FR2379430A2 - Aile a profil variable notamment pour aerodyne - Google Patents

Aile a profil variable notamment pour aerodyne

Info

Publication number
FR2379430A2
FR2379430A2 FR7703283A FR7703283A FR2379430A2 FR 2379430 A2 FR2379430 A2 FR 2379430A2 FR 7703283 A FR7703283 A FR 7703283A FR 7703283 A FR7703283 A FR 7703283A FR 2379430 A2 FR2379430 A2 FR 2379430A2
Authority
FR
France
Prior art keywords
bellows
profile
during flight
aircraft
wing
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.)
Pending
Application number
FR7703283A
Other languages
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 FR7703283A priority Critical patent/FR2379430A2/fr
Publication of FR2379430A2 publication Critical patent/FR2379430A2/fr
Pending 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
    • B64C3/44—Varying camber
    • B64C3/48—Varying camber by relatively-movable parts of wing structures

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tires In General (AREA)

Abstract

L'invention concerne une aile d'aéronef de forme et d'épaisseur variables. Les déformations de cette aile sont obtenues par le transfert d'une partie de carburant embarqué à bord dans une pluralité de cavités déformables séparées qui agissent sur la partie déformable de l'aile et dont les déformations s'effectuent principalement dans une direction privilégiée, de préférence normalement à la partie déformable de l'aile L'invention s'applique à l'aéronautique
FR7703283A 1977-02-04 1977-02-04 Aile a profil variable notamment pour aerodyne Pending FR2379430A2 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7703283A FR2379430A2 (fr) 1977-02-04 1977-02-04 Aile a profil variable notamment pour aerodyne

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7703283A FR2379430A2 (fr) 1977-02-04 1977-02-04 Aile a profil variable notamment pour aerodyne

Publications (1)

Publication Number Publication Date
FR2379430A2 true FR2379430A2 (fr) 1978-09-01

Family

ID=9186349

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7703283A Pending FR2379430A2 (fr) 1977-02-04 1977-02-04 Aile a profil variable notamment pour aerodyne

Country Status (1)

Country Link
FR (1) FR2379430A2 (fr)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3162701A1 (fr) * 2015-10-30 2017-05-03 BAE Systems PLC Aéronef ainsi que procédé et appareil de commande de celui-ci
WO2017072520A1 (fr) * 2015-10-30 2017-05-04 Bae Systems Plc Aéronef et procédé et appareil pour le commander
US10807708B2 (en) 2015-10-30 2020-10-20 Bae Systems Plc Air vehicle and imaging apparatus therefor
US10814972B2 (en) 2015-10-30 2020-10-27 Bae Systems Plc Air vehicle and method and apparatus for control thereof
US10822084B2 (en) 2015-10-30 2020-11-03 Bae Systems Plc Payload launch apparatus and method
US11077943B2 (en) 2015-10-30 2021-08-03 Bae Systems Plc Rotary-wing air vehicle and method and apparatus for launch and recovery thereof

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3162701A1 (fr) * 2015-10-30 2017-05-03 BAE Systems PLC Aéronef ainsi que procédé et appareil de commande de celui-ci
WO2017072520A1 (fr) * 2015-10-30 2017-05-04 Bae Systems Plc Aéronef et procédé et appareil pour le commander
US10807708B2 (en) 2015-10-30 2020-10-20 Bae Systems Plc Air vehicle and imaging apparatus therefor
US10814972B2 (en) 2015-10-30 2020-10-27 Bae Systems Plc Air vehicle and method and apparatus for control thereof
US10822084B2 (en) 2015-10-30 2020-11-03 Bae Systems Plc Payload launch apparatus and method
US11059562B2 (en) 2015-10-30 2021-07-13 Bae Systems Plc Air vehicle and method and apparatus for control thereof
US11077943B2 (en) 2015-10-30 2021-08-03 Bae Systems Plc Rotary-wing air vehicle and method and apparatus for launch and recovery thereof

Similar Documents

Publication Publication Date Title
GB1536331A (en) Aerofoils
JPS5375700A (en) Trianglar wing type aeroplane
FR2246444A1 (en) Aircraft with slow landing speed - wing section is variable between thin and thick in flight
FR2379430A2 (fr) Aile a profil variable notamment pour aerodyne
IL55886A (en) Aircraft controlsystem component with improved ballistic tolerance
GB1357058A (en) Aircraft particularly silplanes and kites
FR2374208A1 (fr) Aile a profil variable, notamment pour aerodyne
GB820009A (en) Improvements in or relating to aircraft capable of flight at supersonic speeds
JPS5338096A (en) Method of rebuilding ship into multiideck ship
FR2309400A1 (fr) Structures demontables d'ailes et de stabilisateurs
IL58240A0 (en) Adjustable aircraft wing with relatively movable parts
RU93032633A (ru) Летательный аппарат
SU797185A1 (ru) Самолет о.а.артемова
ES203341U (es) Avion planeador de juguete.
JPS6474200A (en) Simple flight device
FR2397978A1 (fr) Avion convertible
Pollock A proposal for aerodynamically actuated self streamlining subsonic wind tunnel walls
USD139860S (en) Maycen airplane
TRIEBSTEIN et al. Pressure measurements on harmonically oscillating wing tailplane configurations(Pressure measurements on harmonically oscillating wing-tail configurations in incompressible speed range)
LONG An improved method for calculating generalised airforces on oscillating wings in subsonic flow(Calculation of aerodynamic forces on thin wing oscillating harmonically in subsonic flow using collocation method)
GB612666A (en) Improvements in or relating to aircraft
SCHMIDTLEIN Evaluation of in-flight simulation using a helicopter of variable stability and control with regard to its use as an auxiliary in aircraft development(Evaluation of in-flight simulation of flying platform using helicopter with variable stability and maneuverability)
GB885273A (en) Improvements relating to ornithopters
SU582629A2 (ru) Механизм отклонения аэродинамической поверхности крыла летательного аппарата
LAURENT The American fighter Northrup F-20 Tigershark