Engineering design of tough ceramic matrix composites for turbine components

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Abstract

This paper provides a review of the material design concepts for the toughening of ceramic matrix composites by three-dimensional fiber architecture. To establish a communication link between the structural and the materials engineers, an integrated design methodology is presented with an example. Through a Fabric Geometry Model (FGM), the contribution of three-dimensional fiber architecture is translated into a stiffness matrix for finite element structural analysis. With the feedback from the structural analysis, this design methodology provides an effective means to screen reinforcement materials systems for three-dimensional fabric-reinforced composite components. © 1991 ASME.

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Tan, T. M., Pastore, C. M., & Ko, F. K. (1991). Engineering design of tough ceramic matrix composites for turbine components. Journal of Engineering for Gas Turbines and Power, 113(2), 312–317. https://doi.org/10.1115/1.2906564

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