Abstract

The traditional technique used to modify the surface of a metallic material is shot peening; however, cavitation peening, a more recent technique in which shot is not used, was developed, and improvements in the fatigue strength of metallic materials were demonstrated. In order to compare the fatigue properties introduced by shot peening with those introduced by cavitation peening, crack initiation and crack growth in specimens of austenitic stainless steel (Japanese Industrial Standards JIS SUS316L) treated using these techniques were investigated. With conventional cavitation peening, cavitation is produced by injecting a high speed water jet into water. In the case of submerged laser peening, bubbles are generated using a pulsed laser after laser ablation, and the impact produced when the bubbles collapse is larger than that due to laser ablation. Thus, in this study, cavitation peening using a water jet and submerged laser peening were investigated. To clarify the mechanisms whereby the fatigue strength is improved by these peening techniques, crack initiation and crack growth in specimens with and without treatment were examined by means of a K-decreasing test, where K is the stress intensity factor, and using a constant applied stress test using a load controlled plane bending fatigue tester. It was found that the improvement in crack initiation and the reduction in crack growth were roughly in a linear relationship, even though the specimens were treated using different peening methods. The results presented here show that the fatigue strength of SUS316L treated by these peening techniques is closely related to the reduction in crack growth, rather than crack initiation.

Highlights

  • Austenitic stainless steel is a bioinert material commonly used for implants [1,2]; this type of steel has insufficient fatigue resistance [2]

  • ∆Kmethods and the crack growth rate da/dn obtained by the between the stress intensity factor range and the crack growth rate da/dn obtained by the test

  • At the present condition base on the longer fatigue test changing with processing time per unit length and pulse as described in Section 2.1, and is 2.05 ± 0.23 for laser peening, 2.21 ± 0.05 for shot peening at tp = 0.88 density [17], both ∆Kth and ∆(∆K) of laser peening were slightly smaller than those of shot peening s/mm, and 2.32 ± 0.05 for cavitation peening

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Summary

Introduction

Austenitic stainless steel is a bioinert material commonly used for implants [1,2]; this type of steel has insufficient fatigue resistance [2]. To clarify the mechanism through which the fatigue characteristics are improved by peening, crack initiation and crack growth in peened specimens are usually investigated This has been done for shot peened austenitic stainless steel [5]; it has not been done for cavitation peened stainless steel. The load controlled plane bending fatigue tester was used in these experiments to evaluate crack initiation and growth in surface layers treated by shot peening, cavitation peening, and laser peening. The fatigue properties of austenitic stainless steel after treatment by cavitation peening, laser peening and shot peening were compared To make this comparison, crack initiation and growth in steel specimens were evaluated by a K-decreasing test and a constant applied stress test using a load controlled plane bending fatigue tester, respectively

Crack Growth Test
Photograph
A K-decreasing
Submerged Water Jet System
Schematic
Results
11. Relationship
As shown in Figures
14. Relationship
Discussions
Conclusions
Full Text
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