The Boeing Company

Spirit Acrosystems, Inc.

Troy Lynn Wampler

Robert Ray Wampler

Michael Arthur Champa

Clark Ray Miller

Rodney L Benson

David Scott Anderson

Mark Kenyon Venskus

Edwin H Fenn

Leonard A Bailey

Stephen Eldred Walters

A system and method for assembling a 360-degree section of an aircraft fuselage or nacelle by properly positioning a plurality of assembly panels relative to a machine datum representing an assembly-level datum schema, drilling full-sized holes proximate to a second skin edge of the panels with the machine, net-trimming a second edge of the panels with the machine, then using the full-sized holes proximate to the second skin edges as alignment features to properly orient and attach pairs of the panels together proximate to first skin edges, opposite of the second skin edges with an auxiliary machine, forming panel pairs. Control systems may be installed into the panel pairs separately and independently, then the panel pairs may be joined together, aligning the full-sized holes proximate to the second edges, and inserting fasteners through the aligned full-sized holes proximate to the second skin edges.

System and method for assembling aircraft components

A method and system for clamping a part in an automated tool to produce the part includes selecting a part for production on an automated tool driving a cutter. Deriving a clamping scenario defines the positioning of a plurality of clamps to fix the part to the automated tool. Generating a numeric controlled cutting program is based upon the part and the clamping scenario. Simulating the running of the numeric controlled program predicts interferences between the cutter and any of the plurality of clamps.

Clamp avoidance cutter path regeneration

Growing community of inventors

Derby, KS, United States of America

Troy Lynn Wampler