Traditional garments include a plurality of fabric pieces that are sewn together or otherwise coupled to form the article of clothing. Such coupling forms seams within the garment that may be irritable to the wearer, affect the properties of the garment, as well as limit the performance of the garment.
One embodiment relates to a base layer of a garment. The base layer includes a waist section, an upper leg section, and a lower leg section. The waist section is positioned to correspond with and receive a waist and crotch region of a wearer. The waist section includes a base portion, a mesh portion, a compressive portion, and a durable portion. The upper leg section is positioned to correspond with and receive a thigh and knee region of the wearer. The upper leg section includes the base portion and the mesh portion. The lower leg section is positioned to correspond with and receive a shin and calf region of the wearer. The lower leg section includes the base portion and the compressive portion.
Another embodiment relates to a garment. The garment includes a base layer and a shell layer. The base layer includes a first section, a second section, and a third section. The first section is positioned to correspond with and receive a waist and crotch region of a wearer. The second section is positioned to correspond with and receive a thigh and knee region of the wearer. The third section is positioned to correspond with and receive a shin and calf region of the wearer. Each of the first section, the second section, and the third section includes a plurality of zones manufactured from a first material. Each of the plurality of zones has different material characteristics. The shell layer defines an internal cavity configured to receive the base layer. The shell layer is at least partially manufactured from a second material having a greater durability than the base layer.
Still another embodiment relates to a base layer of a garment. The base layer includes a plurality of sections positioned to correspond with and receive respective anatomical regions of a wearer. The plurality of sections form a continuous and seamless layer. Each of the plurality of sections includes a plurality of portions having different material characteristics.
Yet another embodiment relates to a method for manufacturing a base layer of a garment. The method include providing yarn and knitting the yarn to form a seamless, three-dimensional layer. The seamless, three-dimensional layer includes a plurality of sections positioned to correspond with and receive respective anatomical regions of a wearer. Each of the plurality of sections includes a plurality of portions having different material characteristics. The material characteristics include at least one of (i) a thread count or threads-per-inch, (ii) courses per inch (CPI), (iii) wales per inch (WPI), (iv) a warp thread density or ends-per-inch, (v) a weft thread density or picks-per-inch, (vi) a fabric density, and (vii) a fabric thickness.
The foregoing summary is illustrative only and is not intended to be in any way limiting. In addition to the illustrative aspects, embodiments, and features described above, further aspects, embodiments, and features will become apparent by reference to the drawings and the following detailed description.
The drawings are provided to illustrate example embodiments described herein and are not intended to limit the scope of the disclosure. Throughout the drawings, reference numbers may be re-used to indicate general correspondence between referenced elements.
Various aspects of the disclosure will now be described with regard to certain examples and embodiments, which are intended to illustrate but not to limit the disclosure. Nothing in this disclosure is intended to imply that any particular feature or characteristic of the disclosed embodiments is essential. The scope of protection is defined by the claims that follow this description and not by any particular embodiment described herein. Before turning to the figures, which illustrate example embodiments in detail, it should be understood that the application is not limited to the details or methodology set forth in the description or illustrated in the figures. It should also be understood that the terminology is for the purpose of description only and should not be regarded as limiting.
Embodiments herein generally relate to articles and/or base layers that can provide one or more of ease of dressing, improved movement and flexibility, improved ventilation, improved comfort, improved interaction with other products (e.g., a shell layer, boots, knee pads, etc.), etc. Such articles and/or base layers may be used in a number of activities, including without limitation: sports and athletics, including extreme sports and traditional sports; military and combat activity; law enforcement; outdoor activities such as camping, hiking, and climbing; automotive and cycling activities, including auto racing, motorcycle riding and racing, motocross, bicycling such as BMX, etc.; equestrian and rodeo; while operating recreational vehicles including ATVs, snowmobiles, side-by-sides, and other off-road vehicles; to name just a few. The articles and/or base layers and methods for manufacturing and/or using the same provide various improvements not present in existing articles and/or base layers. Further details are provided herein.
According to an example embodiment, a base layer of a garment includes a plurality of sections that are arranged (e.g., knitted, woven, sewn, etc.) from a single material (e.g., a single spool of yarn, etc.) to form a single, continuous, seamless, three-dimensional layer. The plurality of sections of the base layer may include a plurality of different portions (e.g., base portions, mesh portions, compressive portions, durable portions, etc.) having differing material characteristics (e.g., thread count or threads-per-inch, warp thread density or ends-per-inch, weft thread density or picks-per-inch, fabric density, fabric thickness, etc.). The material characteristics of the various portions may provide specific material properties (e.g., strength, durability, elasticity, mechanical ease, ventilation, joint articulation, etc.) in desired locations of the base layer (e.g., to correspond with certain anatomical regions of the wearer of the base layer, etc.).
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According to an example embodiment, the shell layer 2 includes a first plurality of panels or stretch fabric panels, and a second plurality of panels or rigid panels. According to an example embodiment, the stretch fabric panels of the shell layer 2 are manufactured from a first fabric material, and the rigid panels are manufactured from a second different material. According to an example embodiment, the stretch fabric panels are selectively positioned about the shell layer 2 (e.g., between the rigid panels, etc.) to facilitate independent movement of each of the rigid panels relative to one another (e.g., each of the rigid panels moves independently, etc.). According to an example embodiment, the interaction between the stretch fabric panels and the rigid panels facilitates natural movement of a wearer's body such that as a wearer moves, the front side and the rear side of the shell layer 2 do not sheer away from each other (e.g., which may cause discomfort and restriction in movement, etc.). In one embodiment, at least one of the stretch fabric panels is manufactured from a first stretch fabric material and at least one of the stretch fabric panels is manufactured from a second different stretch fabric material. For example, at least one of the stretch fabric panels may be manufactured from a stretch fabric material and at least one of the stretch fabric panels may be manufactured from a stretch mesh fabric material and/or a mesh fabric material. The different stretch fabric materials may differ in one or more characteristics including elasticity, ventilation, abrasion resistance, heat resistance, penetration resistance, and the like. The stretch mesh fabric and/or the mesh fabric material may be used in areas of the shell layer 2 to facilitate air to flow into and out of the shell layer 2 of the garment (e.g., to provide a cooling effect to the wearer of the shell layer 2, etc.). According to an example embodiment, the stretch fabric material is more durable (e.g., tougher, stronger, heavier, etc.) than the stretch mesh fabric material. In other embodiments, the stretch fabric panels are manufactured from a single stretch fabric material. In an alternative embodiment, the stretch fabric panels are manufactured from a nominal stretch material (e.g., denim, a material having more stretch than a rigid fabric material, a material having less stretch that a stretch fabric material, etc.).
According to an example embodiment, the rigid panels of the shell layer 2 are manufactured to be durable, protective (e.g., heat resistant, abrasion resistant, penetration resistant, etc.), and/or structure giving. In one embodiment, at least one of the rigid panels is manufactured from a first rigid material and at least one of the rigid panels is manufactured from a second different rigid material. The first rigid material and the second rigid material may differ in one or more characteristics including abrasion resistance, penetration resistance, heat resistance, elasticity, and/or other material properties of the rigid materials. For example, at least one of the rigid panels may be manufactured from an abrasion resistant material and at least one of the rigid panels may be manufactured from a heat resistant material. The abrasion resistant material may be used in desired areas of the shell layer 2 (e.g., a thigh area, a shin area, etc.) to shield desired anatomical regions of the wearer from dirt, rocks, and/or other debris that may hit the wearer during use (e.g., while riding a dirt bike, etc.). The abrasion resistant material may include 900D fabric, ballistic nylon, a heavy duty poly-fabric, Kevlar, carbon fiber, plastic, and/or leather, among other possible abrasion resistant materials. The heat resistant material may be used in desired areas of the shell layer 2 (e.g., inner leg area, etc.) to shield desired anatomical regions of the wearer from heat emitted by components (e.g., an engine, engine components, exhaust components, etc.) of a vehicle (e.g., a dirt bike, an ATV, a snowmobile, etc.) being driven by the wearer of the garment (e.g., the shell layer 2 and/or the base layer 10, etc.). The heat resistant material may include leather, Therma-fleece heat resistant fabric, and/or Kevlar, among other possible heat resistant materials. In other embodiments, the rigid panels are manufactured from a single rigid material. In an alternative embodiment, the rigid panels are manufactured from a fabric material.
According to an example embodiment, the independent movement of the rigid panels allows the rigid panels to work independent of each other, thereby providing a greater degree of comfort and less restriction (e.g., while walking, sitting, riding, etc.) without sacrificing the intended function of the shell layer 2, which is to provide protection to the wearer (e.g., a motocross rider, a snowmobile rider, an ATV rider, etc.) from debris and/or heat while driving a vehicle (e.g., a dirt bike, etc.). In some embodiments, the rigid panels are configured (e.g., aerodynamically shaped, formed, etc.) to reduce drag forces experienced by a wearer of the shell layer 2 (e.g., while traveling at increased speeds, etc.). In some embodiments, the rigid panels are woven or otherwise manufactured from a hard and/or durable material (e.g., carbon fiber, Kevlar, 900D fabric, etc.). In other embodiments, the rigid panels are formed (e.g., molded, etc.) from a non-woven material (e.g., plastic, etc.). According to an example embodiment, the shell layer 2 (e.g., the rigid panels, etc.) is at least partially manufactured from a material having a greater durability than the base layer 10.
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According to an example embodiment, the cavity 4 of the shell layer 2 is configured to receive the base layer 10. In one embodiment, the shell layer 2 and the base layer 10 are individual components of the garment (e.g., the base layer 10 is not coupled or attached to the shell layer 2, etc.). In an alternative embodiment, the base layer 10 is disposed within and coupled (e.g., sewn; attached; releasably coupled with hook and loop fasteners, clips, hooks, buttons; etc.) to the shell layer 2. According to an example embodiment, the base layer 10 covers seams formed between the stretch fabric panels and the rigid panels (e.g., such that the seams, the stretch fabric panels, and/or the rigid panels do not come into contact with the wearer, providing increased comfort, reducing chaffing and/or scratching, etc.). In other embodiments, the base layer 10 covers the rigid panels and/or the seams to prevent discomfort and/or chaffing. In some embodiments, the base layer 10 is configured to provide ventilation to the wearer of the garment. In some embodiments, the base layer 10 is configured to provide warmth and/or protection from wind.
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According to an example embodiment, the base layer 10 is configured to be a skintight and/or a one piece layer. In one embodiment, the waist section 12, the upper leg section 14, the lower leg section 16, and/or the foot section 18 form a continuous and seamless layer (e.g., a unitary, seamless, and three-dimensional (3D) layer, etc.). The continuous and seamless layer maybe manufactured from a single, uniform material. According to an example embodiment, the base layer 10 is manufactured using a 3D knitting machine that forms (e.g., knits, etc.) the base layer 10 from the single material (e.g., yarn, fabric, thread, etc.). In one embodiment, the single material includes multi-constituent yarn (e.g., Cordura® yarn, 95% Cordura® nylon and 5% elastane, etc.). By way of example, the yarn may be or include 160D/68F (80D/34F 2 ply air-textured yarn (ATY)) with Lycra 40 denier (den) covering yarn. In other embodiments, a different type of yarn, thread, and/or fabric is used. The base layer 10 may advantageously provide the durability of nylon and the comfort of cotton, be strong yet lightweight, have exceptional abrasion resistance, have high tensile and/or tear strengths for lasting performance, and/or provide excellent temperature and moisture management. The base layer 10 may also advantageously prevent the need to put on multiple undergarments (e.g., socks, compression shorts, a jock strap, etc.) as the multiple undergarments may be integrally formed within the base layer 10 (e.g., providing ease of dressing, etc.).
According to an example embodiment, the continuous and seamless structure of the base layer 10 provides various advantages relative to traditional garments that are cut and sewn or otherwise coupled together. By way of example, without seams, patterns and designs of the base layer 10 remain uninterrupted across the entire garment (e.g., front-to-back, down-the-legs, etc.). 3D knitting may allow the base layer 10 to be reproduced exactly as intended (e.g., minimizes and/or eliminates manufacturing defects associated with traditional garments, each base layer 10 is produced based on digitally programmed data such that item-to-item and batch-to-batch quality remains consistent, etc.). Labor-intensive cutting and sewing processes may be eliminated, and the amount of scrap material thrown away after cutting out each part of a garment may be entirely eliminated (e.g., by knitting a base layer 10 with only the required amount of yarn, etc.). The base layer 10 may also have superior comfort by eliminating irritable seams. The base layer 10 may additionally have superior stretch and mobility by eliminating seams that would otherwise interfere with the natural elasticity of knits. The seamless one-piece construction of the base layer 10 may also facilitate evenly distributing stress throughout the base layer 10, preventing localized pressure points which may cause discomfort. Further, the seamless one-piece construction of the base layer 10 may facilitate incorporating articulated joints in desired areas of the base layer 10 (e.g., in a knee area, in an elbow area, etc.) to further improve stretch and mobility of the base layer 10.
In alternative embodiments, the waist section 12, the upper leg section 14, the lower leg section 16, and/or the foot section 18 are manufactured as two or more (e.g., two, three, four, etc.) individual sections and thereafter joined together (e.g., sewn together, etc.). By way of example, (i) the waist section 12 and the upper leg section 14 may be manufactured as a first continuous portion (e.g., shorts, ¾ pants, etc.) of the base layer 10 and (ii) the lower leg section 16 and/or the foot section 18 may be manufactured as a second continuous portion (e.g., a long sock, a tube sock, etc.) of the base layer 10. By way of another example, (i) the waist section 12, the upper leg section 14, and the lower leg section 16 may be manufactured as a first continuous portion (e.g., pants, etc.) of the base layer 10 and (ii) the foot section 18 may be manufactured as a second continuous portion (e.g., an ankle sock, etc.) of the base layer 10. By way of yet another example, (i) a first half of the base layer 10 (e.g., a front half, a right half, etc. of the waist section 12, the upper leg section 14, the lower leg section 16, and/or the foot section 18) may be manufactured as a first continuous portion of the base layer 10 and (ii) an opposing second half of the base layer 10 (e.g., a rear half, a left half, etc. of the waist section 12, the upper leg section 14, the lower leg section 16, and/or the foot section 18) may be manufactured as a second continuous portion of the base layer 10. The first continuous portion and the second continuous portion may thereafter be coupled (e.g., sewn, using a flat lock stitch, etc.) to form the base layer 10.
According to an example embodiment, each of the waist section 12, the upper leg section 14, the lower leg section 16, and/or the foot section 18 includes a plurality of portions manufactured (e.g., woven, knitted, felted, otherwise arranged into a structure that forms fabric, etc.) from the same material (e.g., the multi-constituent yarn, Cordura® yarn, etc.). Each of the plurality of portions of the waist section 12, the upper leg section 14, the lower leg section 16, and/or the foot section 18 have different material characteristics (e.g., TPI, CPI, WPI, EPI, PPI, fabric density, fabric thickness, etc.), according to an example embodiment. The different material characteristics may facilitate providing various portions having specific material properties (e.g., strength, durability, elasticity, mechanical ease, ventilation, joint articulation, etc.) at desired locations of the base layer 10.
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The various portions (e.g., the base zones 20, the compressive zones 40, the mesh zones 60, the durable zones 80, etc.) of the base layer 10 may include a plurality of fibers that are woven, knitted, felted, or otherwise arranged into a structure that forms the base layer 10. The plurality of fibers may include a single constituent material (e.g., cotton, nylon, polyester, spandex, another elastane material, another synthetic material, another natural material, etc.) or may include a blend of multiple constituent materials (e.g., Cordura® nylon and elastane, etc.). The base layer 10 may include a fabric having a certain degree of elastic stretch, where the fabric elongates when a force is applied due to deformation (e.g., elastic deformation, etc.) of the fibers themselves (e.g., deformation within the elastic region of the fibers when a force or a stress below the yield strength of the fibers is applied, etc.). The fibers may resist the force and return the fabric to the pre-stretch state when the force is released.
The various portions of the base layer 10 may have a certain degree of mechanical ease (i.e., mechanical give), where the fabric elongates when a force is applied due to movement of the fibers within the structure of the various portions. The mechanical ease of the fabric may vary based on the arrangement of the fibers within the structure of the various portions (e.g., warp and weft density, weave, etc.) and the conditions under which the fabric was produced (e.g., speed of weaving, warp insertion rate, warp and weft tension, etc.). In one embodiment, the mechanical ease does not resist pull in the same way (e.g., does not have the same type of rebound, does not have the same pull profile of rebound, etc.) as the elastic stretch associated with the fibers themselves. Rather, the mechanical ease allows the fibers that make up the fabric to move in and out of the empty spaces between the fibers.
The elongation of the fabric (e.g., due to the mechanical ease, due to the elastic deformation of the fibers themselves, due to the both the mechanical ease and the elastic deformation of the fibers themselves, etc.) may be quantified in terms of a stretch factor. The stretch factor may be equal to the pre-stretched dimension of the fabric subtracted from the stretched dimension of the fabric (e.g., with a force applied that produces sub-yield strength stresses, etc.), with the resulting quantity thereafter divided by the pre-stretched dimension of the fabric.
One or more portions of the base layer 10 (e.g., the base zones 20, the compressive zones 40, the mesh zones 60, etc.) may have both mechanical ease and elastic stretch or primarily only elastic stretch while other portions of the base layer 10 (e.g., the durable zones 80, etc.) may have primarily only mechanical ease. In some embodiments, one or more portions of the base layer 10 (e.g., the base zones 20, the compressive zones 40, the mesh zones 60, etc.) have a greater degree of elastic stretch than mechanical ease while other portions of the base layer 10 (e.g., the durable zones 80, etc.) have a greater degree of mechanical ease than elastic stretch. In some embodiments, one or more portions of the base layer 10 (e.g., the base zones 20, the compressive zones 40, the mesh zones 60, etc.) have a stretch factor at least equal to a threshold (e.g., more than zero percent, at least 5%, at least 10%, at least 25%, at least 50%, at least 100%, etc.) in one or both directions (e.g., lateral and/or longitudinal, along x-axis and/or y-axis, etc.), while other portions of the base layer 10 (e.g., the durable zones 80, etc.) have a stretch factor of less than the threshold (e.g., zero percent, less than 5%, less than 10%, less than 25%, less than 50%, less than 100%, etc.) in one or both directions (e.g., lateral and/or longitudinal, along x-axis and/or y-axis, etc.).
In some embodiments, the base zones 20, the compressive zones 40, the mesh zones 60, and/or the durable zones 80 have isotropic (e.g., symmetrical, identical, etc.) stretch properties (e.g., four-ways stretch, uniform stretch characteristics, etc.). By way of example, the base zones 20, the compressive zones 40, the mesh zones 60, and/or the durable zones 80 may have a mechanical ease and/or an elastic stretch that is independent of the direction of an applied force (e.g., stretches the same in a lateral direction as a longitudinal direction, etc.). In some embodiments, the base zones 20, the compressive zones 40, the mesh zones 60, and/or the durable zones 80 have anisotropic (e.g., asymmetrical, etc.) stretch properties (e.g., may have properties that vary with direction, etc.). By way of example, the base zones 20, the compressive zones 40, the mesh zones 60, and/or the durable zones 80 may have at least one of a mechanical ease and an elastic stretch that varies based on the direction of an applied force. For example, the compressive zones 40 may have an elastic stretch that is greater in a first direction (e.g., a cross-grain direction, etc.) than in a second direction (e.g., a grain direction, etc.). The first direction may be angularly offset relative to (e.g., perpendicular to, etc.) the second direction. The first direction (i.e., the direction along which the greater amount of elastic stretch occurs) may define a primary stretch direction of the fabric. Portions of the base layer 10 having a primary stretch direction may have elastic stretch that occurs primarily in a single direction. This characteristic can be observed by physical manipulation of the fabric in both the first and second directions.
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According to an example embodiment, the base zones 20, the compressive zones 40, the mesh zones 60, and the durable zones 80 have different material characteristics relative to each other (e.g., TPI, CPI, WPI, EPI, PPI, fabric density, fabric thickness, etc. of the base zones 20, the compressive zones 40, the mesh zones 60, and the durable zones 80 all can be different). By way of example, the base zones 20 (e.g., the left waist base zone 22, the right waist base zone 24, the left upper leg base zone 26, the right upper leg base zone 28, the central waist base zone 30, the left lateral lower leg base zone 32, the left medial lower leg base zone 34, the right lateral lower leg base zone 36, the right medial lower leg base zone 38, etc.) may have first material characteristics (e.g., a first CPI, a first WPI, etc.). For example, in some embodiments the zone one material can have a CPI of between about 45-58, of about 50-54, or of about 52 (or any sub value or sub range therein, inclusive of endpoints). In some embodiments, zone 1 material can have a WPI of about 15-27, of about 19-23, or about 21 (or any sub value or sub range therein, inclusive of endpoints). The compressive zones 40 (e.g., the left waist compressive zone 42, the right waist compressive zone 44, the left shin compressive zone 46, the right shin compressive zone 48, the left calf compressive zone 52, the right calf compressive zone 54, the left foot compressive zone 56, the right foot compressive zone 58, etc.) may have second material characteristics (e.g., a second CPI, a second WPI, etc.). For example, in some embodiments the zone 2 material can have a CPI of between about 30-42, of about 34-38, or of about 36 (or any sub value or sub range therein, inclusive of endpoints). In some embodiments, zone 2 material can have a WPI of about 20-32, of about 24-28, or about 26 (or any sub value or sub range therein, inclusive of endpoints). The mesh zones 60 (e.g., the left thigh mesh zone 62, the right thigh mesh zone 64, the left anterior knee mesh zone 66, the right anterior knee mesh zone 68, the waist mesh zone 70, the left posterior knee mesh zone 72, the right posterior knee mesh zone 74, the left foot mesh zone 76, the right foot mesh zone 78, etc.) may have third material characteristics (e.g., a third CPI, a third WPI, etc.). For example, in some embodiments the zone 3 material can have a CPI of between about 30-42, of about 34-38, or of about 36 (or any sub value or sub range therein, inclusive of endpoints). In some embodiments, zone 3 material can have a WPI of about 20-32, of about 24-28, or about 26 (or any sub value or sub range therein, inclusive of endpoints). The durable zones 80 (e.g., the left buttocks durable zone 82, the right buttocks durable zone 84, the left ankle durable zone 86, the right ankle durable zone 88, the left heel durable zone 92, the right heel durable zone 94, the left toes durable zone 96, the right toes durable zone 98, etc.) may have fourth material characteristics (e.g., a fourth CPI, a fourth WPI, etc.). For example, in some embodiments the zone 4 material can have a CPI of between about 48-60, of about 52-56, or of about 54 (or any sub value or sub range therein, inclusive of endpoints). In some embodiments, zone 4 material can have a WPI of about 23-35, of about 27-31, or about 29 (or any sub value or sub range therein, inclusive of endpoints). According to an example embodiment, the first material characteristics, the second material characteristics, the third material characteristics, and the fourth material characteristics are all different. By way of example, the durable zones 80 may have the highest tread count (e.g., highest thread density, etc.) to provide the inherent durability. By way of another example, the mesh zones 60 may have the lowest thread count (e.g., lowest thread density, etc.) to provide the loose, mesh structure. By way of example, one or more zones of the base layer 10 (e.g., the base zones 20, etc.) may have a construction of about 40 CPI by about 31 WPI. It should be understood that not all of the zones described have to be different in some or all of their characteristics relative to each other. Some characteristics can be the same, while others differ. For example, 2 or 3 can be similar in one or more of the various characteristics and parameters described here. In some embodiments, the various zone materials can have a weight of between 320-350 g/m2, or 330-340 g/m2, or about 335 g/m2, for example.
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According to an example embodiment, the base layer 100 is configured to be a skintight and/or a one piece layer. In one embodiment, the torso section 112, the left sleeve section 114, and/or the right sleeve section 116 form a continuous and seamless layer (e.g., a unitary, seamless, and three-dimensional (3D) layer, etc.). The continuous and seamless layer maybe manufactured from a single, uniform material. According to an example embodiment, the base layer 100 is manufactured using a 3D knitting machine that forms (e.g., knits, etc.) the base layer 100 from the single material (e.g., yarn, fabric, thread, etc.). In one embodiment, the single material includes a multi-constituent yarn (e.g., Cordura® yarn, 95% Cordura® nylon and 5% elastane, etc.). By way of example, the yarn may be or include 160D/68F (80D/34F 2 ply air-textured yarn (ATY)) with Lycra 40 denier (den) covering yarn. In other embodiments, a different type of yarn, thread, and/or fabric is used. In alternative embodiments, the torso section 112, the left sleeve section 114, and/or the right sleeve section 116 are manufactured as two or more (e.g., two, three, etc.) individual sections and thereafter joined together (e.g., sewn together, etc.).
According to an example embodiment, each of the torso section 112, the left sleeve section 114, and/or the right sleeve section 116 includes a plurality of portions manufactured (e.g., woven, knitted, felted, otherwise arranged into a structure that forms fabric, etc.) from the same material (e.g., the multi-constituent yarn, Cordura® yarn, etc.). Each of the plurality of portions of the torso section 112, the left sleeve section 114, and/or the right sleeve section 116 have different material characteristics (e.g., TPI, CPI, WPI, EPI, PPI, fabric density, fabric thickness, etc.), according to an example embodiment. The different material characteristics may facilitate providing various portions having specific material properties (e.g., strength, durability, elasticity, ventilation, joint articulation, etc.) at desired locations of the base layer 100.
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It is important to note that the construction and arrangement of the elements of the systems, methods, and apparatuses as shown in the example embodiments are illustrative only. Although only a few embodiments of the present disclosure have been described in detail, those skilled in the art who review this disclosure will readily appreciate that many modifications are possible (e.g., variations in sizes, dimensions, structures, shapes and proportions of the various elements, values of parameters, mounting arrangements, use of materials, colors, orientations, etc.) without materially departing from the novel teachings and advantages of the subject matter recited. For example, elements shown as integrally formed may be constructed of multiple parts or elements. It should be noted that the elements and/or assemblies of the enclosure may be constructed from any of a wide variety of materials that provide sufficient strength or durability, in any of a wide variety of colors, textures, and combinations.
Embodiments have been described in connection with the accompanying drawings. However, it should be understood that the figures are not drawn to scale. Distances, angles, shapes, etc. are merely illustrative and do not necessarily bear an exact relationship to actual dimensions and layout of the articles that are illustrated. In addition, the foregoing embodiments have been described at a level of detail to allow one of ordinary skill in the art to make and use the articles, parts, different materials, etc. described herein. A wide variety of variation is possible. Articles, materials, elements, and/or steps can be altered, added, removed, or rearranged. While certain embodiments have been explicitly described, other embodiments will become apparent to those of ordinary skill in the art based on this disclosure.
Conditional language used herein, such as, among others, “can,” “could,” “might,” “may,” “e.g.,” and the like, unless specifically stated otherwise, or otherwise understood within the context as used, is generally intended to convey that certain embodiments include, while other embodiments do not include, certain features, elements and/or states. Thus, such conditional language is not generally intended to imply that features, elements and/or configurations are in any way required for one or more embodiments. The terms “comprising,” “including,” “having,” and the like are synonymous and are used inclusively, in an open-ended fashion, and do not exclude additional elements, features, acts, operations, and so forth. The term “consisting essentially of” can be used anywhere where the terms comprising, including, containing or having are used herein, but consistent essentially of is intended to mean that the claim scope covers or is limited to the specified materials or steps recited and those that do not materially affect the basic and novel characteristic(s) of the claimed invention. Also, the term “consisting of” can be used anywhere where the terms comprising, including, containing or having are used herein, but consistent of excludes any element, step, or ingredient not specified in a given claim where it is used.
Also, the term “or” is used in its inclusive sense (and not in its exclusive sense) so that when used, for example, to connect a list of elements, the term “or” means one, some, or all of the elements in the list. Conjunctive language such as the phrase “at least one of X, Y, and Z,” unless specifically stated otherwise, is otherwise understood with the context as used in general to convey that an item, term, etc. may be either X, Y, Z, X and Y, X and Z, Y and Z, or X, Y, and Z (i.e., any combination of X, Y, and Z). Thus, such conjunctive language is not generally intended to imply that certain embodiments require at least one of X, at least one of Y, and at least one of Z to each be present, unless otherwise indicated.
Additionally, in the subject description, the word “example” and “exemplary” are used to mean serving as an example, instance, or illustration. Any embodiment or design described herein as “exemplary” is not necessarily to be construed as preferred or advantageous over other embodiments or designs. Rather, use of the word exemplary is intended to present concepts in a concrete manner. Accordingly, all such modifications are intended to be included within the scope of the present inventions. Other substitutions, modifications, changes, and omissions may be made in the design, operating conditions, and arrangement of the preferred and other exemplary embodiments without departing from scope of the present disclosure or from the spirit of the appended claims.
This application claims the benefit of U.S. Provisional Patent Application No. 62/416,825, filed Nov. 3, 2016, which is incorporated herein by reference in its entirety.
Number | Date | Country | |
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62416825 | Nov 2016 | US |