The present invention provides a molding method of molding, using a mold, an uncured composition arranged on a substrate as a film continuously covering a surface of the substrate, including obtaining unevenness information concerning an unevenness of a surface of an uncured first composition arranged as the film on the substrate, arranging a droplet of an uncured second composition on a concave portion of the surface of the first composition based on the unevenness information obtained in the obtaining, and after the arranging the droplet is performed, molding a composition including the film of the first composition and the droplet of the second composition by the mold.

A template manufacturing method includes preparing a structure including a first substrate and a stacked body that is provided on the first substrate, the stacked body including a first lower layer including a first material, a first upper layer provided on the first lower layer including a second material different from the first material, and a first cover layer provided on a first cover region of the first upper layer and including a third material different from the second material. The method further includes forming a first resist layer on a portion of the first cover layer and on a first portion of the first upper layer, and exposing a second portion of the upper layer. The method yet further includes removing the second portion of the first upper layer using the first cover layer and the first resist layer as a mask.

Resin pellets (7) supplied to a resin block forming space (150) are heated and melted by a heater unit (300) and the melted resin pellets (7) are cooled and solidified to form a resin layer. Since a lifting mechanism (230) of a lifting unit (200) lowers a bottom surface plate (215) whenever forming each of the resin layers, the resin layers formed by the resin block forming space (150) are sequentially laminated to form a large resin block.

Methods of producing polymer-metal hybrid components that are bonded by C—O-M bonds at the interface using at least one of the hot pressing, rolling, and injection molding methods to create chemical bond formation conditions at the polymer and metal interface. When the thermal cycle and compressive pressure specified herein is combinationally created at the polymer and metal interfaced, strong C—O-M bonds forms at the interface and strongly bonds the metal and polymer together through the reaction carbonyl groups (C═O) in polymer and the metal surface. For polymers lacking enough carbonyl groups, new functional groups can be in-situ generation through introducing distributed air pockets at the polymer-metal interface for forming 3-dimensional distributed C—O-M bonds at the interface.

The present invention relates to a method for preparing a three-dimensional shaped article, comprising the following steps: a) unfolding the three-dimensional profile of the three-dimensional shaped article with a curved surface via a computer-aided design software; b) dividing the unfolded three-dimensional profile obtained in step a) into several elemental layers via the computer-aided design software; c) cutting a continuous fiber reinforced thermoplastic resin based composite sheet to have the same or similar shape and size with the elemental layers; d) stacking the cut composite sheets in order of size to obtain a stack; and g) forming the stack obtained in step d), followed by demoulding and optionally trimming to obtain the three-dimensional shaped article. With the method of the present invention, a continuous fiber reinforced thermoplastic resin based composite sheet can be processed into a three-dimensional shaped article with uneven thickness and a high degree of curvature. The resulting three-dimensional shaped article features a light weight, good impact resistance and compression resistance.

Resin pellets (7) supplied to a resin block forming space (150) are heated and melted by a heater unit (300) and the melted resin pellets (7) are cooled and solidified to form a resin layer. Since a lifting mechanism (230) of a lifting unit (200) lowers a bottom surface plate (215) whenever forming each of the resin layers, the resin layers formed by the resin block forming space (150) are sequentially laminated to form a large resin block.

A system for fabricating composite parts efficiently. Pre-impregnated (prepreg) composite material is drawn as a sheet from a roll and fed by advancement rollers into a stamping and molding station in which a piece of the prepreg material is cut, on a mold, from the sheet. Pressure is applied to cause the prepreg material to conform to a surface of the mold, and the prepreg is cured with ultraviolet light. Additional layers of prepreg may be cut and cured on any layers that have already been cured on the mold. The complete part may be removed from the mold with ejector pins. Scrap prepreg may be recycled in a recycling station that separates reinforcing fiber from uncured resin.

Impact protection plate for a vehicle comprising at least an impact layer with an outer surface for receiving the impact comprising at least one fiber reinforced thermoplastic polymer layer, and whereby the impact protection plate further comprises a spacer layer comprising at least one thermoplastic polymer layer, formed in a 3-dimensional shape with one or more protrusions, and whereby the impact layer and spacer layer are at least over part of their surface materially connected to each other forming one or more cavities between the impact layer and the spacer layer.

The invention proposes a method for manufacturing a grille for a cascade type thrust reverser, of a jet engine, said method including the following steps: a) manufacturing a first component comprising continuous or long fibres, pre-impregnated by a thermoplastic or thermosetting resin; b) manufacturing, subsequently or together with step a), a series of second components each including discontinuous fibres, pre-impregnated by a thermoplastic or thermosetting resin, step b) being carried out such that the second components are, on the one hand, arranged transversally with respect to a longitudinal direction of the first component on at least one side of the first component and, on the other hand, spaced from one another according to this longitudinal direction, so as to form a comb-shaped structure, wherein the second components are consolidated to the first component.

A method for forming a fiber-reinforced thermoplastic control surface may comprise: stacking plies of thermoplastic composite sheets to a first desired thickness to form a first skin; stacking plies of thermoplastic composite sheets to a second desired thickness to form a second skin; forming the first skin in a first contour; forming the second skin in a second contour; forming a stiffening member including a thermoplastic resin, the stiffening member including a shape having a plurality of peaks and troughs; assembling the stiffening member between the first skin and the second skin; and joining the stiffening member to the first skin and the second skin.