B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 25/10 (2006.01) B64C 25/04 (2006.01)
Patent
CA 2431093
Device for assembly of landing gear on an aircraft structure. The device comprises two segments (14a, 14b) of the shaft aligned along the same center line and fixed to a fitting of the landing gear, two support devices (10a, 10b) fixed to the aircraft structure, two ball joint balls (12a, 12b) installed between the corresponding shaft segments and the support devices and a tension bar (24) connecting the two support devices. One (l0a) of the two support devices, preferably turned towards the outside of the aircraft, is deformable by bending or articulation. Advantageously, the tension bar bears on the bearing balls (20a, 20b) and the guide rings are placed between the bar and the shaft segments, to prevent vibrations.
Dispositif qui permet de fixer un train d'atterrissage à la structure d'un avion. Ce dispositif est composé de ce qui suit : deux segments (14a, 14b) d'arbres alignés sur le même axe et fixés à un raccord sur le train d'atterrissage; deux dispositifs de support (10a, 10b), fixés à la structure de l'avion; deux rotules de joint à rotule (12a, 12b), posées entre les segments d'arbres correspondants et les dispositifs de support; une barre de tension (24), raccordée aux deux dispositifs de soutien. Un (l0a) des deux dispositifs de support, préférablement orienté vers l'extérieur de l'avion, est déformable par flexion ou articulation. La barre de tension s'appuie sur les billes de roulement (20a, 20b) et les anneaux de guidage sont placés entre la barre et les segments d'arbres, afin d'empêcher les vibrations.
Airbus France
Airbus Operations Sas
Goudreau Gage Dubuc
LandOfFree
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