Patent classifications
B29B11/16
METHODS FOR PRODUCING SHEET MOLDING COMPOUND AND FOR PRODUCING MOLDED PRODUCT
A method for producing a sheet molding compound including impregnating a resin composition into carbon fibers. The method is characterized in that the bulkiness H.sub.o of the carbon fibers before an impregnation step is 3 mm or more, the compression ratio R.sub.c (H.sub.c/H.sub.o) of the carbon fibers in the impregnation step is less than 1, the thickness of the sheet molding compound is 10 mm or less, and the content Wc of the carbon fibers is 40% by mass or more. The method for producing a sheet molding compound can produce a sheet molding compound having the excellent impregnation property into carbon fibers and thus can be preferably used for exteriors, structures, and the like of an automotive member, a railroad vehicle member, an aerospace vehicle member, a ship member, a housing equipment member, a sport member, a light vehicle member, a civil engineering and construction member, an OA equipment.
THREE-DIMENSIONAL TEXTILE PREFORMS AND COMPOSITE PARTS COMPRISING TEXTILE PREFORMS
Examples are disclosed herein that relate to vehicles, composite parts, and three-dimensional (3D) textile preforms for composite parts. In one example, a 3D textile preform for a composite part comprises a flange portion and a stiffener portion extending upwardly from the flange portion. The stiffener portion comprises a first wall portion that extends from the flange portion and a second wall portion that extends from the flange portion at a location spaced from the first wall portion. A connecting portion connects the first wall portion and the second wall portion at a location spaced from the flange portion.
Moulding method
Method of moulding a moulding material to form a moulded part of carbon fibre-reinforced resin matrix composite material in which a sheet moulding compound is moulded which can provide panels, for example for use as vehicle body panels, which have the combination of very low thickness, very light weight, very low warping and surface defects, and very low anisotropy with regard to localised fibre and resin distribution and their associated appearance and mechanical properties.
Moulding method
Method of moulding a moulding material to form a moulded part of carbon fibre-reinforced resin matrix composite material in which a sheet moulding compound is moulded which can provide panels, for example for use as vehicle body panels, which have the combination of very low thickness, very light weight, very low warping and surface defects, and very low anisotropy with regard to localised fibre and resin distribution and their associated appearance and mechanical properties.
Scrub sponge and preparation method therefor
Disclosed are a scrub sponge and a preparation method therefor. The method for preparing the scrub sponge includes the operations of: obtaining a first mixture by stirring alkalizer, porogen, konjac powder, scrub granule and water, and filling the first mixture into a mold to form a preform, where the preform includes a first sponge layer; forming a parison by sequentially cooking and freezing the preform; and sequentially unfreezing, dehydrating and drying the parison to obtain the scrub sponge.
Scrub sponge and preparation method therefor
Disclosed are a scrub sponge and a preparation method therefor. The method for preparing the scrub sponge includes the operations of: obtaining a first mixture by stirring alkalizer, porogen, konjac powder, scrub granule and water, and filling the first mixture into a mold to form a preform, where the preform includes a first sponge layer; forming a parison by sequentially cooking and freezing the preform; and sequentially unfreezing, dehydrating and drying the parison to obtain the scrub sponge.
Assembly, plant and method for making a preformed shell
An assembly for preforming a reinforced fabric sheet may have at least one frame and a plurality of gripping devices. Each gripping device of the plurality of gripping devices may be suitable for gripping an edge portion of the reinforced fabric sheet. The assembly may have a moving system with a plurality of first moving devices. The movement of each first moving device may be independent of the other first moving devices. Each gripping device of the plurality of gripping devices may be associated with a first moving device. The first moving device may be suitable for moving each gripping device of the plurality of gripping devices independently of the others.
Assembly, plant and method for making a preformed shell
An assembly for preforming a reinforced fabric sheet may have at least one frame and a plurality of gripping devices. Each gripping device of the plurality of gripping devices may be suitable for gripping an edge portion of the reinforced fabric sheet. The assembly may have a moving system with a plurality of first moving devices. The movement of each first moving device may be independent of the other first moving devices. Each gripping device of the plurality of gripping devices may be associated with a first moving device. The first moving device may be suitable for moving each gripping device of the plurality of gripping devices independently of the others.
Method and device for manufacturing a composite part with a complex shape
A method for making a three-dimensional composite part with a thermoplastic matrix and continuous reinforcement. A pre-impregnated fibrous perform is obtained by three-dimensional knitting. The preform is placed on the punch or in the matrix of a tooling, defining between them a sealed closed cavity. The tooling is closed so as to apply a first pressure to the preform. The cavity is brought to the melting temperature of the polymer impregnating the preform by maintaining the first pressure. The cavity comprising the preform is cooled to a temperature suitable for demolding by maintaining the second pressure. The mold is opened and the part is demolded.
Method and device for manufacturing a composite part with a complex shape
A method for making a three-dimensional composite part with a thermoplastic matrix and continuous reinforcement. A pre-impregnated fibrous perform is obtained by three-dimensional knitting. The preform is placed on the punch or in the matrix of a tooling, defining between them a sealed closed cavity. The tooling is closed so as to apply a first pressure to the preform. The cavity is brought to the melting temperature of the polymer impregnating the preform by maintaining the first pressure. The cavity comprising the preform is cooled to a temperature suitable for demolding by maintaining the second pressure. The mold is opened and the part is demolded.