Toward the integration of lattice structure-based topology optimization and additive manufacturing for the design of turbomachinery components

Used in several industrial fields to create innovative designs, topology optimization is a method to design a structure characterized by maximum stiffness properties and reduced weights. By integrating topology optimization with additive layer manufacturing and, at the same time, by using innovative...

Full description

Saved in:
Bibliographic Details
Published inAdvances in mechanical engineering Vol. 11; no. 8
Main Authors Boccini, Enrico, Furferi, Rocco, Governi, Lapo, Meli, Enrico, Ridolfi, Alessandro, Rindi, Andrea, Volpe, Yary
Format Journal Article
LanguageEnglish
Published London, England SAGE Publications 01.08.2019
Sage Publications Ltd
SAGE Publishing
Subjects
Online AccessGet full text

Cover

Loading…
More Information
Summary:Used in several industrial fields to create innovative designs, topology optimization is a method to design a structure characterized by maximum stiffness properties and reduced weights. By integrating topology optimization with additive layer manufacturing and, at the same time, by using innovative materials such as lattice structures, it is possible to realize complex three-dimensional geometries unthinkable using traditional subtractive techniques. Surprisingly, the extraordinary potential of topology optimization method (especially when coupled with additive manufacturing and lattice structures) has not yet been extensively developed to study rotating machines. Based on the above considerations, the applicability of topology optimization, additive manufacturing, and lattice structures to the fields of turbomachinery and rotordynamics is here explored. Such techniques are applied to a turbine disk to optimize its performance in terms of resonance and mass reduction. The obtained results are quite encouraging since this approach allows improving existing turbomachinery components’ performance when compared with traditional one.
ISSN:1687-8132
1687-8140
DOI:10.1177/1687814019859789