Enhancing Cutting Efficiency and Minimizing Forces for Nomex Honeycomb Core Using Grey Relational Analysis and Desirability Function Analysis

Author:

Habib Hassan1,Khan Muhammad Salman1,Munir Adnan1,Zahid Danyal1,McDermott Olivia2ORCID

Affiliation:

1. School of Mechanical and Manufacturing Engineering (SMME) National University of Sciences and Technology (NUST) H‐12 Islamabad 24090 Pakistan

2. College of Science & Engineering University of Galway Galway H91TK33 Ireland

Abstract

AbstractNomex Honeycomb core is the foundational building block for manufacturing aerospace composite components. Its usage requires machining honeycomb in complex aerodynamic profiles where the quality of the core is governed by accuracy and precision of cut profiles. The assessment of accuracy and precision is directly related to forces induced in the cutting tool and cutting efficiency. These two parameters form the basis of a multi‐objective function that this paper aims to optimize for the milling operation. The parameter of depth of cut considered in this paper has not been analyzed in a multi‐objective optimization study of the Nomex Honeycomb core previously. A Taguchi‐based array of Design of Experiments followed by Analysis of Variance and correlation analysis is utilised. The results indicate that the most significant factor is the feed rate, with a percentage contribution of 72% for the cutting forces and depth of cut, with a percentage contribution of 85% in the case of cutting efficiency. The two parameters are optimized using Desirability Function Analysis and Grey Relational Analysis. The results are validated through experimental runs with an error within 5% of the statistical predictions, with the percentage improvement in cutting forces for optimum runs as compared to the worst experimental run at 47.8%. The percentage improvement in cutting efficiency likewise is 11%.

Publisher

Wiley

Subject

General Materials Science,General Chemistry

Reference32 articles.

1. Aerospace Engineering and Operations Technician Bureau of Labor Statistics U.S. Department of Labor “Honeycomb Structures. ” can be found underwww.bls.gov/ooh/architecture‐and‐engineering/aerospace‐engineering‐and‐operations‐technicians.htm#tab‐2. (accessed: November 2023).

2. High velocity impact responses of sandwich panels with metal fibre laminate skins and aluminium foam core

3. Virtual testing of sandwich core structures using dynamic finite element simulations

4. Hexcel at CAMX 2015

5. A 3D FE Modeling of Machining Process of Nomex® Honeycomb Core: Influence of the Cell Structure Behaviour and Specific Tool Geometry

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