Torque tube and conical back plate for aircraft brake systems

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 25/42 (2006.01) F16D 55/00 (2006.01)

Patent

CA 2413973

A torque tube and conical back plate for aircraft brakes including a torque tube having a truncated back plate of thin metal construction extending from the outboard end thereof. The conical back plate is characterized by inner and outer reinforcing rings, such rings providing a compressive force at opposite ends of the truncated cone of the back plate, thus allowing the back plate to resist bending and deflection. In accordance with the invention, the cross sectional centers of mass of the inner and outer reinforcing rings are shifted outboard from a projection of the center plane of the conical back plate, such positioning enhancing the stiffening and reinforcing capabilities of the reinforcing rings.

Un tube de torsion et une plaque d'appui conique pour circuits de freinage d'avion comportant un tube de torsion ayant une plaque d'appui tronquée de construction métallique mince s'étendant de l'extrémité externe de celui-ci. La plaque d'appui conique est caractérisée par des anneaux de renfort intérieurs et extérieurs procurant une force de compression aux extrémités opposées du cône tronqué de la plaque d'appui, permettant ainsi à la plaque d'appui de résister à la flexion et à la réflexion. Conformément à l'invention, les sections transversales des centres de masse des anneaux de renfort intérieurs et extérieurs sont déplacées vers l'extérieur en étant projetées à partir du plan central de la plaque d'appui conique, une position qui rehausse les capacités de raidissement et de renfort des anneaux.

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