The present disclosure relates generally to protective gear for a person's head.
The following paragraphs are not an admission that anything discussed in them is prior art or part of the knowledge of persons skilled in the art.
Helmets are a type of protective gear worn to protect a person's head. Typically, a helmet supplements the skull in protecting the human brain. Helmets are used in various sports (e.g., American football, ice hockey, cycling and skiing), in dangerous work environments (e.g., construction, policing and military applications), and for transportation (e.g., motorcycling).
A turban is a type of headwear based on cloth winding. Turbans can serve as an important religious observance, particularly for members of the Sikh religion. Conventional helmets are generally not compatible with Sikh turbans. To accommodate the religious significance, some jurisdictions exempt Sikhs from wearing motorcycle helmets, for example.
There is need for a garment that can function both as a turban and as protective gear for the wearer's head.
The following is intended to introduce the reader to the detailed description that follows and not to define or limit the claimed subject matter.
In an aspect of the present disclosure, a protective garment assembly may include: an elongate main portion having a length that extends between first and second ends, the main portion including an upper fabric layer and a lower fabric layer; at least one energy-absorbing layer arranged between the upper and lower fabric layers and extending at least partially between the first and second ends; at least one high-strength strip arranged between the upper and lower fabric layers adjacent to the at least one energy-absorbing layer; and a plurality of armor elements arranged between the upper and lower fabric layers adjacent to the at least one energy-absorbing layer and the at least one high-strength strip.
Other aspects and features of the teachings disclosed herein will become apparent, to those ordinarily skilled in the art, upon review of the following description of the specific examples of the present disclosure.
The drawings included herewith are for illustrating various examples of apparatuses and methods of the present disclosure and are not intended to limit the scope of what is taught in any way.
Various apparatuses or methods will be described below to provide an example of an embodiment of each claimed invention. No embodiment described below limits any claimed invention and any claimed invention may cover apparatuses and methods that differ from those described below. The claimed inventions are not limited to apparatuses and methods having all of the features of any one apparatus or method described below, or to features common to multiple or all of the apparatuses or methods described below. It is possible that an apparatus or method described below is not an embodiment of any claimed invention. Any invention disclosed in an apparatus or method described below that is not claimed in this document may be the subject matter of another protective instrument, for example, a continuing patent application, and the applicant(s), inventor(s) and/or owner(s) do not intend to abandon, disclaim or dedicate to the public any such invention by its disclosure in this document.
Referring to
In the example illustrated, the assembly 10 includes an elongate main portion 12 having a length that extends between first and second ends 14, 16, and a width that extends between first and second edges 18, 20.
In the example illustrated, the assembly 10 includes a crown portion 22 secured to the first end 14 of the main portion 12. The crown portion 22 can be secured to the main portion 12 with adhesive and/or stitching.
Referring to
In the example illustrated, the main portion 12 includes energy-absorbing layers 28, high-strength strips 30, and armor elements 32. These protective components are arranged between the upper and lower fabric layers 24, 26, and extend generally between the first and second ends 14, 16 of the main portion 12.
In the example illustrated, there is a first row formed of one of the energy-absorbing layers 28 and one of the high-strength strips 30, a second row formed of one of the energy-absorbing layers 28, the armor elements 32, and one of the high-strength strips 30, and a third row formed of one of the energy-absorbing layers 28 and one of the high-strength strips 30. The rows are parallel to each other and extend along the length of the main portion 12 from the first end 14 towards the second end 16. As illustrated, the rows can be offset from the second end 16 of the main portion 12.
In some examples, in the main portion 12, stitching can be provided between the upper and lower fabric layers 24, 26, on either side of each of the rows, to secure the rows in position. Also, in some examples, the armor elements 32 can be adhered to the energy-absorbing layers 28 to secure each of the armor elements in position. Adhesive 46 is shown in
In the example illustrated, in the first and third rows, the energy-absorbing layers 28 are adjacent to the lower fabric layer 26 and the high-strength strips 30 are adjacent to the upper fabric layer 24. In the second row, the energy-absorbing layer 28 is adjacent to the upper fabric layer 24, the high-strength strip 30 is adjacent to the lower fabric layer 26, and the armor elements 32 are disposed between the energy-absorbing layer 28 and the high-strength strip 30.
Referring to
In the example illustrated, the crown portion 22 includes the energy-absorbing layers 28, the high-strength strips 30, and the armor elements 32. These protective components are arranged between the upper and lower fabric layers 34, 36.
In the example illustrated, there four rows each formed of one of the energy-absorbing layers 28, the armor elements 32, and one of the high-strength strips 30. The rows are parallel to each other and are generally centered within the crown portion 22.
In some examples, in the crown portion 22, stitching can be provided between the upper and lower fabric layers 34, 36, on either side of each of the rows, to secure the rows in position. Also, in some examples, the armor elements 32 can be adhered to their respective energy-absorbing layers 28 to secure the armor elements in position. Adhesive 46 is shown in
In the example illustrated, in each of the rows, the energy-absorbing layer 28 is adjacent to the lower fabric layer 36, the high-strength strip 30 is adjacent to the upper fabric layer 34, and the armor elements 32 are disposed between the energy-absorbing layer 28 and the high-strength strip 30.
As shown in
As shown in
The specific exemplary arrangement of the energy-absorbing layers 28, the high-strength strips 30, and the armor elements 32 within the main and crown portions 12, 22 can be further understood with reference to
Referring to
In the example illustrated, the outer surfaces of armor element 32 have been rounded to remove any sharp points or edges. The shape of the armor element 32 is selected to allow the matrix of hexagon-like shapes to conform and flex to the contour of the person's head as the assembly 10 is tied. In other examples, armor elements can have a general exterior shape selected from square, rectangle, triangle, rhombus, pentagon, and trapezoid.
In the example illustrated, the armor element 32 includes a central hole 42 and a bottom groove 44 surrounding the central hole 42, recessed relative to the bottom surface 40. The central hole 42 can assist with air flow for breathability of assembly 10. The central hole 42 and the bottom groove 44 can assist with reducing material of the armor element 32.
The resulting structure of the armor element 32 is rigid and lightweight. Implemented into the assembly 10, the armor elements 32 are separate components spaced apart from one another, which can allow flexure and movement, and yet cooperate as a matrix to achieve a “chainmail” protective effect. Spacing can be varied. In the example illustrated, the space between adjacent ones of the armor element is more than the diameter or main dimension of each of the armor elements. In some examples, the space between adjacent ones of the armor element can be less than the diameter or main dimension of each of the armor elements.
The following relates to dimensions and materials of the assembly 10, which are intending to be illustrative but non-limiting. It should also be understood that the drawings are schematic in nature and should not be interpreted to express precise dimensions of the assembly 10.
Referring again to
In some examples, the fabric layers 24, 26, 34, 36 can be formed of rubia voile 100% cotton material. This can be a soft, light and durable material, and its use can give the assembly 10 a look and feel that resembles a typical Sikh turban. In a prototype, the inventors used fabric that is 0.0091″ (0.23 mm) thick.
In some examples, the energy-absorbing layers 28 can be formed of a non-Newtonian foam material, e.g., D30® material and/or Poron® XRD™ material. These materials can start out soft and flexible, but stiffen when force is applied, to disperse impact. In a prototype, the inventors used strip foam (McMaster Carr part #93275K117 or 86375K262) that is 1/16″ (1.6 mm) thick.
In some examples, the high-strength strips 30 can be formed of a high-strength fabric with tear resistance, e.g., Dyneema® composite fabric material. In a prototype, the inventors used fabric that is 0.0023″ (0.06 mm) thick (https://ripstopbytheroll.com/products/0-8-oz-dyneema-composite-fabric-ct2e-08).
The armor elements 32 can be formed of various materials, including plastic materials such as acrylonitrile butadiene styrene (ABS), polycarbonate, Delrin®, and glass-reinforced nylon. The armor elements can also be formed of carbon composite materials. In a prototype, the inventors used 3D-printed ABS that is 0.11″ (2.81 mm) thick, 0.74″ (18.67 mm) across, 0.014 oz (0.4 g) in weight, and these armor elements were spaced apart approximately 1″ (25.4 mm) from each other. In other examples, armor elements can be formed by casting of polycarbonate, or carbon composite.
While the above description provides examples of one or more apparatuses or methods, it will be appreciated that other apparatuses or methods may be within the scope of the accompanying claims.
This application claims priority to U.S. Provisional Application No. 63/329,634 filed Apr. 11, 2022, the entire contents of which are hereby incorporated herein by reference.
Number | Date | Country | |
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63329634 | Apr 2022 | US |