Patent classifications
B32B19/06
THERMOSETTING RESIN COMPOSITION, PREPREG, RESIN SHEET, METAL FOIL-CLAD LAMINATE, AND PRINTED WIRING BOARD
A thermosetting resin composition containing a thermosetting resin (A), boron nitride (B), and a dispersant (C) with a pH of 8 or higher.
MODULAR BUILDING SYSTEM
A manufactured building system is described. The building system can include modular components such as floor panels, roof panels, window walls, demising walls, utility walls, end walls, and/or corbel beams.
MODULAR BUILDING SYSTEM
A manufactured building system is described. The building system can include modular components such as floor panels, roof panels, window walls, demising walls, utility walls, end walls, and/or corbel beams.
TRANSPARENT RESIN FILM, DECORATIVE BOARD, AND METHOD FOR PRODUCING DECORATIVE BOARD
The present invention provides a transparent resin film which enables visual check of the adhesion state after lamination of the transparent resin film on a picture layer provided on a substrate, a decorative board including the transparent resin film, and a method for producing the decorative board. Provided is a transparent resin film for protecting a picture layer provided on one side of a substrate, the transparent resin film including at least: a thermoplastic resin layer; and an external haze layer on a picture layer side.
LAYERED COMPOSITE ARTICLES AND METHODS OF MAKING SAME
Described is a method of making a densified fiber batt that includes the steps of: a) providing a fiber batt with a first plurality of fibers having a first melting point and a second plurality of fibers having a second melting point different from the first melting point; and b) subjecting the fiber batt to heat and pressure in a static press, thereby forming a densified fiber batt having a first surface and an opposed second surface.
THERMAL BARRIER MATERIAL FOR ELECTRIC VEHICLE BATTERY APPLICATIONS
A composite thermal barrier material for use in electric and hybrid vehicle battery packs is described herein. The composite material comprises a porous core layer, a pair of flame retardant layers disposed on either side of the porous core layer, and at least one radiant barrier layer disposed between the porous core layer and one of the pair of flame retardant layers. In some exemplary embodiments, the porous core layer is a thermally expandable layer.
METHOD FOR PRODUCING A THERMOPLASTICALLY DEFORMABLE, FIBER-REINFORCED FLAT SEMI-FINISHED PRODUCT
Thermoplastically moldable fiber reinforced planar semifinished products having a composite structure (A-B-A′) or (A-B) are produced by a method of applying to one or both sides of a flat, porous reinforcing-fiber thermoplastic material core layer precursor having an areal weight of 300 to 3,000 g/m.sup.2, a fiber content of 20 to 60 wt.-% and an air void content of 20 to 80 vol.-%, at least one woven or nonwoven reinforcing fiber fabric having an areal weight of 100 to 1,000 g/m.sup.2 and a thermoplastic layer having a low viscosity compared with the thermoplastic material of the core layer precursor and having an areal weight of 50 to 1,000 g/m.sup.2, and heating and pressing the layer structure formed such that the low viscosity thermoplastic layer is melted and penetrates into the applied woven or nonwoven reinforcing fiber fabric and into the core layer and, after cooling, forms an integral bond with the core layer and cover layer.
METHOD FOR PRODUCING A THERMOPLASTICALLY DEFORMABLE, FIBER-REINFORCED FLAT SEMI-FINISHED PRODUCT
Thermoplastically moldable fiber reinforced planar semifinished products having a composite structure (A-B-A′) or (A-B) are produced by a method of applying to one or both sides of a flat, porous reinforcing-fiber thermoplastic material core layer precursor having an areal weight of 300 to 3,000 g/m.sup.2, a fiber content of 20 to 60 wt.-% and an air void content of 20 to 80 vol.-%, at least one woven or nonwoven reinforcing fiber fabric having an areal weight of 100 to 1,000 g/m.sup.2 and a thermoplastic layer having a low viscosity compared with the thermoplastic material of the core layer precursor and having an areal weight of 50 to 1,000 g/m.sup.2, and heating and pressing the layer structure formed such that the low viscosity thermoplastic layer is melted and penetrates into the applied woven or nonwoven reinforcing fiber fabric and into the core layer and, after cooling, forms an integral bond with the core layer and cover layer.
HIGH-TEMPERATURE INSULATION FOR THERMALLY INSULATING PIPES
A high-temperature insulation for thermally insulating pipes includes a carrier layer, wound helically to form a tubular main body and has four or more windings, and has three or more different insulating layers. The inner winding circumferentially surrounds the inner cavity of the tubular main body. The circumference of the inner cavity is at least 50 mm. The insulating layers are arranged in the gaps between the windings of the carrier layer and contact the carrier layer both radially inwardly and radially outwardly. The insulating layers are arranged in the carrier layer have, along the circular path specified by the winding, a length that corresponds to at least 80% of the circumference of the inner cavity of the tubular main body. The carrier layer, the first insulating layer, the second insulating layer, and the third insulating layer each consist of different materials and/or thermal conductivities and/or temperature resistances.
HIGH-TEMPERATURE INSULATION FOR THERMALLY INSULATING PIPES
A high-temperature insulation for thermally insulating pipes includes a carrier layer, wound helically to form a tubular main body and has four or more windings, and has three or more different insulating layers. The inner winding circumferentially surrounds the inner cavity of the tubular main body. The circumference of the inner cavity is at least 50 mm. The insulating layers are arranged in the gaps between the windings of the carrier layer and contact the carrier layer both radially inwardly and radially outwardly. The insulating layers are arranged in the carrier layer have, along the circular path specified by the winding, a length that corresponds to at least 80% of the circumference of the inner cavity of the tubular main body. The carrier layer, the first insulating layer, the second insulating layer, and the third insulating layer each consist of different materials and/or thermal conductivities and/or temperature resistances.