CORDIS Project
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This project focuses on optimizing the lower fuselage structure of an aircraft to reduce weight while ensuring it can withstand structural loads. It explores three manufacturing technologies, including traditional riveting and advanced welding techniques, to achieve a lightweight design using aluminum alloys.
This proposal is for the structural analysis and design optimization of the lower fuselage of an aircraft.
The objective of the structural optimization is minimum weight and the design constraints fall into two categories; firstly the capability to withstand structural loads with sufficient margins, and secondly constraints relating to the manufacturing methods.
The structure to be optimized is a thin-walled metallic structure with stiffening elements (stringers and frames) using three options f…
ATG EUROPE BV
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