B29C70/68

METHOD OF MANUFACTURING AN ADAPTABLE CARBON-FIBER BEAM
20250052226 · 2025-02-13 ·

Provided is a method of manufacturing an adaptable pre-cast resin-infused carbon-fiber beam, which method includes the steps of arranging a plurality of elongate carbon-fiber blocks side by side; arranging sheets to enclose the blocks and to extend over opposing faces of adjacent blocks; arranging the sheets to converge as an outwardly projecting elongate bead at a junction between adjacent blocks; and pulling on the elongate bead to inhibit resin flow between blocks during a resin infusion step. Also provided is a pre-cast adaptable carbon-fiber beam manufactured using that method; a method of manufacturing a wind turbine rotor blade; and a wind turbine rotor blade.

Composition and method to form a composite core material

A composite core material and methods for making same are disclosed herein. The composite core material comprises mineral filler discontinuous portions disposed in a continuous encapsulating resin. Further, the method for forming a composite core material comprises the steps of forming a mixture comprising mineral filler, an encapsulating prepolymer, and a polymerization catalyst; disposing the mixture onto a moving belt; and polymerizing said encapsulating prepolymer to form a composite core material comprising mineral filler discontinuous portions disposed in a continuous encapsulating resin.

Composition and method to form a composite core material

A composite core material and methods for making same are disclosed herein. The composite core material comprises mineral filler discontinuous portions disposed in a continuous encapsulating resin. Further, the method for forming a composite core material comprises the steps of forming a mixture comprising mineral filler, an encapsulating prepolymer, and a polymerization catalyst; disposing the mixture onto a moving belt; and polymerizing said encapsulating prepolymer to form a composite core material comprising mineral filler discontinuous portions disposed in a continuous encapsulating resin.

Composite material reinforcing part of pi-shaped section, in particular a platform for a turbine engine fan, and its method of fabrication
09657583 · 2017-05-23 · ·

A reinforcing part of -shaped section made out of composite material, and a method of making the part, the method including: making a first set of layers of interlinked yarns by three-dimensional weaving to form a first fiber blank portion to form a base preform; making a second set of layers of interlinked yarns by three-dimensional weaving to form a second fiber blank portion to form a stiffener preform, yarns of the second set being interlinked with yarns of the first set by weaving over a central interlinked strip that flares towards side edges of the first fiber blank portion in a zone corresponding to the step of the base; shaping the two fiber blank portions to obtain a single-piece fiber preform having a portion forming a base preform and a portion forming a stiffener preform; and depositing a resin in the fiber preform to form a matrix.

Composite component for a vehicle seat, and vehicle seat

A composite component (110) for a vehicle seat (1), in particular for a motor vehicle seat, includes a plurality of fabric layers (116) of a fibrous material, a matrix material (118) securing the fabric layers (116), and an insert part (140), disposed between at least two of the fabric layers (116), for locally reinforcing the composite component. An insert strand (150) is disposed at least in sections along an edge or an edge surface (141.1) of the insert part (140). A vehicle seat (1) includes the composite component, in particular with a back structure (110) designed as a composite component.

Composite component for a vehicle seat, and vehicle seat

A composite component (110) for a vehicle seat (1), in particular for a motor vehicle seat, includes a plurality of fabric layers (116) of a fibrous material, a matrix material (118) securing the fabric layers (116), and an insert part (140), disposed between at least two of the fabric layers (116), for locally reinforcing the composite component. An insert strand (150) is disposed at least in sections along an edge or an edge surface (141.1) of the insert part (140). A vehicle seat (1) includes the composite component, in particular with a back structure (110) designed as a composite component.

Method for enabling the partial printing of a device

An apparatus and method for multi-stage printing teaches means for removing and replacing a printed component during the printing process and accurately placing the component in the printer for continuation of the printing process. This can be accomplished through the use of a scanner, probe machine, or scanning Additionally, the present invention teaches the use of heating means in combination with a 3D printer to overcome additional issues with multi-sage printing.

Cover for air conditioning device for vehicle, and method for manufacturing same

A cover for an air conditioning device for a railway vehicle is a cover for an air conditioning device for a vehicle, which covers an air-conditioner main body. The cover includes a core made of a foamed material having heat insulating property, and a surface member made of a fiber reinforced plastic, which covers entire surfaces of the core. The core is deformed into a curved shape by elastic deformation.

METHOD FOR BUILDING AND USING THREE-DIMENSIONAL OBJECTS CONTAINING EMBEDDED IDENTIFICATION-TAG INSERTS

A method for building a three-dimensional object containing an identification-tag insert, the method comprising performing a build operation to form layers of the three-dimensional object using a layer-based additive technique, placing the identification-tag insert on at least a portion of the layers during the build operation, and reading information from the identification-tag insert.

METHODS AND APPARATUS FOR MOLDING AND JOINING COMPOSITE PARTS
20170120545 · 2017-05-04 ·

Methods and apparatus for molding and joining composite parts are disclosed. An example apparatus disclosed herein includes a tool base and a base mandrel removably coupled to the tool base, where the tool base and the base mandrel form a support structure base for a first radar assembly or a second radar assembly. A first part mandrel interchangeable with the base mandrel is removably coupled to the tool base, where the first part mandrel has first features to support a first antenna module during assembly of the first radar assembly. A second part mandrel interchangeable with the base mandrel is removably coupled to the tool base, where the second part mandrel having second features to support a second antenna module during assembly of the second radar assembly.