Optimisation of hybrid high-modulus/high-strength carbon fiber reinforced plastic composite drive

TL;DR

This paper presents an optimization method for hybrid high-modulus/high-strength carbon fiber composite drive shafts using genetic algorithms, improving weight and efficiency in helicopter driveline applications.

Contribution

It introduces a comprehensive analytical framework for designing optimized composite drive shafts, including stability and torsional strength criteria, without relying solely on numerical optimization.

Findings

Significant reduction in shaft weight and number of components.

Effective use of hybrid composite materials for high-performance shafts.

Development of general design rules for composite shafts.

Abstract

This study deals with the optimisation of hybrid composite drive shafts operating at subcritical or supercritical speeds, using a genetic algorithm. A formulation for the flexural vibrations of a composite drive shaft mounted on viscoelastic supports including shear effects is developed. In particular, an analytic stability criterion is developed to ensure the integrity of the system in the supercritical regime. Then it is shown that the torsional strength can be computed with the maximum stress criterion. A shell method is developed for computing drive shaft torsional buckling. The optimisation of a helicopter tail rotor driveline is then performed. In particular, original hybrid shafts consisting of high-modulus and high-strength carbon fibre reinforced epoxy plies were studied. The solutions obtained using the method presented here made it possible to greatly decrease the number of shafts and the weight of the driveline under subcritical conditions, and even more under supercritical conditions. This study yielded some general rules for designing an optimum composite shaft without any need for optimisation algorithms.