Arris Composites Inc.

Ethan Escowitz

Erick Matthew Davidson

Riley Reese

J Scott Perkins

Sean Hennessee

Christopher P Bender

Cory Mark Bloome

Todd A Pelman

Sam Pirahanchi

Alexander Darrow

Andrew Mathews

Kameron Butler

Bert D Mannhalter

Arnaud Dyen

Dylan Harper

Kenneth Kirkland

Ryan Satcher

Adam Hansel

Fiber-reinforced composite parts include select portions containing a plurality of co-aligned fiber. The parts are fabricated by placing substantially preforms into a mold cavity to form a layup, and compression molding the layup to consolidate the preforms to provide a fiber-reinforced composite part. Different sections of the part can be derived from preforms having different shapes and different compositions.

Compression-molded fiber-composite parts and methods of fabrication

A preform charge is formed by forming an assemblage of preforms, wherein preforms in the assemblage are bonded to a neighboring preform such that the preform charge effectively becomes a single unit. The preform charge can then be added to a mold to fabricate a part via compression molding.

Preform charges and fixtures therefor

Method and apparatus for splaying fibers for the forming preform charges for the production of composite discs, and for the production of composite disc, wherein rotary compaction is applied to an appropriately arranged assemblage of preforms.

Compaction method for composite discs

A method for improving the impact resistance of a fiber-composite part includes positioning fibers within an expected impact region of the part, wherein at least a portion of most of the positioned fibers is oriented to be within about 45 degrees of parallel to an impact vector of an impact that occurs at the impact region. At least some of the fibers in the impact region should have relatively high impact resistance, such as glass fiber or aramid fiber, and the matrix in the impact region should have relatively high impact resistance.

Impact-resistant molded composites and methods therefor

Fiber-composite parts that incorporate a very thin electrical circuit, and a method for making the parts via compression molding, are disclosed. The electrical circuit is encapsulated by a film having a melting point that exceeds the maximum temperature to which the film is exposed during compression molding. The electrical circuit is disposed in a composite ply, in a lay-up of composite plies, and electrical leads are routed through the composite plies so that the lead are accessible in the molded fiber-composite part.

Fiber composites comprising a circuit, and method therefor

Methods for fabricating fiber-composite truss structures comprise a) individually molding multiple unit cells of a given size, and subsequently fusing them together in a repeating pattern, b) cross members are consolidated with longerons while maintaining continuity of fiber in the longerons, and c) compression-molded truss components are unioned to continuous fiber beams by means of mechanically interlocking joints.

Method for composite truss manufacturing

A multi-material molding apparatus and method includes a single mold having, within a mold cavity, one or more movable partitions that segregate at least first and second molding materials. The first molding material is processed to form a first molded portion of the multi-material part. The second molding material is then flowed, through the movable partition, into contact with the first molded portion. That second molding material is then solidified to form a second molded portion of the multi-material part.

System and method for multi-material molding

A method for designing fiber-composite parts in which part performance and manufacturing efficiency can be traded-off against one another to provide an 'optimized' design for a desired use case. In some embodiments, the method involves generating an idealized fiber map, wherein the orientation of fibers throughout the prospective part align with the anticipated load conditions throughout the part, and then modifying the idealized fiber map by various fabrication constraints to generate a process-compensated preform map.

Method for the design and efficient manufacture of fiber-composite parts

Methods and apparatus for additive manufactures of complex parts using co-aligned continuous fibers are disclosed. Filament subunits having complex shapes are fabricated and inserted into a mold cavity. The layup is compression molded to form a complex part having high tensile strength.

Aligned fiber reinforced molding

A method and apparatus for the continuous fabrication of fiber-bundle-based and composite-tape based preforms and preform charges includes a mandrel about which a constituent material, which is maintained under tension, is wound. The tension is insufficient to fully consolidate the wound material.

Method and apparatus for continuous fabrication of fiber-bundle-based and tape-base preforms

An apparatus for molding a part includes a plunger cavity, a plunger, and a mold cavity, wherein the plunger is oriented out-of-plane with respect to a major surface of the mold cavity, and first and second vents couples to respective first and second portions of the mold cavity. In a method, resin and fiber are forced into the mold cavity from a plunger cavity, and at least some of the fibers and resin are preferentially flowed to certain region in the mold cavity via the use of vents.

Method for composite flow molding

A fiber-composite part having one or more electronic components that are located in arbitrary regions of the internal volume of the part are fabricated using a preform charge. The preform charge has a structure that corresponds to that of the mold cavity in which the part is being formed. By incorporating the electronic components in the preform charge, such components are then precisely located, spatially oriented, and constrained, and such location and orientation is maintained during molding to produce a part with the electronic components in the desired locations and orientations within its internal volume.

Method and compositions for embedding electronics in fiber-composite parts fabricated via compression molding

A method for making structural foam parts having continuous aligned fibers includes placing an assemblage of fiber-bundle-based preforms in an injection mold, creating a melt flow of resin and, optionally, short, loose fiber, and adding foaming agent to the melt flow. When the foaming agent/melt flow mixture is introduced into the injection mold, the foaming agent foams. The assemblage is structured and positioned so that fibers therefrom adopt a desired alignment and position in the final part. Structural foam fills the remainder of the volume of the part.

Structural foam molding method using continuous fiber composites, and parts formed therefrom

A method for forming a composite part involves forming a layup comprising (a) preforms/flat form-factor feedstock, either of which includes a plurality of fibers and a matrix precursor, and (b) a differential-melt polymer. The matrix precursor and the differential-melt polymer differ as to at least one of thermal properties and rheological properties. The layup is subjected to controlled application of heat and pressure to melt the matrix precursor and differential-melt polymer. The polymers are then cooled to form a composite part that displays properties attributable to all the constituents. As a function of a variety of factors, the resulting part can be homogenous or heterogenous, and the properties can be localized or global throughout the part.

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Berkeley, CA, United States of America

Ethan Escowitz