Abstract: A laminate material for an aircraft component is provided. The laminate material includes a first layer, a second layer and a rib disposed between the first and second layer. One or more connectors are configured to couple the ends of the rib to the first layer and the second layer. The connectors comprise a thermoplastic resin. Aircraft components are also provided.

Abstract: A method for manufacturing panel assemblies is provided. The method includes, placing an outer surface of a panel on a mold. The panel includes a carbon fiber. The method further includes placing a channel on an inner surface of the panel. The channel includes a resin. The inner surface opposes the outer surface. The method further includes welding the channel onto the panel by heating the carbon fiber of the panel and placing a rib in the channel. The rib includes a carbon fiber. The method further include welding the rib onto the channel by heating the carbon fiber of the rib.

Abstract: A plastic article is provided wherein a plastic substrate is coated with multiple resin layers including a primer layer comprising a polymer having a UV-absorptive functional group incorporated therein and a weather resistant hardcoat layer comprising a reaction product of alkoxysilyl-containing benzophenone and/or a hydrolyzate thereof.

Abstract: This invention provides a method for molding a continuous fiber prepreg part whereby a continuous fiber prepreg part comprising thermoplastic prepreg tape can be molded in a shape that allows the exhibition of desired physical properties without the sacrifice of productivity. Prepreg tape 11 is wound around a plurality of rods 21 so as to form a rolled continuous fiber prepreg part 12, slack is removed from the prepreg tape 11 by shifting the plurality of rods 21 in opposite directions so as to generate tension in the continuous fiber prepreg part 12, the continuous fiber prepreg part 12 is pressed with a press jig 41 so as to mold the prepreg part into the final shape, and the continuous fiber prepreg part 12 is cured by heating and cooling after heating.

Abstract: With respect to methods of connecting two or more members where at least one of them comprises a resin member, there is provided a method of connecting members that is capable of firmly connecting two or more members with a rivet without causing the matrix resin to crack even when a joining method that uses a self-pierce rivet is applied to the connecting method. The method of connecting members is a method of connecting members in which overlapping portions of two or more members are connected, the method comprising: disposing a resin member, whose matrix resin comprises a thermoplastic resin, at at least a bottom layer forming the overlapping portions; and, with the matrix resin melted by heat treating at least the resin member of the overlapping portions, driving in a self-pierce rivet from above a member at a top layer of the overlapping portions so that it reaches an interior of the resin member, and connecting the overlapping portions by curing the matrix resin.

Abstract: A plastic article is provided wherein a plastic substrate is coated with multiple resin layers including a primer layer comprising a polymer having a UV-absorptive functional group incorporated therein and a weather resistant hardcoat layer comprising a reaction product of alkoxysilyl-containing benzophenone and/or a hydrolyzate thereof.

Abstract: This invention provides a method for molding a continuous fiber prepreg part whereby a continuous fiber prepreg part comprising thermoplastic prepreg tape can be molded in a shape that allows the exhibition of desired physical properties without the sacrifice of productivity. Prepreg tape 11 is wound around a plurality of rods 21 so as to form a rolled continuous fiber prepreg part 12, slack is removed from the prepreg tape 11 by shifting the plurality of rods 21 in opposite directions so as to generate tension in the continuous fiber prepreg part 12, the continuous fiber prepreg part 12 is pressed with a press jig 41 so as to mold the prepreg part into the final shape, and the continuous fiber prepreg part 12 is cured by heating and cooling after heating.

Abstract: A resin composition for an automobile bumper comprising components (A), (B), and (C) described below:(A) 45 to 74% by weight of a crystalline ethylene-propylene block copolymer having (a) a flexural modulus of 15,000 kg/cm.sup.2 or more, (b) an ethylene content of 5 to 20% by weight, (c) an intrinsic viscosity (decalin, 135.degree. C.) of a portion soluble in p-xylene at room temperature of 3 or more, (d) a melt flow index (MI) of 21 to 70 g/10 min., and (e) a content of a portion insoluble in boiling n-heptane of 97% by weight or more;(B) 21 to 35% by weight of elastomer selected from the group consisting of components (I), (II) and (III) and having a weight ratio of (I) : [(I)+(II)+(III)] of from 0.5 to 1.0, (a) said component (1) being an amorphous ethylene-butene copolymer having a butene content of 10 to 25% by weight and a Mooney viscosity value, (ML.sub.1+4, 100.degree. C.

Abstract: A thermoplastic polymer composition comprising: (i) 100 parts by weight of a thermoplastic polymer component which comprises an ethylene-propylene rubber, an ethylene copolymer and a propylene polymer (including an ethylene-propylene block copolymer), and (ii) 0 to 7 parts by weight of talc, the thermoplastic polymer component being composed of, according to fractionation using o-dichlorobenzene as a solvent, component (A) which is a component soluble in the solvent at 40.degree. C., component (B) which is a component insoluble in the solvent at 40.degree. C. but soluble at 110.degree. C., and component (C) which is a component insoluble in the solvent even at 110.degree. C. in such a proportion that the total amount of the components (A) and (B) is from 50 to 70 parts by weight, the weight ratio of the component (A) to the component (B) being from 0.5 to 1.5, and the amount of the component (C) is from 50 to 30 parts by weight.

Abstract: A thermoplastic polymer composition comprising: (i) 100 parts by weight of a thermoplastic polymer component which comprises an ethylene-propylene rubber, an ethylene copolymer and a propylene polymer (including an ethylene-propylene block copolymer), and (ii) 7 to 25 parts by weight of talc, the thermoplastic polymer component being composed of, according to fractionation using o-dichlorobenzene as a solvent, component (A) which is a component soluble in the solvent at 40.degree. C., component (B) which is a component insoluble in the solvent at 40.degree. C. but soluble at 110.degree. C., and component (C) which is a component insoluble in the solvent even at 110.degree. C. in such a proportion that the total amount of the components (A) and (B) is from 50 to 70 parts by weight, the weight ratio of the component (A) to the component (B) being from 0.5 to 1.5, and the amount of the component (C) is from 50 to 30 parts by weight; the composition having a flexural modulus of 10,000 to 20,000 kg/cm.sup.2.

Abstract: A polypropylene thermoplastic resin composition comprising (a) a modified crystalline polypropylene of a crystalline polypropylene comprising said modified crystalline polypropylene and (b) a modified polyamide obtained by partially or wholly grafting a polyamide with a clay mineral. A polypropylene thermoplastic resin composition comprising, in addition to the above polypropylene thermoplastic resin composition comprising the components (a) and (b), one or any combination of the following components (c), (d) and (e): (c) an ethylene-.alpha.-olefin copolymer rubber or a modified ethylene-.alpha.-olefin copolymer rubber, (d) a block copolymer between a monovinyl-substituted aromatic hydrocarbon and a conjugated diene, a hydrogenation product of said block copolymer, or a modification product of said block copolymer, and (e) an inorganic filler.

Abstract: A modified polyolefin-polyester graft copolymer includes (a) 10-90 parts by weight of a polyester having an intrinsic viscosity [.eta.] of 0.30-1.20 and an end carboxyl group content of 15-200 milliequivalent/kg, and (b) 90-10 parts by weight of a modified polyolefin having 0.2-5 mol % of an epoxy group or carboxyl group content and a weight-average molecular weight of 8,000-140,000.A thermoplastic resin composition includes (a) 5-95 weight % of an aromatic polycarbonate, (b) 95-5 weight % of a polyolefin, and (c) 1-30 parts by weight, per 100 parts by weight of (a)+(b), of the graft copolymer.

Abstract: A polypropylene thermoplastic resin composition comprising (a) a modified crystalline polypropylene of a crystalline polypropylene comprising said modified crystalline polypropylene and (b) a modified polyamide obtained by partially or wholly grafting a polyamide with a clay mineral. A polypropylene thermoplastic resin composition comprising, in addition to the above polypropylene thermoplastic resin composition comprising the components (a) and (b), one or any combination of the following components (c), (d) and (e): (c) an ethylene-.alpha.-olefin copolymer rubber or a modified ethylene-.alpha.-olefin copolymer rubber, (d) a block copolymer between a monovinyl-substituted aromatic hydrocarbon and a conjugated diene, a hydrogenation product of said block copolymer, or a modification product of said block copolymer, and (e) an inorganic filler.

Abstract: The polypropylene-based composite resin composition of the invention, which can be molded into a shaped article having excellent surface hardness and impact strength at low temperatures and usable as a shell plate member of automobiles, comprises (a) a polypropylene resin as the matrix phase, (b) particles of rubber-reinforced styrene-based resin as the dispersed phase having a specified area-average particle diameter, of which the rubber particles having a specified area-average particle diameter forms a "salami" structure as dispersed in the styrene-based resin, and (c) a layer of a compatibility improver, such as a styrene-based thermoplastic elastomer, on the surface of the particles of the rubber-reinforced styrene-based resin in a specified thickness.