Research on Multistage Rotor Assembly Optimization Methods for Aeroengine Based on the Genetic Algorithm

<table class="table-group" id="tab2"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td class="align_left">Stage</td><td class="align_center">Mass (kg)</td><td class="align_center">Centroid coordinates (mm)</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td class="align_left">1</td><td class="align_center">17.2630</td><td class="align_center">(0.0036, 0, 35)</td></tr><tr><td class="align_left">2</td><td class="align_center">17.2630</td><td class="align_center">(0.0036, 0, 35)</td></tr><tr><td class="align_left">3</td><td class="align_center">17.2630</td><td class="align_center">(0.0036, 0, 35)</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>The mass parameters of the 3-stage rotor are measured by software.</div>

Complexity

tab2

Table 2

Table 2: Research on Multistage Rotor Assembly Optimization Methods for Aeroengine Based on the Genetic Algorithm 