A polymer spacer element for absorbing impact for an engine-powered vehicle includes an open front extremity and a rear extremity, and a honeycomb structure having channels made in a single piece and at least three channels each of which extends from the first open front extremity towards the second rear extremity. In addition, each channel of the channels is tapered from the first open front extremity towards the second rear extremity or vice-versa and presents an inner rake angle. In addition, each channel includes an elevation and a transversal section having a polygon shape that is regular or irregular, in which the transversal section has an equivalent lateral dimension equal to a diameter of a circumference having minimum diameter which circumscribes the transversal section of each corresponding channel. Each channel presents a ratio between the elevation and the transversal dimension which is lower than or equal to three.

The proposed solution relates to a component that is provided for energy absorption in the event of a force (F) acting on the component (1).

The component (1) is configured with a component structure (10) integrating at least one first energy absorption mechanism and at least one second energy absorption mechanism, by means of which the first and second energy absorption mechanisms can be activated in the event of a force acting on the component (1) and exceeding a threshold value.

A shock absorber includes a three-dimensional structure composed of a unit structure repeatedly, regularly and continuously arranged in at least one direction, the unit structure being a three-dimensional shape formed by a wall having an external shape defined by a pair of parallel planes or curved surfaces. When the unit structure occupies a cuboidal space representing a unit space and defined by mutually orthogonal three sides having a first side extending in an axial direction in which the shock absorber exhibits a shock absorbing function as the shock absorber receives a load and second and third sides each extending from one end of the first side in a direction orthogonal to the axial direction, and the first side has a length L1 and a longer one of the second and third sides has a length L2, the shock absorber satisfies 1.1≤L1/L2≤4.0.

A crash box may include one or more layers arranged to absorb crash energy. In some embodiments, the crash box includes a first layer having an outer skin defining a periphery of the first layer and at least one of: 1) a rib and web structure, and 2) an array of tubes disposed within the outer skin for absorbing crash energy, and a second layer adjacent to the first layer, the second layer having an outer skin defining a periphery of the second layer and at least one of: 1) a rib and web structure, and 2) an array of tubes disposed within the outer skin for absorbing crash energy.

A composite tie bar assembly for distributing loads to a support frame of an automotive vehicle. The tie bar assembly includes a pair of spaced apart. reinforcement bars extending longitudinally between opposing ends. A tie bar shell is supported by the reinforcement bars and extends between opposite first and second distal cods. The tie bar shell has a first support plate extending between the reinforcement bars adjacent the first distal end and a second support plate extending between the reinforcement bars adjacent the second distal end. Bach of the support plates includes a plurality of structural ribs formed Integral therewith for distributing loads from the reinforcement bars to the support frame of the vehicle.

End member assemblies dimensioned for securement to a flexible spring member for forming a gas spring assembly include first and second end member sections. The first end member section includes a plurality of first ribs disposed in spaced relation to one another such that a plurality of first grooves are formed therebetween. The second end member section is disposed in abutting engagement with the first end member section. The second end member section includes a plurality of second ribs disposed in spaced relation to one another such that a plurality of second grooves are formed therebetween. The plurality of first ribs and/or the plurality of second ribs are dimensioned for permanent deflection into a respectively adjacent one of the plurality of first and/or second grooves upon undergoing a kinetic impact from an associated foreign object. Gas spring assemblies and suspension systems are also included.

A composite material includes an upper layer, a lower layer and means arranged so as to diffuse substantially transversely at least part of the kinetic energy induced by an impact on one of said layers, said means cooperating on both sides, with the upper layer and the lower layer. The diffusion means can consist in a network of interassembled base elements and of cavities, forming a three-dimensional structure. A protection device comprising includes an insert consisting of the composite material.

There is provided an energy absorbing landing gear system for attachment to a vertical landing apparatus. The energy absorbing landing gear system includes a linear damper assembly, and a load limiter assembly coupled to the linear damper assembly, the load limiter assembly having at least one deformable element to enhance an energy absorption capability. When the energy absorbing landing gear system is attached to the vertical landing apparatus, during a landing phase, the linear damper assembly contacts a landing surface, and a piston assembly of the linear damper assembly moves a first compression distance toward the load limiter assembly, and when the linear damper assembly reaches a maximum compression, the linear damper assembly moves a second compression distance into the load limiter assembly, and the at least one deformable element deforms.

A crash box may include one or more layers arranged to absorb crash energy. In some embodiments, the crash box includes a first layer having an outer skin defining a periphery of the first layer and at least one of: 1) a rib and web structure, and 2) an array of tubes disposed within the outer skin for absorbing crash energy, and a second layer adjacent to the first layer, the second layer having an outer skin defining a periphery of the second layer and at least one of: 1) a rib and web structure, and 2) an array of tubes disposed within the outer skin for absorbing crash energy.

A landing gear of an aircraft of the present invention, includes a core section with a honeycomb structure, including a plurality of cell walls and a plurality of cell holes defined by the plurality of cell walls; a cover section which covers the core section; and a hole provided in the core section to absorb an impact, the hole having a diameter larger than that of the plurality of cell holes and extending in an extending direction of the plurality of cell holes.