DE3624675C2 - - Google Patents

Info

Publication number
DE3624675C2
DE3624675C2 DE3624675A DE3624675A DE3624675C2 DE 3624675 C2 DE3624675 C2 DE 3624675C2 DE 3624675 A DE3624675 A DE 3624675A DE 3624675 A DE3624675 A DE 3624675A DE 3624675 C2 DE3624675 C2 DE 3624675C2
Authority
DE
Germany
Prior art keywords
flaps
flap
carrier
wing
supports
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
DE3624675A
Other languages
German (de)
English (en)
Other versions
DE3624675A1 (de
Inventor
Johann Theodor Prof. Dr.-Ing. 7997 Immenstaad De Heynatz
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.)
Dornier GmbH
Original Assignee
Dornier GmbH
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 Dornier GmbH filed Critical Dornier GmbH
Priority to DE19863624675 priority Critical patent/DE3624675A1/de
Priority to EP87107332A priority patent/EP0253986A1/de
Priority to US07/076,307 priority patent/US4796840A/en
Publication of DE3624675A1 publication Critical patent/DE3624675A1/de
Application granted granted Critical
Publication of DE3624675C2 publication Critical patent/DE3624675C2/de
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
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • 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
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B64C9/20—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by multiple flaps
    • 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)
  • Transmission Devices (AREA)
  • Air Bags (AREA)
DE19863624675 1986-07-22 1986-07-22 Einrichtung zur verstellung von klappen, insbesondere hochauftriebsklappen an flugzeugtragfluegeln Granted DE3624675A1 (de)

Priority Applications (3)

Application Number Priority Date Filing Date Title
DE19863624675 DE3624675A1 (de) 1986-07-22 1986-07-22 Einrichtung zur verstellung von klappen, insbesondere hochauftriebsklappen an flugzeugtragfluegeln
EP87107332A EP0253986A1 (de) 1986-07-22 1987-05-20 Einrichtung zur Verstellung von Hochauftriebsklappen an Flugzeugtragflügel
US07/076,307 US4796840A (en) 1986-07-22 1987-07-22 Trailing edge flap operation in wings

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19863624675 DE3624675A1 (de) 1986-07-22 1986-07-22 Einrichtung zur verstellung von klappen, insbesondere hochauftriebsklappen an flugzeugtragfluegeln

Publications (2)

Publication Number Publication Date
DE3624675A1 DE3624675A1 (de) 1988-02-04
DE3624675C2 true DE3624675C2 (en, 2012) 1991-05-23

Family

ID=6305664

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19863624675 Granted DE3624675A1 (de) 1986-07-22 1986-07-22 Einrichtung zur verstellung von klappen, insbesondere hochauftriebsklappen an flugzeugtragfluegeln

Country Status (3)

Country Link
US (1) US4796840A (en, 2012)
EP (1) EP0253986A1 (en, 2012)
DE (1) DE3624675A1 (en, 2012)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3912138A1 (de) * 1989-04-13 1990-10-18 Deutsche Forsch Luft Raumfahrt Traeger fuer hinterkantenklappen an tragfluegeln von flugzeugen
US5178348A (en) * 1992-02-05 1993-01-12 The Boeing Company Contoured wing/flap assembly and method
US5294080A (en) * 1993-02-08 1994-03-15 The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration Lift enhancing tabs for airfoils
CA2444560C (en) * 2002-10-21 2008-09-23 The Boeing Company Method and apparatus for rotatably supporting movable components, including canards
IL159186A (en) * 2003-12-04 2006-04-10 Top I Vision Ltd Aircraft wing structure and method for slowing down aircraft flight speed
DE102007036996A1 (de) * 2007-08-06 2009-02-19 Airbus Deutschland Gmbh Hochauftriebssystem für ein Flugzeug
GB0920969D0 (en) * 2009-11-27 2010-01-13 Airbus Operations Ltd Trailing edge flap
GB0920968D0 (en) * 2009-11-27 2010-01-13 Airbus Operations Ltd Trailing edge flap
GB0921007D0 (en) * 2009-11-30 2010-01-13 Airbus Operations Ltd Trailing edge flap
GB0921486D0 (en) * 2009-12-08 2010-01-20 Airbus Operations Ltd Control surface assembly
DE102009060082A1 (de) * 2009-12-22 2011-06-30 Airbus Operations GmbH, 21129 Flügelanordnung mit einer verstellbaren Klappe und Verkleidungselement zum Verkleiden eines Klappenverstellmechanismus eines Flügels
DE102010032224A1 (de) * 2010-07-26 2012-01-26 Airbus Operations Gmbh Aerodynamischer Körper mit Zusatzklappe
EP2746151B1 (en) * 2012-12-19 2017-04-12 Airbus Operations GmbH Flap system for an aircraft, method for adjusting the lift of an aircraft and aircraft comprising a main wing and at least one flap system
US10017243B2 (en) * 2013-09-24 2018-07-10 The Boeing Company Adaptive trailing edge actuator system and method
GB2583959A (en) * 2019-05-16 2020-11-18 Airbus Operations Ltd An arrangement for avoiding clashing on a folding wing tip
CN110877712A (zh) * 2019-12-02 2020-03-13 北京电子工程总体研究所 一种折叠舵面的折叠间隙调节装置
EP4311766A1 (en) 2022-07-29 2024-01-31 Airbus Operations GmbH Wing for an aircraft

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR951122A (fr) * 1947-06-26 1949-10-17 Dispositif de support applicable aux volets d'hypersustentation ou de freinage des aérodynes
US2591000A (en) * 1949-09-14 1952-04-01 North American Aviation Inc Retractable flap support
US2688455A (en) * 1951-08-14 1954-09-07 North American Aviation Inc Retractable surface support
DE2047221C3 (de) * 1970-09-25 1975-07-17 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Tragflügel für Luftfahrzeuge mit einer Doppelspaltlandeklappe
US3977630A (en) * 1973-03-09 1976-08-31 The Boeing Company STOL aircraft
US4172575A (en) * 1975-03-24 1979-10-30 Boeing Commercial Airplane Company Airfoil flap conical extension mechanism
US4434959A (en) * 1981-09-28 1984-03-06 The Boeing Company Airfoil flap assembly with flap track member
US4444368A (en) * 1981-10-30 1984-04-24 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Slotted variable camber flap

Also Published As

Publication number Publication date
DE3624675A1 (de) 1988-02-04
EP0253986A1 (de) 1988-01-27
US4796840A (en) 1989-01-10

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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
8339 Ceased/non-payment of the annual fee