Abstract:
The damping device (10) according to the invention is designed to damp a shock in a longitudinal direction (X). It includes a central pad (12), designed to be secured with a first member (14A) of the coupling device (14), and two side wings (18), each formed by a thin plate extending in the longitudinal direction (X). Each side wing (18) includes at least one first longitudinal region (20), secured to the central pad (12), at least one second longitudinal region (22), designed to be secured with a railroad vehicle, and at least one line of least resistance (24), separating the first (20) and second (22) longitudinal regions from each other, extending over the side wing (18) in the longitudinal direction (X).
Abstract:
A device for fastening a table top to a side wall of a vehicle includes: a structure for fastening to the side wall, and a support structure of the plate. The support structure includes: at least one crosspiece extending along a transverse direction, and at least two beams each extending in a longitudinal direction substantially orthogonal to the transverse direction, with the crosspiece being connected to each of the beams. The support structure includes bending onset zones configured to deform plastically when a force greater than or equal to a predetermined threshold force is applied on the support structure along the transverse direction.
Abstract:
The damping device (10) according to the invention is designed to damp a shock in a longitudinal direction (X). It includes a central pad (12), designed to be secured with a first member (14A) of the coupling device (14), and two side wings (18), each formed by a thin plate extending in the longitudinal direction (X). Each side wing (18) includes at least one first longitudinal region (20), secured to the central pad (12), at least one second longitudinal region (22), designed to be secured with a railroad vehicle, and at least one line of least resistance (24), separating the first (20) and second (22) longitudinal regions from each other, extending over the side wing (18) in the longitudinal direction (X).