Effect of Fine Particle Peening Using Hydroxyapatite Particles on Rotating Bending Fatigue Properties of <i>β</i>-Type Titanium Alloy

Fine particle peening (FPP) using hydroxyapatite (HAp) shot particles was performed to improve the fatigue strength and form a HAp transfer layer on a beta titanium alloy (Ti–22V–4Al). The surface microstructures of the FPP-treated specimen were characterized using scanning electron microscopy, micr...

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Main Authors: Yuki Nakamura, Koichiro Nambu, Toshikazu Akahori, Toshihiro Shimizu, Shoichi Kikuchi
Format: Article
Language:English
Published: MDPI AG 2021-05-01
Series:Applied Sciences
Subjects:
Online Access:https://www.mdpi.com/2076-3417/11/9/4307
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author Yuki Nakamura
Koichiro Nambu
Toshikazu Akahori
Toshihiro Shimizu
Shoichi Kikuchi
author_facet Yuki Nakamura
Koichiro Nambu
Toshikazu Akahori
Toshihiro Shimizu
Shoichi Kikuchi
author_sort Yuki Nakamura
collection DOAJ
description Fine particle peening (FPP) using hydroxyapatite (HAp) shot particles was performed to improve the fatigue strength and form a HAp transfer layer on a beta titanium alloy (Ti–22V–4Al). The surface microstructures of the FPP-treated specimen were characterized using scanning electron microscopy, micro-Vickers hardness testing, energy dispersive X-ray spectrometry, X-ray diffraction, and electron backscattered diffraction. A HAp transfer layer with a thickness of 5.5 μm was formed on the surface of the Ti–22V–4Al specimen by FPP. In addition, the surface hardness of the Ti–22V–4Al was increased, and high compressive residual stress was generated on the specimen surface by FPP. Rotating bending fatigue tests were performed at room temperature in laboratory air over a wide cycle-life region (10<sup>3</sup>–10<sup>9</sup> cycles). In the long cycle-life regime, the fatigue strength at 10<sup>7</sup> cycles of the FPP-treated specimen became higher than that of the untreated specimen. This result is attributed to the formation of a work-hardened layer with high compressive residual stress by FPP. However, the fatigue strength was not improved by FPP in the short cycle-life regime, because fatigue cracks were initiated at surface defects formed during the FPP process. The fatigue fracture mode of the FPP-treated specimens shifted from surface-initiated fracture to subsurface-initiated fracture at a stress amplitude level of 600 MPa.
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spelling doaj.art-97ab10d4f8244afd8515ca9fd10752052023-11-21T19:01:17ZengMDPI AGApplied Sciences2076-34172021-05-01119430710.3390/app11094307Effect of Fine Particle Peening Using Hydroxyapatite Particles on Rotating Bending Fatigue Properties of <i>β</i>-Type Titanium AlloyYuki Nakamura0Koichiro Nambu1Toshikazu Akahori2Toshihiro Shimizu3Shoichi Kikuchi4Department of Mechanical Engineering, National Institute of Technology, Toyota College, Toyota 471-8525, JapanFaculty of Engineering, Osaka Sangyo University, Daito 574-8530, JapanFaculty of Science and Technology, Meijo University, Nagoya 468-8502, JapanDepartment of Mechanical Engineering, National Institute of Technology, Toyota College, Toyota 471-8525, JapanFaculty of Engineering, Shizuoka University, Hamamatsu 432-8561, JapanFine particle peening (FPP) using hydroxyapatite (HAp) shot particles was performed to improve the fatigue strength and form a HAp transfer layer on a beta titanium alloy (Ti–22V–4Al). The surface microstructures of the FPP-treated specimen were characterized using scanning electron microscopy, micro-Vickers hardness testing, energy dispersive X-ray spectrometry, X-ray diffraction, and electron backscattered diffraction. A HAp transfer layer with a thickness of 5.5 μm was formed on the surface of the Ti–22V–4Al specimen by FPP. In addition, the surface hardness of the Ti–22V–4Al was increased, and high compressive residual stress was generated on the specimen surface by FPP. Rotating bending fatigue tests were performed at room temperature in laboratory air over a wide cycle-life region (10<sup>3</sup>–10<sup>9</sup> cycles). In the long cycle-life regime, the fatigue strength at 10<sup>7</sup> cycles of the FPP-treated specimen became higher than that of the untreated specimen. This result is attributed to the formation of a work-hardened layer with high compressive residual stress by FPP. However, the fatigue strength was not improved by FPP in the short cycle-life regime, because fatigue cracks were initiated at surface defects formed during the FPP process. The fatigue fracture mode of the FPP-treated specimens shifted from surface-initiated fracture to subsurface-initiated fracture at a stress amplitude level of 600 MPa.https://www.mdpi.com/2076-3417/11/9/4307fine particle peeninghydroxyapatitebeta titanium alloyrotating bendingvery high cycle fatigue
spellingShingle Yuki Nakamura
Koichiro Nambu
Toshikazu Akahori
Toshihiro Shimizu
Shoichi Kikuchi
Effect of Fine Particle Peening Using Hydroxyapatite Particles on Rotating Bending Fatigue Properties of <i>β</i>-Type Titanium Alloy
Applied Sciences
fine particle peening
hydroxyapatite
beta titanium alloy
rotating bending
very high cycle fatigue
title Effect of Fine Particle Peening Using Hydroxyapatite Particles on Rotating Bending Fatigue Properties of <i>β</i>-Type Titanium Alloy
title_full Effect of Fine Particle Peening Using Hydroxyapatite Particles on Rotating Bending Fatigue Properties of <i>β</i>-Type Titanium Alloy
title_fullStr Effect of Fine Particle Peening Using Hydroxyapatite Particles on Rotating Bending Fatigue Properties of <i>β</i>-Type Titanium Alloy
title_full_unstemmed Effect of Fine Particle Peening Using Hydroxyapatite Particles on Rotating Bending Fatigue Properties of <i>β</i>-Type Titanium Alloy
title_short Effect of Fine Particle Peening Using Hydroxyapatite Particles on Rotating Bending Fatigue Properties of <i>β</i>-Type Titanium Alloy
title_sort effect of fine particle peening using hydroxyapatite particles on rotating bending fatigue properties of i β i type titanium alloy
topic fine particle peening
hydroxyapatite
beta titanium alloy
rotating bending
very high cycle fatigue
url https://www.mdpi.com/2076-3417/11/9/4307
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