B29C70/00

Method for preparing ultra high molecular weight polyethylene composite materials

The present invention provides a method for preparing an ultra high molecular weight polyethylene (UHMWPE) composite material including the following steps: providing a substrate material having medical grade ultra high molecular weight polyethylene powders, drying the substrate material to obtain fully dried UHMWPE powders, and pressing the fully dried UHMWPE powders to form a UHMWPE board; immersing the UHMWPE board into a graphene oxide solution and performing an ultrasonic induction by an ultrasonic processor such that the graphene oxide solution infiltrates into the UHMWPE substrate to obtain an ultra high molecular weight polyethylene composite material with excellent biocompatibility and tribological properties. The graphene oxide can be adsorbed and evenly spread on the surface of UHMWPE substrate by ultrasonic induction to form a lubricating film which can effectively reduce wear.

Method for making sole structure with knitted fabric and sole structure

The present invention provides a method for making a sole structure with a knitted fabric and a sole structure. The method comprises steps of: placing a thermoplastic filling material in a knitted fabric, sealing an opening of the knitted fabric, placing the knitted fabric with the opening sealed in a mold, applying a heating temperature to melt the thermoplastic filling material of the knitted fabric, and restricting a shape of the knitted fabric via the mold to make a sole structure. The sole structure includes a compressible elastomer and a knitting texture wrapped around the compressible elastomer and fused with a surface of the compressible elastomer. The compressible elastomer is formed from the thermoplastic filling material after being melted and cooled. The knitting texture is formed from the knitted fabric and is capable of being directly observed from an appearance of the sole structure.

Heated composite tool and method for building and use

A heated composite tool, useful for forming, debulking, and/or curing prepreg materials, including a composite build structure having a shape of a composite part that is to be produced, configured to receive and support prepreg materials during lay-up, and including a heating structure physically coupled to the composite build structure, and comprising at least one heating element, including a carbon nanotube structured layer defining a current path having first and second ends and first and second electrical terminals electrically coupled to the first and second ends and a first isolation ply disposed between the composite build structure and the at least one heating element, the first isolation ply forming an electrical insulating gap between the at least one heating element and the composite build structure, wherein the carbon nanotube structured layer is responsive to an electromotive force applied across the first and second electrical terminals to heat the tool.

COMPOSITE PARTS WITH IMPROVED MODULUS

A high modulus composite part is disclosed comprising a polymer resin; and a plurality of high-performance unidirectional glass fibers. The high-performance unidirectional glass fibers have an elastic modulus of at least 89 GPa and a tensile strength of at least 4,000 MPa, according to ASTM D2343-09. The composite part comprises a fiber weight fraction (FWF) of no more than 88% and an elastic modulus of at least 60 GPa, according to ASTM D7205.

PREPREG, LAMINATE, AND MOLDING

An object of the present invention is to provide a prepreg and a laminate for producing a laminate suitable as a structural material, which have excellent compressive strength and interlaminar fractural toughness values, and can be firmly integrated with another structural member by welding. The present invention provides a prepreg including the following structural components [A] reinforcing fibers, [B] a thermosetting resin, and [C] a thermoplastic resin, in which [B] has a rubbery state elastic modulus of 10 MPa or more at a temperature obtained by adding 50° C. to a glass transition temperature in a state in which a degree of cure is 90% or more, [C] is present in a surface of the prepreg, and the reinforcing fibers [A] are present, which are included in a resin area including {B] and a resin area including [C] across an interface between the two resin areas.

Elastic abrasive manufacturing method, elastic abrasive manufacturing device, blasting method, and blasting device

A re-circulatory blasting device obtained is capable of performing stable treatment for a prolonged period of time even in cases in which an elastic abrasive employed has abrasive grains adhered to the surface of elastic cores. An elastic abrasive regeneration device provided to the blasting device regenerates elastic abrasive employed for re-circulation. The elastic abrasive regeneration device includes a mixer and a combining unit. Recovered abrasive fed in from an abrasive recovery section is mixed in the mixer with abrasive grains fed in from an abrasive grain feeder, and the abrasive grains are adhered to the surface of the cores of the recovered abrasive. In the combining unit, the abrasive grains are pressed against and combined to the surface of the cores by passing an aggregated state of the recovered abrasive mixed by the mixer along a constricted flow path having a flow path cross-sectional area that gradually narrows.

Elastic abrasive manufacturing method, elastic abrasive manufacturing device, blasting method, and blasting device

A re-circulatory blasting device obtained is capable of performing stable treatment for a prolonged period of time even in cases in which an elastic abrasive employed has abrasive grains adhered to the surface of elastic cores. An elastic abrasive regeneration device provided to the blasting device regenerates elastic abrasive employed for re-circulation. The elastic abrasive regeneration device includes a mixer and a combining unit. Recovered abrasive fed in from an abrasive recovery section is mixed in the mixer with abrasive grains fed in from an abrasive grain feeder, and the abrasive grains are adhered to the surface of the cores of the recovered abrasive. In the combining unit, the abrasive grains are pressed against and combined to the surface of the cores by passing an aggregated state of the recovered abrasive mixed by the mixer along a constricted flow path having a flow path cross-sectional area that gradually narrows.

STRETCHABLE ELECTROCONDUCTIVE MATERIAL, METHOD FOR MANUFACTURING THE SAME, AND DEVICE USING THE STRETCHABLE ELECTROCONDUCTIVE MATERIAL
20230159749 · 2023-05-25 ·

A stretchable electroconductive material includes 100 parts by weight of PEDOT-PSS, 200 parts to 1000 parts by weight of a repair linking agent, 15 parts to 300 parts by weight of an ionic liquid plasticizer, and 15 parts to 200 parts by weight of carbon material particles. The repair linking agent is selected from a group consisting of polyethylene glycol and polyethylene oxide, and any combination thereof. The repair linking agent, the ionic liquid plasticizer, and the carbon material particles are doped in the PEDOT-PSS. A method for manufacturing the stretchable electroconductive material and a device using the stretchable electroconductive material are also provided.

DESIGN AND METHOD OF ASSEMBLY OF CARBON FIBER SPACE FRAMES FOR AEROSPACE STRUCTURES
20230061050 · 2023-03-02 · ·

A method of assembly of a carbon fiber space frame structure eliminates the need for gusset plates at the j oints of the space frame structure. The elimination of the gusset plates at the j oints of the space frame structure reduces the weight of the space frame structure and eliminates stresses that occur at the j oints due to gusset plates attached at the j oints.

Method of mesh generation for resin transfer molding process

The present disclosure provides a method of mesh generation for an RTM process, including operations of: obtaining a geometry of a target object; generating a solid mesh of the target object according to the geometry; obtaining material characteristics of the target object; assembling a runner mesh with the solid mesh, wherein the runner mesh has grid dimensions different from those of the solid mesh; determining process parameters of the RTM process; and generating a forecasted result of the RTM process according to the solid mesh, the runner mesh, the process parameters, and the material characteristics. Generating the solid mesh includes operations of: dividing the geometry into modules; generating a first and second modular meshes corresponding to a first and second modules, wherein the second modular mesh abuts the first modular mesh, and the second modular mesh has grid dimensions different from those of the first modular mesh.