Forming systems and assemblies as disclosed herein comprise a composite material comprising a structural component and a resin component combined with the reinforcing component. A forming element is disposed within the composite material and has a coefficient of thermal expansion that is greater than that of the composite material. The forming element is positioned to provide a desired integral structural reinforcement and/or surface feature to the composite. The composite material may comprise one or more passages extending from a surface thereof to the forming element. The composite material may be cured by heat to take a set configuration and then allowed to cool. The cooling of the composite material and the forming element enables the forming element to contract relative to the composite material and become delaminated therefrom to facilitate easy removal, and thereby provide an improved method and assembly for making structural reinforcing features in composite structures.

A composite structure manufacturing method comprising: a lamination step in which a plurality of fiber-reinforced resin sheets are laminated to form a plate-shaped laminate; a pressing deformation step in which a third roller or similar, which rolls along a plate surface of the laminate, is used to press the plate surface of the laminate, thereby forming a recessed section or a protruding section in a prescribed section of the laminate; a short direction deformation step in which, after the pressing deformation step, the laminate is deformed in the short direction to make the long direction cross-section into a prescribed shape; and a long direction deformation step in which, after the pressing deformation step, the laminate is deformed in the long direction to make the short direction cross-section into a prescribed shape.

A method for renovating the interior of a hollow structure such as a sewerage pit (1) is described. The method provides an access opening (16) to the hollow structure (1); provides a plurality of material sheets (3) comprising reinforcing fibers and a curable resin composition through the access opening (16) and against a wall (11a, 11b) of the hollow structure (1); and provides an inflatable pressure means (4a, 4b) within the hollow structure (1). The pressure means (4a, 4b) are inflated against the wall (11a, 11b). A curing means (6) is then provided within the hollow structure (1) for curing the resin composition; and the resin composition is cured to harden the material sheets and provide a renovated interior of the hollow structure (1).

A fiber reinforced resin hollow molded body 30 in which a resin-integrated fiber sheet is used. The resin-integrated fiber sheet includes unidirectional continuous fibers that are spread fibers of a continuous fiber group and arrayed unidirectionally in parallel, and thermoplastic resin that is present at least on a surface of the unidirectional continuous fibers. In the hollow molded body, in a state where the resin-integrated fiber sheet or a plurality of the resin-integrated fiber sheets 30 are stacked, the resin-integrated fiber sheet or the plurality of resin-integrated fiber sheets are wound to produce a wound body having an overlapping portion. The thermoplastic resin is impregnated in the unidirectional continuous fibers. The resin-integrated fiber sheet or the plurality of resin-integrated fiber sheets are consolidated.

Provided are methods and devices for supporting of variety of different pre-cured composite stringers after forming and prior to curing. A post-forming processing device comprises a base with a channel for receiving hat portions of different stringers. The device also comprises a support structure, at least partially extending within the channel. The support structure is configured to conform to different hat portions and to retain the shape of these hat portions. For example, the support structure is made from a flexible material, which conforms to any shape variations. In some examples, the support structure is made from a jamming material that is reshaped together with each of the pre-cured composite stringers. A post-forming processing device is used for supporting different pre-cured composite stringers while various operations are performed on these stringers, such as stringer trimming, inspection, installation of bladders and noodles, and the like.

A manufacturing method of carbon fiber rackets includes the steps of preparing a core material and setting a blowing bag on the core material, wrapping multiple prepreg layers of carbon fiber materials on the outside of the blowing bag to become a sample to be molded, taking out the core material and placing the sample to be molded into a mold, closing the mold and heating and pressurizing the mold, and inflating the blowing bag to harden the multiple prepreg layers, expelling the air in the blowing bag to reduce the volume of the blowing bag, and opening the mold and drawing out the blowing bag and then taking out the hardened racket frame rough embryo thus obtained.

A tool for forming a part includes a first tool portion including a first tool surface. The tool further includes a second tool portion comprising a second tool surface facing the first tool surface, wherein the first tool surface and the second tool surface define a tool chamber for forming the part. The tool further includes a bladder subassembly disposed in the tool chamber between the first tool surface and the second tool surface. The bladder subassembly includes a plurality of inner bladders disposed within tool chamber, wherein each inner bladder of the plurality of inner bladders includes an inner bladder chamber that is independently inflatable to selectively apply pressure to the part. The bladder subassembly further includes a bladder cover disposed over the plurality of inner bladders within the tool chamber to provide a barrier between the plurality of inner bladders and the part.

According to one implementation, a composite material molding jig 3 includes a tubular member 5 and at least one rigid plate member 6 (6A, 6B) so that a composite material structure O (O1, O2) having a hollow structure can be formed easily. The tubular member 5 has flexibility. The at least one rigid plate member 6 (6A, 6B) reinforces strength of the tubular member 5 partially. The tube is used in a state where air is introduced inside the tube. Further, according to one implementation, a composite material molding method includes using the above-mentioned composite material molding jig 3 in order to produce a composite material structure O (O1, O2) so that the composite material structure O (O1, O2) having a hollow structure can be formed easily.

The present disclosure is directed to a method of producing a surge arrestor module, comprising the acts of (i) providing a plurality of MOV blocks arranged in a stack, (ii) applying an epoxy-reinforced structural layer to an outer surface of the stack, (iii) after the applying, inserting the stack into a flexible bladder, and (iv) curing the epoxy-reinforced structural layer with elevated temperatures while the flexible bladder applies radially aligned pressure to the stack and a tool applies axially aligned pressure to the stack. The present disclosure also includes an apparatus for performing the methods described herein. The apparatus includes an outer case structure and a flexible bladder that fits within the outer case structure. A hollow inner region of the outer case structure is pressurized to force the flexible bladder against the surge arrestor module as the surge arrestor module is curing.

A method and apparatus for forming a composite structure. A plurality of consolidated overbraided thermoplastic preforms are co-consolidated in a circumferential stackup that is circumferentially constrained. Fibers of the plurality of consolidated overbraided thermoplastic preforms are tensioned during co-consolidation.