METHOD, SYSTEM AND APPARATUS FOR AN EFFICIENT FLOOR PANEL MATERIAL FOR AIRCRAFT

摘要

According to an aspect of the present invention, a composite material based on honeycomb core structure made of Kevlar material which is sandwiched between stiffened aluminium panels is developed. A sample material is studied under various physical condition in relations to commonly used materials such as I section and HAT section. It is found that the honeycomb structure made with Kevlar material in between two aluminium sheets provided greater load bearing capacity while lowering the mass for an Aircraft construction.