NASA/TP-3581, Verderaime, V. and Vaughan, R., Aluminum U-Groove Weld Enhancement Based on Experimental Stress Analyses, Structures and Dynamics Laboratory, Science and Engineering Directorate. NASA Marshall Space Flight Center, AL 35812, August 1995, pp. 40, Format(s): PDF 453k |
Though butt-welds are among the most preferred joining methods in aerostructures because of their sealing and assembly integrity and general elastic performance; their inelastic mechanics are 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 tab thickness between the grooves produce severe peaking, which induces bending moment under uniaxial loading. The filler strain hardening decreased with increasing filler pass sequence. These combined effects reduce the weld strength, and a depeaking index model was developed to select filler
pass thicknesses, pass numbers, and sequences to improve the welding process results over the current normal weld schedule.
| Keywords: | weld improvement, weld peaking stress, weld peaking reduction, weld pass properties, u-groove weld analysis, thick weld stresses butt-weld peaking, weld inelastic analysis, weld test strain analysis, weld induced bending |
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| CASI Document ID Number: | 96N10864 |
| Subjects: | Astronautics: Launch Vehicles And Launch Operations: Launch Vehicles |
| ID Code: | 307 |
| Deposited On: | 27 June 2002 |