FR2045801A1 - - Google Patents

Info

Publication number
FR2045801A1
FR2045801A1 FR7020232A FR7020232A FR2045801A1 FR 2045801 A1 FR2045801 A1 FR 2045801A1 FR 7020232 A FR7020232 A FR 7020232A FR 7020232 A FR7020232 A FR 7020232A FR 2045801 A1 FR2045801 A1 FR 2045801A1
Authority
FR
France
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.)
Granted
Application number
FR7020232A
Other languages
French (fr)
Other versions
FR2045801B1 (enrdf_load_stackoverflow
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.)
MINI TECHNO BRITA NI
Original Assignee
MINI TECHNO BRITA NI
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 MINI TECHNO BRITA NI filed Critical MINI TECHNO BRITA NI
Publication of FR2045801A1 publication Critical patent/FR2045801A1/fr
Application granted granted Critical
Publication of FR2045801B1 publication Critical patent/FR2045801B1/fr
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/42Adjusting about chordwise axes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/44Varying camber
    • B64C3/48Varying camber by relatively-movable parts of wing structures
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/52Warping

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)
FR707020232A 1969-06-02 1970-06-02 Expired FR2045801B1 (enrdf_load_stackoverflow)

Applications Claiming Priority (1)

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

Publications (2)

Publication Number Publication Date
FR2045801A1 true FR2045801A1 (enrdf_load_stackoverflow) 1971-03-05
FR2045801B1 FR2045801B1 (enrdf_load_stackoverflow) 1974-07-12

Family

ID=10265314

Family Applications (1)

Application Number Title Priority Date Filing Date
FR707020232A Expired FR2045801B1 (enrdf_load_stackoverflow) 1969-06-02 1970-06-02

Country Status (6)

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

Families Citing this family (15)

* 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
DE19653851C2 (de) * 1996-12-21 1999-09-02 Daimler Chrysler Ag Aerodynamischer Körper mit innenliegenden Stellantrieben
FI112637B (fi) * 1998-09-24 2003-12-31 Raimo Hirvinen Geometrialtaan muuttuva profiili
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
US7913949B2 (en) 2007-06-11 2011-03-29 The Boeing Company Symmetric leading edge device and method to delay flow separation
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
EP2883787B1 (de) 2013-12-12 2019-06-12 Airbus Defence and Space GmbH Antriebsmechanismus für eine verformbare Tragflächenvorderkante
CN106715263B (zh) 2014-09-25 2019-07-05 庞巴迪公司 用于飞机的变形蒙皮
FR3092314B1 (fr) * 2019-02-01 2022-03-04 Airbus Operations Sas Structure portante à profil adaptable de manière passive
CA3048431A1 (en) 2019-07-03 2021-01-03 Jaye Mangione Deforming foil structure for bridging curved fluid-dynamic surface
WO2021037976A1 (en) 2019-08-30 2021-03-04 Airbus Operations Gmbh Flow body for an aircraft having an integrated de-icing system

Citations (4)

* 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
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

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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

Patent Citations (4)

* 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
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

Also Published As

Publication number Publication date
NL169849C (nl) 1982-09-01
SE365474B (enrdf_load_stackoverflow) 1974-03-25
JPS5431279B1 (enrdf_load_stackoverflow) 1979-10-05
GB1296994A (enrdf_load_stackoverflow) 1972-11-22
FR2045801B1 (enrdf_load_stackoverflow) 1974-07-12
DE2026054B2 (de) 1980-11-06
NL169849B (nl) 1982-04-01
DE2026054C3 (de) 1981-08-13
NL7007986A (enrdf_load_stackoverflow) 1970-12-04
DE2026054A1 (enrdf_load_stackoverflow) 1970-12-10

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Legal Events

Date Code Title Description
ST Notification of lapse