Design of an Innovative Aviation integrated Electronic Equipment Rack

摘要

This design is an open-loop aviation electronic equipment rack based on ARINC600 for a aircraft under only air exhaust condition. Conduct tress and stiffness analysis via ANSYS calculating the maximum stress and the maximum distortion. Calculate the maximum power of electronic equipment suitable for this equipment suitable for this equipment rack through heat transfer theory and provide theory basis for electronic equipment layout on the overall aircraft.