Patent classifications
B32B2305/076
SURFACE-MODIFYING SHEET, SURFACE-MODIFIED MEMBER, COATED ARTICLE AND METHOD FOR PRODUCING COATED ARTICLE
The present invention relates to a surface-modifying sheet including a release sheet and a surface-modifying layer, the surface-modifying layer having an average thickness of 0.1 μm to 50 μm, and the difference between the maximum value and the minimum value of the thickness of the surface-modifying layer being less than twice the average thickness; and a surface-modified member, a coated article and a method for producing a coated article, using the surface-modifying sheet.
APPARATUS AND METHOD FOR PEELING A LINER AWAY FROM A SUBSTRATE
An apparatus is provided for peeling a liner away from a substrate. The apparatus comprises a first member rotatable about an axis. The apparatus also comprises a second member disposed on the first member and for generating a suction force to be applied to the liner to peel a portion of the liner away from the substrate when the suction force of the second member is applied to the liner and the first member is rotating about its axis. The apparatus further comprises a third member synchronized to rotation of the first member about its axis such that the third member clamps the peeled portion of the liner against the first member while the second member is applying suction force to the liner and the first member is rotating about its axis.
Material systems and methods of manufacturing material systems
A material system may include: an aluminum layer; a glass composite layer adjacent to the first aluminum layer; and a carbon composite layer adjacent to the first glass composite layer, and opposite to the first aluminum layer. A method of manufacturing a material system may include: stacking an aluminum layer, glass composite layer that may include thermoplastic prepreg plies, and carbon composite layer so that the aluminum layer is adjacent to the glass composite layer, and the glass composite layer is adjacent to the carbon composite layer; and consolidating the thermoplastic prepreg plies to soften the aluminum layer. A method of manufacturing a material system may include: stacking an aluminum layer, glass composite layer that comprises thermoplastic resin, and carbon composite layer so that the glass composite layer is between the aluminum and carbon composite layers; and adjusting temperature and pressure to consolidate the stack.
Apparatus and method for peeling a liner away from a substrate
An apparatus is provided for peeling a liner away from a substrate. The apparatus comprises a first member rotatable about an axis. The apparatus also comprises a second member disposed on the first member and for generating a suction force to be applied to the liner to peel a portion of the liner away from the substrate when the suction force of the second member is applied to the liner and the first member is rotating about its axis. The apparatus further comprises a third member synchronized to rotation of the first member about its axis such that the third member clamps the peeled portion of the liner against the first member while the second member is applying suction force to the liner and the first member is rotating about its axis.
METHOD FOR PRODUCING A LAMINATED VENEER LUMBER BOARD
A method for producing a laminated veneer lumber board adapted to be used for curved modules in which a plurality of laminated veneer lumber boards are laminated to each other to form a curved laminated wood module, where the method includes the steps of: cutting a plurality of veneer plies, placing a first part of a first set of plies in a mould with the wood grain directed in a first direction, placing a second set of plies including one or two plies with the wood grain directed to be perpendicular to the first direction on the first part, placing a second part of the first set of plies with the wood grain directed in the first direction on the second set of plies, and gluing and pressing the plies to each other to form the laminated veneer lumber board.
METHOD FOR MANUFACTURING STRUCTURE, METHOD FOR PREPARING SKIN MATERIAL, AND METHOD FOR SETTING HEATING CONDITION FOR SKIN MATERIAL
A method is for manufacturing a honeycomb structure including a core material in which a hole is formed to penetrate in a thickness direction and is arranged in a plane direction, and a skin material that is stacked on a surface of the core material. The skin material includes a thermosetting resin. The method includes half-curing the thermosetting resin by placing the skin material in a bag and heating the skin material in a state where an inside of the bag is evacuated and an outside of the bag is under an atmospheric pressure; stacking the skin material in which the thermosetting resin is half-cured onto a side of the surface of the core material; and bonding and integrating the core material and the skin material with each other by pressurizing and heating the stacked core material and skin material with the use of a sealing pressurizing heating facility.
METAL-FIBER-REINFORCED RESIN MATERIAL COMPOSITE AND PRODUCTION METHOD THEREOF
A metal-fiber reinforced resin material composite is provided which improves the shear strength between a metallic member and a fiber reinforced material by more strongly bonding the metallic member and the fiber reinforced resin member, and which is very light and has excellent workability while increasing strength.
[Solution]
This metal-fiber reinforced resin material composite is provided with a metallic member and with a fiber reinforced resin material that is stacked on at least one surface of the metallic member and combined with the metallic member, wherein the fiber reinforced resin material comprises a matrix resin containing a thermoplastic resin, a reinforcing fiber material included in the matrix resin, and a resin layer interposed between the reinforcing fiber material and the metallic member and comprising a resin of the same type as the matrix resin. The shear strength of the metallic member and the fiber reinforced resin material is greater than or equal to 0.8 MPa.
LAMINATED SUBSTRATE USING FIBER-REINFORCED THERMOPLASTIC PLASTIC, AND MOLDED PRODUCT MANUFACTURING METHOD USING SAME
Provided is a laminated substrate wherein a sheet-shaped material with a porosity of 50-99% is laminated onto at least one surface of a prepreg substrate which includes a reinforcing fiber and a thermoplastic resin.
METHOD FOR MANUFACTURING MULTILAYER PRINTED WIRING BOARD
A first stack is formed by stacking a first sheet of metal foil, a first prepreg, and a second sheet of metal foil, one on top of another. The first prepreg is thermally cured by thermally pressing these members to make a double-sided metal-clad laminate. Conductor wiring is formed by partially removing the first sheet of metal foil from the double-sided metal-clad laminate to make a printed wiring board. After a third sheet of metal foil has been preheated, the conductor wiring of the printed wiring board, a second prepreg, and the third sheet of metal foil are stacked one on top of another and thermally pressed together. The first insulating layer has a lower linear expansion coefficient than any of the first sheet of metal foil or the second sheet of metal foil does.
Laminate structures comprising fiber-reinforced thermoplastic prepreg plies
A laminate structure may include: an aluminum layer; a glass composite layer adjacent to the aluminum layer; and/or a carbon composite layer adjacent to the glass composite layer, opposite to the aluminum layer. The glass composite layer may include one or more glass-fiber-reinforced thermoplastic prepreg plies. The carbon composite layer may include one or more carbon-fiber-reinforced thermoplastic prepreg plies. A laminate structure may include: a first aluminum layer; a first glass composite layer adjacent to the first aluminum layer; a first carbon composite layer adjacent to the first glass composite layer, and opposite to the first aluminum layer; and/or a second glass composite layer adjacent to the first carbon composite layer, and opposite to the first glass composite layer. The first glass composite layer may include one or more glass-fiber-reinforced thermoplastic prepreg plies. The first carbon composite layer may include one or more carbon-fiber-reinforced thermoplastic prepreg plies.