ATE272532T1 - Flugzeugklappensystem - Google Patents

Flugzeugklappensystem

Info

Publication number
ATE272532T1
ATE272532T1 AT01980765T AT01980765T ATE272532T1 AT E272532 T1 ATE272532 T1 AT E272532T1 AT 01980765 T AT01980765 T AT 01980765T AT 01980765 T AT01980765 T AT 01980765T AT E272532 T1 ATE272532 T1 AT E272532T1
Authority
AT
Austria
Prior art keywords
aircraft flaps
flaps system
aircraft
carriage
system suitable
Prior art date
Application number
AT01980765T
Other languages
English (en)
Inventor
Philip Ian Robinson
Original Assignee
Airbus Uk Ltd
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 Uk Ltd filed Critical Airbus Uk Ltd
Application granted granted Critical
Publication of ATE272532T1 publication Critical patent/ATE272532T1/de

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
    • 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
    • B64C9/18—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single flaps

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
  • Tires In General (AREA)
  • Radio Relay Systems (AREA)
  • Mobile Radio Communication Systems (AREA)
  • Retarders (AREA)
  • Aerials With Secondary Devices (AREA)
  • Air Bags (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Mechanical Control Devices (AREA)
AT01980765T 2000-12-22 2001-11-13 Flugzeugklappensystem ATE272532T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB0031442.7A GB0031442D0 (en) 2000-12-22 2000-12-22 An aircraft flap mechanism
PCT/GB2001/004984 WO2002062660A1 (en) 2000-12-22 2001-11-13 An aircraft flap extension mechanism

Publications (1)

Publication Number Publication Date
ATE272532T1 true ATE272532T1 (de) 2004-08-15

Family

ID=9905731

Family Applications (1)

Application Number Title Priority Date Filing Date
AT01980765T ATE272532T1 (de) 2000-12-22 2001-11-13 Flugzeugklappensystem

Country Status (8)

Country Link
US (1) US7004432B2 (de)
EP (1) EP1343687B1 (de)
AT (1) ATE272532T1 (de)
CA (1) CA2431352C (de)
DE (1) DE60104721T2 (de)
ES (1) ES2221654T3 (de)
GB (1) GB0031442D0 (de)
WO (1) WO2002062660A1 (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0810460D0 (en) * 2008-06-09 2008-07-09 Airbus Uk Ltd Support assembly
US7938000B2 (en) * 2008-09-25 2011-05-10 Airbus Operations Gmbh Method and measuring device for measuring overlap on an aircraft wing
GB0911012D0 (en) * 2009-06-25 2009-08-12 Airbus Operations Ltd Cross-bleed dam
GB0913473D0 (en) * 2009-08-04 2009-09-16 Airbus Operations Ltd Support assembly
DE102011082888B4 (de) * 2011-09-16 2016-01-07 Airbus Defence and Space GmbH Auftriebsklappenanordnung, Tragflügel sowie Flugzeug
JP5956803B2 (ja) * 2012-03-29 2016-07-27 一般社団法人日本航空宇宙工業会 飛行体の高揚力装置
EP2746151B1 (de) * 2012-12-19 2017-04-12 Airbus Operations GmbH Klappensystem für ein Flugzeug, Verfahren zur Einstellung des Auftriebs eines Flugzeugs und Flugzeug mit einem Hauptflügel und mindestens einem Klappensystem
US10532805B2 (en) * 2016-09-20 2020-01-14 Gulfstream Aerospace Corporation Airfoil for an aircraft having reduced noise generation
ES2886667T3 (es) * 2017-12-19 2021-12-20 Asco Ind Nv Sistema de despliegue para un dispositivo de borde de ataque de sustentación elevada de perfil aerodinámico

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3438599A (en) * 1967-10-12 1969-04-15 Mc Donnell Douglas Corp Flap track roller support
DE2100733A1 (de) * 1970-01-12 1971-07-15 Hawker Siddeley Aviation Ltd., Kingston-Upon-Thames, Surrey (Grossbritannien) Vorrichtung an Flugzeugtragflachen
DE3713465A1 (de) 1987-04-22 1988-11-10 Messerschmitt Boelkow Blohm Tandem-landeklappenwagen
US4995575A (en) * 1988-09-26 1991-02-26 The Boeing Company Wing trailing edge flap mechanism
DE4107556C1 (de) * 1991-03-08 1992-05-14 Deutsche Airbus Gmbh, 2000 Hamburg, De
US5788190A (en) * 1996-10-22 1998-08-04 The Boeing Company Slotted cruise trailing edge flap
DE19925560B4 (de) * 1999-06-04 2004-04-22 Deutsches Zentrum für Luft- und Raumfahrt e.V. Zusatzflügel für Hauptflügel von Flugzeugen

Also Published As

Publication number Publication date
ES2221654T3 (es) 2005-01-01
EP1343687A1 (de) 2003-09-17
GB0031442D0 (en) 2001-02-07
WO2002062660A1 (en) 2002-08-15
DE60104721T2 (de) 2005-01-13
CA2431352C (en) 2006-09-05
US20040065783A1 (en) 2004-04-08
EP1343687B1 (de) 2004-08-04
CA2431352A1 (en) 2002-08-15
US7004432B2 (en) 2006-02-28
DE60104721D1 (de) 2004-09-09

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Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties