4.7 Article

Optimized low-cycle fatigue behavior and fracture characteristics of Ti-6Al-4V alloy by Fe microalloying

Journal

JOURNAL OF MATERIALS RESEARCH AND TECHNOLOGY-JMR&T
Volume 15, Issue -, Pages 5277-5287

Publisher

ELSEVIER
DOI: 10.1016/j.jmrt.2021.11.010

Keywords

Titanium alloy; Fe microalloying; Low cycle fatigue; Fractography

Funding

  1. China Scholarship Council [201908320407]
  2. National Natural Science Foundation of China [51931008]
  3. Russian Science Foundation [20-63-47027]
  4. Ministry of Education of the Russian Federation [0838-2020-0006]
  5. State Key Laboratory Open Source for Metal Materials and Applications for Marine Equipment [SKLMEA-K201807]
  6. Primary Research & Developement Plan of Jiangsu Province [BE2019119]
  7. Priority Academic Program Development of Jiangsu Higher Education Institutions
  8. Russian Science Foundation [20-63-47027] Funding Source: Russian Science Foundation

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This study systematically investigates the low cycle fatigue behavior and fracture characteristics of Ti-6Al-4V-0.55Fe alloy with bimodal microstructure. The alloy exhibits continuous softening behavior at both high and low strain amplitudes, with different crack initiation sites and fatigue striation characteristics observed at different strain amplitudes. The LCF life of Ti-6Al-4V-0.55Fe is similar to that of Ti-6Al-4V at high strain amplitudes and much higher at low strain amplitudes due to the extra resistance provided by Fe microalloying.
In the present work, low cycle fatigue (LCF) behavior and fracture characteristic of Ti-6Al-4V-0.55Fe alloy with bimodal microstructure, consisted of equiaxed primary alpha (alpha(p)), lamellar alpha (alpha(1)) and beta matrix, are systematically investigated at room temperature. Results indicate that Ti-6Al-4V-0.55Fe alloy mainly exhibits a continuous softening behavior both at high and low strain amplitudes, due to the interaction of back stress(sigma(b)) and friction stress(sigma(f)) mainly related to the plastic deformation heterogeneity and precipitates shearing, respectively. Compared with Ti-6Al-4V alloy, LCF life of Ti-6Al-4V-0.55Fe is similar at high strain amplitudes (Delta epsilon(t)/2 > 1.0%), while much higher at low strain amplitudes (Delta epsilon(t)/2 < 1.0%), which could be attributed to the extra resistance to dislocation movement and crack propagation produced by Fe microalloying. The fractography shows remarkably different characteristics for these imposed strain amplitudes. At low strain amplitude, there is only one crack initiation site caused by dislocations pile-ups and stress concentration on the specimen surface, accompanied with narrower fatigue striation, while more cracks initiated on the surface with wider fatigue striation due to strain accumulation at high strain amplitudes. (C) 2021 The Author(s). Published by Elsevier B.V.

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