DFMA as Applied to the Swingline 747 Desktop ... - University of Utah
DFMA as Applied to the Swingline 747 Desktop ... - University of Utah
DFMA as Applied to the Swingline 747 Desktop ... - University of Utah
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Part 13: Top Staple Guide:<br />
The <strong>to</strong>p staple guide is made <strong>of</strong> aluminum alloy. No analysis carried out for <strong>the</strong><br />
<strong>to</strong>p staple guide.<br />
Part 14: The End Cap (<strong>747</strong>):<br />
The end cap is made <strong>of</strong> alloy steel.<br />
Analysis Run for Strongest Beam Max Performance, Their Respective Index<br />
Values:<br />
Gray c<strong>as</strong>t iron 21<br />
Ductile iron 43<br />
Malleable iron 30<br />
Mild steel 16<br />
Alloy steel 100<br />
Stainless steel 13<br />
Aluminum alloy 0<br />
Beryllium copper 88<br />
Copper, hard 24<br />
Analysis Run for Strongest Beam and Minimum Weight, Their Respective Index<br />
Values:<br />
Gray c<strong>as</strong>t iron 20<br />
Ductile iron 44<br />
Malleable iron 26<br />
Mild steel 7<br />
Alloy steel 93<br />
Stainless steel 0<br />
Aluminum alloy 100<br />
Beryllium copper 76<br />
Copper, hard 0<br />
45
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