The Boeing Company

Theboeing Company

Sam Meure

Mark Stewart Wilenski

Christopher A Howe

Martin Alexander Szarski

Paul David Evans

Thomas Wilson

Sarah Pearn

A composite structure includes a number of fiber layers. Each fiber layer of the number of fiber layers includes a fiber bundle and a filament layer at least partially covering the fiber bundle. The filament layer includes discontinuous filaments. The discontinuous filaments include at least one of different length filaments, including first length filaments and second length filaments. The first length filaments include a first length and the second length filaments include a second length. The first length is different than the second length. The discontinuous filaments include at least one of different type filaments, including first type filaments and second type filaments. The first type filaments include a first material composition. The second type filaments include a second material composition. The first material composition is different than the second material composition. The composite structure includes a resin binding the number of fiber layers together.

Filament network for a composite structure

Modular tool inserts for composite part manufacturing and related methods are described herein. An example method includes disposing a preform and a diaphragm assembly above a tool housing and disposing the diaphragm assembly on an upper perimeter surface of the tool housing that defines a cavity. The tool housing includes a docking station and a modular tool insert removably coupled to the docking station. The modular tool insert includes a mold disposed within the cavity. The method includes applying a vacuum within the cavity that pulls the diaphragm assembly, along with the preform, into the cavity such that the preform conforms to a shape of the mold. The method includes removing excess portions of the diaphragm assembly from around the modular tool insert and removing the modular tool insert, along with the diaphragm assembly and the preform, from the docking station.

Modular tool inserts for composite part manufacturing and related methods

A filament network for a composite structure may include a number of fiber layers, wherein each fiber layer includes a fiber bundle and a filament layer at least partially covering the fiber bundle, the filament layer including discontinuous filaments including at least one of different length filaments including first length filaments and second length filaments, wherein the first length filaments include a first length and the second length filaments include a second length, and wherein the first length is different than the second length and different type filaments including first type filaments and second type filaments, wherein the first type filaments include a first material composition, wherein the second type filaments include a second material composition, and wherein the first material composition is different that the second material composition, and a resin binding the number of fiber layers together.

Method for forming a composite structure and a fiber layer for a composite structure

Resin permeation of a dry preform having one or more reinforcement plies is locally influenced during resin infusion using a selectively permeable veil applied to at least one of the reinforcement plies.

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Heatherton, Australia

Sam Meure