Abstract

This paper introduces a novel methodology for the optimisation of resonant frequencies in three-dimensional lattice structures. The method uses a multiscale approach in which the homogenised material properties of the lattice unit cell are defined by the spatially varying lattice parameters. Material properties derived from precomputed simulations of the small scale lattice are projected onto response surfaces, thereby describing the large-scale metamaterial properties as polynomial functions of the small-scale parameters. Resonant frequencies and mode shapes are obtained through the eigenvalue analysis of the large-scale finite element model which provides the basis for deriving the frequency sensitivities. Frequency tailoring is achieved by imposing constraints on the resonant frequency for a compliance minimisation optimisation. A sorting method based on the Modal Assurance Criterion allows for specific mode shapes to be optimised whilst simultaneously reducing the impact of localised modes on the optimisation. Three cases of frequency constraints are investigated and compared with an unconstrained optimisation to demonstrate the algorithms applicability. The results show that the optimisation is capable of handling strict frequency constraints and with the use of the modal tracking can even alter the original ordering of the resonant mode shapes. Frequency tailoring allows for improved functionality of compliance-minimised aerospace components by avoiding resonant frequencies and hence dynamic stresses.

Highlights

  • Lightweight structures that are able to mitigate or avoid dynamic loading are a key area of development within the aerospace industry

  • Previous research into the optimisation of resonant frequencies has resulted in several methods being adopted within the industry, such as topology optimisation based on the Solid Isotropic Material with Penalisation (SIMP) (Bendsøe 1989) and Bi-directional Evolutionary Structural Optimisation (BESO) methodologies (Huang et al 2009; Sivapuram and Picelli 2018)

  • A seven-dimensional lattice microstructure uses a database of precomputed simulations to predict homogenised material properties for use in the large-scale optimisation

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Summary

Introduction

Lightweight structures that are able to mitigate or avoid dynamic loading are a key area of development within the aerospace industry. Previous research into the optimisation of resonant frequencies has resulted in several methods being adopted within the industry, such as topology optimisation based on the Solid Isotropic Material with Penalisation (SIMP) (Bendsøe 1989) and Bi-directional Evolutionary Structural Optimisation (BESO) methodologies (Huang et al 2009; Sivapuram and Picelli 2018). A common issue associated with the SIMP approach when resonance is considered is the occurrence of localised modes corresponding to artificially low natural frequencies. These localised modes occur in regions of low-density material where the ratio between the penalised stiffness and the unpenalised mass is very small. The resulting designs may not be representative of a manufacturable structure and often still require heuristic post-processing, causing the resulting structures to be suboptimal (Xu et al 2019)

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