The Boeing Company

Paul David Evans

Max Marley Osborne

Christopher A Howe

Thomas Wilson

Jason J McBain

Weidong Song

Stephen Lee Metschan

Jeffrey Hayden Olberg

Richard V Phillips

Stuart Arthur Bateman

Peter J Lockett

Gwen Marie Lanphere Gross

Manning James Scarfe

Jamie J Langabeer

Sam Meure

Kariza Thea Martin

Hugh A Yap

Martin Leary

Kaustubh Dongre

Nicholas J Zayas

Sarah Pearn

David William Reynolds

Gerard J Gallo

Examples are disclosed herein that relate to vehicles, composite parts, and methods for forming a composite part for a vehicle. In one example, a vehicle comprises a composite part comprising a skin comprising one or more material layers. The composite part further comprises a stiffener comprising one or more material layers, wherein the stiffener comprises a flange and a web. The composite part also includes an additively manufactured sub-structure positioned between at least a portion of the skin and at least a portion of the stiffener. The additively manufactured sub-structure comprises at least one flange portion, at least one radius, and at least one radius filler. A polymer matrix is co-infused within the skin, the stiffener, and the additively manufactured sub-structure.

Composite part with additively manufactured sub-structure

In a method of producing symmetrical carbon fiber reinforced composite parts, a plurality of sheets of fibrous material configured as a single structure are positioned on a tool surface where the single structure is comprised of a first composite part joined to a symmetric, second composite part. The single structure is infused with resin and cured on the tool surface, producing a single cured structure comprised of a first cured composite part joined to a second cured composite part. The single cured structure is then divided along a dividing plane, producing the symmetric first cured composite part and second cured composite part.

Method of manufacturing a first cured part and a second cured part

A method for forming a composite structure includes the steps of: forming a fiber-reinforced polymer paste to a shape of a cavity of a dry fiber preform structure; heating said dry fiber preform structure having said fiber-reinforced polymer in said cavity to an infusion temperature; infusing resin into said dry fiber preform structure and around said fiber-reinforced polymer; and curing said resin-infused fiber preform structure and said fiber-reinforced polymer at a cure temperature higher than said infusion temperature.

Method for forming 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 three dimensional permeable thermoplastic tape useful for joining of layers of fiber tows (plies) together so as to form highly toughened resin infused structures. In one or more embodiments, the tape is manufactured using three dimensional printing and is applied between layers of fiber tows so as to tack the layers of fiber tows in place and prevent movement of the layers of fiber tows.

Three dimensional printed fibrous interlocking interlayers

A tool and its method of use direct a flow of liquid resin through a preform. The tool has a tool surface with a channel recessed into the tool surface to a bottom surface of the channel. A plate is positioned on the tool surface covering over the channel with the plate being supported by the tool in the channel spaced above the bottom surface of the channel and with the top surface of the plate positioned coplanar with the tool surface of the tool. A preform is positioned on the tool surface with the preform covering over the plate. A flow of liquid resin is supplied to the tool surface and a pressure differential communicating with the tool surface draws the flow of liquid resin into the channel, through the channel and through a plurality of perforations through the plate and into the preform.

Apparatus and method for manufacturing liquid molded composites using a discrete network of tool surface resin distribution grooves

A method of infusing liquid resin into a preform involves positioning a preform on a planar section of a tool surface and a trough section of the tool surface, where the planar section of the tool surface is positioned vertically above the trough section of the tool surface and with there being a plurality of grooves in the planar section of the tool surface and a bottom of the trough section of the tool surface. At least one of a fluid impervious sheet, a second tool and a vacuum bag is secured on the tool surface over the preform forming a sealed volume on the tool surface. A pressure differential and a flow of resin is supplied onto the tool surface and the liquid resin is infused into the preform by the pressure differential.

Growing community of inventors

Port Melbourne, Australia

Paul David Evans