DE3721479A1 - Betaetigungsanordnung fuer vorfluegel eines luftfahrzeug-tragfluegels - Google Patents

Betaetigungsanordnung fuer vorfluegel eines luftfahrzeug-tragfluegels

Info

Publication number
DE3721479A1
DE3721479A1 DE19873721479 DE3721479A DE3721479A1 DE 3721479 A1 DE3721479 A1 DE 3721479A1 DE 19873721479 DE19873721479 DE 19873721479 DE 3721479 A DE3721479 A DE 3721479A DE 3721479 A1 DE3721479 A1 DE 3721479A1
Authority
DE
Germany
Prior art keywords
slat
point
wing
actuating arrangement
guide rail
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.)
Granted
Application number
DE19873721479
Other languages
German (de)
English (en)
Other versions
DE3721479C2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html
Inventor
Wilfried Dipl Ing Ellmers
Wilhelm Dipl Ing Martens
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 Operations 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
Priority to DE19873721479 priority Critical patent/DE3721479A1/de
Priority to EP88108852A priority patent/EP0297304B1/de
Priority to US07/213,335 priority patent/US4915327A/en
Publication of DE3721479A1 publication Critical patent/DE3721479A1/de
Application granted granted Critical
Publication of DE3721479C2 publication Critical patent/DE3721479C2/de
Granted legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
    • B64C13/30—Transmitting means without power amplification or where power amplification is irrelevant mechanical using cable, chain, or rod mechanisms
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Blinds (AREA)
DE19873721479 1987-06-30 1987-06-30 Betaetigungsanordnung fuer vorfluegel eines luftfahrzeug-tragfluegels Granted DE3721479A1 (de)

Priority Applications (3)

Application Number Priority Date Filing Date Title
DE19873721479 DE3721479A1 (de) 1987-06-30 1987-06-30 Betaetigungsanordnung fuer vorfluegel eines luftfahrzeug-tragfluegels
EP88108852A EP0297304B1 (de) 1987-06-30 1988-06-03 Betätigungsanordnung für Vorflügel eines Luftfahrzeug Tragflügels
US07/213,335 US4915327A (en) 1987-06-30 1988-06-30 Slat actuation and steering

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19873721479 DE3721479A1 (de) 1987-06-30 1987-06-30 Betaetigungsanordnung fuer vorfluegel eines luftfahrzeug-tragfluegels

Publications (2)

Publication Number Publication Date
DE3721479A1 true DE3721479A1 (de) 1989-01-19
DE3721479C2 DE3721479C2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1990-02-01

Family

ID=6330542

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19873721479 Granted DE3721479A1 (de) 1987-06-30 1987-06-30 Betaetigungsanordnung fuer vorfluegel eines luftfahrzeug-tragfluegels

Country Status (3)

Country Link
US (1) US4915327A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
EP (1) EP0297304B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
DE (1) DE3721479A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2695905B1 (fr) * 1992-09-24 1994-12-16 Aerospatiale Bec kruger rigide, pour bord d'attaque de voilure d'aéronef.
US5927656A (en) * 1996-06-26 1999-07-27 The Boeing Company Wing leading edge flap and method therefor
US6431498B1 (en) * 2000-06-30 2002-08-13 Philip Watts Scalloped wing leading edge
DE10147772C1 (de) * 2001-09-27 2003-09-11 Siemens Ag Verfahren zum Betreiben eines Übertragungssystems und Übertragungssystem in einem Energieversorgungsnetz
CA2515276A1 (en) * 2004-08-23 2006-02-23 Goodrich Corporation Aircraft wing
US7249735B2 (en) * 2005-06-30 2007-07-31 The Boeing Company Translating conduit apparatus for an airplane or equipment
EP1757519B1 (en) * 2005-08-25 2010-03-31 GKN Aerospace Services Limited Aircraft wing slat
DE102006053259A1 (de) * 2006-11-11 2008-05-21 Airbus Deutschland Gmbh Hochauftriebssystem am Tragflügel eines Flugzeugs und Verfahren zu seiner Betätigung
GB0700604D0 (en) * 2007-01-11 2007-02-21 Airbus Uk Ltd A leading edge structure for an aerofoil
EP1972547A1 (en) * 2007-03-21 2008-09-24 Asco Industries Wing leading edge device
DE102007020870A1 (de) * 2007-05-04 2008-11-13 Airbus Deutschland Gmbh Hochauftriebssystem am Tragflügel eines Flugzeugs
GB0721284D0 (en) * 2007-10-31 2007-12-12 Airbus Uk Ltd Actuation system for leading edge high-lift device
DE102008050544A1 (de) * 2008-10-06 2010-04-29 Airbus Deutschland Gmbh An der Tragfläche eines Flugzeugs angeordneter Vorflügel
US8534611B1 (en) 2009-07-17 2013-09-17 The Boeing Company Moveable leading edge device for a wing
US8534610B1 (en) * 2009-07-17 2013-09-17 The Boeing Company Method and apparatus for a leading edge slat on a wing of an aircraft
EP3444182B1 (en) * 2017-08-18 2023-01-18 Airbus Operations GmbH Wing for an aircraft
US12179919B2 (en) * 2023-04-12 2024-12-31 The Boeing Company Slat movement system for aircraft

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1572004A (en) * 1978-03-30 1980-07-23 Hawker Siddeley Aviation Ltd Aircraft wings
US4339970A (en) * 1980-10-10 1982-07-20 Enstrom Rudolph J Serviceable releasable socket retaining ratchet
DE2916040C2 (de) * 1979-04-20 1986-01-02 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Tragflügel für ein Luftfahrzeug mit beweglichen Vorflügeln

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR797675A (fr) * 1935-05-14 1936-05-01 Handley Page Ltd Perfectionnements aux mécanismes de commande pour aéronefs
US3272458A (en) * 1964-12-08 1966-09-13 Gen Dynamics Corp Means for positioning a rotating wing slat device
US4202519A (en) * 1978-09-08 1980-05-13 The Boeing Company Airfoil leading edge slat apparatus
US4399970A (en) * 1980-11-13 1983-08-23 The Boeing Company Wing leading edge slat
US4650140A (en) * 1985-12-30 1987-03-17 The Boeing Company Wind edge movable airfoil having variable camber

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1572004A (en) * 1978-03-30 1980-07-23 Hawker Siddeley Aviation Ltd Aircraft wings
DE2916040C2 (de) * 1979-04-20 1986-01-02 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Tragflügel für ein Luftfahrzeug mit beweglichen Vorflügeln
US4339970A (en) * 1980-10-10 1982-07-20 Enstrom Rudolph J Serviceable releasable socket retaining ratchet

Also Published As

Publication number Publication date
EP0297304A3 (en) 1990-02-28
EP0297304A2 (de) 1989-01-04
US4915327A (en) 1990-04-10
DE3721479C2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1990-02-01
EP0297304B1 (de) 1992-12-23

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Legal Events

Date Code Title Description
OP8 Request for examination as to paragraph 44 patent law
D2 Grant after examination
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: DEUTSCHE AIRBUS GMBH, 2000 HAMBURG, DE

8327 Change in the person/name/address of the patent owner

Owner name: DEUTSCHE AEROSPACE AIRBUS GMBH, 2000 HAMBURG, DE

8327 Change in the person/name/address of the patent owner

Owner name: DAIMLER-BENZ AEROSPACE AIRBUS GMBH, 21129 HAMBURG,

8327 Change in the person/name/address of the patent owner

Owner name: DAIMLERCHRYSLER AEROSPACE AIRBUS GMBH, 21129 HAMBU

8327 Change in the person/name/address of the patent owner

Owner name: EADS AIRBUS GMBH, 21129 HAMBURG, DE

8327 Change in the person/name/address of the patent owner

Owner name: AIRBUS DEUTSCHLAND GMBH, 21129 HAMBURG, DE