Finite element analysis of engine pistons: comparative assessment of aluminium and titanium alloys under combined thermal-structural loading.

Abstract

Finite Element Analysis (ANSYS 19.2) was used to compare four piston materials - Aluminium 7075, Aluminium 2618, Aluminium 4032 and Titanium Ti-6Al-4 V - under combined mechanical and thermal loading. The study reports steady-state thermal and static structural snapshots for comparison. Under the present steady-state setup (uniform crown temperature and static crown pressure), Aluminium 2618 exhibited the lowest total deformation (0.476 mm) compared with Aluminium 7075 (0.951 mm) and Ti-6Al-4 V (0.833 mm), representing ~ 50.0% and ~ 42.9% reductions in deformation, respectively. Al-2618 also showed the lowest maximum heat flux in these steady runs (≈ 2.059 × 10⁻¹² W·mm⁻²) compared to Ti-6Al-4 V (≈ 5.148 × 10⁻¹² W·mm⁻²), and the highest minimum safety factor (6.732), which is ~ 123.7% greater than that of Al-4032 (3.010). These steady-state results suggest Al-2618 offers a favorable combination of dimensional stability and mechanical resilience for the modeled conditions; however, we highlight limitations of steady-state, static loading and recommend transient, cycle-based analyses prior to final material selection.