The Boeing Company

Michael Honea

Christopher J Senesac

Ralph P Heinefield

Jeffrey Lawrence Miller

Christopher Luis Carpenter

Stephen J Dostert

Robert Stephen Strong

Fredrick Carl Rudnick, Iii

Kyle W Lehning

A part analysis tool is used to analyze aspects of a composite part. The part analysis tool includes a verification control unit that compares numerical control data used to control operation of a forming system that is used to form the composite part to computer-aided design (CAD) data that includes an authoritative part definition for the composite part. The verification control unit determines whether the numerical control data is within one or more conformance thresholds related to the CAD data. The part analysis tool may also include an inspection control unit that compares inspection data of one or more plies of the composite part to the CAD data. The inspection control unit determines whether the inspection data is within the conformance threshold(s) related to the CAD data.

System and method for validating and inspecting composite parts

Systems and methods are provided for creating three dimensional (3D) visualizations of in-process products. One embodiment is an apparatus that includes a controller and an interface. The controller is able to generate a 3D scene depicting ongoing assembly of a product by a machine tool. The scene includes a 3D model of the product and a 3D model of the machine tool, and the 3D models are placed within the scene based on a location of the product and a location of the machine tool. The interface is able to receive an update from the machine tool indicating a 3D placement of a part that has been attached by the machine tool to the product. The controller is also able to acquire a 3D model of the part, to insert the 3D model of the part within the scene based on the 3D placement, and to provide the scene for display to a user.

3D visualizations of in-process products based on machine tool input

A method and apparatus for analyzing nonconformances. A volume in an aircraft is identified. The nonconformances within the volume of the aircraft are identified. Graphical indicators are displayed indicating the nonconformances within the volume in a graphical user interface on a display device.

Nonconformance identification and visualization system and method

A method and apparatus for comparing aircraft parts. A first model is identified for a first aircraft for assembly. A second model is identified for a second aircraft that has been assembled. First parts for the aircraft in the first model are compared with second parts for the second aircraft in the second model. Graphical representations of the first parts and the second parts are displayed illustrating a difference between the first parts and the second parts from a comparison of the first parts and the second parts.

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Summerville, SC, United States of America

Michael Honea