Stiffness and strength tailoring of a hip prosthesis made of advanced composite materials.
This work is concerned with the design of hip prostheses using advanced fiber reinforced composite materials. The major focus of the study is to evaluate how the stiffness and strength of composite hip prostheses can be affected by variations in ply orientation and stacking sequence for a selected manufacturing method. This investigation involved both analytical and experimental work. An analytical model was developed which consists of a stress analysis and a failure analysis. A finite element program was developed during the course of the investigation for analyzing stresses, strains, and deformations of composite stems with a simplified configuration. Failure and mode of failure were predicted by appropriately selected failure criteria. Experiments were also performed on T300/976 graphite/epoxy composites to verify the analysis and the computer calculations. Both testing and analysis accounted for the various combinations of in-plane and out-of-plane (torsion) loading that can act on the prosthetic hip. Simplified composite stems with a 120 layer thickness were fabricated and tested. An excellent agreement was found between the measured strain data and the numerical calculations. Using the program, parametric studies were performed. It was found that an optimal design of hip stems can be achieved by using advanced fiber-reinforced composite materials, but great care must be taken when selecting the appropriate ply orientation and stacking sequence for a chosen fabrication method.
Department of Aeronautics and Astronautics, Stanford University, California 94305.
F K
FK
Chang
J L
JL
Perez
J A
JA
Davidson
D001672:Biocompatible Materials / Q000138:chemical synthesis*; D003188:Composite Resins / Q000138:chemical synthesis*; D004548:Elasticity; D004853:Epoxy Resins; D006108:Graphite; D006622:Hip Prosthesis; D006801:Humans; D008422:Materials Testing; D008954:Models, Biological; D011474:Prosthesis Design; D011475:Prosthesis Failure; D013314:Stress, Mechanical
D001672:Biocompatible Materials; D003188:Composite Resins; D004853:Epoxy Resins; D006108:Graphite