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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. The extreme thermal expansion and contraction gradient of the fusion heat input across the groove tab thickness produces severe peaking, which induces bending under uniaxial loading. The filler strain-hardening decreased with increasing filler pass sequence, producing the weakest welds on the last pass side. Current welding schedules unknowingly compound these effects which reduce the weld strength. A depeaking index model was developed to select filler pass thicknesses, pass numbers, and sequences to improve depeaking in the welding process. The intent is to combine the strongest weld pass side with the peaking induced bending tension to provide a more uniform stress and stronger weld under axial tensile loading.
Document ID
19960028780
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
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
April 19, 1996
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-TM-111594
AIAA Paper 96-1576
NAS 1.15:111594
Report Number: NASA-TM-111594
Report Number: AIAA Paper 96-1576
Report Number: NAS 1.15:111594
Meeting Information
Meeting: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Location: Salt Lake City, UT
Country: United States
Start Date: April 18, 1996
End Date: April 19, 1996
Sponsors: American Helicopter Society, Inc., American Inst. of Aeronautics and Astronautics, American Society of Civil Engineers, American Society of Mechanical Engineers, Alpha STAR Corp.
Accession Number
96N29440
Distribution Limits
Public
Copyright
Public Use Permitted.
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