OTIMIZAÇÃO TOPOLÓGICA DE UMA AERONAVE UTILIZANDO O SOFTWARE AUTODESK INVENTOR

Resumo

This work intends to perform the topological optimization of the Cessna 172 Skyhawk
aircraft, with the objective of reduce its mass, using the software Autodesk Inventor. Given a choice
among several options, the optimization is related to the choice that is the best possible, considering
criteria and limitations, such as available resources and design requirements, which directly impact
the analysis, manufacturing, sales research and development of the design of an aeronautical product
(Silva and Brazil, 2017) [1.] After structural and performance studies, each part of the chosen aircraft
will be modelled in the Autodesk Inventor software. Boundary conditions and loading applications will
be carried out, simulating different flight assumptions, in order to make optimization consistent with
the reality; afterwards, the topological optimization will be carried out in this software, followed by
analysis.