Provided are a carbon fiber thermoplastic resin prepreg which is a carbon fiber prepreg obtained by impregnating a PAN-based carbon fiber in which the average fiber fineness of a single fiber is 1.0 dtex to 2.4 dtex with a thermoplastic resin, wherein the thermoplastic resin satisfies 20(FM/FS)40 (where FM: flexural modulus (MPa) of a resin sheet comprising only the thermoplastic resin, and FS: flexural strength (MPa) of the resin sheet), a method for manufacturing the same, and a carbon fiber composite material employing the carbon fiber prepreg.

Provided are a carbon fiber thermoplastic resin prepreg which is a carbon fiber prepreg obtained by impregnating a PAN-based carbon fiber in which the average fiber fineness of a single fiber is 1.0 dtex to 2.4 dtex with a thermoplastic resin, wherein the thermoplastic resin satisfies 20(FM/FS)40 (where FM: flexural modulus (MPa) of a resin sheet comprising only the thermoplastic resin, and FS: flexural strength (MPa) of the resin sheet), a method for manufacturing the same, and a carbon fiber composite material employing the carbon fiber prepreg.

The present invention relates to a method for producing a composite material comprising a step of producing an initial dry preform (101), formed from unidirectional continuous dry fibers, a step of applying non-woven filaments to a first main face (111) of the dry preform, a step of needling said filaments by means of a needling device (5) comprising a plurality of needles (51), each provided with at least one notch, so that filaments are driven by the needles and arranged in a direction substantially perpendicular to the continuous fibers of the dry preform, and a step of impregnating the dry preform with an impregnation polymer, said impregnation polymer constituting the matrix of the composite material part.

A process is disclosed for the preparation of multilayered composite materials comprising, as components: (A) a backing material, (B) optionally at least one tie layer and (C) a polymer layer,
wherein a polymer layer (C) is formed using a mold, optionally at least one organic adhesive is applied all over or partially to backing material (A) and/or to polymer layer (C) and then polymer layer (C) is bonded with backing material (A) in point, strip or two-dimensional fashion, polymer layer (C) and/or at least one tie layer (B) being prepared from aqueous polymer dispersions which comprise at least one crosslinking agent C and from 0.1 to 5% by weight of at least one solvent selected from dipropylene glycol dimethyl ether and/or 1,2-propanediol diacetate.

A method for manufacturing a three-dimensionally shaped product, capable of obtaining a three-dimensionally shaped product having a sufficient mechanical strength without reduction in a shaping speed. A method for manufacturing a three-dimensionally shaped product includes a step of preparing a fiber sheet having a predetermined shape, a step of applying a three dimensional shaping composition to the fiber sheet, and a step of solidifying the three dimensional shaping composition applied to the fiber sheet.

A method of making a panel assembly that includes forming a thermoplastic panel, placing a thermoset portion into a pocket in a mold, placing an attachment member into the pocket in the mold, positioning the thermoplastic panel in the mold, cooling the thermoplastic panel while heating the thermoset portion to flow at least a portion of the thermoset portion into openings defined in the thermoplastic panel, and cooling the panel assembly so that the thermoset portion hardens, thereby securing the attachment member to the thermoplastic panel.

A method of making a panel assembly that includes forming a thermoplastic panel, placing a thermoset portion into a pocket in a mold, placing an attachment member into the pocket in the mold, positioning the thermoplastic panel in the mold, cooling the thermoplastic panel while heating the thermoset portion to flow at least a portion of the thermoset portion into openings defined in the thermoplastic panel, and cooling the panel assembly so that the thermoset portion hardens, thereby securing the attachment member to the thermoplastic panel.

A method of making a carbonized preform for a carbon-carbon composite brake disk may comprise: stacking a plurality of textile fabric layers, each textile fabric layer in the plurality of textile fabric layers including oxidized polyacrylonitrile (PAN) fibers, each textile fabric layer in the plurality of textile fabric layers being more uniform than a typical fabric layer formed from cross-lapping; each fabric layer being thinner than a typical fabric layer from cross-lapping, needling the plurality of textile fabric layers to form a needled non-woven board; cutting a fibrous preform from the needled non-woven board; and carbonizing the fibrous preform. The resultant non-woven carbonized preform maintains a higher fiber volume and more consistent properties throughout than what would otherwise be achieved using a typical fabric layer from cross-lapping.

Processes for making carbon/carbon parts are provided. The process involves compression, carbonization and densification steps. Pressure may be applied to a fibrous preform prior to the carbonization step at a temperature less than an exothermic temperature to increase the fiber volume ratio of the fibrous preform. The densification steps may include filling the voids of the fibrous preform with a carbon matrix.

A method of making a panel assembly that includes forming a thermoplastic panel, placing a thermoset portion into a pocket in a mold, placing an attachment member into the pocket in the mold, positioning the thermoplastic panel in the mold, cooling the thermoplastic panel while heating the thermoset portion to flow at least a portion of the thermoset portion into openings defined in the thermoplastic panel, and cooling the panel assembly so that the thermoset portion hardens, thereby securing the attachment member to the thermoplastic panel.