GB1296994A - - Google Patents

Info

Publication number
GB1296994A
GB1296994A GB2778769A GB1296994DA GB1296994A GB 1296994 A GB1296994 A GB 1296994A GB 2778769 A GB2778769 A GB 2778769A GB 1296994D A GB1296994D A GB 1296994DA GB 1296994 A GB1296994 A GB 1296994A
Authority
GB
United Kingdom
Prior art keywords
jack
skin
frame
leading edge
supported
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
Application number
GB2778769A
Other languages
English (en)
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 filed Critical
Publication of GB1296994A publication Critical patent/GB1296994A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/42—Adjusting about chordwise axes
    • 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
    • B64C3/48—Varying camber by relatively-movable parts of wing structures
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/52—Warping

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Body Structure For Vehicles (AREA)
  • Bridges Or Land Bridges (AREA)
  • Toys (AREA)
  • Transmission Devices (AREA)
GB2778769A 1969-06-02 1969-06-02 Expired GB1296994A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2778769 1969-06-02

Publications (1)

Publication Number Publication Date
GB1296994A true GB1296994A (de) 1972-11-22

Family

ID=10265314

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2778769A Expired GB1296994A (de) 1969-06-02 1969-06-02

Country Status (6)

Country Link
JP (1) JPS5431279B1 (de)
DE (1) DE2026054C3 (de)
FR (1) FR2045801B1 (de)
GB (1) GB1296994A (de)
NL (1) NL169849C (de)
SE (1) SE365474B (de)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000017046A1 (en) * 1998-09-24 2000-03-30 Raimo Hirvinen Profile and process for changing the maximum angle of attack of aprofile
US6070834A (en) * 1996-12-21 2000-06-06 Daimlerchrysler Ag Aerodynamic body with internal actuating drives
GB2450236A (en) * 2007-06-11 2008-12-17 Boeing Co Aircraft tail having leading edge slat
WO2011011161A1 (en) * 2009-07-21 2011-01-27 The Boeing Company Shape-changing control surface
DE102010024121B4 (de) * 2010-06-17 2017-04-06 Airbus Defence and Space GmbH Stellantriebseinheit
US10654557B2 (en) 2014-09-25 2020-05-19 Bombardier Inc. Morphing skin for an aircraft
US11459083B2 (en) 2019-07-03 2022-10-04 National Research Council Of Canada Deforming foil structure for bridging curved fluid-dynamic surface

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3816431A1 (de) * 1988-05-13 1989-11-16 Otilio Nemec Zwischenstufige kruemmungsvorrichtung fuer aerodynamische steuerflaechen
DE19643222C2 (de) * 1996-10-19 1998-12-10 Daimler Benz Ag Auftriebskörper mit veränderbarer Wölbung
DE19852944C1 (de) 1998-11-17 2000-02-10 Daimler Chrysler Ag Adaptiver Strömungskörper
DE19858872C2 (de) 1998-12-19 2001-02-08 Daimler Chrysler Ag Adaptiver Flugzeugtragflügel
AT408216B (de) 1999-05-04 2001-09-25 Ofner Anton Gerald Dr Flugzeugtragflügel
EP2883787B1 (de) * 2013-12-12 2019-06-12 Airbus Defence and Space GmbH Antriebsmechanismus für eine verformbare Tragflächenvorderkante
WO2021037976A1 (en) 2019-08-30 2021-03-04 Airbus Operations Gmbh Flow body for an aircraft having an integrated de-icing system

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE445182C (de) * 1927-06-04 Hanns Freiherr Schertel Von Bu Tragflaeche, deren Prolfil waehrend des Flugs veraenderbar ist
GB110031A (en) * 1916-10-10 1917-10-10 Patent Corp Ltd Improvements in Flying Machines.
FR574803A (fr) * 1922-12-30 1924-07-19 Perfectionnements apportés à des ailes fluido-dynamiques, variables, telles que les ailes pour aéroplanes
FR922899A (fr) * 1946-01-14 1947-06-20 Dispositif pour la variation de courbure des surfaces portantes, empennages et surfaces auxiliaires des appareils de locomotion aérienne
US2650047A (en) * 1949-01-22 1953-08-25 Douglas Aircraft Co Inc Variable camber wing
US3076623A (en) * 1960-10-19 1963-02-05 Donald G Lyon Variable shaped airfoil
US3179357A (en) * 1962-02-27 1965-04-20 Donald G Lyon Variable shaped airfoil

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6070834A (en) * 1996-12-21 2000-06-06 Daimlerchrysler Ag Aerodynamic body with internal actuating drives
WO2000017046A1 (en) * 1998-09-24 2000-03-30 Raimo Hirvinen Profile and process for changing the maximum angle of attack of aprofile
GB2450236A (en) * 2007-06-11 2008-12-17 Boeing Co Aircraft tail having leading edge slat
GB2450236B (en) * 2007-06-11 2009-05-20 Boeing Co Symmetric leading edge device and method to delay flow separation
US7913949B2 (en) 2007-06-11 2011-03-29 The Boeing Company Symmetric leading edge device and method to delay flow separation
WO2011011161A1 (en) * 2009-07-21 2011-01-27 The Boeing Company Shape-changing control surface
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
DE102010024121B4 (de) * 2010-06-17 2017-04-06 Airbus Defence and Space GmbH Stellantriebseinheit
US10654557B2 (en) 2014-09-25 2020-05-19 Bombardier Inc. Morphing skin for an aircraft
US11459083B2 (en) 2019-07-03 2022-10-04 National Research Council Of Canada Deforming foil structure for bridging curved fluid-dynamic surface

Also Published As

Publication number Publication date
FR2045801B1 (de) 1974-07-12
DE2026054C3 (de) 1981-08-13
JPS5431279B1 (de) 1979-10-05
FR2045801A1 (de) 1971-03-05
NL169849C (nl) 1982-09-01
DE2026054B2 (de) 1980-11-06
NL169849B (nl) 1982-04-01
NL7007986A (de) 1970-12-04
DE2026054A1 (de) 1970-12-10
SE365474B (de) 1974-03-25

Similar Documents

Publication Publication Date Title
GB1296994A (de)
GB1424246A (en) Protective shield
IT7826729A0 (it) Dispositivo di carenatura atto alla riduzione della resistenza aerodinamica in veicoli articolati o simili.
SE7701405L (sv) Anordning vid utfellbart fenblad pa granat eller motsvarande
ES441491A1 (es) Una pala de helice, particularmente para embarcaciones.
SE8007615L (sv) Lagring for en rotor
US3147938A (en) Aircraft wing structure having variable angle of incidence
Paterson et al. A survey of drag prediction techniques applicable to subsonic and transonic aircraft design
IT1077273B (it) Dispositivo di carenatura per ridurre la resistenza aerodinamica in veicoli articolati o simili
Vorotyntsev et al. Determination of the moments of aerodynamic forces acting on three-dimensional bodies that move under the'law of locality'
GB1504995A (en) Waterfoil and boats incorporating same
CARTER Interference effects of model support systems(Analysis of interference occurring in subsonic and transonic wind tunnels caused by model support system)
IT7921057A0 (it) Timone per la generazione aerodinamica di momenti su aeroplani.
ES242723U (es) Un deflector aerodinamico para reducir la resistencia aeori-namica de un vehiculo.
BR7705315A (pt) Turbina hidraulica de eixo vertical com roda livre de turbina,volante,gerador e bomba de oleo para o ajuste do rendimento
CH562374A5 (en) Double blade snow plough - each blade pivoted into required position by piston at rear
Gladwell Some reinterpretations of structural analysis
KLEVENHUSEN et al. Contribution to the study of supercritical profile flow
FR2274492A1 (fr) Support passe-partout
ES162168U (es) Dispositivo para aumentar la presión de trabajo del limpiaparabrisas para vehículos
Park Calculation of aerodynamic derivatives in unsteady two-dimensional transonic flow using Dowell's linearization method
PARKINSON et al. Prediction of aerodynamic effects of spoilers on wings(considering effects of base venting)
FR2337646A1 (fr) Balai d'essui-glace pour vehicules
TRIEBSTEIN Investigation of unsteady interference effects on oscillating lifting surface and bodies in incompressible flow
DOWELL et al. Flutter computer program and lifting surface theory with boundary layer[Semiannual Progress Report, 1 Apr.- 1 Oct. 1973]

Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee