On Variable Scale Evolution of Stress and Strain of TA2 Titanium Plate in Combined Hammering

锤子 喷丸 材料科学 酒窝 喷丸 残余应力 粒度 打滑(空气动力学) 复合材料 结构工程 冶金 工程类 航空航天工程
作者
Xudong Xiao,Bolun Zhang,Dan Qiao,Yong Li,Renfeng Zhao,Pengkang Zhao
出处
期刊:Coatings [Multidisciplinary Digital Publishing Institute]
卷期号:12 (12): 1974-1974
标识
DOI:10.3390/coatings12121974
摘要

Combined peening composed of multiple peening processes or peening media is a surface treatment method for comprehensive control of the macro shape and performance of the part. Compared to combined peening, the impact kinetic energy of the combined hammering can be easier to control over a wide range, and the hammer tool head size is larger than the shot. This paper focused on investigating the effect of combined hammering treatment, 6 mm and 14 mm tool heads with peening density 3.7 to 4.2/mm2, on the variable scale evolution of titanium TA2. Three types of contact relation between the tool head and existing dimple were proposed for impacting at the same position. The size of the dimple of combined hammering varies in width or depth direction, resulting in nest morphology composed of different size dimples. The cross-section microstructure of the test plate was observed, and the gradient changes of dislocation, slip, and grain size are smoothed by combined hammering. The change in hammer tool head size makes the target plastic deform at different depths. The hammering sequence has a significant influence on the evolution of stress and strain fields. When the tool head is first large and then small, a large compressive residual stress near the surface is introduced, about 1000 Mpa; on the contrary, the compressive residual stress distributes uniformly in the depth direction, with an affected layer depth of about 4.4 mm. The measured dimple size and residual stress verified the reliability of the simulation results.

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