Residual stress distribution in a laser peened Ti-2.5Cu alloy

被引:43
|
作者
Umapathi, A. [1 ]
Swaroop, S. [1 ]
机构
[1] VIT Univ, Sch Adv Sci, Surface Modificat Lab, Vellore 632014, Tamil Nadu, India
来源
SURFACE & COATINGS TECHNOLOGY | 2016年 / 307卷
关键词
Laser peening without coating; Ti-2.5Cu alloy; Residual stress; Micro hardness; Twinning; Adiabatic heating; HIGH-STRAIN-RATE; ADIABATIC SHEAR BANDS; MICROSTRUCTURE EVOLUTION; THERMAL RELAXATION; CORROSION BEHAVIOR; SURFACE-PROPERTIES; FATIGUE BEHAVIOR; GRAIN-REFINEMENT; STAINLESS-STEEL; ALUMINUM-ALLOY;
D O I
10.1016/j.surfcoat.2016.08.053
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
The goal of the present study is to investigate residual stress distributions and the accompanying deformation mechanisms during the process of laser peening without coating (LPwC), carried out on a Ti-2.5Cu alloy at a fixed power density of 6.97 GW cm(-2) with overlap rates from 50 to 90% (in steps of 10%). Thermal softening near surface (confined to a depth of 50 pm) from laser beam-material interaction was observed. Work-hardening increased with increase in overlap percentage till 80%. The maximum residual stress was found to be - 889 MPa for an optimal 70% overlap. Twinning was found to increase with the increase in overlap rates, indicating the hardening of the sample. The combined effect of adiabatic heating and thermal effects at the surface due to laser beam-material interaction (propagating inside the material), results in the softening of the material. The softening was found to be only in the onset stage, without flow localization. Softening predominates hardening beyond the overlap rates of 80% and the implications for this towards multiple peening are discussed. (C) 2016 Elsevier B.V. All rights reserved.
引用
收藏
页码:38 / 46
页数:9
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