CA1207951A - Shock attenuation system - Google Patents

Abstract

Abstract of the Disclosure A shock attenuation system comprising a plurality of shock attenuating columns of a substantially resilient elastomeric material. The columns are so dimensioned and configured that, when subjected to an axial impact force of predetermined magnitude, they resiliently deform for attenuating the shock resulting from the impact force. The columns then spring back substantially to their undeformed shape.

Description

~;Z0~79Sl The present invention relates generally to a shock attenuation system useful in protective headgear, running shoes and ot'ner shock-attenuating applications, and more particularly to such a system wherein shock attenuation is accomplished by the resilient deformation of elastomeric columns.
This invention represents an improvement on the shock attenuation system disclosed in pending Canadian application Serial No. 375,692, filed April 16, 1981. As described therein, the system comprises a liner secured to the inside surface of an outer protectlve shell which is worn on the head. The liner includes a series of tubes of elastomeric material disposed in generally parallel side-by-side relation with their central axes generally parallel to the inside surface of the shell. The tubes are elastically deformable in the radial direction and sufficiently closely spaced that when one deforms, as when a blow is delivered to the outer shell, it is engageable with the sides of adjacent tubes for deforming them thereby to attenuate the shock felt by the person wearing the headgear.
United States Patents 3,877,076, 2,150,747, and 2,179,148 show various types of shock attenuation apparatus generally in the field of this invention.
Summary of the Invention The invention provides protective apparatus comprising:
an outer shell of substantially rigid material adapted to be posi-tioned on an object to be protected, such as the head; a shock attenuation system on the inside of the shell comprising pad means adapted for engagement with said object, said pad means comprising a multiplicity of spaced-apart resilient columns each constituted ~207~

by a hollow integrally formed one-piece tubular member of resilient synthetic resin material havlng a slenderness ratio of less than 3.0, the slenderness ratio being the ratio of column length to column diameter, said columns being so dimensioned and configured that, when subjected to an axial impact load of pre-determined magnitude, the walls of the columns are adapted resiliently to buckle in irregular and random fashion for attenu-ating the shock resulting from said impact load, said columns then being adapted resiliently to return substantially to their unde-formed shape; and means for fastening said pad means to the insidesurface of said shell with said columns generally at right angles to the shell.
The system preferably provides a higher level of shock attenuation than prior systems and continues to provide an adequate level of shock attenuation after numerous impact loadings. The system may be releasably secured to the outer shell of protective ; headgear, for example, Eor enabling ready removal of the system from the shell, as for inspection and replacement, if necessary.
The system is preferably relatively compact and lightweight, and relatively economical to manufacture.
Other features will be in part apparent and in part pointed out hereinafter.
Brief Description of the Drawings Figure 1 is a front view of a helmet having a shock attenuation system of the present invention, portions of the helmet being broken away for purposes of illustration;
Figure 2 is a bottom view of the helmet shown in Figure l;

~3 ~207ss~
2a Figure 3 is an enlarged horizontal section on line 3--3 of Figure 1 showing the construction of a pad made in accordance with this invention;
Figure 4 is an enlarged vertical section on line 4--4 of Figure l;
Figure 4A is a view similar to Figure 4 showing the operation of the system when subjected to an impact force;

~2{~79~:~

Figs. 5-8 are graphs showing the results of a series of tests conducted on shock attenuation systems of this inven tion;
Figs. 9A - ~D are diagrammatic views illustrating possible ways in which shock-attenuating columns of the pres-ent invention may be arranged;
Fig. 10 is a view illustrating a tubular shock-at-tenuating column having a series of holes therein;
Fig. 11 is a view illustrating a tubular shock-at-tenuating column having a series of slits therein;
Fig. 12 is a cross-sectional view of a helmet having an alternative shock attenuation system of the pr~sent inven~
tion; and Fig. 13 is a plan view of a shock-attenuating module of the shock attenuation system of Fig. 12 Corresponding reference characters indicate corre-sponding parts throughout the several views of the drawings.

~.~
Description of the Preferred Embodiment Referring now to the drawings, and first more par-ticularly to Figs. 1 and 2, there is generally indicated at 1 protective apparatus in the form of headgear (an avia~ion hel-met as shown) comprising an outer impact-receiving member or shell 3, which may be of a suitable substantially rigid mate-rial, such as resin-impregnated fiberglass, having a relative-ly high impact resistance. A shock attenuation system of this invention, generally designated S, is provided on the inside of the shell for attenuating the shock on the head resulting from an impact (or impacts) on the shell. While the use of `system S in pr~tective headgear is considered to be an impor-tant application of the present invention, it is by no means limited to this application. Thus the present system as herein described may be used to protect other parts of the body. In fact, the system may be adapted for virt-ually any application involving shock attenuation.

~L~207~i5~L

As incorporated in the headgear shown in the draw-ings, the shock attenuation system S comprises a plurality of separate pads 7 secured to the interior surface of the shell 3 at positions corresponding to the front (forehead), back, sides and top of the head. As shown best in Figs. 3 and 4, each pad contains a plurality of shock attenuating columns 9 arrayed in a plurality of generally parallel rows (four rows of seven columns each as shown). The spacing S1 between ad-~acent columns in a row is substantially equal, as is the spacing S2 between adjacent rows of columnsO Each column is tubular in shape and formed of a substantially resilient elas-tomeric material, such as vinyl, urethane, or polyethylene.
All of the columns in the array are of substantially uniform diameter and length and have square-cut end faces, i.e., the two end faces of each column lie in planes generally perpen-dicular to the central axis of the column.
Each pad is of layered construction, comprising a first or inner layer 11 of a suitable fabric, for example, adjacent the interior surface of the shell 3, a relatively thick econd layer 13 of cushioning material, such as a vinyl nitrile foam of the type sold under the trademark ~326 Rubatex~ by Rubatex Corporation of Bedford, Virginia, a third layer 15 identical to the first layer, a fourth layer 17 of the same cushioning material as the second layer but not as thick, and a fifth or outer layer 19 of a suitable facing material such as leather. The columns 9 extend between the first and third layers 11, 15 through the cushioning layer 13, the latter of which is of substantially the same thickness as the columns. The columns are secured at their ends by a suit-able adhesive, for example, to the first and third layers 11,15, which may be referred to as carrier sheets. The central axes of the columns extend generally perpendicular to these sheets 11, 15. The carrier sheets 11, 15 and cushioning layer 13 combine to constitute means for supporting the columns in 79~i~

the aforesaid array. Other means for so supporting the col-umns may also be suitable. In this regard, i~ is contemplated that the columns 9 and carrier sheets 11, 15 may be integrally formed te.g., molded).
Each pad 7 is removably mounted on the inside of shell 3 with the central axes of the columns extending gener-ally at right angles to the interior surface of the shell (thereby ensuring axial loading of the columns when the helmet is subjected to an impact) by fastening means comprising a pair of two part fasteners, one part, in the form of a patch 21, of each pair being secured (e.g., glued) to the inside face of the inner carrier sheet 11 of the pad, and the other part, in the form of a patch 23, of each pair being secured (e.g., glued) to the interior surface of the rigid shell 3.
The two patches 21, 23 of each pair are preferably formed from a fabric fastening material available commercially under the trademark VE~CRO, such as shown in Mestral Ur S~ patent

2,717,431, issued September 13, 1955. Thus the patches have cooperable fastening elements thereon which are interengage-able for fastening the pad to the shell, and disengageable forremoval of the pad from the shell ~as for inspection and re-placement, if necessary). It will be understood that addi-tional VELCRO patches 23, or even continuous VELCRO strips may be placed around the interior surface of the shell so that the position of the pads may be adjusted to fit the head of the particular person wearing the headgear. Other means for fas-tening the pads 7 to the helmet may also be used.
In accordance with this invention, the pads are de-signed to attenuate the shock on the head of the wearer re-sulting from an impact on the shell. It will be noted in thisregard that the columns 9 are disposed for axial loading dur ing impact and are so dimensioned and configured that, when subjected to an axial impact force of predetermined magnitude, they are adapted resiliently to deform for attenuating the shock resulting from the force of impact. During the initial ~ ~z~

stages of such deformation, the columns are believed to com-press axially, that is, their effective length as measured in the direction perpendicular ~o the carrier sheets 11, 15 de-creases. This decrease is believed to ~e effected by a bend-ing of the column walls without a substantial increase in the density of the wall material, although it is possible that some actual increase in wall density may occur. During the latter stages of the deformation process, the columns deflect laterally or buckle under the force of impact. This buckling is on a random basis, as illustrated in Fig. 4A, and usually begins with a local crippling at some part of each column.
After the impact force has dissipated, the columns are then adapted to spring back substantially to their undefoxmed (Fig.
4~ shape. Thust unlike many of the prior art shock attenua-tion systems, this system of the present invention is designed for repeated use.
Another important advantage of this invention is that, given a set of design parameters (e.g., weight, overall - thickness, etc.), the system S may be engineered to meet vir-tually any performance requirement over a wide range of re-quirements~ This is accomplished by varying the physical properties and characteristics of the columns 9, such as the material out of which they are made, their length to diameter (slenderness) ratio, the angle at which their ends are cut, and their proximity to one another. The effect of each of ` these factors on the ability of the system to attenuate shock is clearly demonstrated in the graphs of Figs. 5 - 8.
Each of these graphs depicts the results of a series of tests in which a test head form weighing eleven (11~ lbs.
(5.0 kg.) and having a triaxial accelerometer at its center of gravity was dropped in guided free fall from heights of 18, 24, 36 and 48 inches ~45.7, 61~0, 91.4 and 121.9 cm.) onto each of a series of pads 7 incorporating shock attenuation systems S of this invention~ The pads were supported by a rigid steel anvil. The maximum deceleration of the head form lZ~5~

was measured for each drop. The results of the test were then plotted on the graph, with the drop height being represented in inches on the X-axis and the maximum deceleration being represented in "peak G's" on the Y-axis, each G being a unit of deceleration equal to 32 ftJsec.2 (9.8 m/sec.2). The pads 7 used in conducting the tests were constructed in the manner described above and were identical in every respect except as noted hereinafter. Thus, unless otherwise noted, each pad tested was 5-1/2" (14.0 cm.) long, 2-1/2" (6~4 cm.) wide and 3/4" (1.9 cm.~ thick~ and the columns 9 in each pad were tubular in shape with square-cut end faces, of 80-durom-eter (Shore A) urethane, and arrayed in four rows of seven columns each, with the spacing Sl between adjacent columns in each row being approximately 3/4" (1.9 cm.), and the spacing S2 between adjacent rows being approximately 5/8" (1.6 cm.).
Each column had, unless otherwise noted~ an outside diamter of about 1/2" ~1.3 cm.), an inside diameter of about 7/16" ~1.1 cm.), and a length of about 1/2" (1.3 cm.).
The graph of Fig. 5 illustrates the effect of the material out of which a column 9 is made on the ability of the system S to attenuate shock. In obtaining the data for this graph, five different pads; designated 7A - E, were tested in the manner described above. These pads were identical except for the material out of which the columns 9 were made. In this regard, the columns of pads 7A - 7E were constructed out of the f ollowing materials:
Pad Materlal Hardness ~Shore A durometer) 7A Vinyl 30 7B Urethane 40 7C Polyethylene 90 7D Ethylene Vinyl Acetate 90 7E Urethane 80 ~Z~ Sl It will be observed from the graph that pads 7A
and 7B with columns 9 of lower durometer material were gen-erally more effective (i.e., obtained lower "peak G" results~
at lower drop heights (less than about 40" or 101.6 cm.) where the impact energy involved was correspondingly lower, and that pads 7C - 7E with columns of higher durometer material were generally more effective at greater drop heights (more than about 40'l or 101~6 cm.) where the impact energy was higher.
The graph of Fig. 6 illustrates the effect that the column slenderness ratio (the ratio of the length of a column 9 to its diameter) has on the ability of the system to absorb energy. In obtaining the data for this graph, four pads, designated 7A - 7D, were tested. The pads were identi-cal except that the length (and thus the slenderness ratio) of the columns 9 varied from pad to pad as follows:
Pad Column Length Slenderness Ratio 7A 0.50" (1.3 cm.) 1.0 7B 0.75" (1.9 cm.) 1.5 7C 1.0 " (2.5 cm.) 2.0 7D 1.25" (3.2 cm.) 2.5 The test results depicted in the graph of Fig. 6 in-dicate that as the column slenderness ratio increases within the range of 1.0 - 2.5, the effectiveness of the system in attenuating shock also increases. There is some indication, however~ that as the column slenderness ratia approaches 2.5, the ability of the system to attenuate higher impact energies (corresponding to a test drop height of greater than abouf 40"
or 101.6 cm.) decreases. It is preferred that the slenderness ratio not exceed 3Ø
The graph of Fig. 7 illustrates the effect of the angle at which the end faces of columns 9 are cut on the shock attenuation properties of a system S. Again, four pads were used in this test, these being designated 7A - 7D. The pads were identical except that the angle ~designated A in Fig. 7) ~ 1207~35~

at which the column end faces in each pad were cut differed from pad to pad as follows:
Pad An~le of Cut 7~ 37 7D 0 (square cut) It will be observed from the graph that pads 7B and 7C containing columns having angle cuts of 26 and 14, re-spectively, were the most effective at lower drop heights (less than about 30" or 76r2 cm.), and that pad 7D containing columns 9 with square-cut ends was the most effective at higher drop heights (greater than about 30l' or 76.2 cm.).
This suggests that columns with end faces cut at a relatively shallow angle may be the most effective in applications in-volving low impact forces, while square-cut columns may be the most effective for applications in which high impact fvrces are involved.
The graph of Fig. 8 illustrates the effect of column proximity on the shock attenuation characteristics of a system S. Four pads, designated 7A - 7D, were used in obtaining the test data for this graph. The pads were identical except that the number of columns per pad varied from pad to pad. Thus, pads 7~ - 7D contained 11, 14, 20 and 28 columns, respectively arrayed as shown in Figs. 9A - 9D, respectively. It will be observed from the Fig. 8 graph that pads 7A - 7C were gener-ally the most effective at lower drop heights, and that pad 7D
was the more effective at higher drop heights (more than about 28" or 71.1 cm.). This indicates that systems wherein the columns are spaced relatively far apart tas in pads 7A - 7C) may be more effective for attenuating shock in applications involving relatively small impact forces, and that systems wherein the columns are relatively closely spaced (as in pad 7D) may be more effective in applications wherein greater im-pact forces are involved.

)75~

Fig. 10 illustrates another variation of the shock attenuation system S wherein each column 9 is in the form of a round tubular member having openings in the form of holes 31 in its side wall. Four such holes are indicated spaced at 90 intervals circumferentially around the tube approximately in - the central radial plane of the tube. The number of holes may vary~ For a column 9 having an outside diameter of 1/2" (1.3 cm.), an inside diameter of 3/8" (0.65 cm.) and a length of 1/2" (1.3 cm.), the holes may be 5/32" (0.4 cm.)-diameter holes, for example. The holes 31 are provided to reduce the rigidity of the column and thereby enable it gradually to ex-pand or "balloon" outwardly (rather than suddenly buckle) when subjected to axial loading. This is desirable in certain ap-plications since deformation of the column occurs over a longer period of time, thereby increasing the time over which an impact force is dissipated, which decreases the shock ef-fect of the impact.
Alternatively, the openings in the tubular column 9 may be in the form of a narrow slots or slits 33 extending yenerally axially o~ the column from one end of the column toward its other end (see Fig. 11). Four such slots may be provided, for example, spaced at 90 intervals around the column. It will be understood, however, that this number may vary. For a column 9 having an outside diameter of 1/2" (1.3 cm), an inside diameter of 3/8" ~0.65 cm.) and a length of 1/2" (1.3 cm.), the slits 33 may be 5/32" (0.4 cm.) long, for example.
It will be observed from the above that a shock at-tenuation system S of the present invention may be designed to meet virtually any performance requirement within a wide rangP
of requirements simply by varying the physical properties and characteristics of the columns 9. Thus, for applications in-volving relatively low impact energies, it may be desirable to use a system wherein the columns are of low-durometer (e.g., 30 - 40 on the Shore A scale) material and 1 - 1/4" (2.5 - 3.2 ... .

~20~

cm.) long with end faces cut at an angle of 14. Moreover, the columns need not be rela~ively closely spaced. On the other hand, for applications involving relatively high impact energies, it may be appropriate to use a system wherein the columns are of high-durometer (e.g., 80 - 90 on the Shore A
scale) material and about 1" (2.5 cm.) long with square-cut end faces. In such applications it is also preferable to have the columns more closely spaced in a relatively high-density formation.
While the columns 9 shown in the drawings are in the shape of r4und tubes, it will be understood that they may take other forms. For example, the columns may be of solid con-struction and have any suitable cross-sectional configuration (triangular, rectangular, elliptical, etc.) The results of comparative tests clearly reveal the superiority of the shock attenuation system S of the present invention over prior systems. In the comparative tests con-ducted, a test form weighing twelve (12~ lbs. (5.5 kg.) and having a triaxial accelerometer at its center of gravity was dropped in guided free fall from a height of sixty ~60) inches (152.4 cm.) onto the system being tested, which was supported on a rigid steel anvil covered by a layer of high-durometer polyurethane. The maximum deceleration of the head form was measured for each drop. Three systems designated A, B and C
were tested. The overall thickness of each system was 1"(2.5 cm.).
System A was constructed in accordance with the present invention and comprised a pad of the same construction as the one shown in Figs. 3 and 4. Thus, the columns 9 in each pad were tubular in shape with square-cut end faces, of 80-durometer (Shore A) urethane, and arrayed in four rows of seven columns each, with the spacing Sl between adjacent columns in each row being approximately 3/4" (1.9 cm.~, and the spacing S2 between adjacent rows being approximately 5/8"
(1.6 cm.). Each column had an outside diameter of about 1/2"

)7~5~

(1.3 cm.), an inside diameter of about 7/16~ tl.l cm.) and a length of about 1/2~ (1.3 cm.).
System B was of the type shown in the pending Cana-dian application Serial No. 375,692, filed April 16, 1981, comprising a series of horizontal tubes disposed in generally parallel side-by-side relation with their axes generally per-pendicular to the direction of impact force (i.e., generally parallel to the top horizontal surface of the anvil). The tubes were of elastically deformable (80-durometer polyure-thane) material and sufficiently closely spaced that when one deformed during impact it engaged the sides of adjacent tubes for deforming them thereby to attenuate the shock. The tubes used had inside and outside diameters of about 7/16~ (1.1 cm.J
and 1/2~ (1.3 cm.), respectively, and were covered by a 1/2~
(1.3 cm.)- thick layer of vinyl nitrile foam of the type sold under the trademark ~326 Rubatex~ by Xubatex Corporation of Bedford, Virginia, the overall thickness of the system thus being 1~ or 2.5 cm. (1/2~ of tubing and 1/2~ of ~Rubatex~ foam material).
System C was constituted by a flat sheet of 1~ (2.5 cm.)-thick polyurethane foam of the type sold under the trademark ~Poron~ by Rogers Company of Rogers, Connecticut.
Table 1 hereinbelow specifies the maximum decelera-tion (in ~peak G'sn) experienced by the test form as it was dropped on Systems A - C.

System G's It will be observed from these readings that, of the three systems, system A is by far the most effective for at-tenuating shock. Indeed, the 90-G figure achieved by system A
approaches the theoretical minimum of 60 peak G's for a stop-ping distance of 1.0" (2.5 cm.). This 60-G figure is arrived at by assuming that the kinetic energy absorbed by a system 07~

equals the work done by the system. Assuming this to be the case, the following conclusions can be drawn 1/2m y2 ~kinetic energy) = m A d (work) or A 2d where "A" equals the theoretical deceleration experienced by the head form, "m" equals the mass of the head form, "V"
equals the velocity of the head form at the time of impact, and "d" equals the maximum allowable stopping distance. The velocity of the head form at the time of impact ~"V") is equal to 2ax, where "a" equals 32 ft/sec.2 (9.8 m/sec2) and "X" equals the drop height (60 inches or 1.52 m.) of the hel-met. Using this formula, "V" equals 17.9 ft/sec. (5.46 m/sec.). Given a stopping distance ("d") of 1.0 inch ~025 m.), the theoretical deceleration ("A") equals 1928 ft/sec.2 (587.7 m/sec.2) or approximately 60 G's. Thus under the test conditions described above, system A of the present in-vention was 66 percent as efficient as the "idea]" system;
system B was 36 percent as efficient; and system C was 38 per-cent as efficient.
Additional tes~s conducted on a helmet with a shockattenuation system of the present invention also establish that the helmet retains its shock-attenuating capabilities even after repeated impacts. These tests were conducted in accordance with the ANSI Z~0.1 (1973) test method reco~niæed by the Department of Transportation for use in testing motor vehicle helmets. Pursuant to the test method, a helmet having a shock attenuation system S of this invention`is placed on a head form having a triaxial accelerometer at its center of gravity and is dropped in guided free fall from a height of 72" (182.9 cm.) onto a rigid flat anvil, or from a height of 54" (137.2 cm.) onto a hemispherical anvil. The maximum de-celeration of the head form is then measured for each drop.
To meet the Department of Transportativn standards, the magni-tude of deceleration cannot exceed 400 G's at any time. Nor ~2079Sl 1~

can it exceed 200 G's for more than 2 milliseconds (0.002 sec-onds) or 150 G's for more than 4 milliseconds (0.004 seconds).
In a first series of tests, a helmet having a shell of a resin-impregnated fiberglas material was equipped with six pads 7 positioned as shown in ~igs. 1 and 2. The two crown pads measured 5-3/4" (14.6 cm.) long, 3-1/2" (8.9 cm.) wide and about 3/4" (1.9 cm.) thick. The front, rear and side pads measured 6 1/4" (15.9 cm.) long by 3-3/4" (9.5 cm.) wide by about 3/4" (1.9 cm.) thick. The columns 9 in each pad were tubular in shape with square-cut end faces, of 80-durometer ~Shore A~ urethane, and arrayed in four rows of seven columns each, with the spacing Sl between adjacent columns in each row being approximately 3/4" (1.9 cm.), and the spacing S2 between adjacent rows being approximately 5/8" (1.6 cm.). Each column had an outside diameter of about 1/2" (1.3 cm.), an inside diameter of about 7/16" (1.1 cm.), and a length of about 1/2"
(1.3 cm.). Equipped with these pads, the helmet was dropped eleven times from a height of 72" (182.9 cm.) onto a flat rigid anvil, with two of the drops being on a side of the hel-met, two on the front of the helmet, three on the rear of the helmet and four on the top of the helmet. The Department of Transportation standards were met in every instance. The same helmet was also dropped four addi~ional times from a height of 54" (137.2 cm.) onto a rigid hemispherical anvil, with two of the drops being on a side of the helmet and two drops on the front of the helmet. The results also met the Department of Transportation standards, again demonstrating the effective-ness of the present invention to attenuate shock even after repeated impacts.
In a second series of tests, the six pads described above were replaced by six smaller pads, the two crown pads measuring 4-3/4" (12.1 cm~) long, 2-1/2" (6.4 cm.) wide and

3/4" (1.9 cm.) thick and the frontO rear and side pads measur-ing 5-1/4" (13.3 cm.) long, 2-1/2" (6~4 cm.) wide and 3/4"
(1.9 cm.) thick. The columns 9 in the pads were identical in ~20~S~

size, shape and composition to those used in the first series of tests. The columns were arrayed in Eour rows of six col~
umns each, with the spacing between adjacent columns in each row being approximately 5/8" (1.6 cm.), and the spacing S2 between adjacent rows being approximately 5/8" (1.6 cm.).
Equipped with these pads, the helmet was dropped eleven times from a height of 72" tl82.9 cm.) onto a flat rigid anvil, with two of the drops being on a side of the helmet, three drops on the front of the helmet, two drops on the rear of the helmet and four drops on the top of the helmet. As in the first series of tests, the standards of the Department of Transpor-tation were met in every instance, thereby again establishing the effectiveness of the helmet in attenuating shock even after repeated impacts.
A shock attenuation system S of the present inven-tion has particular application to protective headgear, such as aviation, racing and football helmets. Such headgear must be able to effectively attenuate the shock resulting from relatively large impact forces, and yet cannot be excessively bulky or heavy, which would unduly restrict mobility. A sys-tem may readily be designed to meet these requirements. Thus, to minimize bulk and weight, relatively short columns should be used. And to maximize the ability of the system to attenu-ate shock from large impact forces, the columns should be closely spaced and of a high-durometer material, such as 80-durometer urethane, with square-cut ends.
A system S of the present invention is suited for virtually any application involving shock attenuation. Thus it may be incorporated in running shoes, body armor and car bumpers, or example. Indeed, system S may be used in any situation where a person or thing is to be protected from the ; shock of a collision, regardless of whether that person or thing is stationary or moving during the collision. Where ex-ceptionally large impact forces are involved, as in automobile collision applications, a series of systems S (such as pads 7) s~

may be stacked one on another to achieve the necessary shock attenuation. The arrangement and spatial orientation of the pads 7 with respect to one another will vary from application to application depending on the circumstances.
Fig. 12 illustrates a helmet, generally designated 37, incorporating an alternative shock attenuation system sl of the present invention~ System Sl comprises a plurality of shock-attenuating modules each designated 39, positioned on the inside of the shell 41 of helmet 37 at locations generally correspvnding to the locations of pads 7 in headgear 1, and an inner liner, generally designated 43, of cushioning material engageable with the head of a person wearing the helmet 37, modules 39 being disposed between the shell of the helmet and the liner.
Each module 39 comprises a relatively thin ~lat rec-tangular carrier member or sheet 45 (constituting support means) carrying an array of shock-attenuating columns 47 (com-~- parable to column 9 described above) which project from one face of the carrier member toward the inside surface of the shell, the outer tfree) ends of the columns being disposed closely adjacent the shell. The carrier member is flexible which enables it to bend ~o conform to the curvature of the shell so that the axes of the columns extend generally perpen-dicularly with respect to the shell. The carrier member and its respective columns are preferably integrally molded from a synthetic resin material.
The physical properties and configurations of col-umns 47~may vary according to the principles set forth above in regard to the columns 9 of shock attenuation system S. In the embodiment shown, columns 47 are round tubular members, each having four holes 49 therein spaced at 90 intervals around the tube approximately in the central radial plane o~
the tube. However, columns 47 may take other forms and shapes as discussed above with respect to columns 9.

lZ0795~L

The liner 43 comprises a layer 51 of flexible resil-ient relatively slow-recovery foam material (such as an open-cell urethane foam of the type sold under the trademark "Sensafoam" and which is commercially available from Wilshire Foam Products Inc. of Los Angeles, California) encapsulated in a sheath 53 of flexible resilient relatively rapid-recovery foam material (such as a closed-cell polyethylene foam of ~he type sold under the trademark "Microfoam" and which is com-mercially available from Wilshire ~oam Products Inc. of Los ~ngeles, California). The liner is deformable so ~hat it readily conforms to the modules 39 and to the inside surface of the shell in the areas between the modules, and to the head of a person wearing the helmet. In this latter regard, the liner should be sized for a relatively snug fit on the head.
By way of example, the carrier member 45 of each module 39 of system sl may be 4 3/8" ~12.38 cm.) long and 2 1/2" (6~35 cm.) wide and carry an array of four rows of col-umns of seven columns each~ Each column may be 1/2" ~1.3 cm.) long and have an outside diameter of 1/2'l (1.3 cm.). With respect to the liner 43, layer 51 may be 1/2" (1.3 cm.) thick, the inner (head-engaging) ply of sheath 53 may be 1/4" (0.6 cm.) thick, and the outer ply of the sheath may be 1/8" (0.3 cm.) thick.
In view of the above, it will be seen that the several objects of the invention are achieved and other advantageous results attained.
As various changes could be made in the above constructions without departing from the scope of the invention, it is intended that all matter contained in the above description or shown in the accompanying drawings shall be interpreted as illustrative and not in a limiting sense.

Claims (30)

The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows:

1. Protective headgear comprising an outer shell of substantially rigid material adapted to be worn on the head, a plurality of shock-attenuating modules on the inside of the shell, and an inner liner of flexible resilient relatively slow-recovery cushioning material, portions of said inner liner being spaced from the shell to form pockets, said modules being disposed in said pockets between the shell and the liner thereby to locate the modules in fixed predetermined positions with respect to the inside of the shell, each module comprising a multiplicity of spaced-apart generally squat tubular columns of resilient synthetic resin material disposed with their axes generally at right angles to the shell, each column being constituted by an integrally formed one-piece tubular member having a slenderness ratio of less than 3.0, said slenderness ratio being the ratio of column length to column diameter, said columns being so dimensioned and con-figured that, when subjected to an axial impact force of pre-determined magnitude, the walls of the columns are adapted resiliently to deform for attenuating the shock resulting from said impact force, said columns then being adapted resiliently to return substantially to their underformed shape.

2. A shock attenuation system as set forth in claim 1 wherein each module further comprises a relatively thin flexible carrier sheet having said columns on one face thereof extending with their axes generally at right angles to the carrier sheet, said columns and carrier sheet being integrally molded of resilient synthetic resin material.

3. A shock attenuation system as set forth in claim 1 wherein the walls of said tubular columns are formed resili-ently to buckle in irregular and random fashion when subjected to an axial impact force of predetermined magnitude.

4. A shock attenuation system as set forth in claim 1 wherein each column has a slenderness ratio of about 1Ø

5. A shock attenuation system as set forth in claim 1 wherein said columns are made of a material having a Shore A
durometer in the range of 25-100.

6. A shock attenuation system as set forth in claim 1 wherein the end faces of the columns are angle cut, lying in planes which extend obliquely with respect to the central axes of the columns.

7. A shock attenuation system as set forth in claim 1 wherein each tubular member has a side wall with a plurality of openings therein.

8. A shock attenuation system as set forth in claim 7 wherein said openings are spaced circumferentially around the tubular member.

9. A shock attenuation system as set forth in claim 8 wherein said tubular member is round in shape and said open-ings are in the form of holes in the side wall of the member.

10. A shock attenuation system as set forth in claim 9 wherein said holes lie substantially in the central radial plane of the tubular member.

11. A shock attenuation system as set forth in claim 8 wherein said openings are in the form of slits in said side wall extending generally axially of the tubular member from one of its ends toward its other end.

12. Protective headgear comprising;

an outer shell of substantially rigid material adapted to be worn on the head;

a shock attenuation system on the inside of the shell com-prising pad means adapted for engagement with the head, said pad means comprising a relatively thin flexible carrier sheet having a multiplicity of spaced-apart generally squat tubular columns on one face thereof extending generally at right angles to the sheet, said columns and carrier sheet being integrally molded of a substantially resilient synthetic resin material with each column being constituted by an integrally formed one-piece tubular member, and a layer of cushioning material on said one face of the carrier sheet occupying the spaces between said columns, the interiors of said columns being open and free of said cushioning material, said columns being so dimensioned and configured that, when subjected to an axial impact load of predetermined maginitude, the walls of the columns are adapted resiliently to buckle in irregular and random fashion for attenuating the shock resulting from said impact load, said columns then being adapted resiliently to return substantially to their undeformed shape; and means for fastening said pad means to the inside surface of said shell with said one face of said carrier facing the shell and with said columns generally at right angles to the shell.

13. Protective apparatus as set forth in claim 12 wherein said columns are generally short and squat with a slenderness ratio of about 1Ø

14. Protective apparatus as set forth in claim 13 wherein said columns are generally of uniform diameter along their entire lengths.

15. Protective apparatus as set forth in claim 14 wherein said columns are made of a material having a Shore A
durometer in the range of 50-90.

16. Protective apparatus as set forth in claim 12 wherein said fastening means comprises interengageable means on said pad means and said shell for releasably fastening said pad means to the shell.

17. Protective apparatus as set forth in claim 16 wherein said pad means comprises a plurality of separate pads disposed on the inside of the shell.

18. Protective apparatus comprising:

an outer shell of substantially rigid material adapted to be positioned on an object to be protected, such as the head;

a shock attenuation system on the inside of the shell com-prising pad means adapted for engagement with said object, said pad means comprising a multiplicity of spaced-apart resilient columns each constituted by a hollow integrally formed one-piece tubular member of resilient synthetic resin material having a slenderness ratio of less than 3.0, the slenderness ratio being the ratio of column length to column diameter, said columns being so dimensioned and configured that, when subjected to an axial impact load of predetermined magnitude, the walls of the columns are adapted resiliently to buckle in irregular and random fashion for attenuating the shock resulting from said impact load, said columns then being adapted resiliently to return substantially to their unde-formed shape; and means for fastening said pad means to the inside surface of said shell with said columns generally at right angles to the shell.

19, Protective apparatus as set forth in claim 18 wherein said pad means comprises at least one pad comprising a relatively thin flexible carrier sheet having said columns on one face thereof extending with their axes generally at right angles to the carrier sheet, said columns and carrier sheet being integrally molded of a resilient sythetic resin material, said pad being adapted to be mounted on the inside surface of the shell with said one face of the carrier sheet facing the shell.

20. Protective apparatus as set forth in claim 19 wherein said columns are generally short and squat with a slenderness ratio of about 1Ø

21. Protective apparatus as set forth in claim 18 wherein said pad means further comprises a layer of cushioning material occupying the spaces between the columns and having a thickness generally corresponding to the height of the columns.

22. Protective apparatus as set forth in claim 21 wherein said shell comprises a helmet adapted to be worn on the head.

23. Protective apparatus as set forth in claim 22 wherein said pad means comprises a plurality of separate pads disposed on the inside of said helmet, each pad comprising a relatively thin flexible carrier sheet having said columns on one face thereof extending with their axes generally at right angles to the carrier sheet, said columns and carrier sheet being integrally molded of a resilient sythetic resin mater-ial, said pad being adapted to be mounted on the inside sur-face of the shell with said one face of the carrier sheet facing the shell and with said layer of cushioning material between the carrier sheet and the shell.

24. Protective apparatus as set forth in claim 23 wherein said columns are generally short and squat with a slenderness ratio of about 1Ø

25. Protective apparatus as set forth in claim 24 wherein said columns are generally of uniform diameter along their entire lengths.

26. Protective apparatus as set forth in claim 25 wherein said columns are made of a material having a Shore A
durometer in the range of 50-90.

27. Protective apparatus as set forth in claim 18 wherein said fastening means comprises interengageable means on said pad means and said shell for releasably fastening said pad means to the shell.

28. Protective apparatus as set forth in claim 18 wherein said tubular member has a side wall with a plurality of openings therein.

29. Protective apparatus as set forth in claim 28 wherein said openings are in the form of holes spaced cir-cumferentially around the tubular member.

30. Protective apparatus as set forth in claim 28 wherein said openings are in the form of slits in said side wall extending generally axially of the tubular member from one of its ends toward its other end.