B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 25/20 (2006.01) B64C 25/12 (2006.01)
Patent
CA 2384131
An aircraft, aircraft fuselage, aircraft wing and aircraft landing gear are provided. The landing gear (10) comprises a wheeled leg (12) and a series of mounting members (14, 15, 16, 17) to attach the leg to an airframe of the aircraft via respective attachments (14a, 15a, 18, 19). The leg is pivotably movable between a first stowed position within the aircraft and a second deployed position for movement of the aircraft along the ground, and at least one of the attachments (18) is configured to allow retraction movement of the leg to occur about an angularly variable pivot axis and thus avoid obstacles that would be encountered in a conventional retraction path, and also to alleviate forces in the gear that can be caused by four point location of the gear leg.
Cette invention concerne un aéronef, un fuselage, une aile et un train d atterrissage. Le train d'atterrissage (10) comprend un fût avec roues (12) et une série d'éléments de montage (14, 15, 16, 17) assurant la fixation du fût sur la cellule au moyen de liaisons diverses (14a, 15a, 18, 19). Le fût est monté pivotant entre une première positions rentrée dans l'appareil et une seconde position déployée pour le déplacement au sol de l'aéronef, au moins une des liaisons (18) étant conçue pour permettre un mouvement de rappel du fût selon un axe de pivotement angulairement variable, ce qui permet d'éviter les obstacles normalement rencontrés sur un chemin de rappel classique et d'atténuer en outre les forces dans le train d'atterrissage qui peuvent être engendrées par la configuration quatre points dudit train.
Airbus Operations Limited
Airbus Uk Limited
Fetherstonhaugh & Co.
LandOfFree
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