A Methodology for Topology and Lattice Structure Optimization of a Cargo Drone Motor Mount

Author

Nagadurga Srinivas Sripada

Graduation Semester and Year

2017

Language

English

Document Type

Thesis

Degree Name

Master of Science in Mechanical Engineering

Department

Mechanical and Aerospace Engineering

First Advisor

Robert M Taylor

Abstract

This work discusses a CAE driven methodology for designing a lightweight component by performing structural configuration on a given package space, creating a closed surface along this configuration using an interactive geometric modeling tool, and lastly generating lattice members that provide the required stiffness for the structure. The design process is explained starting with topology optimization performed on a single block with specific design constraints. It describes the effect of different parameters on the optimized results and how to analyze these results based on a given volume fraction constraint with the objective of minimizing the compliance. It then talks about why and how a free-form geometry is created using the interactive NURBS surfaces instead of directly using the topology optimized result. Lastly the effect of lattice member size on the total mass and stiffness of the component are studied. The results show that change in lattice cell type and size can cause the mass of the component to increase while the stiffness is reduced considerably.

Keywords

Topology, Lattice, Optimization

Disciplines

Aerospace Engineering | Engineering | Mechanical Engineering

License

This work is licensed under a Creative Commons Attribution-NonCommercial-Share Alike 4.0 International License.

Comments

Degree granted by The University of Texas at Arlington

Recommended Citation

Sripada, Nagadurga Srinivas, "A Methodology for Topology and Lattice Structure Optimization of a Cargo Drone Motor Mount" (2017). Mechanical and Aerospace Engineering Theses. 728.
https://mavmatrix.uta.edu/mechaerospace_theses/728