Abstract: An FRM disc preform for manufacturing an FRM disc used as compressor rotors f aircraft engines. The FRM disc preform (1) of the present invention includes a reinforcing fiber (2) wound in a spiral shape with flat faces and a spray coating (7) of a matrix metal formed on one of the flat faces of the spirally wound reinforcing fiber (2) to hold the spiral shape by fixing the upper layer and the lower layer of the spiral. Thereby, the spiral shape is held tightly without collapsing and handling in a laminating process and a combined forming process becomes extremely simplified, and thus the manufacturing efficiency and accuracy of the FRM disc can be enhanced.

Abstract: A method for fabricating, and a resulting structure for, a seamless, reusable and collapsible mandrel suitable for forming a plurality of seamless and hollow fiber wound vessels upon is disclosed. A destructible mandrel is used to form the seamless reusable mandrel. The destructible mandrel is preferably formed from a material which can be destroyed by dissolving, for example, materials such as foam or plaster. The seamless, collapsible, and reusable mandrel includes a plurality of different layers including a gas impermeable layer, a continuous fiber wound layer, and a release surface forming the outermost layer of the seamless, collapsible, and reusable mandrel. The resulting seamless, reusable and collapsible mandrel has advantages over mandrels which include a seam. Such advantages include a longer useful life and consistently high quality fiber wound vessels at a relatively low cost.

Abstract: The inventions relate to the field of machine manufacturing and more specifically, to shell-type construction of base members used in aviation engineering and rocketry, which operate under conditions of combined stressed state, to the methods of and mandrels for their manufacture.A load-carrying tube-shell comprises a cellular framework 1 made of spiral and annular strips 4, 5 crossing each other to define layers 3 of systems repeated over the thickness of the wall thereof so that stiffening ribs 6, 7 with criss-crosses 8, 9, 10 are thus formed, and outer coating layers 2 respectively made of unidirectional filaments 11 bound by a cured polymeric binder 12. Damping-absorbing layers 14 of resilient-elastic material such as rubber or polyurethane are disposed between the layers 3.A method of the manufacture of the tube-shell comprises a step of introducing intermediate continuous forming strips 20 placed beneath the layers 4, 5 laid down under tension.

Abstract: Pile weatherstripping having rows of pile and longitudinal fins both within and external to the rows of pile. The heights of the fins with respect to the height of the pile may be independently varied and controlled. A travelling endless band receives a pair of first webs providing internal fins on opposite sides of the band. The first webs are indexed to the edges of the band, which defines the heights of the fins. Each web may be independently indexed. Alignment of the webs on the band is provided either by an aligning fixture or by coining the webs to provide lines of indentations which index the webs at the edges of the band. The yarn which forms the pile is wound around the first webs. Second webs providing the external fins are indexed through the yarn and first webs to the edges of the band and are also aligned by a second aligning fixture or by coining. Backing strips are attached, as by ultrasonic welding, along the edges of the band. Then the yarn is slit without cutting into the webs.

Abstract: In a process for manufacturing a handle for a hand tool, resin-coated fibers are pultruded to form an elongate, substantially hollow fiber-resin composite rod having a first end for attachment to a tool head. A glass filament is wound about a longitudinal axis of the composite rod adjacent to the rod's first end, after which an encasement over the filament is molded onto the rod. For increased strength, the filament may be first coated with a thermo-setting resin and, after wrapping the filament about the rod, the resin is cured prior to the molding step. The resultant tool handle, particularly useful in applications with, for example, lopping shears, may be very lightweight and yet exhibit superior strength characteristics in comparison with standard composite handles manufactured in a pultrusion manufacturing process.

Abstract: A method for fabricating, and a resulting structure for, a seamless, reusable and collapsible mandrel suitable for forming a plurality of seamless and hollow fiber wound vessels upon is disclosed. A destructible mandrel is used to form the seamless reusable mandrel. The destructible mandrel is preferably formed from a material which can be destroyed by dissolving, for example, materials such as foam or plaster. The seamless, collapsible, and reusable mandrel includes a plurality of different layers including a gas impermeable layer, a continuous fiber wound layer, and a release surface forming the outermost layer of the seamless, collapsible, and reusable mandrel. The resulting seamless, reusable and collapsible mandrel has advantages over mandrels which include a seam. Such advantages include a longer useful life and consistently high quality fiber wound vessels at a relatively low cost.

Abstract: A method for forming a structure of polymer-impregnated fiber and the structure formed thereby involves the rotation of a mandrel about an axis and the winding of a continuous polymer-impregnated fiber strand about the mandrel. The polymer-impregnated fiber strand is fed to the rotating mandrel so that the mandrel pulls the strand toward and winds the strand about the mandrel surface in an arrangement of windings. As the polymer-impregnated fiber strand is wound about the mandrel, the adjacent windings of the winding arrangement provide the structure with a close radial wrap, the fibers of the strand shift to an off-axis orientation, and the arrangement of windings is shifted along the length of the mandrel as the arrangement is formed to accommodate the feed of subsequent segments of the polymer-impregnated strand to the surface of the mandrel for winding thereabout. The polymer-impregnated strands of the winding arrangement are subsequently permitted to cure, or cool, to a hardened condition.

Abstract: A containment structure for radially deployable devices in the form of a self-coiling composite band. The composite band is fabricated as a lay up of epoxy resin-impregnated ply layers of cloth material that are wrapped about a mandrel and cured in a specific ordered sequence. The ordered sequence of fabrication steps of applying and curing the resin-impregnated cloth layers to the mandrel provides a desired separation of the cured ply layers of the final composite so that they are located at the outer most regions of the composite and are separated by an intermediate resin layer of desired thickness. This ensures a composite band which is effective to function as a negator-spring or composite clock spring and which also exhibits a good combination of mechanical properties, such as elastic modulus, strength, and resilience. In use, the self-coiling composite band is applied about the periphery of a central hub of a radially deployable device by wrapping it therearound in a reverse curl orientation.

Abstract: The invented methods provide a means for reducing or eliminating manual astments that are required during the fabrication (winding) of fiber optic dispensers. This reduction is accomplished through the use of a fiber placement pattern that is permanently generated on the bobbin winding surface. Filaments, such as optical fibers, are precisely guided during the winding of subsequent filament layers by the embedded crossover pattern baselayer. The embedded crossover pattern baselayer is generated by first winding in a given direction a wire of a pre-selected diameter upon the polymer coating on the bobbin surface. The polymer is allowed to cure partially before the wire is unwound and removed. Afterwards a pre-selected optical fiber is wound in the direction opposite that of the wire winding direction thereby creating crossover patterns which are, then, manually adjusted to be in desired locations on the bobbin axis.

Abstract: Apparatus (10) and method for bonding together coils of an electrical wire forming windings (W) of a stator assembly (54) employed in making an electric motor. The apparatus includes a fixture (22) on which the stator assembly is installed during a bonding operation, the fixture also holding the stator assembly during a surge test which precedes the bonding operation. Electrical connectors (38) are used to electrically connect the stator windings to the apparatus, and these electrical connections are used for both the surge test and the bonding operation. A power supply unit (16) is responsive to an indication that the stator windings have successfully passed a surge test to apply a predetermined voltage to the windings. The current flowing through the stator windings as a result of the applied voltage is measured. A bonding control unit (50) controls the bonding operation.

Abstract: The invention discloses a method for fabricating a deployable, inflatable aerodynamic control structure for aerospace vehicles which has a desired noncircular or noncylindrical cross-section. In a preferred embodiment, the control structure is configured as an inflatable airfoil and includes a flexible skin and a plurality of internally disposed airfoil-shaped bulkheads or integral rib members that are arranged, spaced apart, in cross-wise fashion along the axial length of the airfoil shaped control structure. The flexible skin is fabricated as a lay up, in ordered sequence, of plural layers of elastomeric rubber material and plural ply layers of resin-impregnated yarns or fabric. The result is a fiber-reinforced pressure membrane that is flexible and compactly foldable.

Abstract: An optical fiber dispenser for the payout of optical fiber from a moving vehicle so as to maintain a wire communication link with a control station. The dispenser has a bobbin carrying a multi-layer optical fiber pack and holding heating means connectable to a power or heat supply.

Abstract: The present invention relates to oral hygiene and specifically to an improved method for adding chemotherapeutic agents to dental floss containing several multi-fiber bundles, to methods of treating the oral cavity with the improved dental floss and to the improved dental flosses per se.

Abstract: Reduction of the surface friction of a cured elastomer, sealant or adhesive s accomplished through the use of a dry lubricant such as hexagonal boron nitride powder either as an additive to the uncured polymer mix or applied to the uncured polymer surface prior to effecting a cure.

Abstract: A high-speed flywheel includes a composite rim supported for rotation about a central axis which is perpendicular to the plane of the rim. The rim includes at least a pair of rim portions or regions of differing elastic modulus in the circumferential direction of the material forming the rim. Moreover, a radially outer portion of the rim has a higher elastic modulus in the circumferential direction, while a radially inner portion of the rim has a lower elastic modulus in the circumferential direction. This variation of circumferential elastic modulus is achieved by a selected radial variation of the angle of the fiber reinforcement material relative to the circumferential direction of the rim. A result is that the radially inner portion of the rim transfers radial force to the outer portion, with a resulting lower radial stress in the radially inner portion of the flywheel rim. An improved speed of operation and greater energy storage for the flywheel is achieved.

Abstract: A multiple-layered, translatedly rib-stiffened, composite hollow cylinder d method for fabrication thereof utilizing filament winding technique known in the art. Selective utilization of high strain-to-failure viscoelastic matrix material, without resort to secondary processing, results in improved damping characteristics in terms of dissipation of mechanical and acoustic energy as well as improved structural characterics in terms of damage tolerance.

Abstract: An FRP drive shaft wherein the shaft body and the flanges are formed in a body and a method of manufacturing the same are disclosed. The shaft body is formed by winding a resin impregnated fiber on a mandrel having pins on its circumferential surface while hooking the fiber on the pins. The fiber is then circumferentially wound to form a hoop-like reinforcing band near each end of the shaft body. After the pins and end parts of the mandrel are removed, each end portion of the shaft body is expanded by a pressing mold to form a flange. After hot setting, the remaining part of the mandrel is removed.

Abstract: An apparatus for reinforcing an external surface of a stationary vertical column with a reinforcing material includes a supply of a reinforcing material and a guide that directs the reinforcing material from the supply onto the stationary vertical column. A winding device moves the guide means in a spiral pattern relative to the stationary vertical column, to wind spiral layers of the reinforcing material onto the vertical column. The winding device is provided as a multipart structure that may be assembled around the vertical column and later disassembled to permit removal from around the vertical column. In one approach, the reinforcing material is tows of a curable composite material that are wound onto the vertical column and later cured in place after the winding device is removed.

Abstract: Spiral bands having a plurality of convolutions of a high tensile strength composite material are formed by feeding a plurality of continuous high tensile strength fibers through an uncured resin to form a web, depositing the web on a release web having at least one substantially flat surface to form a laminate, winding the laminate around the mandrel to form a plurality of overlapping convolutions, curing the resin in the composite web to set the convolutions in a spiral configuration, and then removing the release web from the composite web. The convolutions of the spiral bands in accordance with this process have substantially flat surfaces and an elastic memory. These bands can be used to reinforce axially extending structures having internal forces directed radially outward therefrom by wrapping the band around the structure with a layer of adhesive applied to hold the convolutions in place.

Abstract: A method for producing vehicle structures such as railway coach bodies includes winding layers and integral annular frame elements of like material. The resulting body is free of metal can include additional longitudinal stiffening elements inserted between the annular frame elements. Windows covered by protective foils are installed in an insulating layer between the wound layers during the winding process. At the conclusion of the winding process, the portions of the inner and outer wound layers covering the windows are removed and the window openings are finished by inserting a reinforcing frame on the outer wound layer and an angle frame on the inner wound layer.

Abstract: Coilable, tape-like structures are disclosed, that contain parallel segments of dental floss. Each segment has a bead on each of its ends for handling by an applicator. The beads can be fixed to the ends of a floss segment, either by melting its ends (without allowing the melted bead to contact a solid surface) or by press fitting the floss into slits in molded beads and fixing them with a bonding agent. The coilable structures can be made, either by mounting the floss segments onto a flexible tape or by fastening beads of adjacent floss segments together. In the latter version, the floss is (optionally) made stiff enough to support its weight, laterally. Apparatus for producing the coilable structures includes an elongated, substantially-flat, rotating chassis on which floss from a tensioning dispenser is wound. In one embodiment, a tape is held onto the upper surface of the chassis while the floss is wound into slits in the edges of the tape.

Abstract: A mandrel assembly has a hollow main tube and two annular sleeves, wherein an inner diameter of the two annular sleeves is larger than an outer diameter of the two main tube ends. The two annular sleeves are sleeved respectively on the two main tube ends, which can be easily disengaged from the mandrel assembly when applied with an external force.

Abstract: Process for manufacturing a composite article comprising a solid body reinforced by winding at least one reinforcing tape around the solid body. The reinforcing tape deposited on the solid body is subjected to a constant tensile force. Downstream of the point where it comes into contact with the solid body, this reinforcing tape is consolidated by a local pressure. The invention also relates to a device for the manufacture of such reinforced composite articles.

Abstract: A carbon fiber spar is provided which comprises a layer of carbon fiber forming a one-piece circumference and having an integral sail-attaching groove formed by a plastic insert bonded together with the layer of carbon fiber during curing so that the fiber layer forms a hollow for receiving the plastic insert in interlocking engagement.

Abstract: A coated abrasive backing consisting of an endless, seamless, loop is provided. The backing loop includes about 40-99% by weight of an organic polymeric binder, based upon the weight of the backing; and an effective amount of a fibrous reinforcing material engulfed within the organic polymeric binder material. The endless, seamless backing loop includes a length with parallel side edges, and at least one layer of fibrous reinforcing material engulfed within the organic polymeric binder material such that there are regions of organic binder material free of fibrous reinforcing material on opposite surfaces of the layer of fibrous reinforcing material. The fibrous reinforcing material can be in the form of individual fibrous strands, a fibrous mat structure, or a combination of the these. A method for preparing the endless, seamless backing loop for a coated abrasive belt is also provided.

Abstract: An optical fiber pack (42) having layers (52) of optical fiber (22) is formed on a bobbin (32) using an ultravlolet-curable adhesive. A layer (50) of a UV-curable adhesive is deposited, and a length of the optical fiber (52) is wound over the layer (50) of ultraviolet-curable adhesive. Ultraviolet radiation is directed at the layer (50) of ultraviolet-curable adhesive through the layer (52) of optical fiber wound over the layer (50) of adhesive, to cure the adhesive. The approach can be used, for example, to apply adhesive to entire layers of the optical fiber, or to tack the ends of the optical fiber layers into place.

Abstract: The present invention relates to a method and to a device for manufacturing parts made from resin and reinforcing fibers by winding. Molding means including a plurality of female forms corresponding each to a print of the part to be manufactured are produced. The forms are arranged one after the other, substantially helically, so as to make a continuous groove, then said groove is filled by winding with fibers coated with a polymerizable resin by rotating the prints round the axis of the helix.

Abstract: The invention relates to a process and apparatus for manufacturing a body to be reinforced with a fiber-composite material, especially bottles or containers or metal or plastic for holding a pressurized gaseous medium, in which a plurality of light, high-strength inorganic or organic, non-conductive or conductive as well as non-metallic yarns are wrapped around the body, whereby individual fiber strands or fibers are unwound and are bundled and, prior to being wound on the body, are impregnated with a plastic material. The wrapping of the yarns is carried out with controllable, pre-tensioned yarns. During wrapping, the individual yarns are again impregnated with a polymer melt of thermoplastic and each individual wrapping layer is smoothed and/or cooled by a temperature-controlled roller.

Abstract: A heated shoe and cooled pressure roller assembly for composite prepreg application is provided. The shoe assembly includes a heated forward contact surface having a curved pressure surface. The following cooled roller provides a continuous pressure to the thermoplastic while reducing the temperature to approximately 5.degree. C. below glass transition temperature. Electric heating coils inside the forward portion of the shoe heat a thermoplastic workpiece to approximately 100.degree. C. above the glass transition. Immediately following the heated contact surface, a cooled roller cools the work. The end sharpened shape of the heated shoe trailing edge tends to prevent slag buildup and maintain a uniform, relaxed stress fabrication.

Abstract: A mandrel assembly has a hollow main tube and two annular sleeves, wherein an inner diameter of the two annular sleeves is larger than an outer diameter of the two main tube ends. The two annular sleeves are sleeved respectively on the two main tube ends, which can be easily disengaged from the mandrel assembly when applied with an external force.

Abstract: A frame for a game racquet such as a tennis racquet is formed by helically winding a tow of filament material and thermoplastic material over an elongated mandrel to form a tube. The tube is positioned in a mold having the shape of a game racquet frame and auxiliary pieces for handle and yoke sections are added. This preform is heated to melt the thermoplastic while the interior of the tube is pressurized. The preform is then allowed to cool and harden to form the game racquet frame.

Abstract: A frame for a game racquet such as a tennis racquet is formed by interspersed winding of filament material over an elongated mandrel to form a tube. The tube is formed from a wound laminate in which some or all of the circuits of the wind patterns are sequenced in an arbitrary manner by the designer. Each circuit is helically wound along a rotating mandrel. The formed tube is placed in a mold having the shape of the frame, auxiliary pieces for handle and yoke sections are added, and together molded to form the frame.

Abstract: A coated abrasive backing consisting of an endless, seamless, loop is provided. The backing loop includes about 40-99% by weight of an organic polymeric binder, based upon the weight of the backing; and an effective amount of a fibrous reinforcing material engulfed within the organic polymeric binder material. The endless, seamless backing loop includes a length with parallel side edges, and at least one layer of fibrous reinforcing material engulfed within the organic polymeric binder material such that there are regions of organic binder material free of fibrous reinforcing material on opposite surfaces of the layer of fibrous reinforcing material. The fibrous reinforcing material can be in the form of individual fibrous strands, a fibrous mat structure, or a combination of the these. A method for preparing the endless, seamless backing loop for a coated abrasive belt is also provided.

Abstract: There is disclosed a process and apparatus for depositing threads such as textile threads and in particular glass fibre threads, the threads being continuously supplied on a curved path onto a support plate and around fixed points which are arranged movably on it, formed by movable pins, so as to be laid down in a controlled manner in any desired configuration, in order for example to form a reinforcement for fibre-reinforced articles made chiefly of plastics, in which the individual threads are arranged directed along the lines of stress and also in the regions of high thread density no excessive thickenings are produced at the points where they cross.

Abstract: The invention provides improvements to a composite member that has a plurality of plies. The improved composite member has (1) an interior ply which functions to dampen or resist sudden forces exerted on the composite member, (2) an intermediate load-carrying ply, and (3) an exterior abrasion-resistant ply. These plies have multiple, often intertwined fiber components disposed or imbedded with a matrix material, preferably Nylon-6 thermoplastic, to inhibit sharp edges during breakage. One or more of the plies typically has "bi-axial" or "tri-axially" braided fiber geometries wherein one or more fibers are helically wound about the circumference of the member. The helically oriented fibers are oriented at a selectively variable angle which influences the overall bending strength of the composite material.

Abstract: An apparatus for winding a coil pack of a fiber such as an optical fiber winds the fiber as a radial coil, and then joins the coil axially to previously wound coils. Each radial coil is wound on a flexible flange that is deformable from a first tapered shape which facilitates the winding against the flange, to a second shape wherein the coil wound thereon conforms to the shape of the last coil affixed to the fiber pack. The flexible flange is preferably made of an elastomer, and its shape change is readily accomplished by an articulated series of nesting cylinders. The apparatus further includes a fiber winding head that winds the fiber onto the flexible flange, and an adhesive applicator head that applies adhesive between succeeding coils of fiber as they are joined to the coil pack.

Abstract: The invention provides improvements to a composite member that has a plurality of plies. The improved composite member has (1) an interior ply which functions to dampen or resist sudden forces exerted on the composite member, (2) an intermediate load-carrying ply, and (3) an exterior abrasion-resistant ply. These plies have multiple, often intertwined fiber components disposed or imbedded with a matrix material, preferably Nylon-6 thermoplastic, to inhibit sharp edges during breakage. One or more of the plies typically has "bi-axial" or "tri-axially" braided fiber geometries wherein one or more fibers are helically wound about the circumference of the member. The helically oriented fibers are oriented at a selectively variable angle which influences the overall bending strength of the composite material.

Abstract: A direct wind coil winding head assembly for depositing coil windings directly onto a coil support mandrel, comprising wire feed means having an input and an output, the wire feed means adapted to receive a continuous length of wire at the input and to cause the wire to exit the output at a first rate, mandrel positioning means for dynamically positioning the coil support mandrel beneath the output and control means coupled to the wire feed means and the mandrel positioning means, the control means operable to cause the mandrel positioning means to dynamically position the coil support mandrel beneath the output such that the exiting wire is deposited onto the mandrel in a predetermined pattern, and further operable to control the wire feed means such that the first rate is substantially equal to a second rate of movement of the coil support mandrel relative to the output, whereby the wire is deposited onto the coil support mandrel with substantially no residual winding stresses.

Abstract: Glass-fibre reinforced plastic tank, for example for liquid petroleum gas under high pressure, compressed air for air brakes or for storage of acetylene. The tank is composed of two halves (10, 12), the open ends of which are conically bevelled to form a male end (20) and a female end (22), which are joined to each other by an adhesive. The reinforcement in the outer and inner layers of the halves contains essentially longitudinal glass-fibre strands and the intermediate layer contains essentially transverse glass-fibre strands. In the half with the male end (20), the longitudinal glass-fibre strands in the inner layer (35) are densely located adjacent to each other, while the longitudinal glass-fibre strands in the outer layer lie in separate groups (30) of densely arranged glass-fibre strands with the predetermined spacing between the groups to form channel-shaped spaces (31). In the half with the female end (22), the order is reverse.

Abstract: The present invention relates to a method for producing a reinforcement for a composite component, said reinforcement including superposed plies of thread, according to which method:straight portions of thread are laid down on a support; andall the superposed plies are consolidated by stitching, without knotting, a continuous thread.According to the invention:said straight portions of thread (4, 5) are laid down by means of a needle, with respect to which the continuous thread (F), of which each of said portions forms part, can slide, said needle being capable of moving relative to said support (6), pulling tight the straight portion of thread (4, 5) above the latter, over an extent equal to the length of said straight portion of thread; andsaid straight portions of thread (4, 5) are fixed by stitching, without knotting, at least one of the ends (4a, 4b; 5a, 5b) of each of said portions of thread into said support (6) using said needle.

Abstract: Spiral bands having a plurality of convolutions of a high tensile strength composite material are formed by feeding a plurality of continuous high tensile strength fibers through an uncured resin to form a web, depositing the web on a release web having at least one substantially planar surface to form a laminate, winding the laminate around the mandrel to form a plurality of overlapping convolutions, curing the resin in the composite web to set the convolutions in a spiral configuration, and then removing the release web from the composite web. The convolutions of the spiral bands in accordance with this process have substantially planar surfaces and an elastic memory. These bands can be used to reinforce axially extending structures having internal forces directed radially outward therefrom by wrapping the band around the structure with a layer of adhesive applied to hold the convolutions in place.

Abstract: The device consists of a placing head whose wire drive roller and placing wheel are interconnected by an intermediate gear which may be retracted so as to disconnect them, said placing head being translation-mobile with respect to the distributing machine/head interface, complementary means providing a variable pressure of the placing head on the shape. Application for wire placing so as to form a complex structural piece.

Abstract: A warp-free laminate is produced by winding a first set of strands or filaments about a flat mandrel with a second set of strands being wound transverse to the first set. The two sets may be perpendicular to each other. The filaments are maintained under a controlled tension while being impregnated with a resin and during subsequent cure of the resin. In order to permit the formation of a warp-free product, the winding pattern is such that it forms a mirror image about a neutral axis or plane of symmetry. The winding pattern may be chosen to provide interstices in a predetermined pattern determining punching out or high speed drilling of hole openings for subsequent printed circuit applications.

Abstract: Textile fabrics, yarns and cords are impregnated with rubber, resin and particulate materials by dipping in an aqueous dispersion comprising an aqueous rubber latex, resin and the particulate material, the dispersion further containing a very minor amount of a water-soluble silicate, such as sodium silicate. After drying, the products can be used as reinforcement for mechanical rubber goods and friction materials such as clutch facings and the like.

Abstract: A hollow, tapered, fiber-reinforced plastic utility pole, and a method for making the pole. The pole is designed by a computer-modelling technique that simulates applying resin-coated, reinforcing strands over the outer surface of a mandrel. A plurality of test stations are incrementally spaced from the tip portion to the butt portion of the pole simulated on the mandrel. The thickess-to-diameter ratio must be equal to or greater than an established constant at each station or additional circuits of resin-coated, reinforcing strands deemed to have been applied, as required. One then calculates the stress resistance at each successive station to determine if the acceptable stress is greater than the stress resistance required. Whatever additional circuits of resin-coated, reinforcing strands are necessary are then deemed to have been applied.

Abstract: According to this method windings of reinforcing fibers are impregnated with resin and are wound, along a given length, around a flexible sheath placed onto a rigid rotary-driven mandrel. At least one additional winding of said impregnated reinforcing fiber around the flexible sheath is wound over a different length and according to a different pitch.

Abstract: A warp-free laminate is produced by winding a first set of strands or filaments about a flat mandrel with a second set of strands being wound transverse to the first set. The two sets may be perpendicular to each other. The filaments are maintained under a controlled tension while being impregnated with a resin and during subsequent cure of the resin. In order to permit the formation of a warp-free product, the winding pattern is such that it forms a mirror image about a neutral axis or plane of symmetry. The winding pattern may be chosen to provide interstices in a predetermined pattern determining punching out or high speed drilling of hole openings for subsequent printed circuit applications.

Abstract: A universal pin ring for use in securing filament in a stationary position with respect to a mandrel during a filament winding process is disclosed. In the preferred embodiment, the universal pin ring has two rows of pins along its length. The pins of the first row are adapted to serve as anchor pins to secure filament in a stationary position with respect to a mandrel. The pins of the second row are adapted to serve as guide pins to cause filament to quickly conform to the contour of a mandrel after turning of the filament during filament winding, thereby minimizing the size of the turnaround area. In some applications, both rows of pins would serve to anchor filament. In other applications the guide pins serve both to guide filament and to anchor filament that has slipped from an anchor pin. Reinforcing ribs and flex grooves on the universal pin ring are also disclosed.

Abstract: A method for fabricating, and a resulting structure for, a seamless, reusable and collapsible mandrel suitable for forming a plurality of seamless and hollow fiber wound vessels upon is disclosed. A destructible mandrel is used to form the seamless reusable mandrel. The destructible mandrel is preferably formed from a material which can be destroyed by dissolving, for example, materials such as foam or plaster. The seamless, collapsible, and reusable mandrel includes a plurality of different layers including a gas impermeable layer, a continuous fiber wound layer, and a release surface forming the outermost layer of the seamless, collapsible, and reusable mandrel. The resulting seamless, reusable and collapsible mandrel has advantages over mandrels which include a seam. Such advantages include a longer useful life and consistently high quality fiber wound vessels at a relatively low cost.

Abstract: A flexible, aerodynamic inflatable nose fairing for use in combination with flat nosed canister launched missiles having a wide circular cylindrical shape. The inflatable nose fairing is fabricated as a fiber-reinforced elastomeric membrane having a laminate construction which includes a silicone rubber inner or base layer as the gaseous pressure membrane or bladder, surrounded by two or more ply layers made up of resin-impregnated yarns. In a preferred embodiment, the silicone rubber bladder is applied to a generally conical shaped mandrel. The first ply layer is fabricated by hoop winding resin impregnated yarns on a constant diameter cylinder and then cutting to form gores. The gores are applied to the conical shaped mandrel such that the gore fibers are oriented in the axial direction of the conical shaped mandrel.