Conformable energy absorber

Information

  • Patent Grant
  • 9415708
  • Patent Number
    9,415,708
  • Date Filed
    Tuesday, February 18, 2014
    10 years ago
  • Date Issued
    Tuesday, August 16, 2016
    8 years ago
Abstract
An energy absorber 10 that has a spine 12 which has a relaxed configuration and a deployment configuration. In the deployment configuration, the spine 12 lies proximate to a substrate 14 to protect the substrate 14 from an impacting object 16. Preferably, the spine 12 is bendable to conform to the substrate 14. The spine includes a number (N) of energy absorbing modules 18, 20, 22, 24, . . ., where 1<=N<=1000. At least some of the modules have a number (L) of mutually supporting energy absorbing vertebral members 30, where 1<=L<=100. Each vertebral member 30 includes a number (U) of coalesced energy absorbing units 32,34, were 2<=U<=10. At least some of the energy absorbing units 32, 34 have a base 36 that preferably but not necessarily is oriented toward the impacting object 16.
Description
TECHNICAL FIELD

A conformable energy absorber interposed between a substrate and an impacting object cushions mechanical forces sustained as a consequence of impact. Partial or complete absorption of such forces protects the impacting object such as the head of a vehicle occupant, the protected substrate such as a seat frame or both.


BACKGROUND

Automotive seats assemblies and restraint systems have long been used with active systems, such as airbags, in an attempt to minimize the risk of serious injury to vehicle occupants involved in a crash. These crashes include frontal, rear, side, rollover and combinations thereof that impart forces on the occupant in numerous directions. The occupants of these vehicles vary in size, weight, and height, and girth. Additionally, seat adjustments create further complexities of occupant positioning relative to the adjacent structures. The combinations of impact speed, impact type, occupant size, and occupant position create a nearly infinite number of impact scenarios which could never practically be tested for. Government and Insurance agencies have created test protocols to cover the most likely impact scenarios. However, serious injuries and fatalities still occur.


Seat manufacturers are continuously challenged to reduce the profile of the seat in an effort to increase the volume of space available for the occupant. As these seat assemblies decrease in thickness, less stroke is provided for impact management in the assembly, thereby necessitating higher efficiency in energy absorbing performance so that more energy can be absorbed in less space. Large foam buns have traditionally been used for both comfort and energy management. However, foam has proven to be less than ideal as an energy absorber due to its slow ramp up in load and poor crush efficiency. Furthermore, the foam density one would choose based on comfort characteristics is far too soft for energy management during a vehicle crash. Therefore a second stage energy absorber is desirable that has improved energy management properties and crush efficiency over the prior art with the resiliency to withstand every day operating loads that are less than one would experience in a vehicle crash.


Automotive interior systems, including vehicle seats, seat backs, consoles, door trim, pillar trim and other interior panels, are designed to withstand the day to day abuse they are likely to see in practical use. The driver's seat in particular, must be capable of withstanding tens of thousands of ingresses and egresses in conjunction with supporting the driver during the operation of the vehicle. Fabric or leather covered polyurethane (PU) foam has been traditionally been used in conjunction with a metal seat frame supporting structure to satisfy both comfort and crash criteria. Mechanical adjusters, heating, cooling, and airbags are also integrated into the seat assembly to enhance comfort and crash characteristics.


Efforts made with PU foam in particular to enhance the performance of the foam system for both comfort and crash include two main groups. Group one consists of using a reactive “dual” density approach where one density is used for comfort and one or more densities are molded for energy absorption following a crash. These may utilize not only changes in density but chemistry as well to obtain desired performance characteristics or both in the seat bun and the seat back. Group two consists of insert molding another foam component, made of EPP foam or some other foam type, and foaming the comfort PU foam around these energy§ absorbing foam components. Group two provides more flexibility to optimize the system crash performance and manage the loads the occupant experiences in a crash. These include changing the shape, density, chemistry, and position of these energy absorbing materials within the foam bun. However, there is still a need to address the inherent inefficiency of prior art foam energy absorbers.


Interior trim parts often cover structural members that are rigid with blunt edges. These structural members may be in the vicinity of the occupant during daily use as well as in a crash event. Contact with these members in a crash could result in serious injury. Therefore, it is desirable to have an energy absorbing structure which would cushion the occupant during an impact, mitigate some of the impacting forces and reduce the risk of serious injury. Ideally, this energy absorbing structure would be engineered in such a way that it would be able to adapt to the shapes of various structural members one would like to protect. In this way, one tool could produce a product that could be applied to a variety of structural members.


SUMMARY OF THE INVENTION

One aspect of the disclosure includes a multi-faceted energy absorber that lies adjacent to or covers in whole or part a substrate such as but not limited to an automobile seat frame. The absorber when positioned and or secured appropriately cushions a blow in that it protects the substrate, the impacting object or both from damage or injury consequent to impact.


In several embodiments, there is provided an energy absorber with a flexible spine that can be molded in a relatively linear configuration yet has flexibility about one or more axes so as to be bent and thus conform to the mating part. Preferably, the spine can be configured to bend up to 180 degrees about one or more axes depending upon the shape of the structure to be protected. Flexibility between energy absorbing units in combination with the shape and spacing of a trim line between units is also provided.





BRIEF DESCRIPTION OF THE DRAWINGS


FIG. 1 is a perspective view of an energy absorbing assembly that partially encapsulates a substrate such as a seat frame;



FIG. 2 is a plan view of a section of an energy absorbing assembly;



FIG. 3 is a side view thereof;



FIG. 4 is an enlarged end view thereof;



FIG. 5 is an alternate embodiment that resembles the view of FIG. 1; and



FIG. 6 is a sectional view of a clamshell configuration.





DETAILED DESCRIPTION

In FIG. 1 there is depicted an energy absorber 10 that has a spine 12. The spine 12 has a relaxed configuration and a deployment configuration. In the deployment configuration, the spine 12 lies proximate to a substrate 14 to protect the substrate 14 from an impacting object 16. Preferably, the spine 12 is bendable to conform to the substrate 14. The relaxed configuration of the spine has a longitudinal axis (X), a lateral axis (Y) and an orthogonal axis (Z) (FIGS. 1, 2).


The spine includes a number (N) of energy absorbing modules 18, 20, 22, 24, . . . (FIG. 2), where 1<=N<=1000. At least some of the modules have a number (L) of mutually supporting energy absorbing vertebral members 30, where 1<=L<=100. Each vertebral member 30 includes a number (U) of coalesced energy absorbing units 32, 34, were 2<=U<=10. At least some of the energy absorbing units 32, 34 have a base 36 that preferably but not necessarily is oriented toward the impacting object 16.


Whether manufactured by such processes as thermoforming, vacuum forming or injection molding, an aperture 38 is defined in the base 36 (FIGS. 3, 4). A curvilinear wall 40 extends from the base 36 in a direction away from the impacting object 16. It will be appreciated that in some configurations and applications the base 36 may be oriented toward the impacting object 16.


As shown in FIGS. 1-4, at least some of the coalesced energy absorbing units 32, 34 have a bottom 42 that extends across the curvilinear wall 40 so that the bottom 42 can be positioned toward the substrate 14 to be protected.


Supporting adjacent coalesced energy absorbing units 32, 34 is a shoulder 44 (FIG. 4) that supports adjacent coalesced energy absorbing units 32, 34 in a vertebral member 30. If desired the shoulder 44 can be hunched or curved to mate with the substrate 14. One or more living hinges 46 link adjacent energy absorbing modules 18, 20, 22, 24, . . . or vertebral members 30 within a module 12. The living hinges 46 are flexible about one or more of the longitudinal axis (X), the lateral axis (Y) and the orthogonal axis (Z) of the spine 12 so that in the deployed configuration, the spine 12 can conform by yaw, roll or pitch and otherwise twisting and bending to the substrate 14 as necessary, thereby protecting the substrate 14 and the impacting object 16 while absorbing forces associated with impact.


In some embodiments, each energy absorbing module has an average energy absorbing characteristic (E), the average energy absorbing characteristics (E1, E2) of adjacent energy absorbing modules being the same or different so that the spine 12 has a gradient of energy absorbing characteristics.


In one exemplary embodiment, N=2 and L=1 so that there are two energy absorbing vertebral members 30 in the spine 12. In another case, U=2 so that there is a pair of energy absorbing units 32, 34 in the vertebral member 30.


If the situation warrants it, the shoulder 44 is concave (FIG. 4) so that the shoulder 44 can accommodate a substrate 14 with a convex region (FIG. 1).


To promote stiffness, a rib 46 can optionally be provided that extends between the curvilinear walls 40 of energy absorbing units 32, 34 in adjacent vertebral members 30 in a module. Preferably, the rib 46 has a ceiling 48 that is above the bottom 42 of an energy absorbing unit 32, 34.


It will be appreciated that a skirt 50 (FIG. 4) may extend around a curvilinear wall 40 of an energy absorbing unit 32, 34 between the wall 40 and the base 36.


As suggested in FIG. 3, the bottom 42 is domed or extends convexedly outwards in at least one embodiment.


Referring to FIG. 1, an energy-absorbing assembly 54 can be provided which has a first spine 56, a second spine 58 and a substrate 14 interposed between the first and the second spines 56, 58.


Thus, in several embodiments, there is provided an energy absorber 10 or assembly 54 with one or more flexible spines 12, 54, 58 that can be molded in a relatively linear configuration. The absorber 10 has flexibility about one or more axes so as to contort and conform to the mating part. Preferably, the spine 12 can be configured to bend up to 180 degrees about one or more axes depending upon the shape of the structure 14 to be protected. Flexibility between modules or energy absorbing units within a module in combination with the shape and spacing of a trim line between units is also provided.


In one embodiment, a spine section 12 is provided without an interconnecting rib 46. This spine section 12 is most flexible about its longitudinal axis. A spine section 12 with an interconnecting rib 46 is most flexible at angles to either side of the spine 12 since the rib 46 provides a collapsing or expanding section that can distort between energy absorbing units 32, 34. By either imparting ribbed sections or eliminating ribbed sections along the longitudinal axis of the spine 12 in combination with the trim profile, the absorber 10 can be molded linearly in one die draw but compelled to bend as desired to protect a particular member 14. Rectangular absorbers in one die draw offer more favorable forming economics and minimize tool complexity.


Some means of retaining the absorber 12 in its installed position is desirable. The product may be in-molded during the foaming cycle wherein the absorber(s) 10 is positioned in the mold prior to foaming. Using a foam locating scheme relative to a seat frame for example serves to position the energy absorber 12 relative to the frame 14. Other traditional means for attaching may also be selected such as welding, snapping, push pins, clips, Velcro and the like.


In some embodiments (see, e.g., FIGS. 5, 6), the energy absorber 12 is integrated into either a seat cushion 52 or into the seat itself. The designer thus offers the possibility of using thermoplastic polyurethane (TPU) as an integral part of a seat component, such as a head rest or seat back or seat cushion. If at least some of the seat components are molded from for example TPU, the energy absorber 12 can be integrated into at least a part of the seat component 52.


Preferably, the energy absorber 12 is molded in the same step as molding the seat component 52. The energy absorber 12 can then be coordinated with a seat component 52 such as the cushion about the skirt 50. Optionally, a tether is provided which allows the energy absorber 12 to coordinate with the seat component, e.g., cushion 52. As used herein the term “tether” includes a connection seam 56 alone or a structure with an elongate spacer 58 having a flexible or rigid connection seam 56 at either or both ends.



FIG. 5 shows an embodiment in which a tether 54 extends from the seat cushion 52 outwardly to the energy absorber 12 that is deployed around at least a part of the seat frame 14. If there is an elongate spacer 58 having a flexible or rigid connection seam 56 at either end, respectively, the seams 56 are associated with the energy absorber 12 and the seat cushion 52 (FIG. 5). As shown, each elongate spacer 54 has an inboard edge 60 and an outboard edge 62. For a given spacer 54, the inboard edge 60 may be wider than the outboard edge 62 or not.


In another embodiment (FIG. 6) the energy absorbers 12 are positioned on opposing sides of a substrate, such as a seat frame 14. In one example, energy absorbers 12 positioned at opposite faces of, for example, a seat frame are connected to each other, much like a clamshell. A bridge portion 64 is provided between opposing energy absorbers 12. In this embodiment, a subassembly comprises two energy absorbers 12 that are connected by the bridge portion 64. The subassembly effectively wraps around at least a part of the substrate 14. If desired the subassembly can be attached to the substrate by convention attachment methods.


In practice, one tool may produce energy absorbers that can wrap around complex geometries 14 like seat back frames, headrest frames, 90 degree metal corners, etc. and apply to multiple programs, thereby minimizing tooling investment. For example, a right/left tool might be used to make an energy absorber 12 for seat backs and frames and an up/down tool might be used for corners and trim. Such absorbers can be insert-molded during the foaming process. If desired, polypropylene components can be welded to the interior trim. Thus there is provided a common tool for multiple applications.


Additionally, several embodiments of the invention have proven to be more efficient than foam in absorbing energy. The space saved can be used to improve safety, and create a more spacious interior, especially in shorter cars and lighter weight vehicles.


As required, detailed embodiments of the present invention are disclosed herein; however, it is to be understood that the disclosed embodiments are merely exemplary of the invention that may be embodied in various and alternative forms. The figures are not necessarily to scale; some features may be exaggerated or minimized to show details of particular components. Therefore, specific structural and functional details disclosed herein are not to be interpreted as limiting, but merely as a representative basis for teaching one skilled in the art to variously employ the present invention.


While exemplary embodiments are described above, it is not intended that these embodiments describe all possible forms of the invention. Rather, the words used in the specification are words of description rather than limitation, and it is understood that various changes may be made without departing from the spirit and scope of the invention. Additionally, the features of various implementing embodiments may be combined to form further embodiments of the invention.

Claims
  • 1. An energy absorber in combination with a seat component and a substrate to be protected, the energy absorber having a spine with a relaxed configuration and a deployment configuration, so that in the deployment configuration, the spine lies adjacent to the substrate to protect the substrate from an impacting object, the spine being bendable to conform to the substrate, the relaxed configuration of the spine having a longitudinal axis, a lateral axis and an orthogonal axis, the spine comprising a thermoplastic polyurethane (TPU) and includinga number (N) of energy absorbing modules, where 1<=N<=1000, at least some of the modules having a number (L) of mutually supporting energy absorbing vertebral members, where 1<=L<=100;at least some of the vertebral members, including a number (U) of coalesced energy absorbing units, were 2<=U<=10, at least some of the energy absorbing units including a base that is oriented toward the impacting object,a curvilinear wall extending from the base in a direction away from the impacting object, anda bottom that extends across the curvilinear wall at a bottom end thereof so that the bottom can be positioned toward the substrate to be protected;a curved shoulder in at least some vertebral members that lies between adjacent coalesced energy absorbing units, the curved shoulder being adapted to allow the at least some vertebral members to be placed adjacent to the substrate; andone or more living hinges that link adjacent energy absorbing vertebral members, the living hinges being flexible about one or more of the longitudinal axis, the lateral axis and the orthogonal axis of the spine so that in the deployed configuration, the spine can protect the substrate, and absorb forces associated with impact,the substrate including a seat frame with a cylindrical member, a portion of the cylindrical member being placed adjacent to the spine, a pair of spines being provided on opposed sides of the cylindrical member,the seat component being selected from the group consisting of a seat cushion, a seat back, and a headrest, anda tether that extends from a seat component to the substrate.
  • 2. The energy absorber of claim 1, wherein each energy absorbing module has an average energy absorbing characteristic (E), the average energy absorbing characteristics (E1, E2) of adjacent energy absorbing modules being different so that the spine has a gradient of energy absorbing characteristics.
  • 3. The energy absorber of claim 1, wherein there is a pair of energy absorbing units in the vertebral member.
  • 4. The energy absorber of claim 3, wherein the shoulder is concave so that the shoulder can accommodate a substrate with a convex region.
  • 5. The energy absorber of claim 1, further including a rib that extends between the curvilinear walls of energy absorbing units in adjacent vertebral members in a module.
  • 6. The energy absorber of claim 5, wherein the rib has a ceiling that is below the bottom of an energy absorbing unit.
  • 7. The energy absorber of claim 1, further including a skirt that extends around a curvilinear wall of an energy absorbing unit between the wall and the base.
US Referenced Citations (83)
Number Name Date Kind
1784511 Carns Dec 1930 A
2090881 Wilson Aug 1937 A
2391997 Noble Jan 1946 A
3011602 Ensrud Dec 1961 A
3018015 Agriss et al. Jan 1962 A
3071216 Jones et al. Jan 1963 A
3196763 Rushton Jul 1965 A
3231454 Williams Jan 1966 A
3535663 Herzog et al. Oct 1970 A
3605145 Graebe Sep 1971 A
3938963 Hale Feb 1976 A
4072334 Seegmiller et al. Feb 1978 A
4597601 Manning Jul 1986 A
4890877 Ashtiani-Zarandi et al. Jan 1990 A
5150935 Glance et al. Sep 1992 A
5390467 Shuert Feb 1995 A
5391251 Shuert Feb 1995 A
5401347 Shuert Mar 1995 A
5444959 Tesch Aug 1995 A
5470641 Shuert Nov 1995 A
5549327 Rusche et al. Aug 1996 A
5572804 Skaja et al. Nov 1996 A
6017084 Carroll, III et al. Jan 2000 A
6098313 Skaja Aug 2000 A
6142563 Townsend et al. Nov 2000 A
6199937 Zetouna Mar 2001 B1
6199942 Carroll, III et al. Mar 2001 B1
6221292 Carroll, III Apr 2001 B1
6247745 Carroll, III et al. Jun 2001 B1
6406081 Mahfet et al. Jun 2002 B1
6443513 Glance Sep 2002 B1
6453476 Moore, III et al. Sep 2002 B1
6550850 Laborie et al. Apr 2003 B2
6669251 Trappe Dec 2003 B2
6679967 Carroll, III et al. Jan 2004 B1
6681907 Le Jan 2004 B2
6682128 Carroll, III et al. Jan 2004 B2
6726262 Marijnissen et al. Apr 2004 B2
6733064 Byma et al. May 2004 B2
6746061 Evans Jun 2004 B1
6749784 Blanchon Jun 2004 B2
6752450 Carroll, III et al. Jun 2004 B2
6777062 Skaja Aug 2004 B2
6848730 Evans Feb 2005 B2
6863322 Hunter et al. Mar 2005 B2
6923494 Shuler et al. Aug 2005 B2
6926321 Zipfel Aug 2005 B2
6938936 Mooijman et al. Sep 2005 B2
7073831 Evans Jul 2006 B2
7328462 Straus Feb 2008 B1
7360822 Cormier et al. Apr 2008 B2
7377577 Cormier et al. May 2008 B2
7384095 Cormier et al. Jun 2008 B2
7404593 Cormier et al. Jul 2008 B2
7625023 Audi et al. Dec 2009 B2
7628444 Cormier et al. Dec 2009 B2
7676854 Berger et al. Mar 2010 B2
7731292 Ishijima et al. Jun 2010 B2
7766386 Spingler Aug 2010 B2
7802320 Morgan Sep 2010 B2
7895681 Ferrara Mar 2011 B2
7908678 Brine, III et al. Mar 2011 B2
7954177 Ide et al. Jun 2011 B2
7958573 Lewis, Jr. et al. Jun 2011 B2
8201671 Cho Jun 2012 B2
8465087 Gerwolls et al. Jun 2013 B2
20020017805 Carroll, III et al. Feb 2002 A1
20020113459 Laborie et al. Aug 2002 A1
20030080573 Marijnissen et al. May 2003 A1
20040036302 Shuler et al. Feb 2004 A1
20040094977 Shuler et al. May 2004 A1
20040174025 Converse et al. Sep 2004 A1
20050057053 Evans et al. Mar 2005 A1
20050161982 Cormier et al. Jul 2005 A1
20050230204 Tamada et al. Oct 2005 A1
20050230205 Springler et al. Oct 2005 A1
20050269824 Steeg et al. Dec 2005 A1
20060028038 Glasgow et al. Feb 2006 A1
20070228745 Cormier et al. Oct 2007 A1
20080120764 Sajic May 2008 A1
20100244469 Gerwolls et al. Sep 2010 A1
20100299812 Maddux et al. Dec 2010 A1
20100326782 Vandenberge et al. Dec 2010 A1
Foreign Referenced Citations (12)
Number Date Country
19947245 Apr 2000 DE
0434834 Jul 1991 EP
0630592 Dec 1994 EP
0863056 Sep 1998 EP
1555109 Jul 2005 EP
2870802 Dec 2005 FR
136582 Oct 1975 JP
9150692 Nov 1995 JP
08085404 Apr 1996 JP
11348699 Dec 1999 JP
20060065554 Jun 2006 KR
0031434 Jun 2000 WO
Non-Patent Literature Citations (4)
Entry
International Search Report and the Written Opinion, International application No. PCT/US06/13656; Applicant Oakwood Energy Management, Inc.
European Search Report and the Written Opinion, for Application No. 06112732.0-2412; dated Aug. 16, 2006, Applicant Oakwood Energy Management, Inc., 9 pages.
International Search Report and the Written Opinion, International application No. PCT/US/2012/070006; date of mailing Feb. 15, 2013.
International Search Report and the Written Opinion, International application No. 2013/036703; date of mailing Jul. 19, 2013.
Related Publications (1)
Number Date Country
20150232053 A1 Aug 2015 US