4.7 Article

Effects of cryogenic temperature and grain size on fatigue-crack propagation in the medium-entropy CrCoNi alloy

Journal

ACTA MATERIALIA
Volume 200, Issue -, Pages 351-365

Publisher

PERGAMON-ELSEVIER SCIENCE LTD
DOI: 10.1016/j.actamat.2020.09.021

Keywords

Medium-entropy alloy; Fatigue-crack propagation; Crack closure; Cryogenic temperatures; Grain size effects

Funding

  1. U.S. Department of Energy, Office of Science, Office of Basic Energy Sciences, Materials Sciences and Engineering Division [DE-ACO2-05CH11231, KC13]
  2. U.S. Department of Energy, Office of Science, Basic Energy Sciences, Materials Sciences and Engineering Division at the Oak Ridge National Laboratory
  3. Office of Science, Office of Basic Energy Sciences, of the U.S. Department of Energy [DE-ACO2-05-CH11231]
  4. German Research Foundation (DFG) [LA 3607/1-1]

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CrCoNi-based high-entropy alloys have demonstrated outstanding mechanical properties, particularly at cryogenic temperatures. Here we investigate the fatigue-crack propagation properties of the equiatomic, single-phase, face -centered cubic, medium-entropy alloy (MEA), CrCoNi, that displays exceptional strength, ductility and toughness, all of which are enhanced at cryogenic temperatures. Fatigue-crack growth is examined, at a load ratio of 0.1 over a wide range of growth rates, from similar to 10(-11) to >10(-7) m/cycle, at room (293 K) and cryogenic (198 K, 77 K) temperatures for two grain sizes (similar to 7 and 68 mu m), with emphasis on near-threshold behavior. We find that the Delta K-th fatigue thresholds are increased with decreasing temperature and increasing grain size: from 5.7 MPa root m at 293 K to 8 MPa root m at 77 K in the fine-grained alloy, and from 9.4 MPa root m at 293 K to 13.7 MPa root m at 77 K in the coarse grained alloy. Mechanistically, transgranular cracking at 293 K transitions to a mixture of intergranular and transgranular at cryogenic temperatures, where the increased propensity of nano-twins appears to inhibit growth rates by deflecting the crack path. However, the main factor affecting near-threshold behavior is roughness-induced crack closure from interference between the crack flanks, which is enhanced by the rougher fracture surfaces at low temperatures, particularly in the coarser-grained microstructure. Fatigue-crack propagation behavior in CrCoNi is comparable to nickel-based superalloys but is superior to that of the high-entropy CrMnFeCoNi (Cantor) alloy and many high-strength steels, making the CrCoNi alloy an excellent candidate material for safety-critical applications, particularly involving low temperatures. Published by Elsevier Ltd on behalf of Acta Materialia Inc.

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