Computational Methodology for Optimal Design of Additive Layer Manufactured Turbine Bracket

H. U. Levatti, Mauro Sebastian Innocente, H. D. Morgan, J. Cherry, N. P. Lavery, S. Mehmood, I. Cameron, J. Sienz

Research output: Chapter in Book/Report/Conference proceedingConference proceeding

Abstract

The design of critical components for aircrafts, cars or any other kind of machinery today is typically subject to two conflicting objectives, namely the maximisation of strength and the minimisation of weight. The conflicting nature of these two objectives makes it impossible to obtain a design that is optimal for both. The most common approach aiming for a single objective optimisation problem in aerospace is to maintain the weight minimisation as the objective, whilst setting strength requirements as constraints to be satisfied. However, manufacturing methods incorporate additional restrictions for an optimal design to be considered feasible, even when satisfying all constraints in the formulation of the optimisation problem. In this context, Additive Layer Manufacturing adds remarkably higher flexibility to the manufacturability of shape designs when compared with traditional processes. It is fair to note, however, that there are still some restrictions such as the infeasibility of building unsupported layers forming angles smaller than 45 degrees with respect to the underlying one. Nowadays, it is common practice to use a set of software tools to deal with these kinds of problems, namely Computer Aided Design (CAD), Finite Element Analysis (FEA), and optimisation packages. The adequate use of these tools results in an increase in efficiency and quality of the final product. In this paper, a case study was undertaken consisting of a turbine bracket from a General Electric challenge (Figure 5). A computational methodology is used, which consists of a topology optimisation considering an isotropic material at first instance, followed by the manual refinement of the resulting shape taking into account the manufacturability requirements. To this end, we used SolidWorks®2013 for the CAD, Ansys Workbench®14.0 for the FEA, and HyperWorks®11 for the topology optimisation. A future methodology will incorporate the automation of the shape optimisation stage, and perhaps the inclusion of the manufacturability restriction within the optimisation formulation.
Original languageEnglish
Title of host publicationKES Transactions on Sustainable Design and Manufacturing
EditorsR. Setchi, R. J. Howlett, M. Naim, J. Sienz
Place of PublicationEngland, UK
PublisherFuture Technology Press
Pages641-652
Number of pages12
Volume1
ISBN (Print)978-0-9561516-5-0, 978-0-9561516-6-7, 978-0-9561516-4-3
Publication statusPublished - 2014
Externally publishedYes
EventInternational Conference on Sustainable Design and Manufacturing - Cardiff, United Kingdom
Duration: 28 Apr 201530 Apr 2015

Conference

ConferenceInternational Conference on Sustainable Design and Manufacturing
Abbreviated titleSDM'2014
CountryUnited Kingdom
CityCardiff
Period28/04/1530/04/15

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  • Research Output

    Computational Methodology for Optimal Design of Additive Layer Manufactured Turbine Bracket

    Levatti, H. U., Innocente, M., Morgan, H. D., Cherry, J., Lavery, N., Mehmood, S., Cameron, I. & Sienz, J., 1 May 2016, In : InImpact: The Journal of Innovation Impact. 7, 2, p. 641-652 12 p.

    Research output: Contribution to journalArticle

    Open Access
  • Cite this

    Levatti, H. U., Innocente, M. S., Morgan, H. D., Cherry, J., Lavery, N. P., Mehmood, S., ... Sienz, J. (2014). Computational Methodology for Optimal Design of Additive Layer Manufactured Turbine Bracket. In R. Setchi, R. J. Howlett, M. Naim, & J. Sienz (Eds.), KES Transactions on Sustainable Design and Manufacturing (Vol. 1, pp. 641-652). [sdm14-037] England, UK: Future Technology Press.