Effect of electron-beam treatment on the nature of fatigue crack propagation and formation of plastic zones on fracture surfaces in TiNi shape memory alloy

S. Meisner, L. Meisner
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Abstract

Influence of surface electron-beam processing on character of fatigue cracks propagation and crack growth rates under cyclic tension in a mode of low-cycle loading of TiNi samples before and after irradiation by low-energy high-current electron beam (LEHCEB) is studied in the work. Correlation between stages of fatigue cracks propagation and formation of plastic zones on surfaces of failure in TiNi samples before and after LEHCEB treatments is established. The LEHCEB treatment of specimen surfaces was carried out at the electron-beam installation “RITM-SP” with the electron beam parameters: energy density ES = 3.7 J/cm2, pulse duration τ = 2.5 μs, number of pulses n = 5. Differences in the stages of propagation of main fatigue cracks during cyclic stretching of TiNi samples before and after LEHCEB have been revealed. Preferential mechanisms of quasistatic and fatigue fracture at different stages of crack propagation are determined. It is shown that LEHCEB treatment leads to a shift of fatigue fracture initiation and the beginning of all stages by ∆N ≥ 3000, increasing the cyclic durability of the specimens by ~ 1.5 times. The greatest influence of surface modification is shown on Stage I of fatigue crack propagation. The lower rate of fatigue crack propagation at this stage in irradiated specimens leads to an increase in its duration as compared to unirradiated specimens. It is concluded that to effectively increase the fatigue life of TiNi specimens by means of LEHCEB treatments it is necessary to create conditions for increasing the number of cycles before the Stage I initiation and maximizing the duration of this stage.
电子束处理对TiNi形状记忆合金疲劳裂纹扩展性质及断口塑性区形成的影响
研究了低能大电流电子束辐照前后的表面电子束处理对TiNi试样低周加载模式下循环拉伸疲劳裂纹扩展特性和裂纹扩展速率的影响。建立了LEHCEB处理前后TiNi试样疲劳裂纹扩展阶段与破坏表面塑性区形成的相关性。在“RITM-SP”电子束装置上对样品表面进行LEHCEB处理,电子束参数为能量密度ES = 3.7 J/cm2,脉冲持续时间τ = 2.5 μs,脉冲数n = 5。揭示了循环拉伸前后TiNi试样主疲劳裂纹扩展阶段的差异。确定了裂纹扩展不同阶段准静态断裂和疲劳断裂的优先机制。结果表明:LEHCEB处理使疲劳断裂起始和各阶段开始发生∆N≥3000的位移,使试件的循环耐久性提高~ 1.5 倍;表面改性对疲劳裂纹扩展的第一阶段影响最大。与未辐照试样相比,辐照试样在这一阶段的疲劳裂纹扩展速率较低,导致其持续时间增加。结果表明,要想通过LEHCEB处理有效提高TiNi试样的疲劳寿命,必须创造条件,增加第一阶段开始前的循环次数,并使该阶段的持续时间最大化。
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