• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:

    公开号:SE538785C2
    申请号:SE1350471
    申请日:2011-08-01
    公开日:2016-11-22
    发明作者:Marz Michael；Dalzell Jeffrey
    申请人:Cortex Armour Inc；
    IPC主号:
    专利说明:

    [1] The present application relates generally to a shock-absorbing layer for protective helmets, more particularly to such a layer which contains multiple shock-absorbing features designed to dampen the energy of a shock and to protect the helmet wearer from damage due to linear and angular accelerations occurring during such a shock.
    [2] Helmets are often worn during sports and other activities to protect against injuries from shocks and / or accelerations to the brain. Helmets can generally be classified into two categories that use different shock absorption techniques: disposable helmets for a single shock effect and reusable helmets for multiple shock effects. Design constraints for each helmet typically include the overall size, weight, aesthetic commercial potential of the concept, and compliance with all regulatory shock standards associated with the type of helmet in question.
    [3] In disposable helmets, such as typical bicycle, ski and motorcycle helmets, the shock absorbing elements are usually subjected to permanent deformation upon impact or impact. In reusable helmets, such as helmets typical of hockey, lacrosse and American football, the shock-absorbing elements are designed to withstand multiple blows and shocks with little to no permanent deformation.
    [4] Some reusable helmets use materials made of either vinyl nitrile (VN) or expanded polypropylene (EPP). These materials may exhibit deteriorated properties after multiple shock effects due to insignificant plastic deformation after each impact, which may cause a decrease in the material thickness in the impact zone and consequently an increase in the material density, which makes the material harder and may result in impaired energy treatment / conversion .
    [5] Other known reusable helmets comprise a shock absorbing layer of compressible cells containing a fluid, e.g. air, the cells being closed except for a small passage which allows the fluid to exit when the cell is compressed. The cell typically has such a structure that it resists compression at the initial stage of the impact, the passage having a throttling effect on the fluid moving at high speed; the cell is then progressively compressed as the fluid slowly exits the passage. However, such a mechanism requires that the individual cells have a relatively large dimension, in order for the fluid in the cells to have an effect on their resistance to the shock. The use of larger cells can prevent optimal coverage of the shock-absorbing layer inside the helmet, so that it does not provide a proper full-coverage protection.
    [6] Due to insufficient measurement methods at the time, it was considered in previous research that linear and angular accelerations were strongly correlated with respect to criteria for head injuries during shocks; this led researchers to focus only on linear accelerations to determine levels of head injuries, as it was the easiest of the accelerations to measure. In itself, today's helmet standards only measure linear accelerations as criteria for pass / fail, without mentioning angular accelerations.
    [7] New research findings seem to indicate that angular accelerations can vary significantly from linear accelerations under certain shock conditions, and potentially even called-on larger forces can therefore cause greater damage if not handled properly. For example, angular accelerations can be significant and even destructive when a shock is received next to the center of mass and consequently causes a greater degree of rotation, a scenario that is very likely in all sports activities where a helmet is needed as protection.
    [8] On the whole, when the density, stiffness, and thickness or height of the shock absorbing elements are varied, proportionally linear shock handling characteristics are obtained. However, known typical shock absorbing elements provide little shock absorption at angular acceleration.
    [9] For example, a type of known impact technique utilizes a plurality of shock absorbing elements that are interconnected by tissue (webbing). The fabric typically allows loads to be transferred between the elements and consequently limits lateral movement during collapse / compression of the interconnected elements. The tissue also increases the bending resistance of the tubular elements and can in itself prevent proper shock absorption during angular acceleration.
    [10] Improvements are thus desirable.
    [11] An object of the invention is therefore to provide an improved shock-absorbing layer, which is particularly suitable for use in reusable helmets but also suitable for use in other helmets and / or other types of sports equipment.
    [12] Therefore, in accordance with the present invention, there is provided a shock absorbing layer for a helmet, the layer comprising: a base plate; and a plurality of spaced shock absorbing members arranged on the base plate and interconnected only therethrough, each shock absorbing member being independently and elastically compressible to at least partially receive a shock load on the helmet, the shock absorbing members being hollow and defining a closed circumferential wall extending upwardly from the base plate to an open upper end which is dimensioned to cause insignificant reduction of fluid flow exiting the shock absorbing member, the closed circumferential wall of each shock absorbing member comprising at least one wall section, each wall section having: a first portion having: opposite inner and outer surfaces each having the shape of a truncated tapered portion, and a second portion extending upwardly from the first portion and formed integrally therewith, the second portion having opposite inner and outer surfaces which were and one has the shape of a stump d tapered portion, the inner surfaces of the first and second portions being interconnected by relatively radially larger ends of their respective truncated tapered portions to define an inner angle less than 180 degrees between the inner surfaces of the first and second portions, and wherein the outer surfaces of the first and second portions are interconnected by relatively radially larger ends of their respective truncated tapered portions to define an outer angle greater than 180 degrees between the outer surfaces of the first and second portions.
    [13] According to the invention there is also provided a shock absorbing layer for a helmet, the shock absorbing layer comprising: a base plate; a plurality of spaced apart and independently compressible primary shock absorbing elements which are hollow and have a closed circumferential wall extending from the base plate to an open upper end, the closed circumferential wall defining at least one wall section having a radially outwardly curved shape forming a diverging shape. converging wall profile defining radially smaller upper and lower ends and a radially larger central portion, the radially larger central portion of the wall section forming a maximum width of the primary shock absorbing member located between the open upper end thereof and the base plate; and a secondary shock absorbing member extending from the base plate within the closed peripheral wall of each primary shock absorbing member and acting independently of the primary shock absorbing member.
    [14] The invention further provides a sports helmet comprising: an outer casing; and a shock absorbing layer comprising a base plate and a plurality of spaced apart and independently acting hollow shock absorbing elements, which are elastically compressible to at least partially receive a shock load on the helmet, shock absorbing elements extending from an outer surface of the base plate and interconnected only through the base plate, the shock absorbing members having an open upper end located adjacent an inner surface of the outer housing and dimensioned to cause a slight decrease in fluid flow exiting the hollow member, the shock absorbing members comprising a closed circumferential wall having at least wall section, each of said wall section having a first portion having opposite inner and outer surfaces, each of which is in the form of a truncated tapered portion, a second portion extending upwardly from the first portion and having opposite inner and outer surfaces each of which is in the form of a truncated tapered portion, wherein the inner surfaces of the first and second portions are interconnected by relatively larger ends of their respective truncated tapered portions, and wherein the outer surfaces of the first and second portions are interconnected by relatively larger ends of their respective truncated tapered portions.
    [15] Reference will now be made to the accompanying drawings, which for the purpose of illustration illustrate a particular embodiment of the present invention and in which:
    [16] FIG. 1 is a perspective view of a shock absorbing layer according to a particular embodiment;
    [17] FIG. 2 is a perspective view of a shock absorbing element of the layer of FIG. 1;
    [18] FIG. 3 is a longitudinal sectional view of the element of FIG. 2;
    [19] FIG. 4 is a perspective view of a shock absorbing element according to another embodiment;
    [20] FIG. 5 is a longitudinal sectional view taken along line 5-5 of the element of FIG. 4;
    [21] FIG. 6 is a longitudinal sectional view taken along line 6-6 of the element of FIG. 4;
    [22] FIG. 7A is a schematic upper cross-section of the elements of FIG. 4;
    [23] FIG. 7B-7C are a schematic upper cross-section of shock absorbing elements according to various embodiments;
    [24] FIG. 8 is a longitudinal sectional view of a shock absorbing member according to a further embodiment; and
    [25] FIG. 9 is a schematic longitudinal sectional view of a helmet incorporated with the shock absorbing layer of FIG. 1.
    [26] Referring to FIG. 1, a shock absorbing layer 10 according to an embodiment of the invention is shown. As schematically shown in FIG. 9, the shock absorbing layer 10 is designed for use as part of the inner structure of a safety helmet 8, such as a helmet used for sports such as hockey, lacrosse, American football, motorsports, winter sports, motorcycle sports and / or cycling. The helmet 8 can be a reusable helmet or a disposable helmet. However, the helmet 8 with the shock-absorbing layer 10 can alternatively be used for other types of sports or in non-sports / sports contexts, such as a protective helmet or "hard hat" used e.g. in the construction industry.
    [27] The shock-absorbing layer of the helmet 8 may be sandwich-like interposed between an inner damping layer 11, made of e.g. foam material, and the rigid outer shell 13 of the helmet, which may be made of hard plastic, although a number of other protective, decorative or comfort-enhancing layers or elements may additionally be provided. Although the damping layer 11 is shown to be continuous, it may alternatively be arranged in a plurality of pieces which abut each other, are arranged at a distance from each other, overlap each other or any combination thereof. Although the outer shell 13 is shown continuously, it may alternatively be arranged in two or more pieces, for example by having front and rear shell portions which slidably engage each other for size adjustment. The shock-absorbing layer 10 can also be arranged in a plurality of cooperating pieces, which will be further described in the following. Other helmet configurations are also possible.
    [28] Returning to FIG. 1, the shock absorbing layer 10 includes a base plate 12 and a plurality of independent, or independently collapsible / compressible, shock absorbing members 14 extending therefrom. Although not shown, the base plate 12 may include holes, openings, etc. thereby delimited in non-critical areas for weight loss purposes, for example between adjacent shock absorbing elements. The shock absorbing elements allow the handling of shock absorption in the helmet by damping both linear and angular accelerations, which will be further explained in the following.
    [29] In a particular embodiment, the shock absorbing elements 14 are injection molded directly on the base plate 12. Alternatively, the elements 14 may be cast separately from the base plate 12 and connected thereto by any suitable method, e.g. by using welding or binder. In a particular embodiment, the base plate 12 and the shock absorbing elements 14 are made of a suitable type of thermoplastic elastomer (TPE), such as, but not limited to, a polyurethane elastomer (TPU), a copolyamide (TPA), a copolyester (TPC). , a ployolefin elastomer (TPO) or a thermoplastic elastomer of polystyrene (TPS). Suitable materials that can be used preferably provide superior flexibility even at low temperatures, good abrasion resistance, high elasticity with sufficient mechanical strength, and are preferably injection moldable.
    [30] The base plate 12 serves as an anchor point for the many shock-absorbing elements 14. The base plate 12 also becomes part of the inner helmet structure. A complete system for a helmet comprises a plurality of cast base plates 12, which are designed, engineered and optimized for special applications. The shock absorbing layer 10 of FIG. 1 is shown in the form of an example; the geometry of the base plate or plates and the amount and location of the shock absorbing elements on each base plate depend on the application. In the embodiment shown, the elements 14 are arranged in lines of identical rows and identical columns extending perpendicular to the rows. Alternative arrangements are also possible, for example rows and / or columns having mutually deviating number of elements, rows extending at an angle deviating from the perpendicular to the columns, distributed in an irregular manner, offset with respect to each other, etc. For example, in a special embodiment not shown, the shock-absorbing layer comprises rows of 3 elements, which alternate with rows of 2 elements.
    [31] Referring to FIG. 2-3, the shock absorbing elements 14 are independent of each other, i.e. they are interconnected only by the base plate 12. Each shock absorbing member 14 includes a hollow primary shock absorbing member 16, which is configured to flex elastically when a sufficient load is applied. The hollow primary shock absorbing member 16 has a closed circumferential wall extending upwardly from the base plate to an open end dimensioned to cause insignificant reduction in fluid flow exiting the shock absorbing member. The closed circumferential wall of each shock absorbing element comprises at least one wall section, each wall section having a radially outwardly curved shape and thereby defining a diamond-shaped or barrel-shaped outer periphery, i.e. one which is diverging-converging to define radially smaller upper and lower ends of the wall section and a radially larger central portion, such as e.g. shown in FIG. Several such sections may be formed in one piece and vertically stacked, such as to form a bellows-like structure, as shown in FIG. 8 and will be described in more detail below. The hollow primary shock absorbing member 16 of FIG. 3 has a bottom portion 18 extending from the base plate 12 and an upper portion 20 extending from the lower portion 18. Each portion 18, 20 has a closed inner circumference formed by one or more walls 22. The lower and upper portions 18, 20 has inner and outer surfaces 24, 26, 28, 30 which each have the shape of a rather tapered truncated part, i.e. the shape of a truncated cone or pyramid, which lies between two parallel planes extending perpendicular to its axis. In the embodiment shown, the inner and outer surfaces 24, 26, 28, 30 of both the lower and upper portions 18, 20 have a truncated conical shape, i.e. has a circular cross-section, so that each of the lower and upper portions comprises a single wall defining its closed circumference. Tapered truncated parts with alternative shapes are also possible, ie. with a cross-section having a non-circular shape.
    [32] The relatively larger (i.e., radially larger) end of the tapered truncated portion of the inner surface 26 of the upper portion 20 is connected to the relatively larger (i.e., radially larger) end of the tapered truncated portion of the inner surface. 24 of the lower portion 18; similarly, the relatively larger end of the tapered truncated portion of the outer surface 28 of the upper portion 20 is connected to the relatively larger end of the tapered truncated portion of the outer surface 28 of the lower portion 18. In itself, it has the wall 22 of the primary element 19 has a radially outwardly curved or curved shape which forms a diamond-shaped profile. In the embodiment shown, the wall 22 of the primary element 16 has a constant thickness; the angle i i between the inner surfaces 24, 26 of the two portions 18, 20 and the angle O 0 between the inner surfaces 28, 30 of the two portions 18, 20 are conjugate angles, i.e. their sum is 360 ° and © i <1800 and 0O> 180 °. Alternatively, the thickness of the wall 22 may vary across the height of the primary element 16, so that the two angles © i, © o are not conjugate angles, while still © i <180 ° and © o> 180 °. Although the lower and upper portions 18, 20 are shown as having the same height, alternatively their height may be different, so that the connection between their tapered truncated parts is not located at the midpoint of the height of the primary element 16.
    [33] The base plate 12 provides that the primary member 16 has a closed lower end 34, while the upper portion 20 defines an open upper end 32 which is dimensioned to cause an insignificant or negligible decrease in the fluid (eg air) which emerges from the primary element 16 upon compression. In the present description and claims, "insignificant reduction of the flow" also includes a configuration in which no flow reduction occurs at all. The fluid can therefore emerge freely or substantially freely from the primary element 16 when it is compressed. Accordingly, the shock absorbing member 14 is not dependent on the fluid contained therein to handle or handle the shock.
    [34] In a particular embodiment, the ratio between the height H of the primary element 16 and its maximum width W, defined by the connection between the lower and upper portions 18, 20, is at least 1, i.e. the height H is at least equal to the maximum width W. In the embodiment shown, the ratio H / W between height and maximum width (or maximum diameter since the lower and upper portions 18, 20 are frustoconical) is approximately 1.28.
    [35] Under axial load, the outwardly curved shape of the wall (s) 22 defining the closed circumferential wall of the primary element 16 allows it to be compressed in a controlled manner after its critical load has been exceeded. In an uncontrolled buckling scenario with an axial load acting on a cylinder of an elastic material which is not broken by a shock, the material will typically be compressed / collapse on itself; uncontrolled collapse usually results in loss of effective shock-absorbing rigidity, and can cause unwanted permanent deformation of the cylinder. Instead of collapsing on its own, the primary element 16 expands radially outward to avoid material compression. This expansion optimizes the control or management of the shock absorption handling by resulting in better consistency of the shock handling as well as improved compression of the primary element. The thickness of the wall (s) 22 is selected to provide a desired level of resistance to linear loads. The distance between adjacent shock-absorbing elements 14 on the base plate 12 is consequently chosen to avoid mutual influence or interference during this radial expansion caused by a shock.
    [36] During a tangential load, such as that caused by an angular acceleration, each primary element 19 can be independently deformed, since the elements 14 are not interconnected except via the base plate 12. An angular acceleration typically generates a tangential load at the upper the part of the element 16, and the elements 16 are deflected as or substantially as a fixed clamped beam which is loaded at its maximum distance from the anchoring point of the beam, which corresponds to the base plate 12.
    [37] The deflection of a fixed clamped beam can be expressed as Image available on "Original document" Where the applied tangential force, / is the clamping length, is the modulus of elasticity of the material, and / (the second) moment of inertia. In themselves, the variables which affect the deflection of the beam are its length /, which in the case of the element 16 corresponds to the height H, and the second moment of inertia /. Usually, the height of the element 16 is determined by the ability of a helmet to pass a standardized test and by the ability of the helmet on the market, since a larger sized helmet could not be commercially successful for aesthetic reasons. While the height H of the element 16 can be varied to achieve the desired deflection to absorb tangential shocks, in most cases the moment of inertia / property of the element 16 which becomes the primary variable for tangential shock absorption. Accordingly, the shape of the element 16, the wall thickness and the ratio of height to maximum width H / W are selected to obtain the moment of inertia / which provides a desired level of resistance to tangential loads. The distance between adjacent shock absorbing elements 14 on the base plate 12 is also selected to avoid mutual interference or interference during the deflection caused by tangential loads.
    [38] The shock absorbing element 14 thus allows handling of angular accelerations by optimizing the ratio of height to maximum width HA / V and the wall thickness of the primary element 16, and handling of linear accelerations by optimizing the wall thickness and wall angles of the primary element 16.
    [39] In the embodiment shown, the angles over the entire length of the primary element 16, shown schematically at 38 in FIG. 3, at least when the primary element 18 is uncompressed (ie in its natural or dormant state). This tubular portion 38 (which does not differ from the rest of the wall 22) acts like a thin-walled bar under an axial load, and as such can provide initial impact load handling until the critical buckling load is reached for this bar. However, this continuously tubular material portion 38 need not be present, i.e. a larger angle © i and a smaller angle 0O can be used in some cases. These may include, but are not limited to, cases where the necessary resistance of the shock absorbing layer 10 is sufficiently small and / or where the resistance of the material used for the primary element 16 is sufficiently large.
    [40] In the embodiment shown, the shock absorbing member 14 further comprises a board 36 located around the open end 32 of the primary member 16 and acting as a stiffening function which helps to prevent the wall (s) 22 from collapsing when an axial or tangential load is applied to the element 14. This stiffening function allows the use of thinner wall structures in order to optimize the construction and reduce the weight; in cases where the thickness of the wall (s) 22 of the primary element 16 is sufficient to guarantee controlled collapse / compression, the board can be dispensed with. In the embodiment shown, the board is rounded and extends only radially from the wall 22 of the primary element 16. Alternatively, the board may extend only radially inwards from the wall or both radially inwards and outwards therefrom, and may have alternative shapes, for example delimited by a tapered cross-section at the upper end of the wall 22. The board 36 is shown as continuous around the open end 32, but may alternatively be formed by a plurality of angularly spaced sections. In the configurations where the board extends radially inwardly, the board is dimensioned to cause a negligible decrease in the flow of fluid exiting the primary member 16 through the open upper end 32 upon compression.
    [41] Referring to FIG. 3, when increased shock resistance is required and handling of a plurality of shock levels, the shock absorbing member 14 further includes a secondary shock absorbing member 40 extending from the base plate 12 within and at the center of each primary member 16. In a particular embodiment, it is the secondary element 40 hollow and also the injection molded directly on the base plate 12, at the same time as the primary shock absorbing element 16, so that the layer 10 is monolithic. In the embodiment shown, the secondary element 40 is a tubular element with a cylindrical configuration and an open upper end 42. In an alternative embodiment, the secondary shock-absorbing element also has two portions shaped as tapered truncated parts, e.g. truncated conical parts, the largest ends of which are interconnected. In this case, the profile of the secondary element 40 may be a mirror image of the primary element 16 (eg equal angles © i, 0O). In another alternative embodiment, the secondary shock absorbing member 40 has a single portion formed as a tapered frustoconical portion, for example, a single frustoconical portion, the relatively smallest end of which is connected to the base plate 12. In another alternative embodiment, the secondary shock absorbing member 40 has a lower portion which is truncated conically, the relatively largest end of which is connected to a cylindrical upper portion. Secondary elements 40 with cross-sections other than circular are also possible. The secondary elements 40 do not necessarily have to be hollow; for example, the secondary elements 40 may be solid and made of a suitable type of shock-rated foam, e.g. vinyl nitrile (VN) or expanded polypropylene (EPP) foam. The primary and secondary elements 16, 40 are independent of each other, i.e. they are interconnected only via the base plate 12. In an alternative embodiment not shown, the primary and secondary elements 16, 40 extend from the base plate 12 in a manner where they are arranged side by side instead of concentrically.
    [42] The height of the secondary element 40 is preferably at least 2 mm and in the embodiment shown extends up to half the height of the primary element 16. The secondary element 40 is arranged for handling shocks with high energy after the wall of the primary element 16 22 has begun to yield, to prevent the shock absorbing member 14 from bottoming out, which could result in higher maximum accelerations.
    [43] Referring to FIG. 4-6 and 7A, a shock absorbing member 114 according to an alternative embodiment of the invention is shown. This embodiment can exhibit an improved independent setting for angular and linear acceleration management compared to the last described embodiment. The independent shock absorbing elements 114 are arranged on a base plate similar to that of FIG. 1 and described above.
    [44] As in the previous embodiment, the member 114 includes a hollow primary shock absorbing member 116 having a lower portion 118 extending from the base plate 12 and an upper portion 120 extending from the lower portion and defining an open upper end 132 which is also dimensioned to cause an insignificant decrease in the flow of the fluid exiting the primary member 216 upon compression. Each portion 118, 120 has a closed circumference formed by one or more walls 122. The relatively larger ends of the tapered truncated portions of the lower and upper portions 124, 126 inner surfaces are directly interconnected, and the relatively larger ends of the tapered portions the truncated portions of the outer surfaces 128, 130 of the lower and upper portions are interconnected by an annular flange 144 extending around the circumference. In an alternative embodiment, the annular flange 144 may be omitted. The element 114 also includes a secondary shock absorbing member 140 similar to the previously described secondary member 40. In an alternative embodiment, the secondary shock absorbing member 140 may be omitted.
    [45] In this embodiment, the shock absorbing member 114 further includes a plurality of vertically oriented flanges 146 which extend only radially outwardly from the wall 122 of the primary member 116, from the base plate 12 to the open upper end 132. Although four flanges 146 are shown, alternative embodiments may have more or fewer flanges. In the embodiment shown, the flanges 146 follow the contour of the wall 122, i.e. they have a radially outwardly curved shape when the element 114 is viewed in longitudinal section (e.g. FIG. 5). Alternatively, the flanges 146 need not follow the wall 122, e.g. they may be formed by two parts extending at an angle deviating from the angles © i, 0O.
    [46] The annular flange 144 provides support for the vertically oriented flanges 146, and the board 136 surrounding the open end 132 includes breaks at the position of the flanges 146. Alternatively, the upper end of the flanges 146 may be formed into a continuous board.
    [47] In an alternative embodiment schematically shown in FIG. 7B, the flanges 146 'extend only radially inwardly from the wall 122'. In another alternative embodiment schematically shown in FIG. 7C, the flanges 146 "extend both radially inwardly and outwardly from the wall122". The flanges 146, 146 ', 146 "are designed to allow controlled outward expansion of the wall 122, 122', 122" during the compression of the primary member 116. The cross section of the flanges 146, 146 ', 146 "may be of any shape. , to the extent that there is a difference in the effective second moments of inertia of the cross section relative to the direction of the load causing the bending moment. , and the flanges 146b and 146d have equally other moments of inertia, which is less than that of the flanges 146a and 146. The flanges 146a and 146c are thus those which provide the primary contribution to the handling of the deflection of the element under the force F, due to their larger second moments of inertia. The varying effective moments of inertia of the flanges 146, 146 ', 146 "allow variable flange interaction and handling of the bending moment on the element. The flanges 146, 146 ', 146 ", acting as beams, offer more resistance to bending when oriented so that their second moment of inertia is the greatest.
    [48] The presence of the flanges 146, 146 ', 146 "may allow improved handling of angular accelerations, while still maintaining optimized handling of linear accelerations. The handling of angular accelerations is mainly affected by the dimensioning of the flanges 146, 146', 146". , while the handling of linear accelerations is affected by the thickness of the wall (s) 122, 122 ', 122 "of the primary element 116 and the radial thickness of the flanges 146, 146', 146"; per se, the axial loads and bending moments can be handled substantially independently, so that the optimization of the shock absorbing element 114 while handling a specific type of load (tangential or linear) has a limited effect on how the element 114 is optimized to handle the second type.
    [49] Referring to FIG. 8 shows a shock absorbing element 214 according to an alternative embodiment. The independent shock absorbing elements 214 are also arranged on a base plate 12 similar to that shown in FIG. 1 and described above. Each element 214 includes a hollow primary shock absorbing member 216 and is shown herein with a secondary shock absorbing member 240 similar to the previously described secondary member 40. In an alternative embodiment, the secondary shock absorbing member 40 may be omitted.
    [50] The primary shock absorbing member 216 has a lower portion 218 extending from the base plate 12, a first intermediate portion 217 extending from the lower portion 218, a second intermediate portion 219 extending from the first intermediate portion 217, and an upper portion 220 extending from the second intermediate portion 219. The upper portion defines an open upper end 232 surrounded by a rim 236, also dimensioned to cause an insignificant reduction in the flow of the fluid exiting the primary element. 216 by compression. Each portion 217, 218, 219, 220 has a closed circumference formed by one or more walls 122. Each portion 217, 218, 219, 220 has an inner surface 123, 124, 125, 126 and an outer surface 127, 128, 129. 130 having the shape of a straight tapered truncated part, preferably a truncated conical shape, although alternative shapes of tapered truncated parts are also possible, e.g. with cross-sections having a non-circular shape. The lower portion 218 and the first intermediate portion 217 have their inner surfaces 124, 123 and their outer surfaces 128, 127 interconnected at the relatively larger ends of their tapered truncated portions. The first and second intermediate portions 217, 219 have their inner surfaces 123, 125 and their outer surfaces 127, 129 interconnected at the relatively smaller (i.e., radially smaller) ends of their tapered truncated portions. The second intermediate portion 219 and the upper portion 120 have their inner surfaces 125, 126 and their outer surfaces 129, 130 interconnected at the relatively larger ends of their tapered truncated portions. In itself, the wall 222 of the primary element 216 is in the form of a bellows, with two sections which are bent outwards at the upper and lower ends and with a radial inward bend between these two sections. In the embodiment shown, the wall 222 of the primary element 216 has a constant thickness, and the two bellows sections, i.e. the section delimited by the lower portion 218 and the first intermediate portion 217 and the section delimited by the second intermediate portion 219 and the upper portion 120, have a similar geometry. In themselves, the two bellows sections are compressed to a similar extent, but need a smaller radial footprint, ie. less radial space to cause the element 16 in FIG. 1 has equal dimensions.
    [52] Alternatively, the thickness of the wall 222 may vary across the height of the primary element 216. Although the portions 217, 218, 219, 220 are shown with equal height, alternatively their height may be different. The connection between the second intermediate portion 219 and the upper portion 120 may also define a different width than the connection between the lower portion 218 and the first intermediate portion 217. Thus, if the two bellows sections have different geometric constructions, they may be designed to be compressed / collapse to varying degrees. This can achieve better energy management from low to high energy within a structure. In this type of construction, the secondary element 240, for example extending up to below the connection between the intermediate portions 217, 219, acts as a third energy handling element.
    [53] The shock absorbing elements 14, 114, 214 consequently allow the handling of both linear and angular accelerations and, by the presence of the secondary element 40, 140, 240, the handling of several shock levels. The geometry of the shock absorbing member 14, 114, 214 provides a controlled compression / collapse, which increases the predictability of its occurrence. The integral shock absorbing elements 14, 114, 214 and the base plate 12 can facilitate manufacturing operations. The shock absorbing layer 10 may be optimized for a particular application by distributing the shock absorbing elements on the base plate 12 and sizing the individual shock absorbing elements 14, 114, 214, which may or may not have the same size and may or may not have the same configuration.
    [54] The above-described embodiments of the invention are intended to be exemplary. One skilled in the art will therefore appreciate that the above description is illustrative only, and that various alternative configurations and modifications may be made without departing from the scope of the present invention. Accordingly, the present invention is intended to include all such alternative configurations, modifications, and variations that fall within the scope of the appended claims.
    权利要求:
    Claims (13)
    [1]
    Shock-absorbing layer (10) for a helmet (8), characterized by: a base plate (12); and a plurality of spaced shock absorbing members (14) arranged on the base plate and interconnected only therethrough, each shock absorbing member (14) being independently and elastically compressible to at least partially receive a shock load on the helmet, the shock absorbing members (14) 14) are hollow and define a closed circumferential wall (22) extending upwardly from the base plate to an open upper end (32) which is dimensioned to cause a slight decrease in fluid flow exiting the shock absorbing member, the closed circumferential wall (22) of each shock absorbing element comprises at least one wall section, each wall section having: a first portion (18) having opposite inner and outer surfaces (24, 28) each having the shape of a truncated tapered portion, and a second portion (20) having extends upwards from the first portion and is formed in one piece therewith, the second portion having opposite inner and outer portions surfaces (26, 30) each having the shape of a truncated tapered portion, the inner surfaces (24, 26) of the first and second portions (18, 20) being interconnected by relatively radially larger ends of their respective truncated tapered portions to define an inner angle (i i) less than 180 degrees between the inner surfaces (24, 26) of the first and second portions, and wherein the outer surfaces (28, 30) of the first and second portions are interconnected by relatively radially larger ends of their respective truncated tapered portions to define an outer angle (0O) greater than 180 degrees between the outer surfaces (28, 30) of the first and second portions.
    [2]
    The shock absorbing layer according to claim 1, wherein each shock absorbing member (14) is a primary shock absorbing member (16), and further having a secondary shock absorbing member (40) extending independently upwardly from the base plate (12) and arranged within the closed the circumferential wall (22) of each primary shock absorbing member (16), the secondary shock absorbing members (40) being independently compressible.
    [3]
    The shock absorbing layer according to claim 2, wherein the secondary element (40) is hollow and has a circular cross section.
    [4]
    The shock absorbing layer according to claim 2, wherein the secondary shock absorbing elements (40) have a smaller height away from the base plate than the height of the primary shock absorbing elements (16).
    [5]
    The shock absorbing layer according to claim 1, wherein the outer surfaces (28, 30) of the first and second portions and the inner surfaces (24, 26) of the first and second portions are oriented relative to each other so that the element comprises a continuous tubular material portion extending from the base plate (12) to the open end when the shock absorbing member (14) is uncompressed.
    [6]
    The shock absorbing layer according to claim 1, wherein the shock absorbing elements (14) comprise a rim (36) extending around and radially from the open end (32) of the closed circumferential wall (22).
    [7]
    The shock absorbing layer of claim 1, wherein each shock absorbing member (14) comprises a plurality of flanges (146) extending at least one of them radially outwardly and radially inwardly of the closed circumferential wall (22), the flanges (146) extending from the base plate to the open upper end (32).
    [8]
    The shock absorbing layer of claim 1, wherein each shock absorbing member has a single one of said wall sections, the first portion (18) of the wall section extending upwardly from the base plate (12) and the second portion (20) of the wall section defining the open upper end of the shock absorbing element (14).
    [9]
    The shock absorbing layer of claim 1, wherein each shock absorbing member (214) has at least two of said wall sections having a first of the sections extending upwardly from the base plate and a second of the sections extending upwardly from the first of the sections and defining the open upper end. (232), wherein the inner surfaces adjacent to the inner surfaces of the first and second sections are interconnected by radially relatively smaller ends of their respective truncated tapered portions, and wherein the outer surfaces adjacent to the outer surfaces of the the first and second sections are interconnected by radially relatively smaller ends of their respective truncated tapered portions.
    [10]
    The shock absorbing layer according to claim 1, wherein each shock absorbing element has a height defined from the base plate to the open upper end and a maximum width defined at the connection between the first and second portions of the wall section, the height being at least equal to the maximum width.
    [11]
    The shock absorbing layer of claim 1, wherein the inner (24, 26) and outer (28, 30) surfaces each have a frustoconical shape.
    [12]
    Protective helmet (8) comprising an outer casing (13) and a shock-absorbing layer (10) according to any one of claims 1-11.
    [13]
    Protective helmet according to claim 12, wherein the protective helmet (8) is a sports helmet.
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    同族专利:
    公开号 | 公开日
    JP2013538950A|2013-10-17|
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    法律状态:
    优先权:
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    PCT/CA2011/050472|WO2012045169A1|2010-10-06|2011-08-01|Shock absorbing layer with independent elements|
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