A1 (fr) * 2002-02-15 2003-08-27 Fairchild Dornier GmbH Aile d'avion avec slat et volet Krueger
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
US6796534B2 (en) 2002-09-10 2004-09-28 The Boeing Company Method and apparatus for controlling airflow with a leading 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
US20050127239A1 (en) * 2003-08-25 2005-06-16 Srivastava Varad N. Flying work station
US6799739B1 (en) 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
US7014142B2 (en) * 2004-02-03 2006-03-21 The Boeing Company Low-drag rotor/wing flap
US6978971B1 (en) 2004-06-15 2005-12-27 The Boeing Company Methods and apparatuses for controlling airflow proximate to engine/airfoil systems
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
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
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
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
US7578484B2 (en) * 2006-06-14 2009-08-25 The Boeing Company Link mechanisms for gapped rigid krueger flaps, and associated systems and methods
GB0700604D0 (en) * 2007-01-11 2007-02-21 Airbus Uk Ltd A leading edge structure for an aerofoil
GB0721284D0 (en) * 2007-10-31 2007-12-12 Airbus Uk Ltd Actuation system for leading edge high-lift device
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
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
DE102010014792A1 (de) * 2010-04-13 2011-10-13 Airbus Operations Gmbh Hochauftriebssystem für ein Flugzeug
DE102011018906A1 (de) * 2011-04-28 2012-10-31 Airbus Operations Gmbh Hochauftriebssystem für ein Flugzeug und Verfahren zum Beeinflussen der Hochauftriebseigenschaften eines Flugzeugs
EP3241740B1 (fr) * 2016-05-03 2020-08-19 Airbus Operations GmbH Système d'entraînement d'un dispositif de lamelle d'une aile d'avion
JP6929809B2 (ja) 2018-03-02 2021-09-01 三菱重工業株式会社 高揚力装置、翼及び航空機

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB991405A (en) * 1960-05-19 1965-05-05 Dehavilland Aircraft Improvements relating to aircraft
US3195836A (en) * 1962-04-16 1965-07-20 Alvarez-Calderon Alberto High lift slotted flap
US3556439A (en) * 1968-11-22 1971-01-19 Boeing Co Methods and high lift systems for making an aircraft wing more efficient for takeoffs and landings
US3743219A (en) * 1971-06-30 1973-07-03 Boeing Co High lift leading edge device
US3917192A (en) * 1973-07-09 1975-11-04 Alvarez Calderon Alberto Flap mechanisms and apparatus
FR2249804B1 (fr) * 1973-11-06 1976-10-01 Aerospatiale
US3910530A (en) * 1973-11-07 1975-10-07 Boeing Co Leading edge flap
DE2355723C3 (de) * 1973-11-08 1979-05-23 Dornier Gmbh, 7990 Friedrichshafen Spaltklappensystem für Flugzeuge
US3941334A (en) * 1975-03-28 1976-03-02 The Boeing Company Variable camber airfoil
US4159089A (en) * 1977-05-31 1979-06-26 Boeing Commercial Airplane Company Variable camber flap
US4189121A (en) * 1978-01-23 1980-02-19 Boeing Commercial Airplane Company Variable twist leading edge flap
US4262868A (en) * 1979-05-29 1981-04-21 The Boeing Company Three-position variable camber flap
US4427168A (en) * 1981-09-29 1984-01-24 The Boeing Company Variable camber leading edge mechanism with Krueger flap
US4445655A (en) * 1982-02-01 1984-05-01 Omac, Inc. Kreuger flap actuating mechanism for delta wing, canard type aircraft
DE3721479A1 (de) * 1987-06-30 1989-01-19 Messerschmitt Boelkow Blohm Betaetigungsanordnung fuer vorfluegel eines luftfahrzeug-tragfluegels
US5158252A (en) * 1991-10-24 1992-10-27 The Boeing Company Three-position variable camber Krueger leading edge flap

Also Published As

Publication number Publication date
FR2695905A1 (fr) 1994-03-25
US5474265A (en) 1995-12-12

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Legal Events

Date Code Title Description
CD Change of name or company name
TP Transmission of property
ST Notification of lapse

Effective date: 20110531