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400℃高周疲劳下TC17超声冲击强化表面状态演化规律研究

谭靓 樊怡 姚倡锋

中国机械工程2025,Vol.36Issue(4):790-801,12.
中国机械工程2025,Vol.36Issue(4):790-801,12.DOI:10.3969/j.issn.1004-132X.2025.04.016

400℃高周疲劳下TC17超声冲击强化表面状态演化规律研究

Investigation on Evolution Laws for Surface States of TC17 Alloy Induced by UIT during High-cycle Fatigue at 400 ℃

谭靓 1樊怡 2姚倡锋1

作者信息

  • 1. 西北工业大学航空发动机高性能制造工业和信息化部重点实验室,西安,710072||西北工业大学航空发动机先进制造技术教育部工程研究中心,西安,710072
  • 2. 陕西艾克斯普机电科技有限责任公司,西安,710061
  • 折叠

摘要

Abstract

Based on UIT experiments,surface state measurement and tension-tension high cycle fatigue tests at 400 ℃,the evolution laws of surface roughness,surface morphology,residual stress,microhardness,and microstructure of TC17 alloy were investigated.Results show that,compared with the surface states of the UIT processed specimen,after 1h heating treatment at 400 ℃,the value of surface roughness Ra increases from 0.46 μm to 0.67 μm,the surface microhardness decreases from 630 HV0.025 to 450 HV0.025,the surface compressive residual stress decreases from—640 MPa to—525 MPa,the maximum value of compressive residual stress decreases from—1088 MPa to—776 MPa,and the depth of plastic deformation layer decreases from 20 μm to 13 μm.After fatigue failure of the specimen at 400 ℃,the value of surface roughness Ra is as 1.22 μm,the depth of compressive residual stress layer is as 70 μm,the depth of plastic deformation layer is as 9 μm,and the subsurface equiaxed α phase transforms into elongated strips,the average grain area increases from 11.8 μm2 to 34 μm2.

关键词

TC17钛合金/超声冲击强化/表面状态/高周疲劳/演化规律

Key words

TC17 titanium alloy/ultrasonic impact treatment(UIT)/surface state/high-cycle fa-tigue/evolution law

分类

航空航天

引用本文复制引用

谭靓,樊怡,姚倡锋..400℃高周疲劳下TC17超声冲击强化表面状态演化规律研究[J].中国机械工程,2025,36(4):790-801,12.

基金项目

陕西省重点研发计划(2024PT-ZCK-63) (2024PT-ZCK-63)

中国机械工程

OA北大核心

1004-132X

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