B29C2043/3655

HOT PRESS CUSHIONING MATERIAL AND MANUFACTURING METHOD THEREOF
20210402726 · 2021-12-30 ·

A hot press cushioning material includes a base material layer that is in the form of a plate and that contains fibers; and an end face seal covering an outer end face of the base material layer. The end face seal includes a heat resistant elastic body having penetrated the outer end face of the base material layer and a heat resistant resin attached to an outer surface of the heat resistant elastic body.

HOT PRESS CUSHIONING MATERIAL AND MANUFACTURING METHOD OF HOT PRESS CUSHIONING MATERIAL
20210402725 · 2021-12-30 ·

A hot press cushioning material includes a cushioning material body in the form of a plate; and surface materials provided on the front and back sides of the cushioning material body. The surface material includes a core layer composed of a heat resistant fiber material for a nonwoven structure, and a front-side resin layer covering the entire front side of the core layer. The core layer has an air permeability of 5 cm.sup.3.Math.cm.sup.−2.Math.s.sup.−1 or less and a bulk density of 0.8 g/cm.sup.3 or more.

Methods For Producing A Structural Component
20220161508 · 2022-05-26 ·

Methods of manufacturing a structural component each include providing a preformed layered structure including a plurality of layers each having reinforcing fibers embedded in a thermoplastic matrix material, heating the layered structure in a cavity formed between a contour surface and an abutment member to a first temperature, which is greater than a melting point of the thermoplastic matrix material, and cooling the layer structure in the cavity to a solidification temperature which is, e.g., less than the melting point of the thermoplastic matrix material, while applying a compression pressure. According to a method, the compression pressure is generated by using a magnet device to generate a magnetic field directed transversely to the contour surface, which pulls or compresses the abutment member and the contour surface relative to each other. According to a further method, inductive heating of the cavity occurs.

Method for using composite tooling to manufacture composite parts
11738526 · 2023-08-29 · ·

A method and apparatus for manufacturing a composite part is provided. A composite laminate is formed upon a first tool that provides a first mold line for the composite laminate. A second tool is placed against the composite laminate in which a tooling surface of the second tool is used to create a second mold line for the composite laminate. The second tool is formed from a plurality of prefabricated sections joined by a joining material in which the tooling surface is formed by a layer adhered to the plurality of prefabricated sections and the joining material.

MOLDING METHOD AND MOLDING JIG FOR LAMINATED BODY
20220024159 · 2022-01-27 ·

A method for molding a laminated body includes laminating a reinforced fiber base material on a molding surface of a molding jig to form a laminated body; attaching a pulling jig to a third lamination portion of the laminated body; forming a protrusive curvature part and a recessed curvature part in the laminated body by curving the laminated body along a protrusive curvature surface and a recessed curvature surface formed on the molding surface while pulling the end of the laminated body with the pulling jig; and densifying the laminated body by heating the curved laminated body while pressurizing the same. The reinforced fiber base material is laminated so that at least a part of a gap between layers of the reinforced fiber base material becomes a non-adhered state in a portion from the protrusive curvature part to the third lamination portion formed in the laminated body.

Method of fabricating a composite structure

A method of fabricating a composite structure is presented. The method comprises laying up a plurality of composite plies over a layup mandrel; positioning a first caul plate and a second caul plate over the plurality of composite plies, leaving composite material exposed; removing at least part of the composite material exposed between the first caul plate and the second caul plate to separate a first composite section from a second composite section; curing the first composite section and the second composite section to form a first composite part and a second composite part; and removing the first composite part and the second composite part from the layup mandrel immediately following curing.

Hot press cushioning material
11787143 · 2023-10-17 · ·

A hot press cushioning material includes a base material layer that is in the form of a plate and that contains fibers; and an end face seal covering an outer end face of the base material layer. The end face seal includes a heat resistant elastic body having penetrated the outer end face of the base material layer and a heat resistant resin attached to an outer surface of the heat resistant elastic body.

INTEGRATED CAUL WITH ELASTOMERIC SEALS
20230356485 · 2023-11-09 ·

A method, apparatus, and system for applying a vacuum-based pressure on an uncured composite structure. Membranes are bonded to a boundary of a caul. The membranes include positive features that define vacuum channels. The membranes are spliced to each other. The positive features that define the vacuum channels in the membranes are aligned to each other during splicing of the membranes. The membranes spliced to each other and bonded to the caul to form an integrated caul. The integrated caul applies a pressure on the uncured composite structure during operation of the integrated caul.

SYSTEM AND METHOD FOR MANUFACTURING PANELS FOR USE IN WIND TURBINE ROTOR BLADE COMPONENTS

A system for manufacturing a panel includes a support frame, a first caul plate arranged atop the support frame, a second caul plate arranged atop the first caul plate, and a heating assembly having a housing defining an inlet and an outlet. The housing includes one or more heaters. The heater(s) is configured to generate heat and the housing is configured to generate a first pressurized gas film. Thus, one or more layers of material to be consolidated may be placed between the first and second caul plates and drawn through the heating assembly as the heating assembly applies pressure to the one or more layers of material to be consolidated via the first pressurized gas film in combination with applying the heat via the one or more heaters, thereby consolidating the panel.

SYSTEM AND METHOD FOR FORMING STACKED MATERIALS

An intensifier mechanism for forming stacked material includes a support, a first body coupled to the support, and a second body having a main portion, a pivoting portion, and a joint. The main portion is coupled to the support and the joint movably couples the main portion to the pivoting portion. The joint allows the pivoting portion to pivot in relation to the main portion when the membrane moves towards the bottom wall.