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)
  • Transmission Devices (AREA)
  • Body Structure For Vehicles (AREA)
  • Bridges Or Land Bridges (AREA)
  • Toys (AREA)
GB2778769A 1969-06-02 1969-06-02 Expired GB1296994A (enExample)

Applications Claiming Priority (1)

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

Publications (1)

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

Family

ID=10265314

Family Applications (1)

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

Country Status (6)

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

Cited By (8)

* 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
CN113874284A (zh) * 2019-02-01 2021-12-31 G·科隆比耶斯 具有被动适应性轮廓的承载结构
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 (8)

* 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
DE102019133497B4 (de) * 2019-12-09 2025-11-20 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Luftleitvorrichtung für eine Kraftfahrzeugkarosserie

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 (11)

* 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
CN113874284A (zh) * 2019-02-01 2021-12-31 G·科隆比耶斯 具有被动适应性轮廓的承载结构
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
DE2026054B2 (de) 1980-11-06
FR2045801B1 (enExample) 1974-07-12
JPS5431279B1 (enExample) 1979-10-05
NL7007986A (enExample) 1970-12-04
SE365474B (enExample) 1974-03-25
DE2026054A1 (enExample) 1970-12-10
NL169849C (nl) 1982-09-01
FR2045801A1 (enExample) 1971-03-05
DE2026054C3 (de) 1981-08-13
NL169849B (nl) 1982-04-01

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Legal Events

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