7 research outputs found

    Tailoring Texture, Microstructure, and Shape Memory Behavior of NiTi Alloys Fabricated by L-PBF-AM

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    Laser Powder Bed Fusion (L-PBF) is one of the most promising Additive Manufacturing (AM) methods to fabricate near net-shape metallic materials for a wide range of applications such as patient-specific medical devices, functionally graded materials, and complex structures. NiTi shape memory alloys (SMAs) are of great interest due to a combination of unique features, such as superelasticity, shape memory effect, high ductility, work output, corrosion resistance, and biocompatibility that could be employed in many applications in automotive, aerospace, and biomedical industries. Due to the difficulties with traditional machining and forming of NiTi components, the ability to fabricate complex parts, tailor properties that can show superelasticity, and fabricating highly textured alloys via AM is a paradigm shift for its shape memory alloy applications. Therefore, this study aims to establish process parameters, building strategy, microstructure, and property relationship of NiTi alloys. It will present that process parameters, sample orientation, loading type, and post heat treatments can be used effectively to tailor the transformation temperatures, grain shapes and sizes, texture, strength, transformation strain, and superelasticity of L-PBF-AM NiTi. The AM process parameters (PPs) govern the solidification characteristics, thermal gradient directions, competitive grain growth mechanisms, partial re-melting of the previous laser tracks and layers, which highly affect the composition, grain shape and size, texture, and thus mechanical properties of fabricated materials. Therefore, a comprehensive and systematic study is conducted to gain an in-depth understanding of the relationship between the AM processing parameters, microstructure, and shape memory properties of NiTi alloys fabricated by using the Ni-rich Ni50.8Ti49.2 (at. %) powder. It was found that the decrease of laser power from 250 to 100 W, scanning speed from 1250 to 125 mm/s, and hatch spacing from 80 to 40 µm alter the texture from the [001] to [111] orientation along the building direction. Moreover, it was revealed that transformation temperatures (TTs), microstructure, and the correlated thermo-mechanical response could be significantly changed with the process parameters. By the careful selection of PPs, as-fabricated NiTi samples can show superelasticity with 6% recovery and a recovery ratio of more than 87%. The shape memory behavior of NiTi alloys is highly texture/orientation dependent. Thus, it was hypothesized that the properties of NiTi alloys can be tailored by not only altering the process parameters but also adjusting the relative position of the sample orientation to the building direction, BD. Fabrication of the samples along different directions (loading directions, LD) relative to the BD impacts the re-melting and reheating processes of the layers, altering the texture of the fabricated samples along the testing direction. Moreover, since the impact of defects (e.g., cracks, pores) and crystallographic orientation formed during L-PBF-AM on the strength and shape memory behavior of NiTi could significantly be different in respect to the loading mode (compression or tension), both dog bone tensile and rectangular compressive samples were fabricated along the selected directions. It was revealed that when the LD was altered from 0 or 90 degrees (respect to the build plate) to 45 degree, the texture along the LD was altered from [100] to [110] orientation and significantly lowered the transformation stress. These texture variations created anisotropic compression-tension behaviors with deformation patterns consistent with single crystals. The [001]-textured parts showed higher strength and lower transformation strain (2.87% @ 200 MPa in tension for 0 degree), while the [110] samples showed higher transformation strain at lower stresses (5.31% @ 150 MPa in tension for 45 degree). Heat treatment is a very efficient method to control the TTs and improve the strength of Ni-rich NiTi alloys. The chemical composition, volume fraction, and coherency of the precipitates highly impact the TTs, matrix strength, hardness, and martensitic morphology and shape memory behavior of Ni-rich NiTi alloys. Therefore, post-heat treatment effects on the transformation characteristics (TTs, thermal hysteresis, and recoverable strain) and the microstructure of the L-PBF-AM Ni-rich NiTi SMAs have been investigated through transmission electron microscopy, thermal cycling under stress, and isothermal stress-strain experiments. L-PBF-AM NiTi samples were fabricated with laser power of 250 W, scanning speed of 1250 mm/s, and hatch spacing of 80 µm to show improved shape memory response as they presented strong [001] texture. It was revealed that post heat treatment at 500 °C for 1.5 h increased the TTs, decrease the hysteresis, and significantly improve the strength of the L-PBF-AM samples due to the formation of coherence precipitates. Perfect superelastic behavior with superelastic strain of 7% and superelastic window of 100 ºC was observed for aged L-PBF-AM samples

    Selective Laser Melting of Ni-Rich NiTi: Selection of Process Parameters and the Superelastic Response

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    Material and mechanical properties of NiTi shape memory alloys strongly depend on the fabrication process parameters and the resulting microstructure. In selective laser melting, the combination of parameters such as laser power, scanning speed, and hatch spacing determine the microstructural defects, grain size and texture. Therefore, processing parameters can be adjusted to tailor the microstructure and mechanical response of the alloy. In this work, NiTi samples were fabricated using Ni50.8Ti (at.%) powder via SLM PXM by Phenix/3D Systems and the effects of processing parameters were systematically studied. The relationship between the processing parameters and superelastic properties were investigated thoroughly. It will be shown that energy density is not the only parameter that governs the material response. It will be shown that hatch spacing is the dominant factor to tailor the superelastic response. It will be revealed that with the selection of right process parameters, perfect superelasticity with recoverable strains of up to 5.6% can be observed in the as-fabricated condition

    Influence of SLM on Compressive Response of NiTi Scaffolds

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    Porous Nickel-Titanium shape memory alloys (NiTi-SMAs) have attracted much attention in biomedical applications due to their high range of pure elastic deformability (i.e., superelasticity) as well as their bone-level modulus of elasticity (E≈12-20 GPa). In recent years, Selective Laser Melting (SLM) has been used to produce complex NiTi components. The focus of this study is to investigate the superelasticity and compressive properties of SLM NiTi-SMAs. To this aim, several NiTi components with different level of porosities (32- 58%) were fabricated from Ni50.8Ti (at. %) powder via SLM PXM by Phenix/3D Systems, using optimum processing parameter (Laser power-P=250 W, scanning speed-v=1250mm/s, hatch spacing-h=120μm, layer thickness-t=30μm). To tailor the superelasticity behavior at body temperature, the samples were solution annealed and aged for 15 min at 350°C. Then, transformation temperatures (TTs), superelastic response, and cyclic behavior of NiTi samples were studied. As the porosity was increased, the irrecoverable strain was observed to be higher in the samples. At the first superelastic cycle, 3.5%, 3.5%, and 2.7% strain recovery were observed for the porosity levels of 32%, 45%, and 58%, respectively. However, after 10 cycles, the superelastic response of the samples was stabilized and full strain recovery was observed. Finally, the modulus of elasticity of dense SLM NiTi was decreased from 47 GPa to 9 GPa in the first cycle by adding 58% porosity

    Laser Powder Bed Fusion of NiTiHf High-Temperature Shape Memory Alloy: Effect of Process Parameters on the Thermomechanical Behavior

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    Laser powder bed fusion has been widely investigated for shape memory alloys, primarily NiTi alloys, with the goal of tailoring microstructures and producing complex geometries. However, processing high temperature shape memory alloys (HTSMAs) remains unknown. In our previous study, we showed that it is possible to manufacture NiTiHf HTSMA, as one of the most viable alloys in the aerospace industry, using SLM and investigated the effect of parameters on defect formation. The current study elucidates the effect of process parameters (PPs) on the functionality of this alloy. Shape memory properties and the microstructure of additively manufactured Ni-rich NiTiHf alloys were characterized across a wide range of PPs (laser power, scanning speed, and hatch spacing) and correlated with energy density. The optimum laser parameters for defect-free and functional samples were found to be in the range of approximately 60–100 J/mm3. Below an energy density of 60 J/mm3, porosity formation due to lack-of-fusion is the limiting factor. Samples fabricated with energy densities of 60–100 J/mm3 showed comparable thermomechanical behavior in comparison with the starting as-cast material, and samples fabricated with higher energy densities (\u3e 100 J/mm3) showed very high transformation temperatures but poor thermomechanical behavior. Poor properties for samples with higher energies were mainly attributed to the excessive Ni loss and resultant change in the chemical composition of the matrix, as well as the formation of cracks and porosities. Although energy density was found to be an important factor, the outcome of this study suggests that each of the PPs should be selected carefully. A maximum actuation strain of 1.67% at 400 MPa was obtained for the sample with power, scan speed, and hatch space of 100 W, 400 mm/s, and 140 µm, respectively, while 1.5% actuation strain was obtained for the starting as-cast ingot. These results can serve as a guideline for future studies on optimizing PPs for fabricating functional HTSMAs

    Energy damping in shape memory alloys: A review

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    In recent years shape memory alloys (SMAs) have gained significant attention as potential damping device materials. This article presents an extensive review of the damping characteristics of SMAs, as well as experimental methods used to characterize their damping properties. The shape memory response and associated damping quality are discussed for three popular families of SMAs; Fe-based, Cu-based, and NiTi-based alloys including their behaviors and limitations. This review article also summarizes the most important parameters that impact the damping behavior of SMAs which are necessary to be investigated by researchers and manufacturers to address the current design challenges

    Laser Powder Bed Fusion of NiTiHf High-Temperature Shape Memory Alloy: Effect of Process Parameters on the Thermomechanical Behavior

    No full text
    Laser powder bed fusion has been widely investigated for shape memory alloys, primarily NiTi alloys, with the goal of tailoring microstructures and producing complex geometries. However, processing high temperature shape memory alloys (HTSMAs) remains unknown. In our previous study, we showed that it is possible to manufacture NiTiHf HTSMA, as one of the most viable alloys in the aerospace industry, using SLM and investigated the effect of parameters on defect formation. The current study elucidates the effect of process parameters (PPs) on the functionality of this alloy. Shape memory properties and the microstructure of additively manufactured Ni-rich NiTiHf alloys were characterized across a wide range of PPs (laser power, scanning speed, and hatch spacing) and correlated with energy density. The optimum laser parameters for defect-free and functional samples were found to be in the range of approximately 60–100 J/mm3. Below an energy density of 60 J/mm3, porosity formation due to lack-of-fusion is the limiting factor. Samples fabricated with energy densities of 60–100 J/mm3 showed comparable thermomechanical behavior in comparison with the starting as-cast material, and samples fabricated with higher energy densities (>100 J/mm3) showed very high transformation temperatures but poor thermomechanical behavior. Poor properties for samples with higher energies were mainly attributed to the excessive Ni loss and resultant change in the chemical composition of the matrix, as well as the formation of cracks and porosities. Although energy density was found to be an important factor, the outcome of this study suggests that each of the PPs should be selected carefully. A maximum actuation strain of 1.67% at 400 MPa was obtained for the sample with power, scan speed, and hatch space of 100 W, 400 mm/s, and 140 µm, respectively, while 1.5% actuation strain was obtained for the starting as-cast ingot. These results can serve as a guideline for future studies on optimizing PPs for fabricating functional HTSMAs
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