Abstract: A composite structural panel for use in bridge structures, and method of manufacturing same, comprises a top panel and a bottom panel separated by and attached to at least one, but preferably a plurality, of structural composite preforms which may be fabricated by a continuous manufacturing process and may be saturated by resin using a continuous wetting process. The composite preforms may take any cross sectional shape but are preferably trapezoidal. The top and bottom panels may be fabricated from a plurality of layers of woven fabric layers and non-woven fabric layers which are saturated with a resin that is subsequently cured using cure processes known in the art. The composite structural panel of the invention is usable as a flat structural member for use as bridge decking, ramps, trestles, and any application requiring a structural panel.

Abstract: A glass and polymer film assembly including a glass film and a polymer film bonded to a surface of the glass film. The polymer film is directly bonded to the glass film by applying the polymer to the glass film when the glass film is above a bonding temperature of the polymer film. The glass film may have a thickness less than about 1 mm and the polymer film may be an oriented semicrystalline homopolymer which is permanently bonded to a major surface of the glass film.

Abstract: The invention relates to a multilayer laid scrim (10, 15) for sheet-like or 3-dimensional high-strength components, consisting of a structure made of a multiplicity of plies of multilayer laid scrim for sheet-like or 3-dimensional high-strength components, consisting of a structure made of a multiplicity of plies made of glass fibres, synthetic fibres, aramid fibres and/or carbon fibres. In order to prevent fan-out of the individual fibres or filaments of the multilayer laid scrim used, it is provided according to the invention that in certain regions structural reinforcement elements (11, 16) are embedded at least into one ply, and/or between at least two plies, of the multilayer laid scrim. Said embedding here can take place over an entire area or else only in the regions which are exposed to a subsequent deformation. The structural reinforcement elements (11, 16) help to generate greater coherence between the individual fibres of the laid scrims, thus preventing fan-out, for example in the edge region.

Abstract: A stacked composite material and a method of preparation, wherein the stacked composite materials comprises of glass fiber layers sandwiched between nanocomposite layers. The nanocomposite layers comprise a nanofiller dispersed in a cured epoxy matrix, wherein the nanofiller is at least one of silicon carbide nanoparticles or aluminum oxide nanoparticles. Adjacent and noncontiguous glass fiber layers are oriented in a unidirectional orientation or a quasi-isotropic orientation.

Abstract: A stacked composite material having at least one glass fiber layer, at least two nanocomposite layers comprising multi walled carbon nanotubes dispersed in an epoxy matrix. Each glass fiber layer is sandwiched between two nanocomposite layers and the glass fiber layers are oriented in a unidirectional or a quasi-isotropic orientation with respect to adjacent and non-contiguous glass fiber layers in the stacked composite material. A method of preparing a stacked composite material comprising applying a nanocomposite layer onto a mold, overlaying a glass fiber layer on top of the nanocomposite layer, rolling an aluminum roller over the glass fiber layer, repeating the applying, overlaying, and rolling to form a stacked composite material.

Abstract: A structural panel and method of fabricating and manufacturing same comprises a top panel and a bottom panel separated by and attached to at least one, but preferably a plurality, of structural composite preforms which may be fabricated by a continuous manufacturing process and may be saturated by resin using a continuous wetting process. The composite preforms may take any cross sectional shape but are preferably trapezoidal. The top and bottom panels may be fabricated from a plurality of layers of woven fabric layers and non-woven fabric layers which are saturated with a resin that is subsequently cured using cure processes known in the art. The composite structural panel of the invention is usable as a flat structural member for use as bridge decking, ramps, trestles, and any application requiring a structural panel.

Abstract: A method of manufacturing camouflage clothing worn by soldiers is provided. The optimum camouflage clothing satisfying clothing functionality, aesthetics, and camouflaging effect, which is an important function for military uniforms, is provided while the optimum camouflage clothing is economical. The camouflage clothing is formed by dyeing threads i.e. row material, using the dyed threads as warp threads and weft threads, and weaving the camouflage clothing using a jacquard weaving machine. Herein, the warp threads and the weft threads are gradationally arranged to form a delicate-colored checked pattern while a three-dimensional pattern is displayed by the jacquard weaving machine.

Abstract: A process of making a reinforced hollow fiber membrane comprises flowing a membrane dope through a casting head while drawing one or more yarns or tows of filaments through the casting head. The filaments are spread apart in the casting head, for example by forcing the yarns or tows around a bend or through a narrow gap in the casting head. The filaments are adapted to bond to the membrane dope or the membrane wall. A reinforced hollow fiber membrane comprises a plurality of filaments individually surrounded by, and bonded to, the membrane wall.

Abstract: Various methods of making a reinforced membrane, devices for making the membranes, and the resulting membranes are described. The methods typically provide a reinforcing structure that includes filaments extending around the circumference of the membrane but without the filaments being part of a braided or woven structure. Some of the reinforcing structures also include longitudinal filaments. The methods and devices can be used to make a supporting structure in line with membrane formation steps, and also allow for a reinforced membrane to be produced that has a ratio of inside-to-outside diameters of 0.5 or more.

Abstract: This invention pertains to an article for use in body armor, comprising a plurality of discrete sheet subassemblies contoured to the shape of a female breast arranged in a stack, without bonding, such that the breast contours are positioned on top of each other, each of the subassemblies comprising at least two nonwoven layers of high tenacity yarns such as par-aramid, a binder and a resin.

Abstract: Various embodiments provide a bi-angle pliable tape for use in forming a composite laminate structure. The bi-angle pliable tape comprises: a longitudinal axis extending in a unidirectional machine direction; a first ply comprising fibers extending in a first orientation, the first orientation being offset relative to the longitudinal axis at a first angle of less than 30°; and a second ply comprising fibers extending in a second orientation, the second orientation being opposite the first orientation relative to the unidirectional machine direction. The first ply and the second ply are further secured substantially adjacently relative to one another by one or more yarns so as to provide a non-crimped configuration such that the bi-angle tape defines a pliable structure. Corresponding composite laminate structures and methods for making the same are provided.

Abstract: A penetration-resistant article is provided comprising two or more layers of woven fabric. The layers of woven fabric each comprise a first series of fibers aligned in a first direction and a second series of fibers interwoven with the first series of fibers and aligned in a second direction perpendicular to the first direction. Two or more layers of woven fabric are loosely stacked together so as to permit relative slippage therebetween and are rotationally offset by an offset angle selected so as to inhibit mechanical interference between opposing adjacent surfaces of the woven fabric layers during slippage therebetween. Also provided are methods for assembling penetration-resistant articles.

Abstract: A structure for use in industrial fabrics such as paper machine clothing and engineered fabrics. The structure is a bicomponent extruded elastomeric netting or mesh having a high degree of both compressibility under an applied normal load and excellent recovery (resiliency or spring back) upon removal of that load.

Abstract: The invention relates to a multilayered material sheet comprising a consolidated stack of unidirection monolayers of drawn ultra high molecular weight polyolefine. The draw direction of two subsequent monolayers in the stack differs. Moreover the thickness of at least one monolayer does not exceed 50 ?m, and the strength of at least one monolayer is comprised between 1.2 GPa and 3 GPa. The invention also relates to a ballistic resistant article comprising the multilayered material sheet and to a process for the preparation of the ballistic resistant article.

Abstract: A reinforcing drywall tape and a method of making the same, the tape having a greige combined with a laid scrim constructed in situ on the greige and bonded to the greige by a resin coating, and a pressure sensitive adhesive fully covering an inward facing surface of the greige wherein the greige is adapted for adherence to drywall sections.

Abstract: The disclosed embodiments concern a curved structural part composed of a composite material with reinforced, continuous fibers whose cross section includes at least two wings, with said fibers extending from one wing to the other, with said structural part having a variation in the width of its section parallel to the local radius of curvature. The structural element that results from assembling the parts in the disclosed embodiments therefore has local widening of the section at the connections between the parts constituting a structural element, such as an aircraft fuselage frame, and widening at the connection with the floor profiles, if such a profile is used to make an aircraft fuselage structure. The disclosed embodiments also concern a process for manufacturing such a part, as well as a device for advantageously implementing such a process.

Abstract: Provided is a sandwich component with a core which comprises a foam material. A fibrous sheet-like material arranged in the foam material at least partially encloses a working region of the sandwich component in a sheet-like manner. At least one strut is incorporated in the foam material and extends from an entry surface of the foam material from outside the working region to at least the fibrous sheet-like material.

Abstract: A method of manufacturing a multi-axial laminate of webs produced from cables stretch broken into strips includes arranging, at an entry of a conveyor table, a first layer of pre-wound pre-cut strips along the longitudinal axis of the table, the strips being partially superimposed; arranging along the table at least two cross lappers transferring and depositing in an oblique and/or divergent position at predetermined angles a stretch broken strip; and arranging the strips in successive superimpositions on the first layer of pre-cut strips in different planes, to form a multi-axial web of stretch broken strips. The web then being treated by a fixing device. Movement of the support belt of the table taking place in steps to ensure the superimposition of the different layers of pre-broken strips deposited by the cross lappers. Implementation of the method taking place without any prior cohesion treatment of each strip.

Abstract: A composite material made of multiple filament bands is disclosed. The filament bands are wound to create a composite material. The filament bands may be impregnated with a solid or semi-solid resin. The filament bands are wound in multiple orientations to form a sheet of composite material. Additionally, the composite material may be made to have a varying number of layer and fiber orientations throughout the sheet of composite material. In another embodiment, a composite component requiring multiple layers and fiber orientations may be substantially manufactured during a filament winding process.

Abstract: A composite board having a sorghum stalk material component and a thermoplastic binder component is disclosed together with a corresponding method of manufacture. To prepare the composite board, the sorghum stalk material is harvested, dried and refined into fibers, particles or slit-stalks. In some cases, the stalk material is first combined with a thermosetting binder such PMDI. Next, the stalk material is arranged into one or more layers and then combined with a thermoplastic binder, such as HDPE film, in a stack. In some instances, recycled HDPE may be used. The stack is thermocompressed in a press at a preselected temperature to compress the sorghum and thermoplastic binder to a preselected board thickness. The board is then cooled to below the softening temperature of the thermoplastic resin. After cooling, the board can be cut or trimmed to its final desired dimensions.

Abstract: A composite board having a sorghum stalk material component and a binder component is disclosed together with a corresponding method of manufacture. To prepare the composite board, the sorghum stalk material is harvested, dried and refined into fibers. The fibers are then combined with a binder such as a thermosetting resin. The resin coated fibers are then arranged into a stack having several layers. Within each layer, the resin coated fibers are aligned along a predetermined layer axis. Next, the stack is thermocompressed in a press at a preselected temperature to compress the resin coated fibers to a preselected board thickness.

Abstract: Provided is a method of manufacturing an electronic device having a first electronic component having a first terminal and a second electronic component having a second terminal, wherein the first electric component is electrically connected to the second electronic component by connecting the first terminal to the second terminal with solder, the method including: providing a resin layer having a flux action between the first terminal and the second terminal to obtain a laminate including the first electronic component, the second electronic component, and the resin layer, wherein a solder is provided on the first terminal or the second terminal; soldering the first terminal and the second terminal; and curing the resin layer while pressing the laminate with a pressurized fluid.

Abstract: A composite material comprises: an open grid comprising at least two sets of strands. Each set of strands has openings between adjacent strands. The sets are oriented at a substantial angle to one another. A tack film is laminated to the open grid. The tack film has first and second major surfaces, such that a material of the tack film at its first and second major surfaces includes about 50% or more of resinous non-asphaltic component and about 50% or less of asphaltic component.

Abstract: A composite material comprises: an open grid comprising at least two sets of strands. Each set of strands has openings between adjacent strands. The sets are oriented at a substantial angle to one another. A tack film is laminated to the open grid. The tack film has first and second major surfaces, such that a material of the tack film at its first and second major surfaces includes about 50% or more of resinous non-asphaltic component and about 50% or less of asphaltic component.

Abstract: A friction member for a brake mechanism in a camera shutter is provided. The friction member includes at least two carbon nanotube composite layers stacked on each other, each carbon nanotube composite layer includes a polymer and a carbon nanotube structure including a number of carbon nanotubes substantially oriented along a same direction. An angle defined by the carbon nanotubes oriented along the same direction in adjacent carbon nanotube composite layers ranges from greater than 0 degrees, and less than or equal to 90 degrees. The camera shutter using the friction member is also provided. The camera shutter includes a brake mechanism and a drive mechanism including a blade driving lever having a moving path. The brake mechanism includes two abovementioned friction members and a brake lever clamped between the two friction members. The brake lever is located at a termination of the moving path to brake the blade driving lever.

Abstract: An advanced grid structure has high strength and low thermal expansion, and includes first, second, and third tape prepreg groups each including a plurality of tape prepregs. Each tape prepreg includes carbon fibers that are aligned in a first, second, or third direction and that form respective first, second, and third grid sides. A plurality of each the first, second, and third grid sides are spaced apart at equal intervals in the respective first, second, or third direction to form respective first, second, and third grid side groups. A structure ratio of the advanced grid structure is larger than 0 and 0.107 or less, 0.053 or less, or 0.040 or less. A thermal expansion coefficient of the advanced grid structure is ?0.9 ppm/K or more and 0.9 ppm/K or less. The carbon fibers have a tensile modulus of elasticity of 280 GPa or more and 330 GPa or less.

Abstract: A fiber structure that can be embedded in a matrix for obtaining a piece made of composite material, includes a first fiber element having a first support surface, at least one L-shaped fiber element having a base that is flattened against the support surface of the first fiber element at a junction zone and a wing that is not flattened against the first fiber element, and another fiber element having one part flattened against the wing of the at least one L-shaped fiber element. The elements are assembled by tapping fibers from a second surface of the first fiber element so as to form loops, at least certain fibers being oblique relative to the second surface, in a plane that is perpendicular to the junction zone, wherein certain loops of the oblique fibers protrude to the outside of the outer surface of a wing of at least one L-shaped fiber element.

Abstract: Provided are three-dimensional truss type periodic cellular materials, wherein a plurality of internal cells are formed periodically and part of the internal cells are filled with solid material like as metal, ceramic, synthetic resin, or composite materials for the purpose of preventing buckling of the truss elements when external compressive or shear loads is applied to the truss structure. By filling only parts of internal cells provided in the truss with appropriate solid materials, the buckling of truss elements can be suppressed maximally and effectively, and even if the buckling accidentally occurs, the sharp decline of strength can be prevented so as to ensure sufficient structural stability of the truss type periodic cellular materials.

Abstract: Biomimetic tendon-reinforced” (BTR) composite structures feature improved properties including a very high strength-to-weight ratio. A basic structure comprises a plurality of spaced-apart stuffer members, each having a first end and a second end defining a length. A plurality of tendon elements interconnect with the first and second ends of the stuffer members in alternating fashion, such that the tendon elements criss-cross each other between the stuffer members. A first panel is bonded or attached to the first ends of the stuffer members, and a second panel is bonded or attached to the second ends of the stuffer members. In the preferred embodiments, the first panel, the second panel, or both the first and second panels are curved. An efficient manufacturing process based upon hollow stuffers and tendon elements in the form of bent wires is also disclosed.

Abstract: This method of producing a planar multi-axial composite product, comprises in particular the steps consisting of: (a) forming a mat (13) having a longitudinal direction and a transverse direction, multi-layer comprising at least the steps consisting in: laying up on a manufacturing support surface a first layer comprising juxtaposed tapes of unidirectional reinforcing fibers preimpregnated with resin, the tapes of the first layer presenting a first angle relative to the longitudinal direction of the mat, laying up on the first layer (10), at least one second layer (11, 12) comprising juxtaposed unidirectional tapes of reinforcing fibers pre-impregnated with resin, the tapes of the second layer presenting a second angle to the longitudinal direction of the mat, (b) carrying out a compaction on the at least two layers, (c) cutting the mat (13) into at least one planar multi-axial composite product having homogeneous deformability properties, in particular for double curvature, that allow members of comple

Abstract: A method and a device for realizing a curved composite material profile made of composite material, and to the resulting profile (63), in which the profile is made from at least one composite strip (11) extending along a longitudinal axis. The strip is formed by stacking at least two tapes of unidirectional reinforcing fibers (4, 5, 6) arranged in orientations.

Abstract: An improved structure for a dust-collecting fabric, which is fluffy and tough, is made by overlapping plural layers of continuous filaments longitudinally and obliquely in a staggered manner. The dust-collecting fabric is not subjected to a hot pressing process, and portions of the continuous filaments are connected to each other by resin to make the whole structure fluffier. The continuous filaments are made from polyester fibers or polypropylene fibers to increase their electrostatic attractive forces. With this arrangement, the strength of the entire structure is increased and the dust-collecting capacity is improved. Furthermore, both surfaces of the duct-collecting fabric can be used.

Abstract: Methods and resulting laminate structures are provided wherein the lay-up of composite materials is accomplished more symmetrically and more continuously as compared to prior techniques to form a composite structure from two composite parts in which their principal laminate directions form a non-singular angle.

Abstract: An insulating film includes a first polymer layer, a second polymer layer and an electromagnetic shielding layer sandwiched between the first polymer layer and the second polymer layer. The electromagnetic shielding layer includes a number of carbon nanotube films that are substantially parallel to the first and second polymer layer. Each of the carbon nanotube films includes a number of carbon nanotubes that are substantially parallel to each other. The insulating film can provide anti-EMI effect in printed circuit boards without employing additional electromagnetic shielding layers.

Abstract: A quasi-isotropic sandwich structure is provided for resisting loads along multiple axes. The structure includes a core material sandwiched by fiberglass reinforcements. Fiberglass rovings are inserted through the structure such that the rovings are oriented along three axes, with adjacent axes separated by approximately 120°. Machines and methods for forming the structures are also disclosed. In one case, a machine having a single stitch head is reconfigured in each of three passes of the material to form the sandwich structure. In other cases, a machine having three stitch heads is used to form the structure with a single pass of the material. In some embodiments, the machine includes an indexing stitch head oriented at approximately 0° and two stationary stitch heads oriented at approximately ?60° and +60° with respect to the machine direction. In other embodiments, the machine includes three stationary stitch heads oriented at approximately 90°, ?30°, and +30°.

Abstract: A fiber fabric includes a first fiber layer formed of a plurality of first fiber bundles, a second fiber layer formed of a plurality of second fiber bundles, a retaining thread group formed of a plurality of retaining threads, and a constraint thread group formed of a plurality of constraint threads. The first fiber layer is laminated in adjacent to the second fiber layer. The first fiber bundles diagonally intersect the second fiber bundles at an angle of 45 degrees. Accordingly, it is possible to improve a production efficiency of an overlapped sheet which gives excellent moldability and a strength, and has an increased thickness by overlapping the fiber fabrics.

Abstract: An apparatus and method is disclosed for forming a compacted powder slug coated with a film. The powder, e.g. of a medicament, is compacted and enrobed to produce compacted powder slugs by preferably mechanically compacting a powder and forming a film of a material, preferably hydroxy propyl methyl cellulose, by vacuum or pressure differential, about the surface of the powder thus compacted.

Abstract: A sheet of thermally reflective material (1) has a surface texture comprising a plurality of reflecting elements (2), wherein each element has a first facet (4) which is substantially reflective at thermal infrared wavelengths and wherein the respective first facets (4) form an angle ? with the plane of the sheet (A-B) (0°<?<90°). Preferably, the first facets (4) are aligned such that, in use, thermal radiation is reflected from a common direction. By orienting the sheet of thermally reflective material to reflect cold regions of the sky, a marking material exhibiting a cold spot in a thermal imager can be provided.

Abstract: An oriented strand board panel and a method for making the same are provided. The OSB panel has at least three layers, namely, a top surface layer, a core layer, and a bottom surface layer. A first cover layer may be provided on the top surface layer. Likewise, a second cover layer may be provided underneath the bottom surface layer. The first cover layer and/or the second cover layer may have a smaller strand angle, defined by an average deviation of strands from a longitudinal axis, than the top surface layer and the bottom surface layer. The smaller strand angles for the first cover layer and/or the second cover layer provide the OSB panel with greater stiffness and strength along the strong direction of the panel without significant compromise of strength and/or stiffness in the weak direction of the panel.

Abstract: An interface material comprising a resin mixture and at least one solder material is herein described. The resin material may comprise any suitable resin material, but it is preferred that the resin material be silicone-based comprising one or more compounds such as vinyl silicone, vinyl Q resin, hydride functional siloxane and platinum-vinylsiloxane. The solder material may comprise any suitable solder material, such as indium, silver, copper, aluminum and alloys thereof, silver coated copper, and silver coated aluminum, but it is preferred that the solder material comprise indium or indium-based compounds and/or alloys. The interface material, or polymer solder, has the capability of enhancing heat dissipation in high power semiconductor devices and maintains stable thermal performance. The interface material may be formulated by mixing the components together to produce a paste which may be applied by dispensing methods to any particular surface and cured at room temperature or elevated temperature.

Abstract: An armor assembly for protecting a body disposed behind said armor assembly, wherein the armor assembly comprises at least one layer of material made of an essentially brittle material, said layer extending slanted relative the expected trajectory of an oncoming firearm projectile.

Abstract: A shear-resistant Z-axis fiber-reinforced composite laminate structure includes a core material; an upper laminate; a lower laminate; and a plurality of contiguous cured resin Z-axis fiber bundles disposed in the core material between the upper laminate and the lower laminate to form high moment-of-inertia solid composite structural elements in the core material.

Abstract: A heat-resistant fiber paper-like sheet comprises 40 to 97% by mass of heat-resistant organic synthetic polymers staple fibers, 3 to 60% by mass of heat resistant organic synthetic polymer fibrid and or an organic resin binder, in a portion of the staple fibers, each staple fiber having two flat end faces having an inclining angle of 10 degrees or more from a plane crossing the fiber axis at a right angles, and is useful as a base material for laminate materials for electrical circuit boards.

Abstract: Papermachine clothing comprising a woven or non-woven support layer, a non-woven layer comprising ultra-coarse non-continuous fibers orientated close to the intended running directions of the clothing and two further layers of batt each comprising conventional somewhat finer staple fibers predominantly aligned close to the cross-machine direction. The ultra-coarse non-continuous fiber layer may comprise two such layers, one of which is biassed at an angle A to the running direction X of the clothing, the other of which is biased at an opposite angle B to the running direction X to provide a layer whose fibers while being substantially orientated in the machine direction also have a bi-axial construction with a cross-orientation.

Abstract: A nonwoven papermaker's fabric, usable in the dryer section of a paper machine, has a spiral wound machine direction (MD) base layer of raw stock which is wound around a pair of parallel rolls or cylinders until the desired length and width is achieved. The spiral wound MD layer is overlaid with a cross-machine direction (CD) layer of similar or dissimilar raw stock and mated by any of a number of means. The spiral wound MD layer can also be mated to another MD layer spiraled in the opposite direction and in one embodiment further mated to a CD layer. The fabric is preferably produced so that its neutral line is oriented toward the paper side of the fabric so that the paper sheet will stretch less than when typical dryer fabrics are used to turn the paper sheet and fabric around the dryer cylinders.

Abstract: The present invention is directed to thermoplastic elastomer films and bags made from thermoplastic elastomer films and also to methods for making thermoplastic elastomer films and bags. The thermoplastic elastomer films of the present invention are composed of thermoplastic elastomers and non-elastic polyesters. The bags of the present invention are fabricated using blended monolayer thermoplastic films that include a blend of thermoplastic elastomer and a non-elastic polyester, or co-extruded multi-layer films that include at least one layer of thermoplastic elastomer and at least one layer of non-elastic polyester. The blended monolayer thermoplastic films of the present invention are useful in the food handling industry and particularly in the meat packaging industry and for use in cooking bag applications. The co-extruded films of the present invention are also useful in the food handling industry and particularly the meat packaging industry and for use in meat casing applications.

Abstract: A sheet of unidirectionally-oriented fiber strands includes unidirectional fibers, bonding fibers interwoven with the unidirectional fibers to form a fiber panel, and thermoplastic film laminating the fiber panel there between. In one embodiment, a second sheet of laminated unidirectional fibers is joined to the first sheet of laminated unidirectional fibers with the unidirectional fibers running in a second direction as compared to the first fibers. In yet another embodiment, individual laminated sheets of unidirectional fibers are stitched together to form packets of sheets which may be used singularly or multiple packets may be bundled together.

Abstract: An on-machine-seamable industrial fabric comprising rings connected by pintles. In one principal embodiment, the rings are oriented in the machine direction and the pintles extend at an angle, connecting the rings. Such configuration improves the strength of the fabric and provides resistance to needling damage. In another principal embodiment, the rings are oriented in the cross-machine direction and the pintles extend in the machine direction, joining the rings.

Abstract: This invention relates to airships, with a volume of 15 to 60 million cubic feet of Helium. More particularly, it relates to improved structural envelope/gas bags or outer covers for lighter-than-air and neutral buoyancy airships. In detail, the material is a multi-layer cloth assembly including at least two plies of fiber cloth, said cloth comprising 56 by 56 yarns/inch with a total weight of 150 to 450 g/m2, with the fiber of the individual cloth layers having a denier generally between 180 and 280 and with the fill of the individual plies at 90 degrees to each other. Preferably, the filaments should be between 200 and 215 denier. The fibers of each layer of cloth are selected from the group consisting of extended chain polyethylene polymer or a thermotropic liquid (melt spun) crystalline polymer. The extended chain polyethylene fiber is a woven modified rip stop weave architecture, while the thermotropic liquid (melt spun) crystalline polymer fiber is a 2×2 basket weave architecture.

Abstract: The invention relates to a ballistic-resistant moulded article containing a compressed stack of monolayers, with each monolayer containing unidirectionally oriented reinforcing fibers and at most 30 wt. % of a plastic matrix material and with the fiber direction in each monolayer being rotated with respect to the fiber direction in an adjacent monolayer, characterized in that the density (?p) of the compressed stack is at least 98.0% of the theoretical maximum density. The invention also relates to a process for manufacturing the moulded article. The ballistic-resistant article may be used in, for instance, helmets, as inserts in bullet-proof vests, as armoring on military vehicles and in ballistic-resistant panels.