To increase a compactness of damping systems intended to operate in the event of a dynamic landing of an aircraft, a damping system comprises a primary damper device and a secondary damper device. The primary damper device comprises at least one beam, each beam extending along a direction of a longitudinal axis. The damping system is configured so that at rest, the primary damper device has a stiffness greater than a stiffness of the secondary damper device in the direction of the longitudinal axis. When a force is applied to the damping system along the direction of the longitudinal axis, with a value less than a limit value, each beam remains in a compression state. When the force applied has a value greater than or equal to the limit value, each beam undergoes buckling and the secondary damper device undergoes elastic deformation.

A steering column assembly includes a lower jacket assembly extending along a steering column axis. Also included is an upper jacket assembly at least partially received within the lower jacket assembly, the upper jacket assembly translatable along the steering column axis relative to the lower jacket assembly. Further included is an energy absorption strap operatively coupled to the upper jacket, the energy absorption strap having an aperture defined therein. Yet further included is a rake bolt extending through the lower jacket and through the aperture of the energy absorption strap.

A rotational energy absorber typically for use in a fall arrest system has a coiler, a length of plastically deformable strip and a deformer structure. The plastically deformable strip has a first end attached to the coiler and a second free end and extends past the deformer structure at a position between the first and second ends. Relative rotation of the coiler member and deformer structure causes the strip to be drawn past the deformer structure, plastically deforming the strip and winding the strip coil form about the coiler member.

A damper includes an upper connector configured to be connected to a cable. The damper also includes a lower connector configured to be connected to a load. The damper also includes a body extending between and connecting together the upper and lower connectors. The body includes a first portion and a second portion. The first portion is configured to experience greater plastic strain than the second portion.

An impact energy absorbing apparatus includes: a base, an axial crush component, a top plate, and an energy transfer component. The base is fastened to a protected object, and a tapered hole is provided on a top surface of the base. A bottom end face of the metal hollow rod of the axial crush component is joined with the top surface of the base. The energy transfer component includes a force bearing plate and a guiding rod extending outwards, where the force bearing plate is superimposed on a top surface of the metal hollow rod, the guiding rod is inserted to a position corresponding to the tapered hole in the metal hollow rod, an outer diameter of the guiding rod is less than a greatest diameter of the tapered hole, an inner diameter of the guiding rod is greater than a smallest diameter of the tapered hole.

A metal pipe has a circular cross section with an outer diameter D and a length not less than 6D. The metal pipe includes a high-strength portion (1A) and low-strength portions (1B). The high-strength portion (1A) is disposed along the entire circumference of the metal pipe to extend a dimension, as measured in the longitudinal direction of the metal pipe, that is not less than (2/3)D and not more than 3D of the metal pipe. The high-strength portion (1A) has a yield strength not less than 500 MPa (or a tensile strength not less than 980 MPa). The low-strength portions (1B) are disposed along the entire circumference of the metal pipe to be arranged in the longitudinal direction of the metal pipe to sandwich the high-strength portion (1A). The low-strength portions (1B) have a yield strength of 60 to 85% of that of the high-strength portion (1A).

A buckling control assembly for a steering column energy absorption strap assembly is provided. The buckling control assembly includes an inner energy absorption strap operatively coupled to a steering column jacket. Also included is an outer energy absorption strap surrounding at least a portion of the inner energy absorption strap and operatively coupled to the steering column jacket. Further included is a strap constraining structure disposed on a constraint side of the outer energy absorption strap to inhibit buckling of the outer energy absorption strap in a first direction, the outer energy absorption strap having a free side unconstrained to accommodate buckling of the outer energy absorption strap.

An energy absorption strap assembly for a steering column includes a first strap. Also included is a second strap, the first and second strap having respective edge regions that are laterally engageable with each to switch the energy absorption strap assembly between a high load condition and a low load condition.

An energy absorption strap assembly for a steering column is provided. The assembly includes an upper jacket. The assembly also includes a first energy absorption strap extending from a first end to a second end, the first energy absorption strap operatively coupled to the upper jacket proximate the second end of the first energy absorption strap. The assembly further includes a second energy absorption strap surrounding a portion of the first energy absorptions strap, the second energy absorption strap not directly coupled to the upper jacket.

An impact mitigating assembly includes an elongate member formed from a plurality of triangulated cylindrical origami (TCO) unit cells that exhibit coupled rotational and axial motion. The unit cells include an end portion and a tubular member fixed to the end portion. The tubular member has a plurality of concave sides. Each side has a first triangular portion and a second triangular portion sharing an elastic connecting edge with the second triangular portion. The first triangular portion also shares an angled upright edge with the second triangular portion of an adjacent side. Compressing the tubular member longitudinally causes the connecting edge and the angled upright edge to elastically deform, for example by stretching, and causes the second end of the tubular member to rotate with respect to the first end of the tubular member.