FR1531596A - Dispositif de liaison entre le fuselage et les ailes mobiles d'un avion à géométrie variable - Google Patents

Dispositif de liaison entre le fuselage et les ailes mobiles d'un avion à géométrie variable

Info

Publication number
FR1531596A
FR1531596A FR107508A FR107508A FR1531596A FR 1531596 A FR1531596 A FR 1531596A FR 107508 A FR107508 A FR 107508A FR 107508 A FR107508 A FR 107508A FR 1531596 A FR1531596 A FR 1531596A
Authority
FR
France
Prior art keywords
airplane
fuselage
geometry
variable
connection device
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
FR107508A
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.)
Dassault Aviation SA
Original Assignee
Avions Marcel Dassault Breguet Aviation SA
Dassault Aviation SA
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 Avions Marcel Dassault Breguet Aviation SA, Dassault Aviation SA filed Critical Avions Marcel Dassault Breguet Aviation SA
Priority to FR107508A priority Critical patent/FR1531596A/fr
Priority to GB5159467A priority patent/GB1209189A/en
Priority to DE1967A0057767 priority patent/DE1531384C3/de
Application granted granted Critical
Publication of FR1531596A publication Critical patent/FR1531596A/fr
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
    • B64C3/40—Varying angle of sweep

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Tires In General (AREA)
  • Transmission Devices (AREA)
FR107508A 1967-05-23 1967-05-23 Dispositif de liaison entre le fuselage et les ailes mobiles d'un avion à géométrie variable Expired FR1531596A (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR107508A FR1531596A (fr) 1967-05-23 1967-05-23 Dispositif de liaison entre le fuselage et les ailes mobiles d'un avion à géométrie variable
GB5159467A GB1209189A (en) 1967-05-23 1967-11-13 A device for pivotally connecting the variable sweep wings of a variable geometry aircraft to the aircraft fuselage
DE1967A0057767 DE1531384C3 (de) 1967-05-23 1967-12-21 Gelenkverbindung zwischen dem Rumpf und den Tragflügeln eines Flugzeuges

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR107508A FR1531596A (fr) 1967-05-23 1967-05-23 Dispositif de liaison entre le fuselage et les ailes mobiles d'un avion à géométrie variable

Publications (1)

Publication Number Publication Date
FR1531596A true FR1531596A (fr) 1968-07-05

Family

ID=8631405

Family Applications (1)

Application Number Title Priority Date Filing Date
FR107508A Expired FR1531596A (fr) 1967-05-23 1967-05-23 Dispositif de liaison entre le fuselage et les ailes mobiles d'un avion à géométrie variable

Country Status (3)

Country Link
DE (1) DE1531384C3 (fr)
FR (1) FR1531596A (fr)
GB (1) GB1209189A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4212441A (en) * 1978-05-11 1980-07-15 The United States Of America As Represented By The Secretary Of The Air Force Wing pivot assembly for variable sweep wing aircraft
FR2463052A1 (fr) * 1979-08-11 1981-02-20 Messerschmitt Boelkow Blohm Dispositif de raccordement principal pour les ailes d'aeronefs

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2812936A1 (fr) * 1986-08-12 2002-02-15 Aerospatiale Missile a voilure variable
US8708286B2 (en) * 2012-06-21 2014-04-29 The Boeing Company Swing tip assembly rotation joint
US9296471B2 (en) * 2013-10-06 2016-03-29 The Boeing Company Swing wing tip system, assembly and method with dual load path structure
GB2560900A (en) * 2017-03-27 2018-10-03 Airbus Operations Ltd Foldable aerodynamic structure with slewing bearing

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1388089A (fr) * 1963-12-27 1965-02-05 Aviation Louis Breguet Sa Avion à configuration variable
GB1026093A (en) * 1964-03-24 1966-04-14 British Aircraft Corp Ltd Improvements in aeroplanes
US3279721A (en) * 1964-10-30 1966-10-18 Boeing Co Bearing arrangement for variable sweep wing aircraft
GB1183921A (en) * 1967-01-06 1970-03-11 British Aircraft Corp Ltd Improvements relating to Wing Pivots for Aircraft having Variable Sweep-back Wings

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4212441A (en) * 1978-05-11 1980-07-15 The United States Of America As Represented By The Secretary Of The Air Force Wing pivot assembly for variable sweep wing aircraft
FR2463052A1 (fr) * 1979-08-11 1981-02-20 Messerschmitt Boelkow Blohm Dispositif de raccordement principal pour les ailes d'aeronefs

Also Published As

Publication number Publication date
DE1531384B2 (de) 1978-03-16
GB1209189A (en) 1970-10-21
DE1531384C3 (de) 1981-05-07
DE1531384A1 (de) 1970-03-05

Similar Documents

Publication Publication Date Title
FR2302911A1 (fr) Avion a decollage et atterrissage verticaux
FR2033384A1 (fr) Avion a decollage et atterrissage court et vertical
NL187005B (nl) Vliegtuigvleugel met ten minste een beweegbaar aangebrachte neusklep.
FR2302912A1 (fr) Avion a fuselage et ailes en delta
IT1088681B (it) Dispositivo di comando per superfici di controllo di portanza su tutte le ali di aeromobile
FR1492163A (fr) Dispositif de guidage et d'arrimage dans l'avion des plates-formes de parachutage
FR1531596A (fr) Dispositif de liaison entre le fuselage et les ailes mobiles d'un avion à géométrie variable
FR1460813A (fr) Avion à géométrie variable comportant deux axes d'articulation des ailes sur le fuselage
BE759331A (fr) Dispositif antidetournement d'avion
FR1515159A (fr) Dispositif d'obturateur mobile entre voilure et structure fixe pour avions ou aérodynes à géométrie variable
FR2115468A2 (fr) Mécanisme de sortie et de rentrée de volet d'aile d'avion
FR2305342A1 (fr) Mecanisme de montage et de manoeuvre des volets de bord de fuite des ailes d'un avion
FR1347243A (fr) Installation d'auto-pilotage pour avion à décollage vertical et avion ou analogue pourvu de ladite installation
FR1473951A (fr) Avion à géométrie variable et son train d'atterrissage
FR1497434A (fr) Dispositif de volet pour aile d'avion
FR1469367A (fr) Avion à volets d'atterrissage et à ailerons montés sur les surfaces portantes
FR1281653A (fr) Avion à décollage et atterrissage verticaux
FR1210930A (fr) Aile d'avion
FR1317103A (fr) Perfectionnements aux ailes d'avion
FR1485635A (fr) Fuselage d'avion équipé d'ailes pliantes pour le vol plané
Dee et al. Flight determination of wing flow patterns and buffet boundaries for the Fairey Delta 2 aircraft at Mach numbers between 0. 4 and 1. 3, and comparison with wind tunnel results(Flight and wind tunnel tests compared to visualize wing flow patterns for Fairey Delta 2 aircraft between Mach numbers 0. 4 and 1. 3)
FR1372548A (fr) Aile d'avion supersonique
FR1258619A (fr) Aile d'avion
FR1299154A (fr) Avion à décollage et atterrissage sur un coussin d'air
FR1458854A (fr) Avions équipés de moteurs, notamment pour le décollage et l'atterrissage vertical, à collecteurs d'air externes