Research on the Design and Analysis Method of the Bird Collision-Resistant Structure of Electric Aircraft Composite Cap-Type-Reinforced Wall Panel-Filled Battery Integration

<table class="table-group" id="tab10"><tr><td><table class="table"><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr class="thead"><td class="align_left">Impact location</td><td class="align_center">Maximum displacement (mm)</td><td class="align_center">Maximum strain</td><td class="align_center">Minimum clearance (mm)</td></tr><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr><td class="align_left">A</td><td class="align_center">1.636</td><td class="align_center">0.0005256</td><td class="align_center">2.326</td></tr><tr><td class="align_left">B</td><td class="align_center">1.937</td><td class="align_center">0.0009682</td><td class="align_center">2.228</td></tr><tr><td class="align_left">C</td><td class="align_center">1.573</td><td class="align_center">0.0005474</td><td class="align_center">2.322</td></tr><tr class="table-tr"><td colspan="4"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Response of battery box under bird impact at different impact points.</div>

International Journal of Aerospace Engineering

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Table 10

Table 10: Research on the Design and Analysis Method of the Bird Collision-Resistant Structure of Electric Aircraft Composite Cap-Type-Reinforced Wall Panel-Filled Battery Integration 

Table 10 | Research on the Design and Analysis Method of the Bird Collision-Resistant Structure of Electric Aircraft Composite Cap-Type-Reinforced Wall Panel-Filled Battery Integration 