NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
U-Groove Aluminum Weld Strength ImprovementThough butt-welds are among the most preferred joining methods in aerostructures, their strength dependence on inelastic mechanics is generally the least understood. This study investigated experimental strain distributions across a thick aluminum U-grooved weld and identified two weld process considerations for improving the multipass weld strength. One is the source of peaking in which the extreme thermal expansion and contraction gradient of the fusion heat input across the groove tab thickness produces severe angular distortion that induces bending under uniaxial loading. The other is the filler strain hardening decreasing with increasing filler pass sequences, producing the weakest welds on the last weld pass side. Both phenomena are governed by weld pass sequences. Many industrial welding schedules unknowingly compound these effects, which reduce the weld strength. A depeaking index model was developed to select filler pass thickness, pass numbers, and sequences to improve depeaking in the welding process. The result was to select the number and sequence of weld passes to reverse the peaking angle such as to combine the strongest weld pass side with the peaking induced bending tension component side to provide a more uniform stress and stronger weld under axial tensile loading.
Document ID
19970022285
Acquisition Source
Marshall Space Flight Center
Document Type
Reprint (Version printed in journal)
Authors
Verderaime, V.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Vaughan, R.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1997
Publication Information
Publication: Journal of Spacecraft and Rockets
Publisher: American Institute of Aeronautics and Astronautics
Volume: 34
Issue: 1
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-CR-204659
NAS 1.26:204659
Report Number: NASA-CR-204659
Report Number: NAS 1.26:204659
Accession Number
97N22858
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available