Helmet

Information

  • Patent Grant
  • 11641904
  • Patent Number
    11,641,904
  • Date Filed
    Wednesday, November 9, 2022
    a year ago
  • Date Issued
    Tuesday, May 9, 2023
    a year ago
Abstract
A helmet that includes a subliner shell comprised of a hard impact resistant material. The shell has inner and outer surfaces. A subliner element having a first foam pad having a top surface and a bottom surface. The top surface is attached to the inner surface of the shell. A second foam pad is constructed of an energy absorbing viscoelastic foam material that is radially partitioned into individual segments. The segments are nested with respect to each other such that the nested segments have side surfaces in slidable direct contacting engagement with side surfaces of adjacent nested segments. The second foam pad has a top surface attached to the bottom surface of the first foam pad. A third foam pad has a top surface and a bottom surface, with the top surface of the third foam pad being attached to the bottom surface of the second foam pad.
Description
BACKGROUND OF THE INVENTION

The present disclosure generally relates to a helmet whose purpose is to protect a wearer's head during a head impact. Extending radially outward from the wearer's head, the helmet may consist of one or multiple liner portions and one or multiple shell portions. Either way, there is typically a liner portion in contact with the wearer's head initially or during impact, that liner portion being herein defined as the subliner. The subliner may be comprised of individual subliner elements. The subliner is typically attached to an inner shell portion, the term inner having been added to unambiguously differentiate it from an outer shell portion in the case of a helmet with multiple shell portions. In helmets having just a single liner portion and a single shell portion, the liner portion would be the same as the subliner and the shell portion would be the same as the inner shell portion. In some helmets (typically hockey helmets) the inner shell portion may consist of individual shell segments. The subliner and inner shell portion together are herein defined as the helmet subliner system, and the present disclosure comprises an improved helmet subliner system, and an improved outer liner portion in the case of multiple shell helmets, to better protect the wearer from sustaining concussions and other head injuries.


Especially in multiple liner, multiple shell helmets, the subliner, as defined herein has been used primarily for obtaining the best fit and best comfort for the wearer. But as will be shown in this specification, the subliner, and more generally the subliner system may also be used to substantially improve the head protection performance of the helmet. The disclosure recognizes and takes advantage of the fact that all the forces that are applied to the wearer's head during a head impact are preferably applied through the subliner and its elements.


Recent postmortem brain investigations have found a high instance of chronic traumatic encephalopathy, or CTE, in the donated brains of deceased NFL football players, many of whom had suffered debilitating symptoms during their lifetimes, including unexplained rage, extreme mood swings, and substantial cognitive degeneration, all of which may have begun years after their football playing ended. Current research shows that CTE can almost always be traced back to long term repetitive head impacts which may include both concussive and sub-concussive impacts. It is believed those impacts would have been characterized by a high level of head angular acceleration, sometimes called rotational acceleration. The improved helmet subliner system configuration of the present disclosure is specifically designed to help reduce the level of head angular acceleration during a head impact.


The present disclosure generally relates to a helmet whose purpose is to protect a wearer's head during an impact. More specifically, it relates to an improved version of the helmet disclosed in U.S. Pat. No. 10,869,520, the contents of which are hereby incorporated by reference in their entirety. U.S. Pat. No. 10,869,520 discloses a subliner element to be located at the top of the head when the helmet is worn. The term subliner refers to liner elements that may come in contact with a wearer's head. The top subliner element is comprised of an energy absorbing viscoelastic foam material capable of exhibiting a compressive stress of at least 50 psi for a dynamic compression of 50%, and the element has a substantially flat lower surface which is also substantially tangent to the surface of the wearer's head beneath it when the helmet is worn. That latter requirement is to enable the liner element to slide by the wearer's head in the event of a horizontal impact while imparting little or no horizontal force to the wearer's head and to thereby substantially reduce the resulting angular acceleration (the main cause of concussions) about a horizontal axis oriented perpendicular to the impact direction. The design concept works well, but could function better where the mostly horizontal impact is accompanied by a substantial downwardly directed impact force. In that case the lower surface of the foam element may be pushed downward to at least partially conform with the curved top surface of the wearer's head, thereby precluding the element from sliding by the wearer's head without exerting a substantial horizontal force as was the desired purpose.


The present invention describes three alternative, structurally different designs of the top subliner element to result in, in the case of a significant horizontal impact in the presence of a significant downwardly directed impact force, a substantially lessened horizontal force being applied to the wearer's head at the place where it contacts the top subliner element.


SUMMARY OF THE INVENTION

Briefly stated, the present disclosure is directed to a helmet adapted to be worn on a head of a wearer. The head has a top area centered about a top of the wearer's head encompassing approximately 0.44 to 7 square inches. The helmet includes a subliner shell comprised of a hard impact resistant material. The shell has inner and outer surfaces. The shell is adapted to surround at least a portion of the cranial part of the wearer's head with the inner surface of the shell being spaced from the wearer's head at an initial pre-impact relative position when the helmet is worn. At least one subliner element extends from the inner surface of the shell at a location such that the subliner element is adapted to be aligned with the top area when the helmet is worn. The at least one subliner element includes a first foam pad constructed of an energy absorbing viscoelastic foam material having a top surface and a bottom surface. The top surface is attached to the inner surface of the shell. A second foam pad is constructed of an energy absorbing viscoelastic foam material that is radially partitioned into individual and independent segments. The independent segments are nested with respect to each other such that the nested segments have side surfaces in slidable direct contacting engagement with side surfaces of adjacent nested segments. The second foam pad has a top surface attached to the bottom surface of the first foam pad. A third foam pad is constructed of an energy absorbing viscoelastic foam material having a top surface and a bottom surface, with the top surface of the third foam pad being attached to the bottom surface of the second foam pad. The bottom surface of the third foam pad is a substantially flat surface which is substantially tangent to the surface of the wearer's head beneath it when the helmet is worn.


Briefly stated, in another aspect the present disclosure is directed to a helmet adapted to be worn on a head of a wearer. The head has a pair of eyebrows, a pair of ears and an annular headband shaped area encircling the wearer's head. The headband shaped area is approximately 0.75 to 1.25 inches wide and has a lower edge defining a plane positioned approximately 0.5 to 1.5 inches above the eyebrows and approximately 0.25 to 0.75 inches above an upper junction of the ears and the wearer's head. A top area is centered about a top of the wearer's head and encompasses approximately 0.44 to 7 square inches. A middle area of the head is defined between the headband area and the top area. The helmet includes a subliner shell comprised of a hard impact resistant material. The shell has inner and outer surfaces and is adapted to surround at least a portion of the cranial part of the wearer's head with the inner surface of the shell being spaced from the wearer's head at an initial pre-impact relative position when the helmet is worn. A subliner, at least a part of which is adapted to be in contact with the wearer's head when the helmet is worn prior to an impact and during an impact, includes a plurality of a first type of subliner elements extending from the inner surface of the shell at a location such that the first type of subliner elements are adapted to be aligned with the headband area when the helmet is worn. The first type of subliner elements are constructed of an energy absorbing viscoelastic foam material and are radially partitioned into individual and independent segments. The independent segments are nested with respect to each other with double-sided nano tape positioned therebetween such that the nested segments have side surfaces in direct contacting engagement with the nano tape. At least one of a second type of subliner element extends from the inner surface of the shell at a location such that the at least one of the second type of subliner element is adapted to be aligned with the middle area when the helmet is worn. The at least one of the second type of subliner element is constructed of a foam material. A third type of subliner element extends from the inner surface of the shell at a location such that the third type of subliner element is adapted to be aligned with the top area when the helmet is worn. The third type of subliner element includes a first foam pad constructed of an energy absorbing viscoelastic foam material having a top surface and a bottom surface. The top surface is attached to the inner surface of the shell. A second foam pad is constructed of an energy absorbing viscoelastic foam material and is radially partitioned into individual and independent segments. The independent segments are nested with respect to each other such that the nested segments have side surfaces in slidable direct contacting engagement with side surfaces of adjacent nested segments. The second foam pad has a top surface attached to the bottom surface of the first foam pad. A third foam pad is constructed of an energy absorbing viscoelastic foam material having a top surface and a bottom surface, The top surface of the third foam pad being attached to the bottom surface of the second foam pad. The bottom surface of the third foam pad is a substantially flat surface which is substantially tangent to the surface of the wearer's head beneath it when the helmet is worn. The at least one of the second type of subliner element is positioned between the plurality of the first type of subliner elements and the third type of subliner element.


Briefly stated, in another aspect the present disclosure is directed a helmet adapted to be worn on a head of a wearer. The head has a top area centered about a top of the wearer's head encompassing approximately 0.44 to 7 square inches. The helmet includes a subliner shell comprised of a hard impact resistant material. The shell has inner and outer surfaces. The shell is adapted to surround at least a portion of the cranial part of the wearer's head with the inner surface of the shell being spaced from the wearer's head at an initial pre-impact relative position when the helmet is worn. At least one subliner element extends from the inner surface of the shell at a location such that the subliner element is adapted to be aligned with the top area when the helmet is worn. The at least one subliner element extending from the inner surface of the shell at a location such that the subliner element is adapted to be aligned with the top area when the helmet is worn. The at least one subliner element includes a first foam pad constructed of an energy absorbing viscoelastic foam material having a top surface and a bottom surface, with the top surface being attached to the inner surface of the shell. The bottom surface is generally planar and has a first fluoropolymer coating adhered thereto. A second foam pad is constructed of an energy absorbing viscoelastic foam material having a top surface and a bottom surface. The top surface of the second foam pad is generally planar and has a second fluoropolymer coating adhered thereto. The first and second foam pads are positioned with the first and second fluoropolymer coatings in sliding facing engagement. The bottom surface of the second foam pad is a substantially flat surface which is substantially tangent to the surface of the wearer's head beneath it when the helmet is worn.


Briefly stated, in another aspect the present disclosure is directed to a helmet adapted to be worn on a head of a wearer. The head has a pair of eyebrows, a pair of ears and an annular headband shaped area encircling the wearer's head. The headband shaped area is approximately 0.75 to 1.25 inches wide and has a lower edge defining a plane positioned approximately 0.5 to 1.5 inches above the eyebrows and approximately 0.25 to 0.75 inches above an upper junction of the ears and the wearer's head. A top area is centered about a top of the wearer's head and encompasses approximately 0.44 to 7 square inches. A middle area of the head is defined between the headband area and the top area. The helmet includes a subliner shell comprised of a hard impact resistant material. The shell has inner and outer surfaces and is adapted to surround at least a portion of the cranial part of the wearer's head with the inner surface of the shell being spaced from the wearer's head at an initial pre-impact relative position when the helmet is worn. A subliner, at least a part of which is adapted to be in contact with the wearer's head when the helmet is worn prior to an impact and during an impact, includes a plurality of a first type of subliner elements extending from the inner surface of the shell at a location such that the first type of subliner elements are adapted to be aligned with the headband area when the helmet is worn. The first type of subliner elements is constructed of an energy absorbing viscoelastic foam material and is radially partitioned into individual and independent segments. The independent segments are nested with respect to each other with double-sided nano tape positioned therebetween such that the nested segments have side surfaces in direct contacting engagement with the nano tape. At least one of a second type of subliner element extends from the inner surface of the shell at a location such that the at least one of the second type of subliner element is adapted to be aligned with the middle area when the helmet is worn. The at least one of the second type of subliner element is constructed of a foam material. A third type of subliner element extends from the inner surface of the shell at a location such that the third type of subliner element is adapted to be aligned with the top area when the helmet is worn. The third type of subliner element includes a first foam pad constructed of an energy absorbing viscoelastic foam material having a top surface and a bottom surface. The top surface being attached to the inner surface of the shell. The bottom surface is generally planar and has a first fluoropolymer coating adhered thereto. A second foam pad is constructed of an energy absorbing viscoelastic foam material having a top surface and a bottom surface. The top surface of the second foam pad is generally planar and has a second fluoropolymer coating adhered thereto. The first and second foam pads being positioned with the first and second fluoropolymer coatings being in sliding facing engagement. The bottom surface of the second foam pad is a substantially flat surface which is substantially tangent to the surface of the wearer's head beneath it when the helmet is worn. The at least one of the second type of subliner element is positioned between the plurality of the first type of subliner elements and the third type of subliner element.





BRIEF DESCRIPTION OF THE DRAWINGS

The foregoing summary, as well as the following detailed analysis of the physical principles and detailed descriptions of the preferred embodiments will be better understood when read in conjunction with the appended drawings. For the purpose of illustrating the disclosure, particular arrangements and methodologies of preferred embodiments are shown in the drawings. It should be understood, however, that the disclosure is not limited to the precise arrangements or instrumentalities shown or the methodologies of the detailed description. In the drawings:



FIG. 1 is a perspective side view of a wearer's head with defined areas, planes, and points in accordance with the present disclosure;



FIG. 2 is a perspective upper side view of a wearer's head showing the three types of subliner elements as they would be located in their respective designated areas, in accordance with a first embodiment of the present disclosure;



FIG. 2A is a perspective upper side view of a wearer's head showing the three types of subliner elements as they would be located in their respective designated areas, in accordance with a second embodiment of the present disclosure;



FIG. 3 is an exploded perspective view of a partitioned subliner element and its attachment to a portion of the inner shell, showing the portion of the inner shell, the hook part and the loop part of a hook and loop fastener mechanism, the partitioned segments, and an optional covering;



FIG. 4 is cross-sectional side view at the midsagittal plane of a wearer's head, showing the subliner elements of FIG. 2 and the inner shell to which they are attached forming a subliner system in accordance with the present disclosure;



FIG. 4A is an exploded top perspective view of a first embodiment of a third type of subliner element in accordance with the present disclosure;



FIG. 4B is a top perspective view partially in cross section of a second embodiment of a third type of subliner element in accordance with the present disclosure;



FIG. 4C is a top perspective view partially in cross section of a third embodiment of a third type of subliner element in accordance with the present disclosure;



FIG. 5 is a left side elevational view showing the inner shell of FIG. 4 positioned on a wearer's head;



FIG. 6 is a cross-sectional side view at the midsagittal plane of a wearer's head, of a two liner, two shell helmet embodiment, where the subliner elements and the inner shell shown in FIG. 4 and FIG. 5 make up a subliner system, to which is added a second liner and an outer shell, the second liner being attached to both the inner shell and the outer shell in accordance with the present disclosure;



FIG. 7a illustrates, in top plan view, a first partitioning arrangement for the second liner elements of FIG. 6.



FIG. 7b is a cross-sectional view of FIG. 7a taken along line 7b-7b.



FIG. 8a illustrates, in top plan view, a second partitioning arrangement for the second liner elements of FIG. 6.



FIG. 8b is a cross-sectional view of FIG. 8a taken along line 8b-8b.



FIG. 9a illustrates, in top plan view, a third partitioning arrangement for the second liner elements of FIG. 6.



FIG. 9b is a cross-sectional view of FIG. 9a taken along line 9b-9b.



FIG. 10a illustrates, in top plan view, a fourth partitioning arrangement for the second liner elements of FIG. 6.



FIG. 10b is a cross-sectional view of FIG. 10a taken along line 10b-10b.



FIG. 11a illustrates, in top plan view, a fifth partitioning arrangement for the second liner elements of FIG. 6.



FIG. 11b is a cross-sectional view of FIG. 11a taken along line 11b-11b.



FIG. 12a illustrates, in top plan view, a sixth partitioning arrangement for the second liner elements of FIG. 6.



FIG. 12b is a cross-sectional view of FIG. 12a taken along line 12b-12b.



FIG. 13a illustrates, in top plan view, a seventh partitioning arrangement for the second liner elements of FIG. 6.



FIG. 13b is a cross-sectional view of FIG. 13a taken along line 13b-13b.



FIG. 14a illustrates, in top plan view, an eighth partitioning arrangement for the second liner elements of FIG. 6.



FIG. 14b is a cross-sectional view of FIG. 14a taken along line 14b-14b.



FIG. 15a illustrates, in top plan view, a ninth partitioning arrangement for the second liner elements of FIG. 6.



FIG. 15b is a cross-sectional view of FIG. 15a taken along line 15b-15b.



FIG. 16 is a left side elevational view showing the outer shell of FIG. 6 positioned on a wearer's head; and



FIG. 17 is a left side elevational view of a wearer's head showing a face guard attached to the outer shell of FIG. 16, and a chin strap positioned on the wearer's chin and attached to the inner shell of FIG. 5.





DETAILED DESCRIPTION OF THE INVENTION

Certain terminology is used in the following description for convenience only and is not limiting. The words “lower,” “bottom,” “upper” and “top” designate directions in the drawings to which reference is made. The words “inwardly,” “outwardly,” “upwardly” and “downwardly” refer to directions toward and away from, respectively, the geometric center of the helmet, and designated parts thereof, in accordance with the present disclosure. Unless specifically set forth herein, the terms “a,” “an” and “the” are not limited to one element, but instead should be read as meaning “at least one.” The terminology includes the words noted above, derivatives thereof and words of similar import. The terms “angular acceleration” and “rotational acceleration” should be taken as synonymous from a force vector perspective. Similarly, the words “acceleration” and “deceleration” should also be taken as synonymous from a force vector perspective. It should also be understood that the terms “about,” “approximately,” “generally,” “substantially” and like terms, used herein when referring to a dimension or characteristic of a component of the disclosure, indicate that the described dimension/characteristic is not a strict boundary or parameter and does not exclude minor variations therefrom that are functionally similar. At a minimum, such references that include a numerical parameter would include variations that, using mathematical and industrial principles accepted in the art (e.g., rounding, measurement or other systematic errors, manufacturing tolerances, etc.), would not vary the least significant digit.


Referring now to FIGS. 1, 2 and 4, to best understand the configuration of the helmet subliner system or subliner 10, which is a subject of this disclosure, it will be useful to first define certain areas of a potential wearer's head 12 which could come in contact with various types of subliner elements of the helmet 14. In this regard, all the following will be defined: first area A, first plane A1, second plane B1, point b, second area B, and third area C.



FIG. 1 is a perspective side view of a wearer's head 12 having a pair of eyebrows 26 (only one is shown) and a pair of ears 28 (only one is shown). The head 12 includes a first area A, first plane A1, second plane B1, point b, second area B, and third area C. First area A is an annular headband shaped area encircling the wearer's head 12. The first or headband shaped area A being approximately 0.75 to 1.25 inches wide, and preferably approximately 1.0 inch wide, and having a lower edge defining a plane positioned approximately 0.5 to 1.5 inches, and preferably approximately 1.0 inch, above the eyebrows 26 and approximately 0.25 to 0.75 inches, and preferably approximately 0.5 inches, above a location where the ears 28 join the wearer's head 12 at the top or, stated differently, an upper junction of the ears 28 and the wearer's head 12. The first plane A1 is a hypothetical plane defined by the lower edge of first area A. Picture second plane B1 as a lower cover of an imaginary hard cover book being balanced horizontally atop the wearer's head 12 while the wearer's head 12 is maintained in an upright position, tilted neither right nor left, nor forward nor backward and where point b is approximately the center of the contact area between the lower cover of the imaginary book and the wearer's head 12. Notice that first plane A1 is tilted upward in the forward direction (the direction toward the face of the wearer) relative to second plane B. In FIG. 1, the second plane B1 is shown as transparent so that the contact area with the wearer's head 12, point b, is apparent. The second or top area B is formed by a planar projection of an approximate 2-inch diameter circle (not shown) formed in the second plane B1 centered about point b onto the wearer's head. That is, the second area B is generally circular and is centered about a top of the wearer's head 12 and extends 0.75 to 3 inches, and preferably 2 inches, in diameter in all lateral directions. As will be discussed, the second area B needn't be 2 inches in diameter, nor even circular. That is, the second area B can range from 0.44 to 7 square inches, or preferably 3.14 square inches. The third or middle area C is the area on the wearer's head 12 between first area A and second area B.


Referring again to FIGS. 1, 2 and 4 and as will be described in detail in subsequent sections of the specification, subliner elements of a first type 16 are to be located in the first area A; subliner elements of a second type 18 are to be utilized in third area C, and a subliner element of a third type 20 is to be used in second area B. Each type of subliner element 16, 18, 20 has its own specific physical characteristics in accordance with the purpose of the disclosure which is to be able to reduce the level of head angular acceleration imparted to a wearer's head 12 during a head impact, regardless of the location or direction of the impact. Each of the subliner elements 16, 18, 20 is to be attached to an inner surface 22 of the inner shell 24 of the helmet 14, preferably utilizing a commonly employed hook and loop type of fastener arrangement which allows for the simple assembly of, and changeout of, individual subliner elements 16, 18, 20 during a fitting process, with each subliner element 16, 18, 20 being positioned and sized in its thickness direction to best fit the size and shape of a wearer's head 12. It will be appreciated by one skilled in the art, that other fastening elements could be used to releasably secure the subliner elements 16, 18, 20 to the inner surface 22 of the inner shell 24 of the helmet 14, such as a releasable adhesive (not shown).



FIG. 2 is a perspective upper side view of a wearer's head 12 showing the first, second and third types of subliner elements 16, 18, 20 as they would be located in their respective designated areas shown in FIG. 1, in accordance with a first embodiment of the present disclosure. The individual subliner elements 16, 18, 20 are not attached to the wearer's head 12 (as could be falsely assumed from FIG. 2) but are merely illustrated in the figure where they would be located with respect to the wearer's head 12 when the helmet 14 is worn. Typically, they would be attached to the inner surface 22 of the inner shell 24 of the helmet 14, as shown in FIG. 4, preferably utilizing a commonly employed hook and loop type of fastener arrangement, describe below. The upper side viewpoint enables a fuller view of a first embodiment of a subliner element of the third type 20, which is preferably disc or oval shaped, oriented generally in the second plane B1, and is centered about point b at the top, or crown, of the head 12. Subliner element of the third type 20 has a flat (or nearly flat), horizontal (or nearly horizontal), lower surface 20a which may be either initially in contact with the wearer's head 12 or slightly spaced therefrom but may come into contact with the wearer's head 12 during an impact. Subliner element of the third type 20 is shown here as a circular disc having a two-inch diameter to accommodate any misalignment of the center of the disc with the initial actual point of contact with a wearer's head 12 and to accommodate lateral displacements between the inner shell 24 and the wearer's head 12 during an impact. In general, the subliner element of the third type 20 need not be circular, but it may be of any suitable contiguous shape typically having that approximate area or greater. The important thing is that its lower surface 20a be of sufficient area to enable the accommodations described above, and that it be predominately flat and horizontal such that it is substantially tangent to the surface of the wearer's head 12 beneath it when the helmet 14 is worn.


To be able to appreciate why the lower surface 20a of subliner element of the third type 20 is preferred to be flat and horizontal, one may perform a simple experiment with one's own hand and one's own head. First, using one's hand, firmly cup the top of one's head. Then while still firmly cupping the head, forcefully move the cupping hand's forearm forward and backward, and side to side, and notice how the head is forced into violent motion likely involving significant head angular accelerations. Next, repeat the experiment while the hand is held flat and horizontal. The result:


almost no forced motion of the head, and thus no head angular acceleration.


Referring now to FIGS. 2, 4 and 4A, the subliner element of the third type 20 is comprised of a first foam pad 110 constructed of an energy absorbing viscoelastic foam material having a top surface 110a and a bottom surface 110b, the top surface 110a being attached to the inner surface 22 of the shell 24. The first foam pad 110 is generally disk shaped and preferably made of relatively stiff, very energy absorbent, viscoelastic foam material, capable of exhibiting a compressive stress of 20 psi for a static compression of 50% and at least 50 psi for a dynamic impact type compression of 50%, for example a vinyl nitrile foam such as IMPAX®, VN600, VN740, or VN1000 by Dertex Corporation, or a polyurethane foam such as LAST-A-FOAM®, FP 8015 by General Plastics Manufacturing Company.


The subliner element of the third type 20 further includes a second foam pad 112 being constructed of an energy absorbing viscoelastic foam material that is the same as the material in the first foam pad 110. The second foam pad 112 is radially partitioned into individual and independent segments 114. The independent segments 114 are nested with respect to each other such that the nested segments 114 have side surfaces 116 in slidable direct contacting engagement with side surfaces 116 of adjacent nested segments 114. The second foam pad 112 has a top surface 112a attached to the bottom surface 110b of the first foam pad 110.


The segments 114 are in the form of a plurality of side-by-side, vertically oriented, slender foam columns or segments 114 that have substantially less sidewise stiffness than a solid foam portion. The resulting sidewise stiffness is lessened if the columns 114 are made longer, or made more slender even though that results in more columns 114 to fill the same area. The foam material of the segments 114 is preferably the same material as the rest of the first foam pad 110, although another foam material may be substituted if the other material still is capable of exhibiting a compressive stress of at least 50 psi for a dynamic compression of 50%. To make sure the segments 114 stay together during a compressive impact the second foam pad 112 and/or segments 114 are tightly surrounded by a generally inelastic cord made of a high strength, low elongation material such as KEVLAR®. The second foam pad 112 has a length or height and the cord 118 is positioned generally in the middle of the length or height.


The subliner element of the third type 20 further includes a third foam pad 120 constructed of an energy absorbing viscoelastic foam material which is the same material as the first foam pad 110. The third foam pad 120 is generally disk shaped and similarly shaped to the first foam pad 110. The third foam pad 120 has a top surface 120a and a bottom surface 120b. The top surface 120a of the third foam pad 120 is attached to the bottom surface 112b of the second foam pad 112. The bottom surface 120a of the third foam pad 120 is a substantially flat surface which is substantially tangent to the surface of the wearer's head 12 beneath it when the helmet 14 is worn. The bottom surface 120a of the third foam pad 120 forms the horizontal lower surface 20a, described above. The first, second and third foam pads 110, 112 and 120 are preferably secured together using a suitable adhesive that works well with foam. That is, the adhesive is preferably flexible in its cured condition to accommodate any stretching or compressing of the foam materials during an impact, as is well understood by those of ordinary skill in the art. Preferably, the slender foam columns 114 in totality enable a sidewise relative displacement between the first and second foam pads 110, 112 of at least one-half inch in response to a sidewise force of less than 100 pounds. After an impact, the slender foam columns 114 are able to return the first and second foam pads 110, 112 to their pre-impact relative position.


Referring now to FIG. 4B, there is shown a second embodiment of a subliner element of the third type 20′, which includes a first foam pad 110′ constructed of an energy absorbing viscoelastic foam material having a top surface 110a′ and a bottom surface 110b′. The top surface 110a′ is attached to the inner surface 22 of the shell 24, as described above. The bottom surface 110b′ is generally planar and has a first fluoropolymer coating or layer 122 adhered thereto.


The second embodiment of a subliner element of the third type 20′ further includes a second foam pad 112′ constructed of an energy absorbing viscoelastic foam material having a top surface 112a′ and a bottom surface 112b′. The top surface 112a′ of the second foam pad 112′ is generally planar and has a second fluoropolymer layer or coating 124 adhered thereto. The first and second foam pads 110′, 112′ being positioned with the first and second fluoropolymer coatings 122, 124 in sliding facing engagement. The bottom surface 112b′ of the second foam pad 112′ is a substantially flat surface which is substantially tangent to the surface of the wearer's head 14 beneath it when the helmet 12 is worn. The bottom surface 112a′ of the second foam pad 112′ forms the horizontal lower surface 20a, described above. Both the first and second foam pads 110′, 112′ are generally disk shaped.


Each fluoropolymer layer 122, 124 is pre-treated on just one side to enable it to be strongly adhered to another surface. The adhering agent is an adhesive which is flexible in its cured condition to be able to accommodate any stretching or compressing of the foam materials during an impact. The first foam pad 110′ has a first side surface 110c′ extending between the top and bottom surfaces 110a′, 110b′. The second foam pad 112′ has a second side surface 112c′ extending between the top and bottom surfaces 112a′, 112b′. A first rib or band 126 is secured to the first side surface 110c′ of the first foam pad 110′. A second rib or band 128 is secured to the second side surface 112c′ of the second foam pad 112′. The upper and lower ribs 126, 128 surround the first foam pad 110′ and the second pad 112′, respectively, at near the mid height of each first side surface 110c′ and second side surface 112c′. Each rib 124, 126 is preferably constructed of a polymeric material and has several holes 130 to accommodate metal pins 132 which are long enough to hold each of the ribs 126, 128 in place by being embedded in the foam. Preferably there would be between six and sixteen holes 130 and pins 132 to properly secure each rib 126, 128 to the underlying foam portion.


A biasing element extends between the first and second ribs 126, 128 to force the first and second fluoropolymer coatings 122, 124 toward each other. That is, preassembled onto the ribs 126, 128 before they are pinned into place are a plurality of small elastomer bands 134 spaced around periphery of the first and second foam pads 110′, 112′. Preferably there would be a total of eighty to one hundred sixty elastomer bands 134 distributed around the circumference, each one being stretched between the upper and lower ribs 126, 128. And preferably, each elastomer band 134 is pre-twisted one time between the upper and lower ribs 126, 128 so that the two free lengths of each elastomer band 134 are equal. The free length being that section of an elastomer band 134 stretched around the upper and lower ribs 126, 128. The first and second fluoropolymer coatings 122, 124 are biased toward each other by a force applied to the first and second foam pads 110′, 112′ as result of the elastomer bands 134.


The material of the elastomer band 134 should have an elastic elongation capability of greater than 100% to be able to elastically accommodate the required stretch of their free lengths as the first and second fluoropolymer coatings 122, 124 slide relative to each other in response to an impact. Then after an impact the elastomer bands 134 return the first and second foam pads 110′, 112′ to their pre-impact relative position.


Referring now to FIG. 4C, there is shown a third embodiment of a subliner element of the third type 20″. The third embodiment of the subliner element of the third type 20″ is identical to the second embodiment of the subliner element of the third type 20′, except that the plurality of elastomer bands 34 have been replaced with a plurality of spring elements 136 described in more detail below. Accordingly, only the differences between the third embodiment of the subliner element of the third type 20″ and the second embodiment of the subliner element of the third type 20′ will be described, with like double prime element numbers being used for the third embodiment of the subliner element 20″. The spring element 136 is preferably in the form of a generally V-shaped wire. The spring elements 136 shown in FIG. 4C are shown in an installed, mostly unstressed configuration. Each spring element 136 would be typically comprised of metal or polymer plastic. If metal, it could be hardened stainless steel having a yield strength of greater than 200,000 psi. If polymer plastic, it could be a polymer having very good spring properties such as acetal. The spring elements 136 illustrated in FIG. 4C exhibit a high yield strength and are constructed of 10 mil diameter stainless steel spring having a length of approximately 1 inch in its long dimension. Each spring element 136 has two flattened and curved hook-like terminal ends 136a that fit securely behind the upper and lower ribs 126″, 128″ with the spring elements 136 extending outward radially. Typically, there could be a total of up to one hundred eighty or less spring elements 136. The spring elements 136 elastically deform as the as the first and second fluoropolymer coatings 122, 124 slide relative to each other in response to an impact. Then after an impact the spring elements 136 return the first and second foam pads 110′, 112′ to their pre-impact relative position.


The subliner element of the third type 20 should be thick enough not to compress all the way to its full densification condition under a peak normal impact force which could easily reach, and possibly even exceed, a thousand pounds. Although the weight of a full helmet would likely be substantially less than that (being typically under five pounds), if all the helmet weight were to be required to be supported by the subliner element of the third type 20, with its high dynamic stiffness designed to accommodate a dynamic force of over a thousand pounds, the supporting area around point b for a static force of just five pounds could be so small that the supporting pressure could be uncomfortably high for the wearer were it not for the subliner elements of the second type 18, shown in third area C.


Subliner elements of the second type 18, located in third area C, would preferably be made of a much more compliant material than that used for the subliner element of the third type 20, preferably at least five times more compliant and perhaps more than an order of magnitude more compliant than the stiffer materials recommended for subliner element of the third type 20. Such a material could be an extra soft polyurethane foam such as LAST-A-FOAM®, EF-4003 by General Plastics Manufacturing Company, or EZ-Dri foam by Crest Foam Industries, both having, a relatively flat static and dynamic compression stress vs. deflection characteristic (the former 2.6 psi at 10%, 2.7 psi at 20%, 2.8 psi at 30%, 3.0 psi at 40%, and 3.4 psi at 50% and the latter 0.3 psi at 10%, 0.35 psi at 20%, 0.4 psi at 30%, 0.45 psi at 40% and 0.55 psi at 50%), so when incorporating the proper total area to accomplish the function of supporting the full weight or nearly the full weight of the helmet with the latter material enabling about five times the support area for extreme comfort, the exact location and thickness of the subliner elements of the second type 18 would not be that critical for the subliner elements of the second type 18 to be able to successfully support all, or almost all, of the weight of the helmet, yet contribute very little side force to the wearer's head 12 during an impact. However, the second type of subliner elements 18 are preferably positioned generally equidistantly about and between the first and third type of subliner elements 16, 20 in the third area C.



FIG. 2A shows a second embodiment of the present disclosure wherein there is at least one of a second type of subliner element 18. That is, instead of a plurality of the second type of subliner elements 18 as shown in FIG. 2, the second type of subliner elements 18 in accordance with the second embodiment are instead formed as a single annular ring 18′. Using a single annular ring 18′ has the advantage of easier assembly and greater simplicity. Otherwise, all other elements of the subliner system 10 of the second embodiment are identical to the first embodiment.



FIG. 1 schematically shows the cervical spine 13 and its seven cervical vertebrae labeled Atlas (C1), Axis (C2), C3, C4, C5, C6 and C7. For both centered (directed toward the center of gravity of a wearer's head) and non-centered impacts having a large horizontal force component, almost all the side forces (and torques) that would be imparted to a wearer's head 12 during an impact would be imparted through the subliner elements of the first type 16, which would be located, or substantially located, in first area A and generally evenly distributed/spaced thereabout. First area A places the point of application of these impact forces as close as possible to the head's two natural pivot points for angular acceleration: a lower pivot point 12a where the C7 cervical vertebrae (which can be located by the prominent bone at the base of the back of the neck) meets the Ti thoracic vertebrae, and an upper pivot point 12b where the C1 cervical vertebrae (the atlas bone) meets the paired occipital condyle projections of the skull to enable forward and backward rotation (a “yes” motion) of the head and where the atlas bone meets the C2 cervical vertebrae (the axis bone) enabling axial rotation (a “no” motion) and side-to-side rotation of the head, this latter pivot being located approximately just above and slightly in front of the ear lobes. Thus, all the head angular accelerating torques imparted to the user's head during an impact would be kept as small as possible for a given force as a result of this lowest practical positioning of subliner elements of the first type 16.


As stated previously, each embodiment of the subliner element of the third type 20, due to its flat horizontal lower surface 20a, typically does not impart a significant horizontal force to the wearer's head 12. The following description of the first embodiment of the subliner element of the third type 20, is equally applicable to the second and third embodiments of the subliner element of the third type 2020″. There may be certain impacts during which the lower surface 20a of the subliner element of the third type 20 would not remain flat but instead would tend to cup around the surface of the wearer's head 12. One such type of impact is obvious: a direct downward impact to the crown, or top, of the helmet 14, centered toward the center of gravity (e.g.) of the wearer's head 12. Although that type of impact would result in cupping the lower surface of subliner element of the third type 20 around the wearer's head 12, little or no horizontal force would be imparted to the wearer's head 12.


Another impact case that could cup the lower surface of the subliner element of the third type 20 might be a downward impact to the top of the helmet at a point located away from the crown and generally directed toward the body of the wearer. Picture a running back diving over the goal line, his helmet getting struck in midair by the shoulder pad of a linebacker diving the other way to stop him. Here, in addition to a significant downward force through the subliner element of the third type 20 (downward here meaning downward toward the body of the running back), there could be a not-insignificant horizontal force (horizontal here meaning horizontal relative to the body of the running back) imparted to the running back's head through subliner element of the third type 20, as well as through the subliner elements of the first type 16; for the most part the former would tend to rotate point b on the running back's head about the aforementioned upper pivot point toward the impact location, while the latter would tend to rotate point b about the aforementioned lower pivot point away from the impact location. So even in this case where the subliner element of the third type 20 cannot avoid imparting a horizontal (sideways) force, the structure of the total subliner system 10 still tends to cancel the above two rotational head motions and thereby reduce the resultant angular acceleration of the wearer's head 12.


Further reductions of imparted torque levels can be achieved by lowering the impact force levels, which can be accomplished by a proper choice of material for the subliner elements of the first type 16, and by including specific structural features in the subliner elements of the first type 16. Especially during an impact involving mostly a horizontal force component, only about one third of the subliner elements of the first type 16 (those located in the wide general region beneath the impact point) would be imparting most of the side normal force and side tangential force to the wearer's head 12 since the remaining subliner elements of the first type 16 would have tended to move away from the wearer's head 12 during the impact as the force-imparting subliner elements of the first type 16 compress and/or flex as a result of the high impact forces. The force levels could be of the same order of magnitude as those potentially experienced by the subliner element of the third type 20 (up to, and perhaps even more than a thousand pounds), and so the same energy absorbing viscoelastic foam materials cited for subliner element of the third type 20 would be in order for subliner elements of the first type 16, where their high energy absorption capability will help reduce the level of the high impact forces. The radial (thickness) dimension of the subliner elements of the first type 16 should be of sufficient length and have sufficient area to be able to avoid full densification at the maximum expected peak dynamic impact force, which could still be in the thousand-pound range for the total aggregate number of forces imparted on the subliner elements of the first type 16. On average the radial thickness of the subliner elements of the first type 16 would be approximately 0.25 to 1.25 inches, and preferably 0.75 inches in a two shell case, and approximately 1.0 to 2.0 inches, and preferably 1.5 inches in a single shell case.


In a preferred embodiment, to increase lateral compliance to help further reduce the imparted tangential side forces, the subliner elements of the first type 16 may be partitioned into multiple segments or columns which emanate in a substantially perpendicular direction from the inner surface 22 of the inner shell 24. The partitioning may be in the form of like-shaped segments having a particular cross-sectional shape, or it could be in the form of different shaped segments, as for instance an outer square cross-sectional shaped segment 36 having a centered circular cutout 38, along with a circular cross-sectional segment 40 to fill the circular cutout space, see FIG. 3. In order to best achieve the goal of reduced imparted side forces, the side surfaces of the partitioned side-by-side segments should be at least partially able to frictionally slide relative to each other in the segments' general radial direction. More particularly, double-sided nano tape 39 is preferably positioned between the nested side surfaces such that the side surfaces are in direct contacting engagement with the nano tape 39. Thus, when adjacent side surfaces slide relative to each other during an impact, the highly viscous nano tape gets sheared across its thickness and additional energy is absorbed. It will be understood by those skilled in the art that nano tape 39 may be any nano tape which is commercially available. In general, nano tape 39 is an elastic tape that includes a nanofiber or nanotube structure which adheres to an adjacent surface due to Van der Waals forces. In one embodiment, the nano tape 39 is a comprised of carbon nanotube arrays provided on a backing layer formed of a flexible polymer, such as polyurethane, with Van der Waals interactions occurring between the carbon nanotube arrays and individual nanotubes and the adjacent surface. The nano tape is in the range of 0.5 to 2.0 mm thick and most preferably 1.0 mm thick. To assemble the subliner element of the first type 16 shown in FIG. 3, the nano tape 39 is wrapped around the circular cross-sectional segment 40 which is then inserted into the circular cutout 38 such that that nano tape 39 is positioned therebetween, as described in more detail below. The segment's generally parallel partitioned surfaces cannot be exactly radial from the standpoint of the wearer's head 12 due to the width of the partitioned element, but they are substantially radial. The partitioning or segmenting might be implemented using a simple “cookie cutter” approach. Other examples of partitioning subliner elements that could be used for the first type of subliner element 16 are described below in FIGS. 7a-7b through 15a-15b. These and their subsets, are themselves a small subset of all of the partitioning configurations that may be utilized.



FIG. 3 is an exploded perspective view of a partitioned subliner element of the first type 16 and its attachment to a portion of the inner surface 22 of the inner shell 24, showing the portion of the inner shell 24, the hook part 30 and the loop part 32 of a hook and loop fastener mechanism of a type in common usage today for such applications, along with an optional covering 34 over the subliner element of the first type 16. Any of the subliner elements, of any of the three subliner element types 16, 18, 20 may include a full covering 34 formed from a fabric or a film 34 to improve the comfort of the wearer, to improve the durability of the subliner element types 16, 18, 20, or to improve the functioning of the subliner element types 16, 18, 20, the latter possibly including, but not being limited to, its ability hold partitioned columns of a subliner element type 16, 18, 20 in place, its ability to protect against moisture and contaminants, its ability to improve air flow, and its ability to improve moisture dissipation. The optional covering 34 need not be full as shown but may be partial if the circumstances warrant. The fabric of choice may be any of a wide range of suitable fabrics, while the film of choice could be any suitable polymer or elastomer film having a suitable thickness for the application.


Referring still to FIG. 3, the subliner element of the first type 16 preferably includes a generally inelastic cord 41 surrounding the subliner element of the first type 16. The subliner element of the first type 16 has a length extending away from the inner surface 22. The inelastic cord 41 is positioned generally in the middle of the length. The inelastic cord 41 is preferably constructed of KEVLAR®, but other like materials could be substituted. The purpose of the inelastic cord 41 is to prevent the subliner element of the first type 16 from bulging in the center area to ensure that the circular cross-sectional segment 40 and the centered circular cutout 38 maintain good surface to surface contact with the nano tape 39. While the inelastic cord 41 is shown being positioned directly around the outer square shaped the segment 36, it could also be positioned about the cover 34.



FIG. 4 is a cross-sectional side view located at the midsagittal plane of the wearer's head 12 showing the three types of subliner elements 16, 18, 20 as located in FIG. 2 and the inner shell 24 to which they are attached. The inner shell 24 may be part of a single liner, single shell helmet 14 as illustrated in the figure, or it may be part of a multiple liner, multiple shell helmet, as discussed in more detail below. The relative size of the inner shell 24 shown in FIG. 4 at the lower end of the indicated radial thickness range would be consistent with the former case if the helmet were for example an equestrian helmet or a ski helmet, and the relative size of the inner shell shown in FIG. 4 would also be consistent with the latter case if the helmet were for example a football helmet or a motorcycle helmet. A football helmet or a motorcycle helmet of the single liner, single shell type would typically have a larger subliner system 10 at the higher end of the indicated radial thickness range, which in that case would also be the outer shell. Thus, in a football helmet or motorcycle helmet of the single liner, single shell type embodiment, the radial spacing of the inner shell 24 from the head 12 would typically be greater than that shown in FIG. 4 and the subliner elements of the first, second and third types 16, 18, 20 would accordingly have a greater radial dimension.


With continued reference to FIG. 4, the inner surface 22 of the inner shell 24 above subliner element of the third type 20 is shown to have a flat horizontal surface 42 rather than a concave surface. The inner shell 24 may be molded that way to achieve the flat horizontal surface 42. The flat horizontal surface 42 is not absolutely necessary but it is preferred to enable subliner element of the third type 20 to be flat on its upper surface as well as its lower surface 20a, which helps to assure a horizontal lower surface 20a, and makes it simpler and more controllable to determine, select, and properly align and apply a proper thickness subliner element of the third type 20 so that it's lower surface 20a remains horizontal and preferably barely touches the wearer's head 12. As shown in FIG. 4, the two cross-sectioned subliner elements of the second type 18 are shown in the third area C, properly radially compressed, as would be all of the other subliner elements of the second type 18 not shown in the cross-section, when all are supporting the full weight of the helmet, even though the full helmet with all its potential parts, including a potential face guard and a potential chin strap or jaw strap system, is not shown in FIG. 4. Finally, the subliner elements of the first type 16 in the first area A each have a thickness to yield a snug but not uncomfortable fit with the wearer's head 12.



FIG. 5 is a left side elevational view of the wearer's head 12 showing the inner shell 24 of FIG. 4 located over the wearer's head 12 with all the subliner elements of the first, second and third type 16, 18, 20 positioned as shown in phantom and as in FIG. 2; all of the subliner elements of the first, second and third type 16, 18, 20 being attached to the inner surface 22 of the inner shell 24, typically by the easy-on, easy-off, hook and loop fastener mechanism 30, 32 shown in FIG. 3. The easy-on, easy-off capability helps in being able to customize the helmet for an individual wearer. The potential materials to be used for the inner shell 24 would depend upon which embodiment it is being used in. In the single liner, single shell helmet embodiment the inner shell 24 (which is now also the outer shell) must be able to handle a direct impact, so an impact resistant material such as polycarbonate or high impact ABS would be appropriate. In the multiple liner, multiple shell helmet embodiment described in more detail below, the inner shell 24 need not handle a direct impact, but it still would need to be able to handle high forces so a high strength polymer composite containing either glass fibers, carbon fibers, or KEVLAR® fibers (commonly understood as heat-resistant and strong synthetic fibers) or a composite utilizing a combination of different fibers could be appropriate. Also, for this embodiment, the inner shell 24 could be constructed of a thin metal, such as stainless steel or an aluminum alloy (either perforated, or not perforated), and in large quantities could be fabricated by pressing it to shape in a die with a large machine press. Such a thin metal shell, perhaps a thirty-second of an inch or less in thickness, could weigh even less than a comparable strength polymer composite shell.



FIG. 6 is a cross-sectional side view located at the midsagittal plane of a wearer's head 12, showing a two liner, two shell, helmet 14 embodiment of the present disclosure. FIG. 6 shows the subliner system 10 of FIG. 4, plus a second or outer liner 44 and a second or outer shell 46 which together form an outer shell system 48. Five outer liner elements 50 are shown in the second liner 44 because they cross the midsagittal plane. Typically, there may be ten to fifteen additional liner elements 50 in the second liner 44 which are not shown in FIG. 6 because they do not cross the midsagittal plane. That would add up to a likely total of fifteen to twenty total liner elements 50 in the second liner 44, spread out more or less equidistantly throughout the available space between the inner shell 24 and the second or outer shell 46.


All the liner elements 50 of the second liner 44 are firmly attached to both the outer surface of the inner shell 24 and the inner surface of the outer shell 46. By contrast, subliner elements of the first, second and third types, 16, 18, 20 in the subliner system 10 can only be attached to the inner shell 24 (they cannot be attached to a wearer's head). The firm attachment of the liner elements 50 of the second liner 44 to both the inner and outer shells 24, 46 enables liner elements 50 to experience not just high compression forces, but high shear forces and high tensile forces as well. As a result, the attachment requirement here is beyond the capability of a standard hook and loop fastener and is more in the realm of a high strength, wide temperature range, flexible adhesive, such as LOCTITE® 4902, or LOCTITE® Plastic Bonder, both by Henkel Corporation. The former is a one-part adhesive, the latter a two-part adhesive, and both are quick curing.


These flexible, high strength attachments make it possible for all the liner elements 50 of the second liner 44 to participate in mitigating any impact to the wearer's head 12, regardless of the impact's location or direction. That mitigation is accomplished through the widespread positioning of the liner elements 50 and their ability to efficiently absorb energy in three different modes: compression, shear, and tension. For example, for any centered impact the liner elements 50 of the second liner 44 generally located in the region beneath the impact will experience compression, those located to the side of the impact will experience shear, and those located opposite the impact will experience tension, while those located in between will experience some combination of compression, shear, and tension. For any non-centered impact most of the liner elements 50 of the second liner 44 will experience a higher degree of shear. Because every impact is different in its location and direction, each liner element 50 in the second liner 44 must be able to absorb energy at all the expected possible levels of compression, shear, and tension, and combinations thereof.


Furthermore, in order to even be in a position of optimally absorbing energy, each liner element 50 of the second liner 44 must become deformed during an impact to its full extent by the outer shell 46, not just those liner elements 50 beneath the impact, but those to the side of the impact, and those opposite the impact as well, and the outer shell 46 must remain rigid enough during the impact to be able to accomplish that. Because the outer shell 46 is relatively thin and typically made of a polycarbonate or high impact ABS, this requires that the outer shell 46 be rigidized, especially near its opening to accommodate a wearer's head 12, which is the place where it is the weakest. Notice in the figure, that there are two molded-in internal rings 52 near the opening to accomplish the rigidizing, but other rigidizing approaches such as severe contouring or metal banding (not shown) would also be acceptable.


Achieving the optimum energy absorption by all the liner elements 50 of the second liner 44 also requires they be fabricated of a material having an inherent high energy absorbing capability, and that the material also have a proper level of dynamic stiffness for the total second liner element 50 footprint area. To meet these criteria, the liner elements 50 of the second liner 44 may be fabricated from the same list of materials recommended for subliner elements of the first and third types 16, 20, the list including: a vinyl nitrile foam such as IMPAX® VN600, VN740, or VN1000 by Dertex Corporation, or a polyurethane foam such as LAST-A-FOAM® FP 8015 by General Plastics Manufacturing Company. However, in block form, each material likely presents too much dynamic stiffness in shear as compared to its dynamic stiffness in compression and tension. So to reduce a second liner element's dynamic stiffness in shear, without at the same time reducing its dynamic stiffness in compression or tension, partitioning of each liner element 50 into discrete adjacent segments is preferred, somewhat similar to what has been previously discussed for subliner elements of the first type 16, but even more so for the second liner elements 50 because the potential shear levels experienced by the second liner elements 50 are greater.


The cross-sectioning of the second liner elements 50 in FIG. 6 reveals each element to be partitioned into five equal segments 50a, 50b, 50c, 50d, 50e. However, one skilled in the art will understand that there are several partitioning possibilities, all of which could be acceptable options if they can achieve the proper level of reduction in the total shear force as compared to the total compression and tensile forces.



FIGS. 7a through 15a show nine such partitioning possibilities, illustrated in plan view (from the viewpoint of the outer shell 46) to be able to see what they actually could represent. Cross-sectional views in FIGS. 7b through 15b show the same sectional view as what is shown in FIG. 6. However, even these nine are still an extremely reduced sample of what may be possibly used as partitioning arrangements for the second liner elements 50. FIGS. 7a and 7b show twenty-five equal square shaped segments or foam columns 54 arranged in a 5×5 square array. That is, the foam columns 54 form a plurality of generally radially oriented side-by-side flexible individual and independent foam columns or segments 54. The columns or segments 54 are preferably formed entirely of foam and having a top surface 54a, a bottom surface 54b, and foam side surfaces 54c where the top surface 54a is directly attached to the inner surface of the outer shell 48 and the bottom surface is directly attached to the outer surface of the inner shell 24. The foam side surfaces 54c of adjacent columns or segments 54 are positioned side-by-side with respect to each other preferably with double-sided nano tape 39 positioned therebetween such that the segments 54 are nested in slidable direct contacting frictional engagement with the nano tape 39. FIGS. 8a and 8b show a liner element 50 having an outer circumferential square wall 56 and an inner square cutout 58, filled with nine equal square shaped segments arranged in a 3×3 square array. Nano tape 39 is positioned between the outer circumferential square wall 56 and the nine equal square shaped segments as well as between the nine equal square shaped segments themselves. FIGS. 9a and 9b show a liner element 50 having an outer annular wall 60, an inner annular wall 62 complementarily positioned in the outer annular wall 60 and an innermost cylinder 64 complementarily positioned within the inner annular wall 62. Nano tape 39 is positioned between the outer annular wall 60, the inner annular wall 62 and the innermost cylinder 64. FIGS. 10a and 10b show a liner element 50 having a square outer annular wall 66, a square inner annular wall 68 complementarily positioned in the square outer annular wall 66 and an innermost generally square in cross section cylinder 70 complementarily positioned within the square inner annular wall 68. Nano tape 39 is positioned between the square outer annular wall 66, the square inner annular wall 68 and the innermost generally square in cross section cylinder 70. FIGS. 11a and 11b show a liner element 50 having octagonal outer annular wall 72, an octagonal inner annular wall 74 complementarily positioned in the octagonal outer annular wall 72 and an innermost generally octagonal in cross section cylinder 76 complementarily positioned within the octagonal inner annular wall 74. Nano tape 39 is positioned between the octagon all outer annular wall 72, the octagon oh inner annular wall 74 and the innermost generally octagonal in cross section cylinder 76. FIGS. 12a and 12b show a liner element 50 having a hexagonal outer annular wall 78, a hexagonal inner annular wall 80 complementarily positioned in the hexagonal outer annular wall 78 and an innermost generally hexagonal in cross section cylinder 82 complementarily positioned within the hexagonal inner annular wall 80. Nano tape 39 is positioned between the hexagonal outer annular wall 78, the hexagonal inner annular wall 80, and the innermost generally hexagonal in cross section cylinder 82. FIGS. 13a and 13b show a liner element 50 having square outer annular wall 84, a square inner annular wall 86 complementarily positioned in the square outer annular wall 84 and an innermost generally circular in cross section cylinder 88 complementarily positioned within the square inner annular wall 86. Nano tape 39 is positioned between the square outer annular wall 84, the square inner annular wall 86 and the innermost generally circular in cross section cylinder 88. FIGS. 14a and 14b show a liner element 50 having octagonal outer annular wall 90, an octagonal inner annular wall 92 complementarily positioned in the octagonal outer annular wall 90 and an innermost generally circular in cross section cylinder 94 complementarily positioned within the octagonal inner annular wall 92. Nano tape 39 is positioned between the octagon all outer annular wall 90, the octagon oh inner annular wall 92 and the innermost generally circular in cross section cylinder 94. FIGS. 15a and 15b show a liner element 50 having a hexagonal outer annular wall 96, a hexagonal inner annular wall 98 complementarily positioned in the hexagonal outer annular wall 96 and an innermost generally circular in cross section cylinder 100 complementarily positioned within the hexagonal inner annular wall 98. Nano tape 39 is positioned between the hexagonal outer annular wall 96, the hexagonal inner annular wall 98 and the innermost generally circular in cross section cylinder 100.



FIGS. 7a and 7b show a specific case of the general class of a radially partitioned second liner element 50 into side-by-side segments. FIGS. 8a and 8b through FIGS. 15a and 15b show specific cases of the general class of radially partitioned second liner elements 50 into nesting and nested segments. Note that some segments can be both nesting and nested. Also note FIG. 3 shows an example of a nesting and nested segmented element, although not a second liner element 50 but a subliner element of the first type 16.


In general, the segment boundaries of the liner elements 50 (all formable by a “cookie cutter type slicer”) would be oriented in a substantially radial direction (from the standpoint of the wearer's head 12, or the outer shell 46, etc.) but most can never be oriented exactly in the radial direction, in part due to the extended width dimensions of a liner elements 50. Nevertheless, for simplification purposes, this specification will still be referred to them as “radial.” During an impact that results in a shearing motion of the liner elements 50, at least some of the adjacent segment surfaces may move relative to each other along their boundaries where the nano tape 39 is located in the radial direction to form S curves (not shown), and through dynamic friction to thereby provide some additional energy absorption. The use of the nano tape 39 increases the dynamic friction between adjacent moving segments resulting in greater energy absorption. The concept of absorbing energy through adjacent surfaces moving relative to each other to form S curves is fully described in U.S. Pat. No. 9,032,558 but without nano tape, which is hereby incorporated by reference in its entirety. The addition of nano tape results in greater energy absorption and is thus an improvement.



FIG. 16 illustrates a left side elevational view showing the outer shell 46 of FIG. 6 positioned on a wearer's head 12. The size and shape of the outer shell 46 might be typical of a football helmet.



FIG. 17 is a left side elevational view of a wearer's head 12 showing a face guard 102 attached to the outer shell 46 of FIG. 8, and a chin strap 104 positioned on the wearer's chin and attached to the inner shell 24 of FIG. 5, both typical of a football helmet application.


Finally, although only a first preferred embodiment having a subliner system 10, and a second preferred embodiment having a subliner system 10 and an outer shell system 48 have been described in significant detail, the addition of a third liner and a third shell (not shown) would still be within the scope of the present disclosure. It will also be appreciated by those skilled in the art that changes, or modifications could be made to the above described embodiments without departing from the broad inventive concepts of the disclosure. Therefore, it should be appreciated that the present disclosure is not limited to the particular use or particular embodiments disclosed but is intended to cover all uses and all embodiments within the scope or spirit of the described disclosure.

Claims
  • 1. A helmet adapted to be worn on a head of a wearer, the head having a top area centered about a top of the wearer's head encompassing approximately 0.44 to 7 square inches, the helmet comprising: a subliner shell comprised of a hard impact resistant material, the shell having inner and outer surfaces, the shell adapted to surround at least a portion of the cranial part of the wearer's head with the inner surface of the shell being spaced from the wearer's head at an initial pre-impact relative position when the helmet is worn; anda subliner, at least a part of which is adapted to be in contact with the wearer's head when the helmet is worn prior to an impact and during an impact, the subliner comprising:at least one subliner element extending from the inner surface of the shell at a location such that the subliner element is adapted to be aligned with the top area when the helmet is worn, the at least one subliner element comprising: a first foam pad constructed of an energy absorbing viscoelastic foam material having a top surface and a bottom surface, the top surface being attached to the inner surface of the shell,a second foam pad being constructed of an energy absorbing viscoelastic foam material, the second foam pad being radially partitioned into individual and independent segments, the independent segments are nested with respect to each other such that the nested segments have side surfaces in slidable direct contacting engagement with side surfaces of adjacent nested segments, the second foam pad having a top surface attached to the bottom surface of the first foam pad, anda third foam pad constructed of an energy absorbing viscoelastic foam material having a top surface and a bottom surface, the top surface of the third foam pad being attached to the bottom surface of the second foam pad, the bottom surface of the third foam pad being a substantially flat surface which is substantially tangent to the surface of the wearer's head beneath it when the helmet is worn.
  • 2. The helmet as recited in claim 1, further including a generally inelastic cord surrounding the second foam pad.
  • 3. The helmet as recited in claim 2, wherein the second foam pad has a length and the cord is positioned generally in the middle of the length.
  • 4. The helmet as recited in claim 3, wherein the cord is constructed of synthetic fiber.
  • 5. The helmet as recited in claim 1, wherein the first, second and third foam pads are comprised of an energy absorbing viscoelastic foam material capable of exhibiting a compressive stress of at least 50 psi for a dynamic compression of 50%.
  • 6. A helmet adapted to be worn on a head of a wearer, the head having a pair of eyebrows and a pair of ears, the head having an annular headband shaped area encircling the wearer's head, the headband shaped area being approximately 0.75 to 1.25 inches wide and having a lower edge defining a plane positioned approximately 0.5 to 1.5 inches above the eyebrows and approximately 0.25 to 0.75 inches above an upper junction of the ears and the wearer's head, a top area centered about a top of the wearer's head encompassing approximately 0.44 to 7 square inches, and a middle area of the head defined between the headband area and the top area, the helmet comprising: a subliner shell comprised of a hard impact resistant material, the shell having inner and outer surfaces, the shell adapted to surround at least a portion of the cranial part of the wearer's head with the inner surface of the shell being spaced from the wearer's head at an initial pre-impact relative position when the helmet is worn; anda subliner, at least a part of which is adapted to be in contact with the wearer's head when the helmet is worn prior to an impact and during an impact, the subliner comprising:a plurality of a first type of subliner elements extending from the inner surface of the shell at a location such that the first type of subliner elements are adapted to be aligned with the headband area when the helmet is worn, the first type of subliner elements being constructed of an energy absorbing viscoelastic foam material;at least one of a second type of subliner element extending from the inner surface of the shell at a location such that the at least one of the second type of subliner element is adapted to be aligned with the middle area when the helmet is worn, the at least one of the second type of subliner element being constructed of a foam material; anda third type of subliner element extending from the inner surface of the shell at a location such that the third type of subliner element is adapted to be aligned with the top area when the helmet is worn, the third type of subliner element comprising: a first foam pad constructed of an energy absorbing viscoelastic foam material having a top surface and a bottom surface, the top surface being attached to the inner surface of the shell,a second foam pad being constructed of an energy absorbing viscoelastic foam material, the second foam pad being radially partitioned into individual and independent segments, the independent segments are nested with respect to each other such that the nested segments have side surfaces in slidable direct contacting engagement with side surfaces of adjacent nested segments, the second foam pad having a top surface attached to the bottom surface of the first foam pad, anda third foam pad constructed of an energy absorbing viscoelastic foam material having a top surface and a bottom surface, the top surface of the third foam pad being attached to the bottom surface of the second foam pad, the bottom surface of the third foam pad being substantially flat surface which is substantially tangent to the surface of the wearer's head beneath it when the helmet is worn,the at least one of the second type of subliner element being positioned between the plurality of the first type of subliner elements and the third type of subliner element.
  • 7. The helmet as recited in claim 6, further including a generally inelastic cord surrounding the second foam pad.
  • 8. The helmet as recited in claim 7, wherein the second foam pad has a length and the cord is positioned generally in the middle of the length.
  • 9. The helmet as recited in claim 8, wherein the cord is constructed of synthetic fiber.
  • 10. The helmet as recited in claim 6, wherein the first, second and third foam pads are comprised of an energy absorbing viscoelastic foam material capable of exhibiting a compressive stress of at least 50 psi for a dynamic compression of 50%.
  • 11. The helmet as recited in claim 6 further comprising: an outer shell comprised of a hard impact resistant material, the outer shell having inner and outer surfaces, the outer shell surrounding at least a portion of the subliner shell, the inner surface of the outer shell being spaced from the outer surface of the subliner shell at an initial pre-impact relative position; anda plurality of outer liner elements located in the space between the outer surface of the subliner shell and the inner surface of the outer shell and attached to both the outer surface of the subliner shell and the inner surface of the outer shell wherein at least one of the outer liner elements is comprised of an energy absorbing viscoelastic foam.
  • 12. The helmet as recited in claim 11 the outer liner elements being radially partitioned into individual and independent segments, the independent segments are nested with respect to each other with double-sided nano tape positioned therebetween such that the nested segments have side surfaces in direct contacting engagement with the nano tape.
  • 13. The helmet as recited in claim 6 wherein the first type of subliner elements are radially partitioned into individual and independent segments, the independent segments are nested with respect to each other with double-sided nano tape positioned therebetween such that the nested segments have side surfaces in direct contacting engagement with the nano tape.
  • 14. The helmet as recited in claim 6, wherein the headband area is approximately 1 inch wide and the plurality of first type of subliner elements are adapted to be located to overlap the width of the headband area.
  • 15. A helmet adapted to be worn on a head of a wearer, the head having a top area centered about a top of the wearer's head encompassing approximately 0.44 to 7 square inches, the helmet comprising: a subliner shell comprised of a hard impact resistant material, the shell having inner and outer surfaces, the shell adapted to surround at least a portion of the cranial part of wearer's head with the inner surface of the shell being spaced from the wearer's head at an initial pre-impact relative position when the helmet is worn; anda subliner, at least a part of which is adapted to be in contact with the wearer's head when the helmet is worn prior to an impact and during an impact, the subliner comprising:at least one subliner element extending from the inner surface of the shell at a location such that the subliner element is adapted to be aligned with the top area when the helmet is worn, the at least one subliner element comprising: a first foam pad constructed of an energy absorbing viscoelastic foam material having a top surface and a bottom surface, the top surface being attached to the inner surface of the shell, the bottom surface being generally planar and having a first fluoropolymer coating adhered thereto; anda second foam pad constructed of an energy absorbing viscoelastic foam material having a top surface and a bottom surface, the top surface of the second foam pad being generally planar and having a second fluoropolymer coating adhered thereto, the first and second foam pads being positioned with the first and second fluoropolymer coatings being in sliding facing engagement, the bottom surface of the second foam pad being a substantially flat surface which is substantially tangent to the surface of the wearer's head beneath it when the helmet is worn.
  • 16. The helmet as recited in claim 15, wherein the first and second fluoropolymer coatings are biased toward each other by a force applied to the first and second foam pads.
  • 17. The helmet as recited in claim 15, wherein the first foam pad has a first side surface extending between the top and bottom surfaces thereof, the second foam pad has a second side surface extending between the top and bottom surfaces thereof, a first rib secured to the first side surface, a second rib secured to a second side surface and a biasing element extending between the first and second ribs to force the first and second fluoropolymer coatings toward each other.
  • 18. The helmet as recited in claim 15, wherein the first and second foam pads are comprised of an energy absorbing viscoelastic foam material capable of exhibiting a compressive stress of at least 50 psi for a dynamic compression of 50%.
  • 19. A helmet adapted to be worn on a head of a wearer, the head having a pair of eyebrows and a pair of ears, the head having an annular headband shaped area encircling the wearer's head, the headband shaped area being approximately 0.75 to 1.25 inches wide and having a lower edge defining a plane positioned approximately 0.5 to 1.5 inches above the eyebrows and approximately 0.25 to 0.75 inches above an upper junction of the ears and the wearer's head, a top area centered about a top of the wearer's head encompassing approximately 0.44 to 7 square inches, and a middle area of the head defined between the headband area and the top area, the helmet comprising: a subliner shell comprised of a hard impact resistant material, the shell having inner and outer surfaces, the shell adapted to surround at least a portion of the cranial part of wearer's head with the inner surface of the shell being spaced from the wearer's head at an initial pre-impact relative position when the helmet is worn; anda subliner, at least a part of which is adapted to be in contact with the wearer's head when the helmet is worn prior to an impact and during an impact, the subliner comprising:a plurality of a first type of subliner elements extending from the inner surface of the shell at a location such that the first type of subliner elements are adapted to be aligned with the headband area when the helmet is worn, the first type of subliner elements being constructed of an energy absorbing viscoelastic foam material;at least one of a second type of subliner element extending from the inner surface of the shell at a location such that the at least one of the second type of subliner element is adapted to be aligned with the middle area when the helmet is worn, the at least one of the second type of subliner element being constructed of a foam material; anda third type of subliner element extending from the inner surface of the shell at a location such that the third type of subliner element is adapted to be aligned with the top area when the helmet is worn, the third type of subliner element comprising: a first foam pad constructed of an energy absorbing viscoelastic foam material having a top surface and a bottom surface, the top surface being attached to the inner surface of the shell, the bottom surface being generally planar and having a first fluoropolymer coating adhered thereto; anda second foam pad constructed of an energy absorbing viscoelastic foam material having a top surface and a bottom surface, the top surface of the second foam pad being generally planar and having a second fluoropolymer coating adhered thereto, the first and second foam pads being positioned with the first and second fluoropolymer coatings being in sliding facing engagement, the bottom surface of the second foam pad being a substantially flat surface which is substantially tangent to the surface of the wearer's head beneath it when the helmet is worn,the at least one of the second type of subliner element being positioned between the plurality of the first type of subliner elements and the third type of subliner element.
  • 20. The helmet as recited in claim 19, wherein the first and second fluoropolymer coatings are biased toward each other by a force applied to the first and second foam pads.
  • 21. The helmet as recited in claim 19, wherein the first foam pad has a first side surface extending between the top and bottom surfaces thereof, the second foam pad has a second side surface extending between the top and bottom surfaces thereof, a first rib secured to the first side surface, a second rib secured to a second side surface and a biasing element extending between the first and second ribs to force the first and second fluoropolymer coatings toward each other.
  • 22. The helmet as recited in claim 21 wherein the biasing element consists of one or more elastic spring elements.
  • 23. The helmet as recited in claim 22 wherein the elastic spring elements are constructed of a material selected from the group consisting of metal, polymer and elastomer.
  • 24. The helmet as recited in claim 19, wherein the first and second foam pads are comprised of an energy absorbing viscoelastic foam material capable of exhibiting a compressive stress of at least 50 psi for a dynamic compression of 50%.
  • 25. The helmet as recited in claim 19 further comprising: an outer shell comprised of a hard impact resistant material, the outer shell having inner and outer surfaces, the outer shell surrounding at least a portion of the subliner shell, the inner surface of the outer shell being spaced from the outer surface of the subliner shell at an initial pre-impact relative position; anda plurality of outer liner elements located in the space between the outer surface of the subliner shell and the inner surface of the outer shell and attached to both the outer surface of the subliner shell and the inner surface of the outer shell wherein at least one of the outer liner elements is comprised of an energy absorbing viscoelastic foam.
  • 26. The helmet as recited in claim 25 wherein the outer liner elements are radially partitioned into individual and independent segments, the independent segments are nested with respect to each other with double-sided nano tape positioned therebetween such that the nested segments have side surfaces in direct contacting engagement with the nano tape.
  • 27. The helmet as recited in claim 19 wherein the first type of subliner elements are radially partitioned into individual and independent segments, the independent segments are nested with respect to each other with double-sided nano tape positioned therebetween such that the nested segments have side surfaces in direct contacting engagement with the nano tape.
US Referenced Citations (147)
Number Name Date Kind
2835313 Dodge May 1958 A
3425061 Webb Feb 1969 A
3577562 Holt May 1971 A
3877076 Summers et al. Apr 1975 A
3943572 Aileo Mar 1976 A
4290149 Aileo Sep 1981 A
4307471 Lovell Dec 1981 A
4345338 Frieder, Jr. et al. Aug 1982 A
4534068 Mitchell et al. Aug 1985 A
4586200 Poon May 1986 A
5030501 Colvin et al. Jul 1991 A
5204998 Liu et al. Apr 1993 A
5589016 Hoopingarner et al. Dec 1996 A
5713082 Bassette et al. Feb 1998 A
5815846 Calonge Oct 1998 A
5956777 Popovich Sep 1999 A
5970550 Gazes Oct 1999 A
6070271 Williams Jun 2000 A
6070905 Renault Jun 2000 A
6219850 Halstead et al. Apr 2001 B1
6298497 Chartrand Oct 2001 B1
6308490 Saebi Oct 2001 B1
6324700 McDougall Dec 2001 B1
6453476 Moore, III Sep 2002 B1
6658671 Von Holst et al. Dec 2003 B1
6871525 Withnall et al. Mar 2005 B2
6934971 Ide et al. Aug 2005 B2
6968575 Durocher Nov 2005 B2
7240376 Ide et al. Jul 2007 B2
7367898 Hawkins et al. May 2008 B2
7461726 Hawkins et al. Dec 2008 B2
7603725 Harris Oct 2009 B2
7676854 Berger et al. Mar 2010 B2
7774866 Ferrara Aug 2010 B2
7802320 Morgan Sep 2010 B2
7832023 Crisco Nov 2010 B2
7900279 Kraemer et al. Mar 2011 B2
7930771 Depreitere et al. Apr 2011 B2
7954177 Ide et al. Jun 2011 B2
7954178 Durocher et al. Jun 2011 B2
8015624 Baldackin et al. Sep 2011 B2
8127373 Fodemski Mar 2012 B1
8166574 Hassler May 2012 B2
8191179 Durocher et al. Jun 2012 B2
8196226 Schuh Jun 2012 B1
8347421 Krueger Jan 2013 B2
8365315 Ortiz et al. Feb 2013 B2
8387164 Maddux et al. Mar 2013 B2
8402715 Uhllg et al. Mar 2013 B2
8578520 Halldin Nov 2013 B2
8640267 Cohen Feb 2014 B1
8931606 Hawkins et al. Jan 2015 B2
8955169 Weber et al. Feb 2015 B2
9032558 Leon May 2015 B2
9578917 Cohen Feb 2017 B2
9975032 Frey May 2018 B2
10869520 Leon Dec 2020 B1
11547166 Leon Jan 2023 B1
20010031350 Day et al. Oct 2001 A1
20020023291 Mendoza Feb 2002 A1
20020056521 Chen et al. May 2002 A1
20030140400 Ho Jul 2003 A1
20040117896 Madey et al. Jun 2004 A1
20040250340 Piper et al. Dec 2004 A1
20050246824 Berger et al. Nov 2005 A1
20060031978 Pierce Feb 2006 A1
20060059606 Ferrara Mar 2006 A1
20060070170 Copeland et al. Apr 2006 A1
20060112477 Schneider Jun 2006 A1
20070068755 Hawkins et al. Mar 2007 A1
20080066217 Depreitere et al. Mar 2008 A1
20080120764 Sajic May 2008 A1
20080155735 Ferrara Jul 2008 A1
20080256685 Lampe et al. Oct 2008 A1
20090000377 Shipps et al. Jan 2009 A1
20090024406 Rawls-Meehan Jan 2009 A1
20090151056 Desjardins et al. Jun 2009 A1
20090218185 Lin Sep 2009 A1
20090265839 Young et al. Oct 2009 A1
20090320185 Hassler Dec 2009 A1
20100005573 Rudd et al. Jan 2010 A1
20100299812 Maddux et al. Dec 2010 A1
20100319109 Field Dec 2010 A1
20110072587 Cao et al. Mar 2011 A1
20110107503 Morgan May 2011 A1
20110117310 Anderson et al. May 2011 A1
20110131695 Maddux et al. Jun 2011 A1
20110171420 Yang Jul 2011 A1
20110252544 Abernethy Oct 2011 A1
20110271427 Milsom Nov 2011 A1
20110277221 Ide et al. Nov 2011 A1
20120047635 Finiel et al. Mar 2012 A1
20120096631 King et al. Apr 2012 A1
20120143526 Benzel et al. Jun 2012 A1
20120151663 Rumbaugh Jun 2012 A1
20120151664 Kirshon Jun 2012 A1
20120186002 Bhatnagar et al. Jul 2012 A1
20120186003 Heger et al. Jul 2012 A1
20120192337 Divine et al. Aug 2012 A1
20120198604 Weber et al. Aug 2012 A1
20120198605 Maddux et al. Aug 2012 A1
20120204329 Faden et al. Aug 2012 A1
20120207964 Faden et al. Aug 2012 A1
20120208032 Faden et al. Aug 2012 A1
20120216339 Nimmons et al. Aug 2012 A1
20120233745 Veazie Sep 2012 A1
20120266365 Cohen Oct 2012 A1
20120266366 Ferrara Oct 2012 A1
20120297525 Bain Nov 2012 A1
20120304366 Daoust Dec 2012 A1
20120304367 Howard et al. Dec 2012 A1
20120317705 Lindsay Dec 2012 A1
20120324634 Coyle Dec 2012 A1
20130000016 Hall et al. Jan 2013 A1
20130000017 Szalkowski et al. Jan 2013 A1
20130000018 Rudd et al. Jan 2013 A1
20130007950 Arai Jan 2013 A1
20130019384 Knight Jan 2013 A1
20130019385 Knight Jan 2013 A1
20130025031 Laperriere et al. Jan 2013 A1
20130025032 Durocher et al. Jan 2013 A1
20130025033 Durocher et al. Jan 2013 A1
20130036531 Belanger et al. Feb 2013 A1
20130040524 Halldin et al. Feb 2013 A1
20130042397 Halldin Feb 2013 A1
20130055488 Garneau Mar 2013 A1
20130061371 Phipps et al. Mar 2013 A1
20130061372 Goldstein Mar 2013 A1
20130061375 Bologna et al. Mar 2013 A1
20130111654 Gorsen et al. May 2013 A1
20130122256 Kleiven et al. May 2013 A1
20130185837 Phipps et al. Jul 2013 A1
20130254978 McInnis et al. Oct 2013 A1
20130291289 Szalkowski et al. Nov 2013 A1
20130340147 Giles Dec 2013 A1
20140013492 Bottlang et al. Jan 2014 A1
20140020158 Parsons et al. Jan 2014 A1
20140096311 Halldin Apr 2014 A1
20140170372 Fink Jun 2014 A1
20140196198 Cohen Jul 2014 A1
20140196998 Nauman et al. Jul 2014 A1
20150000018 Brandt Jan 2015 A1
20150223546 Cohen Aug 2015 A1
20160021965 Mayerovitch Jan 2016 A1
20170065018 Lindsay Mar 2017 A1
20180249778 Brandt et al. Sep 2018 A1
20190029352 Sadegh et al. Jan 2019 A1
Foreign Referenced Citations (6)
Number Date Country
101850638 Oct 2010 CN
4226588 Feb 1994 DE
1142495 Oct 2001 EP
2530309 Mar 2016 GB
2004032659 Apr 2004 WO
2020236930 Nov 2020 WO
Non-Patent Literature Citations (27)
Entry
Rowson et al., “Linear and Angular Head Acceleration Measurements in Collegiate Football,” Journal of Biomechanical Engineering, Vo. 131, 7 pages (Jun. 2009).
Broglio et al., “Biomechanical Properties of Concussions in High School Football,” Medicine and Science in Sports Exercise; www.medscape.com, pp. 1-10, (Nov. 23, 2010).
Greenwald et al., “Head Impact Telemetry System (HITSTM) for Measurement of Head Acceleration in the Field,” American Society of Biomechanics—2003 Annual Meeting, 2 pages.
Daniel et al., “Head Impact Exposure in Youth Football,” Annals of Biomedical Engineering, 6 pages (Feb. 15, 2012).
ASTM F 1446-04, “Standard Test Methods for Equipment and Procedures Used in Evaluating the Performance Characteristics of Protective Hedgear,” ASTM International, pp. 1-11 (date: unknown).
“Head Injuries in Football,” The New York Times, pp. 4 (Nov. 16, 2011).
Rousseau et al., “A Comparison of Peak Linear and Angular Headform Accelerations Using Ice Hockey Helmets,” Journal of ASTM International; www.astm.org, vol. 6, No. 1, 11 pages (Feb. 20, 2009).
Rowson et al., “Development for the STAR Evaluation System for Football Helmets: Integrating Player Head Impact Exposure and Risk of Concussion,” Annals of Biomedical Engineering, 11 pages (May 7, 2011).
Rousseau et al., “The Influence of Deflection and Neck Compliance on the Impact Dynamics of a Hybrid III Headform,” Proceedings of the Institution of Mechanical Engineers, vol. 223, Part P: J. Sports Engineering and Technology, pp. 89-97 (Apr. 3, 2009).
“2011 Concussion Report—End of Regular Season,” 4 pages (Jan. 10, 2012).
Shipley, “Traumatic Brain Injury and Diffuse Axonal Injury,” Trial Image Inc.; www.trialimagestore.com, pp. 1-5 (Feb. 18, 2011).
Newman et al., “A New Biomechanical Assessment of Mild Traumatic Brain Injury Part 2—Results and Conclusions,” 11 pages, (date: unknown).
King et al., “Is Head Injury Caused by Linear or Angular Acceleration?,” IRCOBI Conference, pp. 1-12 (Sep. 2003).
NOCSAE Doc (ND) 001-11M11, “Standard Test Method and Equipment Used in Evaluating the Performance Characteristrics of Protective Headgear Equipment,” NOCSAE/National Operating Committee on Standards for Athletic Equipment, pp. 1-25 (Jan. 2012).
NOCSAE Doc (ND) 002-11m11a, “Standard Performance Specification for Newly Manufactured Football Helmets,” NOCSAE/National Operating Committee on Standards for Athletic Equipment, pp. 1-6 (Feb. 2012).
“NOCSAE receives $1.1M Research Grants to Advance Science of Sports Medicine,” 2 pages (Jun. 20, 2011).
“Helmet Safety Group Approves Research Grants,” SFGate.com, 1 page (Jun. 18, 2011).
Bartholet, “The Collision Syndrome,” Scientific American, pp. 68-71 (Feb. 2012).
Kluger, “Headbanger Nation. Concussions are clobbering U.S. kids. Here's why,” Time Magazine, pp. 42-51 (Jan. 31, 2011).
“Concussion,” Wikipedia, 17 pages (page last modified on May 21, 2012).
“Frustoconical,” Wiktionary, N.p., n.d. Web. Aug. 4, 2015.
“Frustum.” Wiktionary. N.p., n.d. Web. Aug. 4, 2015.
“EZ Dri.” INOAC. INOAC, n.d. Web Mar. 2, 2016.
“Outdoor Foam Cushion, Waterproof Foam, Patio Cushion, Furniture Cushions.” Outdoor Foam Cushion, Waterproof Foam, Patio Cushion, Furniture Cushions. N.p., n.d. Web Mar. 2, 2016.
“Reticulated Polyurethane Foam”, Producer of Custom-Engineered Components, Products & Packaging, 4 pages (Oct. 2016).
Qi, HJ and Boyce, MC, Stress-strain Behavior of Thermoplastic Polyurethane. Submitted to Mechanics of Materials. Submitted Dec. 2003, Revised Jul. 2004.
Orringer, et al., Crash Padding Research, vol. 1, Material Mechanical Properties, Final Report, Accessed through the National Academies of Sciences, Engineering Medicine, 1986-87.