D.H. Lammlein PhD Dissertation - Vanderbilt University

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Figure 100: Macrosection view of the split protrusion type defect experienced in cupped shoulder (Ø 5/8”), threaded probe (Ø 0.20”) tool weld made without a backing ring anvil at 50% material penetration in a butt weld configuration. It was concluded that the large, flat surface of the probe bottom contributed most significantly to this weld material distortion and an alternative probe geometry had to be selected for successful welding without an internal ring-anvil. It was found that a tool consisting of only a simple 100º conical probe (no shoulder) redirected weld forces in such a way as to eliminate the protrusion or splitting defect on the backside of the material at penetration depths approaching 60% of the material thickness in both bead on plate and butted weld configurations. Additionally, a conical tool geometry with a small diameter (0.025”) snub nose was desired for use in a taper retraction or tapered extraction type weld disengagement procedure. It was found that a 0.015” diameter hemispherical cup cut into the snub of the tool relieved influences on the weld material root to an extent which allowed a 50% (0.10”) penetration weld in a butted configuration without the assistance of an inner anvil ring. No protrusion or splitting was experienced at this depth and with this tooling within the parameter range tested. Figure 101 shows the typical appearance of a sample welded with this tool geometry. It was found that without a cupped recess in the snubbed nose of the tool that deformation occurred at the base of the joint in the weld material at some parameters. The conventional probe tool was not tested 114
with a cupped recess. It is however the belief of the authors that a cupped recess in the probe bottom of the conventional probe tool would allow for unsupported welding without deformation at the material base at some shallow penetration depth, possibly 15% of the material thickness. Figure 101: Surface appearance for a butt configuration weld made with a 100º conical tool (Ø 0.025” snub-nose and Ø 0.015” cupped nose recess). No backing ring anvil was used. Subsequently, the applicability of various tool extraction procedures was tested using the cone-snub-cup tool, initially in a bead on plate weld configuration. The goal was disengagement from the weld material without a serious defect. The procedure involved a steady state weld period at the desired weld depth followed by a gradual decrease in the tool depth via a computer controlled vertical motor. In some cases the rotation rate (analogous to traverse rate) of the weld hemispheres was decreased to some lower but constant value when the retraction procedure was triggered. Additionally, the spindle speed is increased during the tapered retraction, in some instances at multiple instants during the retraction (e.g. from 900 rpm to 2000rpm in 100rpm increments on some time interval). It was found the extraction could be performed rather cleanly and leaving essentially no indentation as shown in Figure 102. 115
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FRICTION STIR WELDING OF SPHERES, C
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TABLE OF CONTENTS TABLE OF FIGURES
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Appendix ..........................
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Figure 16: Left(FE streamline), Mid
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Figure 51: A thermal camera image t
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for a similar conventional weld (3/
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Figure 102: Tapered retraction proc
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setting are indicated. Note that st
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Unsupported welds of this kind with
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Figure 157: A thermal camera image
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ottom sample is a tungsten inert ga
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N - newton (force unit) n - visco-p
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INTRODUCTION Friction Stir Welding,
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educed conduction lengths. In small
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CHAPTER I LITERATURE REVIEW: COMPUT
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frictional condition at the interfa
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contact. The contact area can inclu
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For horizontal sections, a heat inp
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(1.11) where r p is the probe (pin)
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This efficiency term, η pd , is kn
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The heat input on the tool surface
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The added complication of these met
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Figure 5: Lateral cross sections of
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Flow stress in aluminum alloys is d
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Figure 8: Three flow fields a) rota
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and post-weld cool-down. This model
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Williams et al. [60] use a 2D-axisy
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Figure 16: Left(FE streamline), Mid
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Figure 18: Temperature contour over
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Figure 22: Temperature distribution
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Figure 24: Lateral velocity contour
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Figure 26: Experimental(white) vers
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Figure 28: Top view schematic of tu
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[5] Taylor RE, Groot H, Goerz T, Fe
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[41] Heinz B., Skrotzki B., Eggler
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CHAPTER II COMPUTATIONAL ANALYSIS O
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Figure 30: Blind t-joint setup with
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Figure 33: Process forces and later
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Figure 35: Experimental Welds, Axia
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Figure 37: FEA boundary conditions
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A 4500 N axial force is applied eve
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axial force with lateral offset dur
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Figure 42: Contour plot of von Mise
Page 87 and 88: Figure 44: Deformation contour for
Page 89 and 90: Figure 46: Quarter-plate model for
Page 91 and 92: Figure 49: Contour plot of deflecti
Page 93 and 94: where P is the weld power (W), Q is
Page 95 and 96: Figure 52: Fluent CFD model zones.
Page 97 and 98: Figure 55: Thermal contour of weld
Page 99 and 100: Figure 59: Thermal contour of weld
Page 101 and 102: Figure 61: Velocity vectors for 0.0
Page 103 and 104: Figure 65: Contour of velocity magn
Page 105 and 106: CHAPTER III THE APPLICATION OF SHOU
Page 107 and 108: Figure 66: A shoulder-less, conical
Page 109 and 110: Figure 68: Typical axial(Z-axis) fo
Page 111 and 112: Figure 71: 90° conical tool macros
Page 113 and 114: Figure 75: Run 3, 80° conical tool
Page 115 and 116: Figure 79: (90º tool) Ultimate ten
Page 117 and 118: Figure 83: (90º tool) Lateral forc
Page 119 and 120: Figure 87: (80º tool) Lateral forc
Page 121 and 122: The Eulerian, finite volume, CFD so
Page 123 and 124: Figure 92 shows the increasing elem
Page 125 and 126: Figure 91: CFD model geometry consi
Page 127 and 128: Figure 95: Lateral cross-section of
Page 129 and 130: Figure 96: Attempts a probe tapered
Page 131 and 132: CHAPTER IV THE FRICTION STIR WELDIN
Page 133 and 134: applications for its high strength
Page 135 and 136: Figure 97: Experimental weld sample
Page 137: Figure 99: Split protrusion type de
Page 141 and 142: of tapered retraction (i.e. move th
Page 143 and 144: The adjustments in vertical positio
Page 145 and 146: manners the assigned depth was main
Page 147 and 148: Figure 108: Lateral macrosections f
Page 149 and 150: Figure 110: (Supported, cupped tool
Page 155 and 156: apparent strength of 26% parent whi
Page 157 and 158: with a 100º conical tool (0.025”
Page 159 and 160: Figure 119: Macrosection view of an
Page 161 and 162: and tooling. Torque is highly depen
Page 163 and 164: locally in proportion to the local
Page 165 and 166: Figure 126: (threaded tool) Contour
Page 167 and 168: Figure 128: (conical tool) Geometry
Page 169 and 170: Figure 131: (threaded tool) Lateral
Page 171 and 172: The results presented here show tha
Page 173 and 174: Figure 136:(from left: Tapered retr
Page 175 and 176: [8] Metallurgical analysis of ablat
Page 177 and 178: CHAPTER V FRICTION STIR WELDING OF
Page 179 and 180: Collaboration between Advanced Meta
Page 181 and 182: eccentricity, the method of interio
Page 183 and 184: gas tungsten arc welding of small d
Page 185 and 186: Full penetration welds of 4.2” (1
Page 187 and 188: Figure 143: The curvature of the pi
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Figure 144: Experimental axial forc
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Together, a fine wall thickness tol
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Figure 147: Axial force history for
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The weld macrosections show complet
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Figure 154: Macrosections of welds
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Figure 157: A thermal camera image
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Figure 159: Average tool shank temp
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471,146 faces. The meshes are fine
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Figure 162: A closeup view of mesh
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4 2 3 4 5 16 " 1.745 2 0.24
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applied heat locally in proportion
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Figure 164: Modeled temperature con
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Figure 172: Model pathlines for the
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Figure 174: Model pathlines for the
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later speed setting, the tool welds
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Figure 178: Zoom view of a macro ta
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Figure 180: The superficial appeara
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Figure 182: The rotary welding appa
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Figure 185: A diagram illustrating
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CONCLUSION AND FUTURE WORK Conclusi
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new FSW process environment is reso
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D.H. Lammlein PhD Dissertation - Vanderbilt University

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