DE9113090U1 - Flügel oder flügelartiges Bauteil - Google Patents

Flügel oder flügelartiges Bauteil

Info

Publication number
DE9113090U1
DE9113090U1 DE9113090U DE9113090U DE9113090U1 DE 9113090 U1 DE9113090 U1 DE 9113090U1 DE 9113090 U DE9113090 U DE 9113090U DE 9113090 U DE9113090 U DE 9113090U DE 9113090 U1 DE9113090 U1 DE 9113090U1
Authority
DE
Germany
Prior art keywords
wing
edge
flap
gap
plate
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 - Lifetime
Application number
DE9113090U
Other languages
German (de)
English (en)
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to DE9113090U priority Critical patent/DE9113090U1/de
Publication of DE9113090U1 publication Critical patent/DE9113090U1/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
    • B23Q1/00—Members which are comprised in the general build-up of a form of machine, particularly relatively large fixed members
    • B23Q1/25—Movable or adjustable work or tool supports
    • B23Q1/26—Movable or adjustable work or tool supports characterised by constructional features relating to the co-operation of relatively movable members; Means for preventing relative movement of such members

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Toys (AREA)
DE9113090U 1991-10-21 1991-10-21 Flügel oder flügelartiges Bauteil Expired - Lifetime DE9113090U1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE9113090U DE9113090U1 (de) 1991-10-21 1991-10-21 Flügel oder flügelartiges Bauteil

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE9113090U DE9113090U1 (de) 1991-10-21 1991-10-21 Flügel oder flügelartiges Bauteil

Publications (1)

Publication Number Publication Date
DE9113090U1 true DE9113090U1 (de) 1992-01-16

Family

ID=6872468

Family Applications (1)

Application Number Title Priority Date Filing Date
DE9113090U Expired - Lifetime DE9113090U1 (de) 1991-10-21 1991-10-21 Flügel oder flügelartiges Bauteil

Country Status (1)

Country Link
DE (1) DE9113090U1 (zh)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1619117A1 (de) * 2004-07-23 2006-01-25 Airbus Deutschland GmbH Klappen-Kopplungssytem für Luftfahrzeuge
EP1695904A1 (en) * 2005-02-25 2006-08-30 Northrop Grumman Corporation Aircraft with articulated leading edge of fuselage and wings
DE102006036389A1 (de) * 2006-08-02 2008-02-14 Eads Deutschland Gmbh Spaltfreies aerodynamisches Profil, insbesondere Rotorblatt
WO2009136949A1 (en) * 2008-05-09 2009-11-12 The Boeing Company Aircraft fillet fairings with fixed and moveable portions, and associated systems and methods
EP2514668A1 (en) * 2011-04-18 2012-10-24 Claverham Limited Active gurney flap
US8695926B2 (en) 2011-04-18 2014-04-15 Claverham Ltd. Active gurney flap
US8757557B2 (en) 2011-04-18 2014-06-24 Claverham Ltd. Active gurney flap
DE102013012169A1 (de) 2013-07-20 2015-01-22 Airbus Defence and Space GmbH Formvariable Spaltabdeckung zwischen Steuerflächen und angrenzenden Struktur-Bauteilen an Flugzeugen

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT69568B (de) * 1913-04-01 1915-08-10 Luft Verkehrs Ges Ag Quersteuerklappe für Flugzeuge.
DE713600C (de) * 1939-04-25 1941-11-11 Theodor Schneider Ruder fuer Schiffe
US2526929A (en) * 1948-05-29 1950-10-24 Curtiss Wright Corp Airplane flap extension
US3670685A (en) * 1970-08-03 1972-06-20 Aldo Milessa Flexible rudder
GB1395549A (en) * 1971-08-05 1975-05-29 Stocznia Szczecinska Ships rudder device
US3977630A (en) * 1973-03-09 1976-08-31 The Boeing Company STOL aircraft
DE2804254A1 (de) * 1978-02-01 1979-08-02 Burkhart Dipl Ing Grob Tragfluegel mit klappe
DE3149629C1 (de) * 1981-12-15 1983-04-21 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Einrichtung zum Abdichten eines Luftspaltes an einer Flugzeugklappe

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT69568B (de) * 1913-04-01 1915-08-10 Luft Verkehrs Ges Ag Quersteuerklappe für Flugzeuge.
DE713600C (de) * 1939-04-25 1941-11-11 Theodor Schneider Ruder fuer Schiffe
US2526929A (en) * 1948-05-29 1950-10-24 Curtiss Wright Corp Airplane flap extension
US3670685A (en) * 1970-08-03 1972-06-20 Aldo Milessa Flexible rudder
GB1395549A (en) * 1971-08-05 1975-05-29 Stocznia Szczecinska Ships rudder device
US3977630A (en) * 1973-03-09 1976-08-31 The Boeing Company STOL aircraft
DE2804254A1 (de) * 1978-02-01 1979-08-02 Burkhart Dipl Ing Grob Tragfluegel mit klappe
DE3149629C1 (de) * 1981-12-15 1983-04-21 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Einrichtung zum Abdichten eines Luftspaltes an einer Flugzeugklappe

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
DE-Z: BRIX J.: Ein verbessertes und energie- sparendes Halbschweberuder. In: HANSA-Schiffahrt- Schiffbau-Hafen, 118.Jg., Nr.18, 1981, S.1314-15 *
GB-Z: MILNE, Peter: Rudders and rudder/skeg, com- binations have a direct effect upon handling. Aeration and vortices cause drag and reduce per- formance. Here are some improvements. In: YachtingWorld, March 1984, S.100 *

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1619117A1 (de) * 2004-07-23 2006-01-25 Airbus Deutschland GmbH Klappen-Kopplungssytem für Luftfahrzeuge
EP1695904A1 (en) * 2005-02-25 2006-08-30 Northrop Grumman Corporation Aircraft with articulated leading edge of fuselage and wings
US7204454B2 (en) 2005-02-25 2007-04-17 Northrop Grumman Corporation Aircraft with articulated leading edge of fuselage and wings
DE102006036389A1 (de) * 2006-08-02 2008-02-14 Eads Deutschland Gmbh Spaltfreies aerodynamisches Profil, insbesondere Rotorblatt
DE102006036389B4 (de) * 2006-08-02 2013-08-08 Eads Deutschland Gmbh Spaltfreies aerodynamisches Profil, insbesondere Rotorblatt
WO2009136949A1 (en) * 2008-05-09 2009-11-12 The Boeing Company Aircraft fillet fairings with fixed and moveable portions, and associated systems and methods
CN102745327A (zh) * 2011-04-18 2012-10-24 克拉弗哈姆有限公司 有源格尼襟翼
EP2514668A1 (en) * 2011-04-18 2012-10-24 Claverham Limited Active gurney flap
US8616504B2 (en) 2011-04-18 2013-12-31 Claverham Ltd. Active gurney flap
US8695926B2 (en) 2011-04-18 2014-04-15 Claverham Ltd. Active gurney flap
US8757557B2 (en) 2011-04-18 2014-06-24 Claverham Ltd. Active gurney flap
CN102745327B (zh) * 2011-04-18 2015-01-14 克拉弗哈姆有限公司 有源格尼襟翼
DE102013012169A1 (de) 2013-07-20 2015-01-22 Airbus Defence and Space GmbH Formvariable Spaltabdeckung zwischen Steuerflächen und angrenzenden Struktur-Bauteilen an Flugzeugen
WO2015010676A1 (de) 2013-07-20 2015-01-29 Airbus Defence and Space GmbH Formvariable spaltabdeckung zwischen steuerflächen und angrenzenden struktur-bauteilen an flugzeugen
US10150557B2 (en) 2013-07-20 2018-12-11 Airbus Defence and Space GmbH Shape-variable gap covering between control surfaces and adjacent structural components on aircrafts

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