Elastically averaged alignment systems and methods
US-2015194650-A1 · Jul 9, 2015 · US
US9447840B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9447840-B2 |
| Application number | US-201313915177-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 11, 2013 |
| Priority date | Jun 11, 2013 |
| Publication date | Sep 20, 2016 |
| Grant date | Sep 20, 2016 |
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An elastically deformable energy management assembly includes a first component. Also included is at least one protrusion extending from the first component, the at least one protrusion having an outer surface. Further included is a second component comprising at least one aperture defined by an aperture wall, the aperture wall in slideable engagement with the outer surface of the at least one protrusion, wherein at least one of the protrusion and the aperture wall comprises an elastically deformable material.
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What is claimed is: 1. An elastically deformable energy management assembly comprising: a first component; at least one protrusion extending from the first component in a first direction, the at least one protrusion having an outer surface, the protrusion formed of an elastically deformable material; a second component comprising at least one aperture defined by an aperture wall, the aperture wall in slideable engagement with the outer surface of the at least one protrusion, the aperture comprising a slot having a first closed end and a second closed end, the protrusion slideable within the slot in a direction perpendicular to the first direction of the at least one protrusion; and a detent of the slot configured to retain the protrusion in an unloaded condition up to a predetermined force, the detent having a width greater than the width of the remainder of the slot, the protrusion moveable into the remainder of the slot upon application of a force in excess of the predetermined force. 2. The elastically deformable energy management assembly of claim 1 , wherein the detent is disposed proximate a mid-portion along a longitudinal direction of the slot. 3. The elastically deformable energy management assembly of claim 1 , wherein the slot is molded into the second component. 4. The elastically deformable energy management assembly of claim 1 , wherein the slot is formed in a bracket insertable into the second component. 5. The elastically deformable energy management assembly of claim 1 , wherein the first component is disposed in a fixed, stationary position, wherein the second component is moveable relative to the first component. 6. The elastically deformable energy management assembly of claim 5 , wherein the second component is rotatable relative to the first component. 7. The elastically deformable energy management assembly of claim 6 , further comprising a pivot element operatively coupled to the second component. 8. The elastically deformable energy management assembly of claim 1 , wherein the second component remains in a contact interference condition with the outer surface of the protrusion over a range of positions of the second component. 9. The elastically deformable energy management assembly of claim 1 , further comprising a plurality of protrusions of the first component disposed within a plurality of apertures of the second component. 10. The elastically deformable energy management assembly of claim 9 , wherein an amount of deformation of each of the plurality of protrusions is averaged in aggregate. 11. The elastically deformable energy management assembly of claim 1 , wherein the elastically deformable energy management assembly is disposed in a vehicle. 12. A method of managing energy absorption with an elastically deformable energy management assembly comprising: engaging an outer surface of a protrusion of a first component with an aperture wall of a second component upon insertion of the protrusion in a first direction into an aperture defined by the aperture wall, the aperture comprising a slot and the protrusion slideable within the slot in a direction perpendicular to the first direction; elastically deforming the protrusion upon engagement with the second component; retaining the protrusion within a detent of the slot in an unloaded condition, the detent having a width greater than the width of the remainder of the slot; and transferring energy between the protrusion and the aperture wall during imposition of a load condition on the elastically deformable energy management assembly. 13. The method of claim 12 , further comprising engaging a plurality of protrusions with a plurality of aperture walls and elastically deforming the plurality of protrusions, wherein the plurality of protrusions comprises an elastically deformable material. 14. The method of claim 13 , further comprising performing an elastic averaging of the amount of deformation of each of the plurality of protrusions. 15. The method of claim 12 , further comprising engaging a plurality of protrusions with a plurality of aperture walls and elastically deforming the plurality of aperture walls, wherein the plurality of aperture walls comprises an elastically deformable material. 16. The method of claim 15 , further comprising performing an elastic averaging of the amount of deformation of each of the plurality of aperture walls. 17. An energy management assembly for a vehicle zone comprising: a potential contact zone component; at least one protrusion extending from the potential contact zone component in a first direction, the at least one protrusion having an outer surface, the protrusion formed of an elastically deformable material; and a mated component comprising at least one aperture defined by an aperture wall, the aperture wall in slideable engagement with the outer surface of the at least one protrusion, the aperture comprising a slot having a first closed end and a second closed end, the protrusion slideable within the slot in a direction perpendicular to the first direction of the at least one protrusion; and a detent of the slot configured to retain the protrusion in an unloaded condition up to a predetermined force, the detent having a width greater than the width of the remainder of the slot, the protrusion moveable into the remainder of the slot upon application of a force in excess of the predetermined force. 18. The energy management assembly of claim 17 , wherein the potential contact zone component is disposed in a vehicle interior.
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