Transient Response of a Simulated Aeroengine with a Fusing Structure during a Fan-Blade Out Event

<table class="table-group" id="tab2"><tr><td><table class="table"><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr class="thead"><td class="align_left">Shaft number</td><td class="align_center">Length (mm)</td><td class="align_center">Internal diameter (mm)</td><td class="align_center">External diameter (mm)</td></tr><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr><td class="align_left">L4</td><td class="align_center">200</td><td class="align_center">70</td><td class="align_center">80</td></tr><tr><td class="align_left">L5</td><td class="align_center">600</td><td class="align_center">70</td><td class="align_center">80</td></tr><tr><td class="align_left">L6</td><td class="align_center">100</td><td class="align_center">70</td><td class="align_center">80</td></tr><tr class="table-tr"><td colspan="4"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Dimensions of shafts in the high-pressure rotor.</div>

International Journal of Aerospace Engineering

tab2

Table 2

Table 2: Transient Response of a Simulated Aeroengine with a Fusing Structure during a Fan-Blade Out Event 