Skip to main content
Log in

Work of fracture in aluminum metal-matrix composites

  • Published:
Metallurgical Transactions A Aims and scope Submit manuscript

Abstract

The effect of isothermal exposure and thermal cycling on the toughness of B/Al (1100), B/Al (6061), and A12O3/A1 composites has been investigated. In B/Al (1100), isothermal exposure at 773 K for 45 × 104 s (125 hours) reduced toughness, measured by the work of fracture, from 76 kJm-2 to 10 kJm-2, and a similar reduction occurred after equivalent thermal cycling. The corresponding reduction in toughness after isothermal exposure in B/Al (6061) was from 44.5 kJm-2 to 8 kJm-2; however, the effect of thermal cycling was less detrimental. In the FP-A12O3/A1 composite, the work of fracture was insensitive to both forms of thermal treatment. Changes in the toughness of the B/Al composites have been correlated with and analyzed in terms of modifications to matrix, fiber, and interface properties, in particular, matrix softening, interface reaction products, and fiber notch sensitivity.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Similar content being viewed by others

References

  1. J. F. Haskins and J. R. Kerr: “Time-Temperature-Stress Capabilities of Composite Materials for Supersonic Cruise Aircraft Applications”, 1977, NASA Technical Report #N-77-18035.

  2. M. A. Wright:Metall. Trans. A, 1975, vol. 6A, p. 129.

    Google Scholar 

  3. H.H. Grimes, R. A. Lad, and J. E. Maisel:Metall. Trans. A, 1977, vol. 8A, p. 1999.

    CAS  Google Scholar 

  4. M. K. White and M. A. Wright: “Investigations into the Mechanics of Thermal Cycling Damage in Metal Matrix Composites”, University of Tennessee Space Institute, December 1976, ONR Technical Report, Contract #N00014-75-C-0352.

  5. W.H. Kim, M. J. Koczak, and A. Lawley:ICCM/2, Proceedings of the 1978 International Conference on Composite Materials, B. Noton, R. Signorelli, K. Street, and L. Phillips, eds., The Metallurgical Society of AIME, New York, NY, 1978, p. 487.

    Google Scholar 

  6. H.E. Tattersall and G. Tappin:J. Mat. Sci., 1966, vol. 1, p. 296.

    Article  Google Scholar 

  7. J. E. Hack and G.C. Strempek: “Fabrication of Aluminum Oxide Fiber-Reinforced Aluminum Matrix Composites,” NASA Report #CR-165184 (Contract NAS3-21013), Fiber Materials, Inc., Biddeford, ME, November 1980.

    Google Scholar 

  8. G. Thomas:J. Inst. Metals, 1961-62, vol. 90, p. 57.

    CAS  Google Scholar 

  9. G. S. Doble, “Fabrication Process Development of Boron/Aluminum Fan Blades for High Bypass Engines,” NASA #CR-165252, TRW, Inc., Cleveland, OH, February 1981.

    Google Scholar 

  10. F. Galasso, M. Salkind, D. Kuehl, and V. Patarni:Trans. TMS-AIME, 1966, vol. 236, p. 1747.

    Google Scholar 

  11. M. Basche, R. Fanti, and F. Galasso:Fiber Science and Technology, 1968, vol. 1, p. 19.

    Article  CAS  Google Scholar 

  12. G.A. Cooper and A. Kelly:J. Mech. Phys. Solids, 1967, vol. 15, p. 279.

    Article  CAS  Google Scholar 

  13. L.E. Dardi and K.G. Kreider:Failure Modes in Composites I, I. Toth, ed., TMS-AIME, New York, NY, 1973, p. 231.

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Additional information

The latter currently on

The latter currently on

Rights and permissions

Reprints and permissions

About this article

Cite this article

Skinner, A., Koczak, M.J. & Lawley, A. Work of fracture in aluminum metal-matrix composites. Metall Trans A 13, 289–297 (1982). https://doi.org/10.1007/BF02643319

Download citation

  • Received:

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF02643319

Keywords

Navigation