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Solution to the problem of the poor cyclic fatigue resistance of bulk metallic glasses

Launey, Maximilien E. and Hofmann, Douglas C. and Johnson, William L. and Ritchie, Robert O. (2009) Solution to the problem of the poor cyclic fatigue resistance of bulk metallic glasses. Proceedings of the National Academy of Sciences of the United States of America, 106 (13). pp. 4986-4991. ISSN 0027-8424. PMCID PMC2663983. https://resolver.caltech.edu/CaltechAUTHORS:20090603-090319582

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Abstract

The recent development of metallic glass-matrix composites represents a particular milestone in engineering materials for structural applications owing to their remarkable combination of strength and toughness. However, metallic glasses are highly susceptible to cyclic fatigue damage, and previous attempts to solve this problem have been largely disappointing. Here, we propose and demonstrate a microstructural design strategy to overcome this limitation by matching the microstructural length scales (of the second phase) to mechanical crack-length scales. Specifically, semisolid processing is used to optimize the volume fraction, morphology, and size of second-phase dendrites to confine any initial deformation (shear banding) to the glassy regions separating dendrite arms having length scales of ≈2 μm, i.e., to less than the critical crack size for failure. Confinement of the damage to such interdendritic regions results in enhancement of fatigue lifetimes and increases the fatigue limit by an order of magnitude, making these “designed” composites as resistant to fatigue damage as high-strength steels and aluminum alloys. These design strategies can be universally applied to any other metallic glass systems.


Item Type:Article
Related URLs:
URLURL TypeDescription
http://dx.doi.org/10.1073/pnas.0900740106DOIArticle
http://www.ncbi.nlm.nih.gov/pmc/articles/pmc2663983/PubMed CentralArticle
Additional Information:© 2009 by the National Academy of Sciences. Contributed by William L. Johnson, January 22, 2009 (sent for review December 12, 2008). Published online before print March 16, 2009. M.E.L. and R.O.R. acknowledge financial support from the Director, Office of Science, Office of Basic Energy Sciences, Division of Materials Sciences and Engineering, of the U.S. Department of Energy under Contract DE-AC02-05CH11231. D.C.H. acknowledges financial support from the Department of Defense through the National Defense Science and Engineering Graduate Fellowship program. D.C.H. and W.L.J acknowledge funding support through the Office of Naval Research. Author contributions: M.E.L., D.C.H., W.L.J., and R.O.R. designed research; M.E.L. and D.C.H. performed research; M.E.L., D.C.H, W.L.J., and R.O.R. analyzed data; and M.E.L., D.C.H., W.L.J., and R.O.R. wrote the paper. The authors declare no conflict of interest.
Funders:
Funding AgencyGrant Number
Department of Energy (DOE)DE-AC02-05CH11231
National Defense Science and Engineering Graduate (NDSEG) FellowshipUNSPECIFIED
Office of Naval Research (ONR)UNSPECIFIED
Subject Keywords:composites; damage confinement; endurance limit; semisolid processing
Issue or Number:13
PubMed Central ID:PMC2663983
Record Number:CaltechAUTHORS:20090603-090319582
Persistent URL:https://resolver.caltech.edu/CaltechAUTHORS:20090603-090319582
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:14355
Collection:CaltechAUTHORS
Deposited By: Tony Diaz
Deposited On:17 Aug 2009 18:56
Last Modified:03 Jun 2020 18:01

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