An Optimization Method for the Main Influence Factors on the Performance of Aerostatic Spindle

<table class="table-group" id="tab1"><tr><td><table class="table"><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr class="thead"><td class="align_left" rowspan="2">Optimization values</td><td class="align_center" colspan="3">Optimization parameters</td></tr><tr class="thead"><td class="align_center"><i>h</i> (<i>μ</i>m)</td><td class="align_center"><i>d</i><sub>3</sub> (mm)</td><td class="align_center"><i>d</i><sub>2</sub> (mm)</td></tr><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr><td class="align_left"><i>W</i> <i>=</i> 1254.2 N</td><td class="align_center">8.301</td><td class="align_center">3.213</td><td class="align_center">82.531</td></tr><tr><td class="align_left"><i>K</i> <i>=</i> 135.4 N/<i>μ</i>m</td><td class="align_center">12.342</td><td class="align_center">2.912</td><td class="align_center">82.125</td></tr><tr class="table-tr"><td colspan="4"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Optimal results of single objective function.</div>

Shock and Vibration

tab1

Table 1

Table 1: An Optimization Method for the Main Influence Factors on the Performance of Aerostatic Spindle 