3026. Electron Beam Welding of F-22 Aft Fuselage Primary Structures

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Title3026. Electron Beam Welding of F-22 Aft Fuselage Primary Structures
Publication TypeConference Paper
Paper Number3026
Year of Publication2000
AuthorsZenas, Robert
Paper Category27. WEIGHT REDUCTION - MATERIALS
Conference59th Annual Conference, St. Louis, Missouri, June 5-7
Conference LocationSt. Louis, Missouri
PublisherSociety of Allied Weight Engineers, Inc.
Date Published6/5/00
Abstract

Two major components of the rear fuselage of the F-22 Raptor fighter, the forward and aft boom assemblies, were designed and fabricated as monolithic weldments in order to achieve a significant weight savings. This was a challenging task, as these components are fracture/durability critical, load bearing structures that attach the wings and vertical stabilizers to the fuselage and support the horizontal stabilizers. They also form part of the engine bay compartment, have aerodynamic surfaces/contours, and provide internal fuel storage. These highly efficient structures are made from over 90 separate pieces of 6Al-4V titanium alloy. Over 3,600 inches of full penetration electron beam welding are required to fabricate the four assemblies for each ship set.

Pages21
Key Words27. Weight Reduction - Materials
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