The Boeing Company

Other

Michael Palmore Matlack

Jeffrey H Wood

Kurt A Burton

Steven Michael Shewchuk

John A Baumann

Randall Dow Wilkerson

James Rodney Fox

Amy Marie Helvey

Timothy J Luchini

Ryan Joseph Merriman

Dylan Edward Polus

Philip P Steinacher

Dennis Ray Mathis

David L Fritsche

Keith A Young

Eric Eldon Deck

Zeaid F Hasan

Richard J Lederich

Ravi Verma

Scott Anthony Martin

Donald C Besselsen

David Phillip Bruk

Justin Joseph Schell

Francis J Samalot

Emily E McDonald

Christopher M Weingart

Dylan E Polus

Emily E Mcdonald

James A Witte

A thermoplastic welding assembly and method for joining a plurality of thermoplastic support components to a thermoplastic component is provided. The thermoplastic welding assembly includes a frame, a plurality of heat sinks, and a plurality of individually actuatable pressurizers. The frame includes a plurality of welding slots. Each heat sink of the plurality of heat sinks is positioned within one of the welding slots. Each pressurizer of the plurality of individually actuatable pressurizers includes an alignment actuator configured to move one thermoplastic support component into alignment with one welding slot, and a clamping actuator configured to move the one thermoplastic support component into contact with the thermoplastic component. In some implementations, the thermoplastic welding assembly further includes a plurality of actuators configured to move the alignment actuator and the clamping actuator.

Thermoplastic composite induction welding tooling for ribs

A method and apparatus for a continuous compression molding machine. The continuous compression molding machine comprises a tooling die, extending through a heating zone and a cooling zone, a tooling sleeve, and a biasing system. The tooling sleeve corresponds to the tooling die and is for use in forming a thermoplastic composite part from a thermoplastic composite charge when the tooling sleeve with the thermoplastic composite charge is moved with respect to the tooling die through the heating zone and the cooling zone. The biasing system is configured to hold the thermoplastic charge at a first angle within the heating zone and hold the thermoplastic composite charge at a second angle within the cooling zone, as the tooling sleeve moves through the heating zone and the cooling zone with the thermoplastic composite charge. The first angle is different from the second angle.

Thermoplastic composite part manufacturing system and method

A method of heating a tool assembly includes the step of joining a first piece of the tool assembly with a second piece of the tool assembly via a first joint portion and a second joint portion. The method further includes the step of inserting a fastener through the first joint portion and the second joint portion of the tool assembly. The method further includes the step of applying heat to the tool assembly, wherein upon heating, interlock surfaces of the first joint portion and the second joint portion tighten against each other.

Tool assembly for composite part fabrication

A composite manufacturing system and method are provided. The composite manufacturing system comprises a press and a bladder. The press has an upper portion having a desired shape for a composite structure and a lower portion configured to receive layers of composite material. The bladder is associated with the upper portion of the press and is configured to reach a superplastic state when heated such that the bladder forms to the composite structure by applying heat and pressure to the layers of composite material. The bladder cools without appreciable shrinkage, applying a desired amount of pressure to the composite structure during the entire cooling cycle. Once one composite structure is formed using the bladder, the bladder may be reused to form similar structures.

Method and system for manufacturing composite structures using a magnesium bladder

A system and method of forming a composite structure includes heating an outer mold line surface of a tool to a processing temperature, positioning an inner mold line surface with a composite preform disposed thereon within the outer mold line surface, and extracting the inner mold line surface and the composite preform in a gelled state from the outer mold line surface.

System and method for manufacturing composite structures

A system and method for manufacturing a composite structure includes a tool having an outer mold line surface, a mandrel removably disposed within the tool and having an inner mold line surface, and a heating element connected to the tool. The heating element is configured to set a process temperature of the outer mold line surface when the mandrel is placed within the tool.

A coating system operations vehicle. Related methods are provided for filling a tank and operating coating equipment on a vehicle. The methods include pumping coating from containers into a tank on the vehicle and dispensing the coating for application on a surface. A method also includes removing residual coating from the containers after pumping out coating and adding the residual coating material to the tank. If the level of coating is at the desired level in the tank, a layer of water may be formed over the coating in the tank.

Systems and methods for providing coating operations

A press tool for a press assembly includes an additive manufactured body including a plurality of stacked layers of additive manufacturable material extending between an interior side and an exterior side. The interior side has a part forming surface including a surface profile for forming a part. The exterior side has a plurality of hollow cores defined by longitudinal walls and lateral walls meeting at joints. Press inserts are coupled to the longitudinal walls and the lateral walls at the exterior side. The press inserts are configured to be pressed inward by a pressing load during a pressing operation for forming the part. The press inserts distribute the pressing load along the longitudinal and lateral walls.

Press assembly having a press tool

A tool assembly includes a first piece, a second piece, and a fastener. The first piece has a first joint portion including a top surface and at least a first interlock surface. The second piece has a second joint portion configured to interlock with the first joint portion. The second joint portion includes a top surface and at least a second interlock surface that is complementary to the first interlock surface. The fastener extends through the first and second joint portions. The first interlock surface and the top surface of the first joint portion form an obtuse angle corner and the second interlock surface and the top surface of the second joint portion form an acute angle corner. The first interlock surface is configured to contact the second interlock surface to inhibit relative movement between the first piece and the second piece along a longitudinal axis of the tool assembly.

A method and apparatus for a composite structure manufacturing system. The system comprises a heating system and one or more smart bladders that encompass the heating system. The heating system and the one or more smart bladders form a curing tool defining a volume for the composite structure when one or more smart bladders in the one or more smart bladders is in a rigid state.

Unitized composite structure manufacturing system

A tool assembly includes a support frame including support beams and support mounts supporting the support beams. The support frame is rigid and used to transport the tool assembly. A support tool is supported by the support frame and includes a faceplate and a supporting grid structure formed with the faceplate as a monolithic structure defined by a series of AM layers. The faceplate has a supporting surface at a top of the support tool for supporting a working component. The supporting grid structure engages the support beams such that loads are transferred between the support tool and the support frame through the support beams. The support frame maintains dimensional stability of the support tool during transport and when resting within an allowable tolerance of the support tool.

Additive manufactured tool assembly

A method for filling a tank with a coating material on a vehicle. The method includes providing containers of coating material to a location of the vehicle and inserting a draw tube into one of the containers. The method also includes pumping coating material using a draw pump and into the tank on the vehicle. The method also includes removing residual coating material from the containers and adding the residual coating material to the tank. If the coating material level is not at a desired level, the inserting, pumping, removing, and adding steps are repeated with another container of coating material. If the coating material level is at the desired level, a layer of water may be formed over coating material in the tank.

System and method for filling tanks on a customized paint vehicle

One aspect of the disclosure relates to a friction stir welding apparatus. The friction stir welding apparatus includes a spindle housing and a pin tool concentric with an axis and rotatable relative to the spindle housing about the axis. The friction stir welding apparatus also includes a first shoulder not substantially rotatable relative to the spindle housing about the axis and a second shoulder not substantially rotatable relative to the spindle housing about the axis. The pin tool is rotatable relative to the first shoulder and the second shoulder.

Growing community of inventors

St. Charles, MO, United States of America

Michael Palmore Matlack