In a method for manufacturing a laminated iron core from a thin sheet, the method includes coining the thin sheet from above to form a thinned bridge portion on an outer peripheral portion of an iron core piece, blanking the iron core piece downwardly from the thin sheet using a set of an outer-shape blanking punch and a die after forming the bridge portion, wherein the outer-shape blanking punch includes a projection portion fitted into the bridge portion when blanking, and laminating the iron core piece on another iron core piece to manufacture the laminated iron core.

A system for pre-fabricating a plurality of synthetic turf strips at an indoor facility. The indoor facility is separate from an installation facility for assembling the plurality of strips into a synthetic field. The system includes a plurality of strips for creating the synthetic field and equipment at the indoor facility for prefabricating the plurality of strips. The indoor facility is capable of storing the equipment performing the prefabrication. A floor at the indoor facility is provided, the floor including dimensions that correspond to locations on a field at the installation facility. The dimensions correspond to markings on an underside of each of the plurality of strips.

A bamboo composite material for structural applications and method of fabricating the same are provided. The method can comprise the steps of providing a bamboo culm; separating a slice or sheet from the bamboo culm such that the slice or sheet has a longitudinal axis along a fiber direction of the bamboo culm; at least partially detaching individual fiber bundles of the slice or sheet from each other along the longitudinal axis of the slice or sheet; applying a glue to the slice or sheet; and curing the glued slice or sheet.

A method for producing a composite multi-layered absorbent article. At least two of the layers include a colored region.

A method of making a laminated shingle is provided. The method includes coating a shingle mat with roofing asphalt to make an asphalt-coated sheet, adhering a reinforcement member to a portion of the asphalt-coated sheet, covering the asphalt-coated sheet, and optionally covering the reinforcement member, with granules to make a granule-covered sheet, dividing the granule-covered sheet into an overlay sheet and an underlay sheet, wherein the overlay sheet has a tab portion normally exposed on a roof and a headlap portion normally covered-up on a roof, the headlap portion having a lower zone adjacent the tab portion and an upper zone adjacent the lower zone, and wherein the reinforcement member is adhered to the lower zone of the headlap portion and laminating the overlay sheet and the underlay sheet to make the laminated shingle.

A fiber placement system for manufacturing composite components includes at least one material storage enclosure including a material spool assembly, a swiveling roller assembly, and a redirect roller assembly, for each tow to be produced per course, at least one material feeding/cutting station configured with a nip roller drive system, and a cutting mechanism, at least one material transfer station configured with an individual, moveable guide tray for each tow to be produced per course, the moveable guide trays respectively being configured with a vacuum system, and at least one layup station comprising a vacuum table/layup surface, and a pick-and-place device equipped with an end-effector.

A system fabricating composite preforms includes a layer assembly stage with a first stage for receiving new layers, such as layer N; and a second stage for holding up to K layers, such as layers N1 to NK. An interlayer reinforcement insertion mechanism inserts interlayer reinforcements Q through layer N and the layers N1 to NK, using a first layer spacing between layer NK and layer NK1 in a completed layer stage. Following the interlayer reinforcements Q insertion, the layer assembly stage transfers the layer NK to the completed layer stage; closes the first layer spacing, bringing layers NK and NK1 into contact; and transfers the layer N to the second stage. The system repeats this cycle of receiving new layers, inserting interlayer reinforcements using layer spacings between the second and completed layer stages, closing these layer spacings, and transferring layers to construct composite preforms with arbitrary numbers of layers.

A laminated core manufacturing method for performing rotational lamination by conveying a band-shaped material to be stamped 10 to a die apparatus to successively perform presswork, stamping out and dropping manufactured core pieces 20 into a blanking die 21 and rotating the blanking die 21 by a predetermined angle, in which a positioning mechanism for the blanking die 21, which has rotational lamination guide pins and rotational lamination guide holes 23-30, is disposed inward from both ends in a width direction of the band-shaped material to be stamped 10 and temporary holes 13-16 for the rotational lamination guide pins to be inserted are provided in the band-shaped material to be stamped 10. The structure allows downsizing of the die apparatus.