Electromagnetic-Thermal Integrated Design Optimization for Hypersonic Vehicle Short-Time Duty PM Brushless DC Motor

<table class="table-group" id="tab3"><tr><td><table class="table"><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr class="thead"><td class="align_left">Items</td><td class="align_center">MP1</td><td class="align_center">MP2</td><td class="align_center">MP3</td></tr><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr><td class="align_left">Analytical (°C)</td><td class="align_center">21.4</td><td class="align_center">42.0</td><td class="align_center">61.9</td></tr><tr><td class="align_left">FEA (°C)</td><td class="align_center">20.4</td><td class="align_center">40.1</td><td class="align_center">59.0</td></tr><tr><td class="align_left">Measured (°C)</td><td class="align_center">22.7</td><td class="align_center">40.8</td><td class="align_center">57.4</td></tr><tr class="table-tr"><td colspan="4"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

The analytical, FEA, and measured winding temperature rise of MP1, MP2, and MP3.

International Journal of Aerospace Engineering

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Table 3

Table 3: Electromagnetic-Thermal Integrated Design Optimization for Hypersonic Vehicle Short-Time Duty PM Brushless DC Motor 