The Alpha‐Case Formation Effect on Very High Cycle Fatigue and Fracture of Ultrafine‐Grained Near β Titanium Alloy

ABSTRACT Ultrasonic testing was conducted to investigate for the first time the impact of alpha‐case formation during air aging (450°C, 5 h) on the very high cycle fatigue (VHCF) and failure of an ultrafine‐grained (UFG) near β Ti‐5Al‐5V‐5Mo‐1Cr‐1Fe alloy. The research findings indicate that air aging results in the development of an alpha‐case layer, diminishing the fatigue properties of the UFG titanium alloy produced by radial shear rolling during VHCF testing. The fatigue limit of the alloy samples with an oxide layer decreased from approximately 620 to 520 MPa based on 10 9 cycles. Examination of the fatigue failure mechanisms revealed that the alpha‐case layer does not significantly impact crack initiation at stress amplitudes below 650 MPa but does accelerate crack propagation. In the alloy without an oxide layer, at all stress amplitudes, the crack initiation is internal. Oxidation leads to a change in the crack initiation mechanism from internal to subsurface at stress amplitudes above 650 MPa with low‐cycle fatigue failure.

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Publication Details

Journal
Fatigue & Fracture of Engineering Materials & Structures
Published
2025-05-19
DOI
https://doi.org/10.1111/ffe.14681
Primary Topic
Titanium Alloys Microstructure and Properties
Type
article
Field-Weighted Citation Impact
0.00

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article

The Alpha‐Case Formation Effect on Very High Cycle Fatigue and Fracture of Ultrafine‐Grained Near β Titanium Alloy

E. V. Naydenkin, Vladimir Oborin, I. P. Mishin, A. I. Manisheva
Fatigue & Fracture of Engineering Materials & Structures
Titanium Alloys Microstructure and Properties
article

The Alpha‐Case Formation Effect on Very High Cycle Fatigue and Fracture of Ultrafine‐Grained Near β Titanium Alloy

E. V. Naydenkin, Vladimir Oborin, I. P. Mishin, A. I. Manisheva
article en

Abstract

ABSTRACT Ultrasonic testing was conducted to investigate for the first time the impact of alpha‐case formation during air aging (450°C, 5 h) on the very high cycle fatigue (VHCF) and failure of an ultrafine‐grained (UFG) near β Ti‐5Al‐5V‐5Mo‐1Cr‐1Fe alloy. The research findings indicate that air aging results in the development of an alpha‐case layer, diminishing the fatigue properties of the UFG titanium alloy produced by radial shear rolling during VHCF testing. The fatigue limit of the alloy samples with an oxide layer decreased from approximately 620 to 520 MPa based on 10 9 cycles. Examination of the fatigue failure mechanisms revealed that the alpha‐case layer does not significantly impact crack initiation at stress amplitudes below 650 MPa but does accelerate crack propagation. In the alloy without an oxide layer, at all stress amplitudes, the crack initiation is internal. Oxidation leads to a change in the crack initiation mechanism from internal to subsurface at stress amplitudes above 650 MPa with low‐cycle fatigue failure.

Fatigue & Fracture of Engineering Materials & StructuresVol. 48(8)
Institute of Strength Physics and Materials Science (RU), Institute of Continuous Media Mechanics (RU)
Siberian Branch, Russian Academy of Sciences, Russian Academy of Sciences
Openalex Percentile: Top 93%
Titanium Alloys Microstructure and Properties
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