Compatibility Considerations for Metal-Matrix Composites

670822

02/01/1967

Authors
Abstract
Content
Research on metal-matrix composites for turbine compressors has demonstrated that four areas of compatibility are very important in composite design, and all must be considered in detail when specifying metal-matrix composites for structural applications. These areas comprise: chemical compatibility between matrix and filament, elastic strain compatibility, physical property compatibility, and manufacturing process compatibility. The designer must have detailed knowledge of every step in the composite manufacturing process to predict structural performance. Control of the manufacturing process to achieve maximum reinforcement from the filaments is considered the most important single factor. Asymmetrical elastic properties introduced by residual stresses or area ratio variation appear to be the most difficult aspect to appraise. A result of such asymmetry is dimensional and structural instability in a changing temperature environment.
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DOI
https://doi.org/10.4271/670822
Pages
9
Citation
Compton, W., and Steward, K., "Compatibility Considerations for Metal-Matrix Composites," SAE Technical Paper 670822, 1967, https://doi.org/10.4271/670822.
Additional Details
Publisher
Published
Feb 1, 1967
Product Code
670822
Content Type
Technical Paper
Language
English