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Optimisation of hybrid high-modulus/high-strength carbon fibre reinforced plastic composite drive shafts
Affiliation:1. Écoles d’Officiers de l’Armée de l’air (EOAA), Centre de Recherche de l’Armée de l’air (CReA), BA 701, 13361 Salon Air, France;2. Laboratoire de Mécanique et d’Acoustique (LMA), 31 chemin Joseph Aiguier, 13402 Marseille Cedex 20, France;1. Aix Marseille Univ, CNRS, Centrale Marseille, LMA, Marseille, France;2. Centre de Recherche de l’Armée de l’Air, École de l’air, B.A. 701, 13661 Salon-Air, France;1. Faculty of Engineering, University of Porto, Portugal;2. Laboratory of Mechanics, Modeling and Production, LA2MP, National Engineering School of Sfax, University of Sfax, Tunisia;1. School of Integrated Design Engineering, Keio University, 3-14-1 Hiyoshi, Kohoku-ku, Yokohama 223-8522, Japan;2. Department of Micro Engineering, Graduate School of Engineering, Kyoto University, C3 Kyotodaigaku Katsura, Nisikyo-ku, Kyoto 615-8540, Japan;1. School of Mechanical and Electronic Engineering, Wuhan University of Technology, Wuhan 430070, China;2. Wuhan Heavy Duty Machine Tool Group Corporation, Wuhan 430070, China;1. Department of Mechanical Engineering, Rajalakshmi Institute of Technology, Kuthambakkam, Chennai 600124, India;2. Department of Mechanical Engineering, Koneru Lakshimahia Education Foundation, Green Fields, Vaddesswaram, Andra Pradesh 522502, India
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.
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