The Boeing Company

Other

Alexander Rubin

Randall Dow Wilkerson

James Rodney Fox

Charles Richard Prebil

Patrick Bickford Stickler

Marc Rollo Matsen

Jeffery Lee Marcoe

Amol Ogale

Gregory James Schoepen Hickman

Samuel J Tucker

Michael Marcus Vander Wel

Francis J Samalot

Ulrich Sachs

Carla E Reynolds

Pedro Pablo Martin Alonso

Mike P Matlack

Phillip John Crothers

Lee Charles Firth

Steven Michael Shewchuk

Gregory J Hickman

Gregg Robert Bogucki

Stephen R Heinz

Troy Winfree

Carey E Wilkinson

Timothy J Luchini

Andrew Lawrence Bauer

Joshua David Kalin

Bret Alan McGinness Voss

Dustin D Fast

Ying Shi

Francisco Raul Sacchetti

Yannick Martijn Buser

Marcos Pantoja

Sharon Wong

Pedro Pablo MARTÍN Alonso

Carla Elizabeth Reynolds

A laminate structure may include: an aluminum layer; a glass composite layer adjacent to the aluminum layer; and/or a carbon composite layer adjacent to the glass composite layer, opposite to the aluminum layer. The glass composite layer may include one or more glass-fiber-reinforced thermoplastic prepreg plies. The carbon composite layer may include one or more carbon-fiber-reinforced thermoplastic prepreg plies. A laminate structure may include: a first aluminum layer; a first glass composite layer adjacent to the first aluminum layer; a first carbon composite layer adjacent to the first glass composite layer, and opposite to the first aluminum layer; and/or a second glass composite layer adjacent to the first carbon composite layer, and opposite to the first glass composite layer. The first glass composite layer may include one or more glass-fiber-reinforced thermoplastic prepreg plies. The first carbon composite layer may include one or more carbon-fiber-reinforced thermoplastic prepreg plies.

Methods of making laminate structures

A method for joining a first thermoplastic substrate and a second thermoplastic substrate, each including a polyaryletherketone material having a first melting temperature. The method includes co-consolidating a first semicrystalline thermoplastic film with the first thermoplastic substrate to yield a first co-consolidated structure. The first semicrystalline thermoplastic film defines a first bonding surface of the first co-consolidated structure and includes a polyaryletherketone material having a second melting temperature that is less than the first melting temperature. The method further includes co-consolidating a second semicrystalline thermoplastic film with the second thermoplastic substrate to yield a second co-consolidated structure. The second semicrystalline thermoplastic film defines a second bonding surface of the second co-consolidated structure and includes a polyaryletherketone material having a third melting temperature that is less than the first melting temperature. The method further includes fusing the first bonding surface to the second bonding surface. The method yields a stacked structure.

Methods for joining a first thermoplastic substrate with a second thermoplastic substrate

A material system may include: an aluminum layer; a glass composite layer adjacent to the first aluminum layer; and a carbon composite layer adjacent to the first glass composite layer, and opposite to the first aluminum layer. A method of manufacturing a material system may include: stacking an aluminum layer, glass composite layer that may include thermoplastic prepreg plies, and carbon composite layer so that the aluminum layer is adjacent to the glass composite layer, and the glass composite layer is adjacent to the carbon composite layer; and consolidating the thermoplastic prepreg plies to soften the aluminum layer. A method of manufacturing a material system may include: stacking an aluminum layer, glass composite layer that comprises thermoplastic resin, and carbon composite layer so that the glass composite layer is between the aluminum and carbon composite layers; and adjusting temperature and pressure to consolidate the stack.

Methods of manufacturing material systems

A method of manufacturing a composite structure includes accessing design data for the composite structure that is manufactured according to a process including forming a layup of plies of fibers using a machine tool. The method includes applying the design data to an ANN classifier to classify a localized inconsistency of a type of inconsistency on the composite structure, the localized inconsistency spatially referenced to a location on the composite structure. The method includes performing a root cause analysis to identify one or more of process parameters as a potential cause of the type of inconsistency, and modifying one or more of the geometric model, the layup design, or values of the one or more of the process parameters to address the potential cause.

Composite manufacturing using data analytics

A thermoplastic composition includes a thermoplastic polymer and a polyaryletherketone polymer in admixture with the thermoplastic polymer.

Thermoplastic films and methods for coating thermoplastic substrates with thermoset materials

Methods and apparatus for manufacturing a thermoplastic structure include laying a first plurality of braided plies on a mandrel, and laying one or more unidirectional plies on the plurality of braided plies. A second plurality of braided plies is laid on the one or more unidirectional plies. The layup thereby forms a thermoplastic structure having combined braided and unidirectional plies.

Methods and apparatus for manufacturing a thermoplastic structure

Systems and methods are provided for controlling welding. One embodiment is a method for controlling welding. The method includes initiating induction welding by operating an induction coil along a weld interface of a first composite part comprising a matrix of thermoplastic reinforced by fibers, in order to join the first composite part to a second composite part, determining a measured magnetic field strength at a location distinct from the induction coil, and determining a welding temperature at the weld interface of the first composite part based on the measured magnetic field strength.

Remote detection of induction weld temperature

A system to aid in design for manufacturing an object includes a processor and a memory configured to store instructions. The processor is configured to receive first data representing a design of the object to be manufactured and second data representing a machine-learning model. The processor is configured to execute the instructions to generate third data using the first data and the second data. The third data indicates at least one of a modification to the design of the object or process conditions for production of the object. The processor is configured to send the design of the object, the process conditions, or both, to a manufacturing tool to enable production of the object. The machine-learning model is representative of production data and based at least partially on one or more of: object features, process parameters, environmental factors, and quality data.

Object design using machine-learning model

Systems and methods are provided for controlling welding. One embodiment is a method for controlling welding of a composite part. The method includes locating a linear fiber optic sensor along a composite part comprising a matrix of thermoplastic reinforced by fibers, measuring temperatures along the weld line via the linear fiber optic sensor, performing induction welding at the composite part along the weld line, determining a continuum of weld temperatures along the weld line, and controlling the induction welding based on the continuum of weld temperatures.

This disclosure is directed to a thermoplastic composite material forming method and tooling used to perform the method. More specifically, this disclosure is directed to a method of fabricating large, complex thermoplastic composite part shapes with a consolidation tool having a conformable tooling bladder that heat thermoplastic material in the tool and provide thermoplastic material consolidation pressure in directions in the tool to form a part shape of thermoplastic composite material. A novel tooling concept is used to fabricate large, complex thermoplastic composite part shapes which are not easily producible using traditional methods. The tooling concept employs a consolidation tool that provides a method to apply thermoplastic material consolidation pressure by a conformable tooling bladder that provides thermoplastic material consolidation pressure in directions in the tool that are not achievable by conventional clamshell type molds where the mold parts move in substantially vertical tool opening and tool closing directions.

Fabrication method and apparatus for creating large and/or complex thermoplastic composite components

Material systems and methods of manufacturing material systems

Laminate structures comprising fiber-reinforced thermoplastic prepreg plies

An apparatus for thermoplastic welding includes at least one tool configured to support first and second thermoplastic composite parts in a first welding position having one or more joint lines between the first and second thermoplastic composite parts. The tool includes a plurality of induction coils. The apparatus further includes a susceptor removably positioned along the one or more joint lines. The susceptor is configured to heat the one or more joint lines when exposed to a magnetic flux generated by the plurality of induction coils to bond the first and second thermoplastic composite parts along the one or more joint lines. The apparatus also includes a susceptor removal device coupled to the susceptor and configured to remove the susceptor during bonding of the first and second thermoplastic composite parts.

Methods and apparatus for thermoplastic welding

An elongate thermoplastic composite member is fabricated by a continuous molding process. A pre-consolidated thermoplastic laminate is softened by heating it to a temperature below its melting layup, and is fed substantially continuously through multiple sets of tool dies. The tool dies incrementally mold portions of softened laminate over a mandrel to form the laminate into a shape having a closed cross section.

Continuous molding of thermoplastic laminates

Thermoplastic laminates are fabricated in a continuous compression molding production line. A lay-up of laminate plies is placed in a recess on a carrying tool, and the tool is moved through successive forming operations on the line, including preforming and consolidation operations. The tool is separated from the fully formed part at the end of the line and may be reused. Use of the carrying tool reduces material scrap.

Method and material efficient tooling for continuous compression molding

Growing community of inventors

St. Louis, MO, United States of America

Alexander Rubin