首页> 外文会议>International Manufacturing Science and Engineering Conference >EFFECT OF HATCH ANGLE ROTATION ON THE THERMAL AND MECHANICAL PROPERTIES OF MICRO SELECTIVE LASER MELTED NITI SHAPE MEMORY ALLOY
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EFFECT OF HATCH ANGLE ROTATION ON THE THERMAL AND MECHANICAL PROPERTIES OF MICRO SELECTIVE LASER MELTED NITI SHAPE MEMORY ALLOY

机译:舱口角旋转对微选择性激光熔化NITI形状记忆合金的热和力学性能的影响

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NiTi shape memory alloy (SMA) has been widely used for bio-medical and aerospace applications due to its unique properties, i.e. shape memory effect and pseudoelasticity. However, the high ductility and work-hardening effect of NiTi lead to poor machinability. Additive manufacturing (AM), with excellent capability of fabricating complicated structures, has been used to fabricate NiTi components. To meet the increasing demand of product miniaturization, micro selective laser melting (uSLM) system equipped with finer laser beam has been developed to improve manufacturing resolution. This work studies the fabrication of NiTi SMA parts by uSLM for the first time. The effect of hatch angle rotation on the thermal and mechanical behaviors of μSLMed NiTi is analyzed. Columnar grains accompanied with equiaxed grains are observed in μSLMed NiTi. Laser rotation angles of 45/60/90° lead to weak crystallographic texture. Ti-rich secondary phases including Ti_2Ni/Ti4Ni_2O_x and TiC_(1-x)N_x are detected in the raw NiTi powder and the as-printed NiTi parts, respectively. The as-printed parts under different hatch angles show similar phase constitution. The thermal-induced transformation behavior was depressed with absence of transformation peak. The variation of hatch angle cannot activate the transformation peak. Varying hatch angle from 45 ° to 90 °, the compressive strength and ductility reduce, and the hardness increases. The depressed thermal-/stress-induced phase transformation of the U.SLM NiTi can be attributed to the Ti-rich secondary phases, which cause variation of matrix Ni/Ti ratio and inhomogeneous microstructure.
机译:由于其独特的特性,NITI形状记忆合金(SMA)已广泛用于生物医疗和航空航天应用,即形状记忆效应和假性弹性。然而,NITI的高延展性和工作硬化效果导致可加工性差。添加剂制造(AM)具有优异的制造复杂结构的能力,已用于制造NITI组分。为了满足产品小型化需求不断增加,已经开发出配备有更精细激光束的微选择性激光熔化(USLM)系统以提高制造分辨率。这项工作首次通过USLM制造NITI SMA零件。分析了舱口角旋转对μSLMEDniti的热和机械行为的影响。在μSLMEDNITI中观察到伴随等轴晶粒的柱状晶粒。激光旋转角度为45/60/90°导致弱晶体纹理。富含Ti_2NI / TI4NI_2O_X和TIC_(1-X)N_X的TI的二次相分别在原始NITI粉末和AS印刷的NITI零件中检测到。在不同的舱口角下的印刷部件显示出类似的相位构成。没有转化峰的抑制热诱导的转化行为。舱口角的变化不能激活变换峰值。不同的舱口角度从45°到90°,压缩强度和延展性减小,并且硬度增加。 U.SLM Niti的抑制的热/应力诱导的相变可归因于富含Ti的二次相,这导致基质Ni / Ti比和不均匀微观结构的变化。

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