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ITMI981598A0 - "ala portante con ipersostentatore di atterraggio" - Google Patents

"ala portante con ipersostentatore di atterraggio"

Info

Publication number
ITMI981598A0
ITMI981598A0 IT98MI001598A ITMI981598A ITMI981598A0 IT MI981598 A0 ITMI981598 A0 IT MI981598A0 IT 98MI001598 A IT98MI001598 A IT 98MI001598A IT MI981598 A ITMI981598 A IT MI981598A IT MI981598 A0 ITMI981598 A0 IT MI981598A0
Authority
IT
Italy
Prior art keywords
load
landing support
bearing wing
wing
bearing
Prior art date
Application number
IT98MI001598A
Other languages
English (en)
Inventor
Claus Bauer
Original Assignee
Daimler Benz 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 Daimler Benz Ag filed Critical Daimler Benz Ag
Publication of ITMI981598A0 publication Critical patent/ITMI981598A0/it
Publication of ITMI981598A1 publication Critical patent/ITMI981598A1/it

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
    • B64C9/18—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single flaps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/44—Varying camber
    • B64C3/50—Varying camber by leading or trailing edge flaps
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Seal Device For Vehicle (AREA)
  • Soil Working Implements (AREA)
  • Wind Motors (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
IT98MI001598A 1997-07-31 1998-07-13 "ala portante con ipersostentatore di atterraggio" ITMI981598A1 (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19732953A DE19732953C1 (de) 1997-07-31 1997-07-31 Tragflügel mit Landeklappe

Publications (2)

Publication Number Publication Date
ITMI981598A0 true ITMI981598A0 (it) 1998-07-13
ITMI981598A1 ITMI981598A1 (it) 2000-01-13

Family

ID=7837452

Family Applications (1)

Application Number Title Priority Date Filing Date
IT98MI001598A ITMI981598A1 (it) 1997-07-31 1998-07-13 "ala portante con ipersostentatore di atterraggio"

Country Status (5)

Country Link
US (1) US6076775A (it)
DE (1) DE19732953C1 (it)
FR (1) FR2767111B1 (it)
GB (1) GB2331734B (it)
IT (1) ITMI981598A1 (it)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19858435C1 (de) * 1998-12-17 2000-06-29 Daimler Chrysler Ag Deckhaut-Steg-Struktur
GB2386884B (en) * 2002-03-28 2005-09-14 Richard Linsley-Hood Aerofoil with variable camber
CA2518080C (en) * 2003-03-03 2014-02-25 Flexsys, Inc. Adaptive compliant wing and rotor system
US6827311B2 (en) 2003-04-07 2004-12-07 Honeywell International, Inc. Flight control actuation system
DE10325950A1 (de) * 2003-06-07 2005-01-05 Airbus Deutschland Gmbh Flügel, insbesondere Tragflügel eines Flugzeugs, mit veränderbarem Profil
DE102004006940B4 (de) * 2004-02-12 2009-02-26 Airbus Deutschland Gmbh Landeklappenführung für Luftfahrzeuge
DE102004049504A1 (de) * 2004-10-11 2006-04-13 Airbus Deutschland Gmbh Flugzeugflügel, Verfahren zum Betreiben eines Flugzeugflügels und Verwendung einer schwenkbaren Hinterkante an einem Hauptflügel eines Flugzeugflügels zum Justieren der Form und Breite eines Luftspalts
US20070138341A1 (en) * 2004-12-07 2007-06-21 Joshi Shiv P Transformable skin
DE102005045759A1 (de) 2005-09-23 2007-04-12 Airbus Deutschland Gmbh Fortschrittlicheflügelhinterkante am Flügel eines Flugzeugs
DE102005061750A1 (de) * 2005-12-21 2007-07-05 Eads Deutschland Gmbh Flexible Steuerfläche für ein Luftfahrzeug
DE102006036464B4 (de) * 2006-08-04 2009-08-20 Airbus Deutschland Gmbh Hochauftriebssystem für ein Flugzeug
DE102007036996A1 (de) * 2007-08-06 2009-02-19 Airbus Deutschland Gmbh Hochauftriebssystem für ein Flugzeug
EP3670330B1 (en) * 2018-12-20 2022-02-09 Bombardier Inc. Aircraft flap deployment system
ES3042557T3 (en) * 2022-06-01 2025-11-21 Asco Ind Nv Trailing edge flap assembly
EP4446218A1 (en) * 2023-04-11 2024-10-16 Airbus Operations GmbH Aircraft system
EP4446219B1 (en) 2023-04-11 2026-01-21 Airbus Operations GmbH Aerodynamic system for an aircraft
EP4484279A1 (en) 2023-06-30 2025-01-01 Airbus Operations GmbH Trailing edge system for an aircraft and method for operating a trailing edge movable of a trailing edge system
EP4484281A1 (en) 2023-06-30 2025-01-01 Airbus Operations GmbH Trailing edge system for an aircraft and method for operating a trailing edge movable of a trailing edge system
EP4484280A1 (en) 2023-06-30 2025-01-01 Airbus Operations GmbH Trailing edge system for an aircraft and method for manufacturing a trailing edge system
US12434811B2 (en) * 2023-08-03 2025-10-07 The Boeing Company Flap support systems and methods for a wing of an aircraft

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US32907A (en) * 1861-07-23 Churn
DE703375C (de) * 1939-01-12 1941-03-07 Gerhard Fieseler Steuerflaeche fuer Luftfahrzeuge
US3042371A (en) * 1958-09-04 1962-07-03 United Aircraft Corp Variable camber balding
FR1496151A (fr) * 1966-06-20 1967-09-29 Giravions Dorand Volet déviateur pour jet de fluide
US3583660A (en) * 1969-08-18 1971-06-08 Lockheed Aircraft Corp Lift and control augmenter for airfoils
US4053124A (en) * 1975-08-22 1977-10-11 The Boeing Company Variable camber airfoil
DE2804254C2 (de) * 1978-02-01 1985-02-07 Grob, Burkhart, Dipl.-Ing. ETH, 8023 Großhesselohe Tragflügel mit Klappe
US4247066A (en) * 1978-02-21 1981-01-27 General Dynamics Corporation Airfoil variable cambering device and method
US4395008A (en) * 1980-01-22 1983-07-26 British Aerospace Public Limited Company Aircraft wing and flap arrangement
US4351502A (en) * 1980-05-21 1982-09-28 The Boeing Company Continuous skin, variable camber airfoil edge actuating mechanism
DE3133961A1 (de) * 1981-08-27 1983-04-07 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen "betaetigungsanordnung fuer fluegelklappen"
USRE32907E (en) 1981-09-28 1989-04-18 The Boeing Company Airfoil flap assembly with flap track member
US4427169A (en) * 1982-06-08 1984-01-24 Boeing Commercial Airplane Company Variable camber flap end seal
US4899284A (en) * 1984-09-27 1990-02-06 The Boeing Company Wing lift/drag optimizing system
DE3527497A1 (de) * 1985-07-31 1987-02-12 Airbus Gmbh Tragfluegel mit ausfahrbarer klappe und veraenderbarer woelbung
DE4107556C1 (it) * 1991-03-08 1992-05-14 Deutsche Airbus Gmbh, 2000 Hamburg, De
US5150864A (en) * 1991-09-20 1992-09-29 Georgia Tech Research Corporation Variable camber control of airfoil
DE4243203A1 (de) * 1992-12-19 1994-06-23 Schempp Hirth Flugzeugbau Gmbh Tragflügel- oder Leitwerkprofil für Flugzeuge, insbesondere Segelflugzeuge
US5839700A (en) * 1996-06-03 1998-11-24 The United States Of America As Represented By The Secretary Of The Navy Articulated fin
DE19707392A1 (de) * 1997-02-25 1998-08-27 Deutsch Zentr Luft & Raumfahrt Aerodynamisches Bauteil, wie Landeklappe, Tragflügel, Höhen- oder Seitenleitwerk, mit veränderbarer Wölbung
US5839698A (en) * 1997-10-23 1998-11-24 Northrop Grumman Corporation Control surface continuous seal
US5887828A (en) * 1997-11-13 1999-03-30 Northrop Grumman Corporation Seamless mission adaptive control surface

Also Published As

Publication number Publication date
GB2331734A (en) 1999-06-02
GB2331734B (en) 2002-01-16
DE19732953C1 (de) 1999-03-11
FR2767111B1 (fr) 2003-05-16
ITMI981598A1 (it) 2000-01-13
FR2767111A1 (fr) 1999-02-12
US6076775A (en) 2000-06-20
GB9816546D0 (en) 1998-09-30

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