Gradient microstructure and fatigue properties of TC21 titanium alloy processed by laser shock peening

被引:20
|
作者
He, Dongsheng [1 ]
Li, Liuhe [1 ]
Zhang, Yongxin [1 ]
Chi, Jiaxuan [2 ]
Zhang, Hepeng [3 ]
Sun, Rujian [4 ]
Che, Zhigang [4 ]
Zhang, Hongqiang [1 ]
Guo, Wei [1 ]
机构
[1] Beihang Univ, Sch Mech Engn & Automat, Beijing 100191, Peoples R China
[2] Beihang Univ, Sch Mat Sci & Engn, Beijing 100191, Peoples R China
[3] AECC Shenyang Liming Aeroengine Co LTD, Shenyang 110043, Peoples R China
[4] AVIC Mfg Inst, Sci & Technol Power Beam Proc Lab, Beijing 100024, Peoples R China
基金
北京市自然科学基金; 中国国家自然科学基金;
关键词
TC21 titanium alloy; Laser shock peening; Gradient microstructure; Phase transformation; Fatigue performance; GRAIN-REFINEMENT MECHANISM; RESIDUAL-STRESS; EVOLUTION; BEHAVIOR; STRENGTH;
D O I
10.1016/j.jallcom.2022.168139
中图分类号
O64 [物理化学(理论化学)、化学物理学];
学科分类号
070304 ; 081704 ;
摘要
The gradient microstructure evolution, microhardness, residual stress, and fatigue properties of TC21 ti-tanium alloy subjected to laser shock peening (LSP) were investigated. In this study, the different effects of LSP on alpha-Ti and beta-Ti were researched in detail. Results show that LSP could induce a large number of dislocation structures, among which dislocation lines (DLs), dislocation walls (DWs), and dislocation net-works (DNs) were mainly distributed in alpha-Ti, while dislocation tangles (DTs) were mainly distributed in beta-Ti and acicular alpha'. Sub-grain boundaries were formed by these DWs, DNs and DTs. It is worth noting that a large number of parallel twin structures also formed in alpha-Ti, and the formation of these twin structures was the result of the transformation of hexagonal close-packed Ti (HCP-Ti) to face-centered cubic Ti (FCC-Ti). The orientation relationship between the HCP-Ti and FCC-Ti can be described as (0002)HCP//(111)FCC and [2110]HCP//[110]FCC, which is consistent with the classic Shoji-Nishiyama relationship and HCP/FCC trans-formations. The coarse grains were divided by the sub-grain boundaries and twins, the microstructure was improved. As the depth from the peened surface increased, the dislocation density decreased and the twin structures gradually disappeared, the microstructures presented a gradient distribution. As for fatigue performance, the fatigue life of the TC21 was increased from 1.8 x 105 cycles to 4.7 x 105 cycles at 750 MPa stress level after LSP treatment, an increase of about 161%. Under the combined action of the microstructure and the compressive residual stress, the crack initiation and crack growth rate of the TC21 titanium alloy were delayed, and the fatigue life was finally improved.(c) 2022 Elsevier B.V. All rights reserved.
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页数:11
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