The Boeing Company

Thang D Phung

Joseph Warren

Dan Dresskell Day

William Thomas Kline

Geoffrey Allen Butler

Erik Lund

Luis A Perla

Charles Yuanxin Hu

Thomas Joseph Kennedy

Robert G Meyer

Peter J VanVoast

Charles J Nelson

Curtis M Groth

Richard A Ransom

Justin L Holland

Joseph F Warren

A method for forming a structural member and a structural member produced thereby includes positioning a first composite section and a second composite section within a tool. The tool has an inner surface and a wall intersection and is supported by a tool platform. The tool platform and a pressure platform are relatively movable between an open position and a closed position. The tool has a non-planar outer surface against which the member may be pressed. A composite splice member is positioned at least partially overlapping both the first composite section and the second composite section to form a joint in the composite structural member. The composite structural member is pressed against the non-planar outer surface of the tool by applying pressure to the joint from a pressure bladder. Heat is applied to the composite structural member at the joint to cure the composite splice member to the first composite section and the second composite section.

Aircraft skin attachment system

Growing community of inventors

Burien, WA, United States of America

Thang D Phung