摘要
超弹性钛镍合金用于制造航空航天功能性器件,采用选区激光熔化成形方法可显著提高功能性器件设计和制造的自由度与复杂度。通过对选区激光熔化成形后的试样进行微观组织特征和超弹性行为分析,研究了材料在不同加载工况下的超弹性性能。研究结果表明:在20次循环试验中,超弹性行为表现优异且具有>6%应变范围的相变平台,马氏体相变开始与结束应力出现约4MPa的小幅衰减,相变应力稳定,累积残余应变仅为1.8%;随着应变幅值的增加,合金变形过程中消耗的能量值从23N·mm增至156N·mm,耗能值与应变幅值成线性增长关系;在不同应变速率下,合金的超弹性行为未发生明显变化。不同加载工况下,选区激光熔化成形的钛镍合金与传统方式制造的钛镍合金相比,超弹性行为表现得更加稳定,利于制造性能稳定的功能性器件。
The superelastic TiNi alloy can be used in the manufacture of aerospace functional devices, and the method of selective laser melting can obviously improve the freedom and complexity of the design of functional devices.The superelasticity of TiNi is studied through analyzing microstructure of TiNi alloy and condcuting the superelasticity cycling tests. The results show that in 20 times cycling tests, superelasticity behaves well and has a phase transition platform of more than 6% strain, martensitic transformation start and end stress have a small attenuation about 4 MPa, phase transformation stress is stable, and the cumulative residual strain is only 1.8%; Under different strain amplitude, the energy consumption in the alloy deformation increases from 23 N · mm to 156 N · mm, and the energy consumption linearly increases with strain amplitude; The superelastic property of the alloy does not significantly change at different strain rates. Under different loading conditions, the TiNi alloy manufactured by selective laser melting has a more stable superelastic behavior compared with the TiNi alloy manufactured by traditional way, and is more conducive to manufacture the stable functional devices.
引文
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