A method for producing a reinforcement rod from a fibrous composite material comprising continuous mineral fibers and at least one resin, the resin being mixed with the dry mineral fibers, then wrapped with a strand of material, and the resin then being instantaneous or nearly instantaneously cured (e.g., snap cured) to form an optionally round rod with an optionally helical rib. In aspects, a mixture comprising an environmentally friendly and zero or low volatile organic compound (VOC) emitting resin and a resin-curing agent mixture is used. In aspects, helical ribs are added to the surface of the rod in a manner not to disrupt the longitudinal orientation of the core reinforcing mineral fibers. In aspects, ultraviolet irradiators are used to snap cure the reinforcement. When cured, corrosion resistant mineral fibers are encapsulated in a corrosion resistant matrix. The process allows for a simplified, condensed, and single operation for producing a corrosion resistant fibrous composite reinforcement rod.

A composite part is provided and includes a component, a first set of first composite plies with finite lengths and a second set of second composite plies with finite lengths. A respective end of each of the first composite plies is wrapped around the component in a clockwise wrapping direction and includes first fibers. A respective end of each of the second composite plies is wrapped around the component in a counter-clockwise wrapping direction and includes second fibers.

A method for producing a reinforcement rod from a fibrous composite material comprising continuous mineral fibers and at least one resin, the resin being mixed with the dry mineral fibers, then wrapped with a strand of material, and the resin then being instantaneous or nearly instantaneously fully cured (e.g., snap cured) to form an optionally round rod with an optionally helical rib. In aspects, a mixture comprising an environmentally friendly and zero or low volatile organic compound (VOC) emitting resin and a resin-curing agent mixture is used. In aspects, helical ribs are added to the surface of the rod in a manner not to disrupt the longitudinal orientation of the core reinforcing mineral fibers. In aspects, ultraviolet irradiators are used to snap cure the reinforcement. When fully cured, corrosion resistant mineral fibers are encapsulated in a corrosion resistant matrix. The process allows for a simplified, condensed, and single operation for producing a corrosion resistant fibrous composite reinforcement rod.

A railroad crosstie (tie) may be fabricated from a composite material including a fiber reinforced polymer shell manufactured by pultrusion or other process, and filled by a suitable material, typically selected from expanded elastomeric polymer (such as polyurethane resin or other polymer), concrete, lightweight concrete formed by conventional aggregate, sand, cement, water, and an ultra light filler such as natural materials, sawdust, beads of expanded polymer such as expanded polystyrene, microspheres of glass or plastic, a recycled wooden tie in conjunction with any of the above, or the like. Fasteners may be driven such as spikes, threaded, such as screws, lag screws, spreading screws, rivets, or the like into apertures, pilot holes, or directly into fill absent apertures therein.

A method is provided of designing and producing a carbon fiber composite wrist pin using a combination of a carbon fiber composite pultruded rod that is overwrapped with a carbon fiber prepreg fabric. The use of the carbon fiber pultruded rod and the carbon fiber prepreg fabric results in a rod with optimal flexural strength properties to endure the flexural stress placed on a wrist pin during the cycling of an internal combustion engine. In addition, the overwrapping of the pultruded rod with a carbon fiber prepreg fabric allows for one pultruded rod blank to produce multiple wrist pin sizes by allowing one to change the outer diameter of the wrist pin by changing the thickness of the carbon fiber prepreg fabric overwrapping. After overwrapping, the rod blank is cut to a chosen specific length, optionally inserted into a metal sleeve, and coated with a thermal barrier coating. The wrist pin is then ground to a chosen specific tolerance and coated with an anti-friction coating.

A joining structure according to one embodiment of the present invention includes a first member and a second member, the first member having a hole extending along an axis direction, the second member including a shaft member, the shaft member being formed of a fiber-containing composite material and having a shape to fit in the hole, the second member being joined to the first member via the shaft member so that movement thereof in the axis direction is restricted.

A method is provided of designing and producing a carbon fiber composite wrist pin using a combination of a carbon fiber composite pultruded rod that is overwrapped with a carbon fiber prepreg fabric. The use of the carbon fiber pultruded rod and the carbon fiber prepreg fabric results in a rod with optimal flexural strength properties to endure the flexural stress placed on a wrist pin during the cycling of an internal combustion engine. In addition, the overwrapping of the pultruded rod with a carbon fiber prepreg fabric allows for one pultruded rod blank to produce multiple wrist pin sizes by allowing one to change the outer diameter of the wrist pin by changing the thickness of the carbon fiber prepreg fabric overwrapping. After overwrapping, the rod blank is cut to a chosen specific length, optionally inserted into a metal sleeve, and coated with a thermal barrier coating. The wrist pin is then ground to a chosen specific tolerance and coated with an anti-friction coating.

The manufacture of structural elements for aircraft requires the use of complex and costly methods, particularly in the case of parts of elongate overall shape and variable thickness or cross section made of composite material. The disclosure herein proposes to overcome this problem by a method that allows the manufacture of a structural part from a preform made of composite material of simple shape obtained by pultrusion and of one or more reinforcing elements made of composite material and secured by cocuring with the preform to a region of this preform which region is to be reinforced.

A continuous length composite sucker rod assembly is provided for use in down-hole wells. The assembly can include a plurality of parallel composite strands forming an elongate rod. The strands can be encapsulated with a thermoplastic polymer by co-extrusion. A terminus can be affixed to both ends of the length of sucker rod by splaying the strands out into a conical cavity within the terminus and casting a polymer wedge plug. The resulting sucker rod assembly can be readily coiled in a transportable diameter by virtue of the composite strands being able to twist when the rod is coiled and untwist when the rod is un-coiled.

A novel collapsible plant support includes a collapsible coil adapted to rest on a flat surface. In a particular embodiment, the collapsible plant support includes a plurality of vertical support structures coupled to the collapsible coil so as to provide additional support. In another particular embodiment, a collapsible plant support includes plant receptacle receiving element that supports both a collapsible coil and also a plant receptacle. In a more particular embodiment, the plant receptacle receiving element includes fluid ducts for connecting multiple plant receptacle receiving elements into a fluid network. In another embodiment, the coil is disposed within a helical sleeve coupled to a flexible, cylindrical mesh.