Properties of soft magnetic Fe-Co-V alloy produced by laser powder bed fusion

Tuomas Riipinen (VTT Technical Research Centre of Finland Ltd, Espoo, Finland)
Sini Metsä-Kortelainen (VTT Technical Research Centre of Finland Ltd, Espoo, Finland)
Tomi Lindroos (VTT Technical Research Centre of Finland Ltd, Espoo, Finland)
Janne Sami Keränen (VTT Technical Research Centre of Finland Ltd, Espoo, Finland)
Aino Manninen (VTT Technical Research Centre of Finland Ltd, Espoo, Finland)
Jenni Pippuri-Mäkeläinen (VTT Technical Research Centre of Finland Ltd, Espoo, Finland)

Rapid Prototyping Journal

ISSN: 1355-2546

Article publication date: 18 February 2019

Issue publication date: 12 July 2019



The purpose of this paper is to report on the developments in manufacturing soft magnetic materials using laser powder bed fusion (L-PBF).


Ternary soft magnetic Fe-49Co-2V powder was produced by gas atomization and used in an L-PBF machine to produce samples for material characterization. The L-PBF process parameters were optimized for the material, using a design of experiments approach. The printed samples were exposed to different heat treatment cycles to improve the magnetic properties. The magnetic properties were measured with quasi-static direct current and alternating current measurements at different frequencies and magnetic flux densities. The mechanical properties were characterized with tensile tests. Electrical resistivity of the material was measured.


The optimized L-PBF process parameters resulted in very low porosity. The magnetic properties improved greatly after the heat treatments because of changes in microstructure. Based on the quasi-static DC measurement results, one of the heat treatment cycles led to magnetic saturation, permeability and coercivity values comparable to a commercial Fe-Co-V alloy. The other heat treatments resulted in abnormal grain growth and poor magnetic performance. The AC measurement results showed that the magnetic losses were relatively high in the samples owing to formation of eddy currents.

Research limitations/implications

The influence of L-PBF process parameters on the microstructure was not investigated; hence, understanding the relationship between process parameters, heat treatments and magnetic properties would require more research.


The relationship between microstructure, chemical composition, heat treatments, resistivity and magnetic/mechanical properties of L-PBF processed Fe-Co-V alloy has not been reported previously.



Riipinen, T., Metsä-Kortelainen, S., Lindroos, T., Keränen, J.S., Manninen, A. and Pippuri-Mäkeläinen, J. (2019), "Properties of soft magnetic Fe-Co-V alloy produced by laser powder bed fusion", Rapid Prototyping Journal, Vol. 25 No. 4, pp. 699-707.



Emerald Publishing Limited

Copyright © 2019, Tuomas Riipinen, Sini Metsä-Kortelainen, Tomi Lindroos, Janne Sami Keränen, Aino Manninen and Jenni Pippuri-Mäkeläinen.


Published by Emerald Publishing Limited. This article is published under the Creative Commons Attribution (CC BY 4.0) licence. Anyone may reproduce, distribute, translate and create derivative works of this article (for both commercial and non-commercial purposes), subject to full attribution to the original publication and authors. The full terms of this licence may be seen at

1. Introduction

Soft magnetic Fe-Co-V alloys are used in applications where a combination of excellent magnetic properties and good mechanical strength are required, such as aircraft motors, generators and transformers. Binary Fe-Co alloys have the highest known saturation magnetization of any known material, as well as high permeability, low magnetic coercivity and high Curie temperature. They are, however, not very commercially viable materials because of high electrical conductivity and inherent brittleness, making the processing into thin sheets difficult. Processing the material into thin sheets is essential for reducing electromagnetic losses caused by eddy currents. For that reason, a small amount of vanadium (<3 wt%) is typically added as an alloying element to improve the ductility of the alloy while still retaining good magnetic properties. The traditional manufacturing method of stacking insulated sheets to build up a component includes many processing steps, such as casting, rolling and heat treatment, which increase the manufacturing cost (Chen et al., 2015). Soft magnetic components are also manufactured by compacting the alloy powder into a tool cavity, followed by a sintering step, resulting in homogenous high-precision components. Powders can be coated with an insulating layer to increase the electrical resistivity that helps to decrease the eddy current losses (Höganäs, 2013). The downside with this approach is the necessity of having the tools for the compacting phase, which can be costly to manufacture for small series.

Laser-based additive manufacturing technologies such as L-PBF provide new, interesting possibilities for the optimization of the shapes, materials, volume and mass of the magnetic cores, e.g. the use of magnetic material where it is really needed. Having the possibility to realize topologically optimized geometries with few restrictions opens new possibilities and challenges in guiding the magnetic flux for improved performance. Ultimately, our goal is to achieve improved torque density that is especially beneficial in aerospace applications. For this purpose, the combination of the L-PBF process and the Fe-Co-based materials offer great potential. The are some publications on the research of magnetic materials produced via additive methods other than L-PBF (Conteri et al., 2017; Li et al., 2017; Mikler et al., 2017a, 2017b; Sung and Rudowicz, 2003), but for the Fe-Co-V alloy, the amount of published research is very limited. Kustas et al. (2018) produced ring-shaped samples for material characterization from commercial gas atomized Fe-Co-1.5V powder using laser engineered net shaping (LENS) technology. The printed and annealed material exhibited harder magnetic properties compared to an annealed wrought material, mainly because of the presence of heterogeneous bimodal grain size. The as-built microstructure consisted of fine equiaxed grains, not very typical for materials processed using LENS and other welding based processes for which columnar grains and epitaxial growth is more common. Materials investigated in association with L-PBF include Ni-Fe14-Cu5-Mo4 (Bauer et al., 2016), Fe-Ni (Zhang et al., 2013a, 2013b) and Fe-6.9 wt% Si steel (Garibaldi et al., 2016, 2018a, 2018b), where the latter has been studied most extensively. Bauer et al. (2016) used a re-melt scanning strategy and observed that it resulted in a more homogeneous microstructure compared to single scan strategy and increased porosity as well as grain size. Zhang et al. (2013a, 2013b) found that the grain size could be coarsened by using higher laser scanning speeds, and it was proposed that the nucleation rate decreases with higher scanning speed as a result of a decrease in Marangoni flow. Garibaldi et al. (2016) found that the grain morphology of printed parts was affected by the laser energy input, where a shallower melt pool shape led to coarser and more homogeneous grain morphology in Fe-6.9 wt% Si steel. The printed samples had a <001> type fiber texture, and the intensity of the texture increased with higher laser energy input. The best magnetic properties, i.e. lowest coercivity, power loss and highest permeability and flux density, were obtained with the 1,150°C anneal. Lower annealing temperatures did not result in a homogenous microstructure. This suggested that the growth of grains with <001> orientation was more likely to grow during annealing owing to their larger size compared to grains with other orientations. Annealing at 700°C is enough to relieve internal stresses but not enough to induce grain growth.

Based on earlier studies of binary Fe-Co alloys manufactured by L-PBF, a need for a mechanically stronger alloy was recognized (Lindroos et al., 2017). This led to the research reported here on L-PBF manufactured Fe-49Co-2V alloy. First, the process parameters were optimized with the goal of minimizing porosity in printed samples, followed by printing of test samples for material characterization, the results of which are reported and discussed in this paper.

2. Materials and methods

A small batch (∼5 kg) of Fe-49Co-2V powder was produced at VTT, using a Hermiga Gas Atomizing unit. The powder was sieved using a 63 µm mesh and air-classified to remove the smallest particles. The morphology of the powder was analyzed using a scanning electron microscope (SEM), and the particle size distribution was measured using a Malvern laser diffraction analyzer (Figure 1). The particle size distribution is presented using Dv(x) values that indicate the volume fraction percentage (x) below particle size (Dv). The Dv (10), Dv (50) and Dv (90) values were measured as 18.6 µm, 37.1 µm and 62.7 µm, respectively. The powder had good flowability based on tests done using a Hall Flowmeter.

The samples were built using an SLM Solutions GmbH 125HL machine, which has a fiber laser with a maximum power output of 400 W. The build chamber was purged with argon gas (purity level 99.996 per cent) before the operation, and a constant gas flow was maintained during the experiment. Oxygen content in the build chamber was maintained below 0.1 vol% during the process. The samples were built directly onto a 1.4841 (AISI 314) austenitic stainless steel substrate, which was heated and kept at 200°C during the process to reduce the thermal gradients in the material. Before processing with the SLM 125HL, the powder was dried in a vacuum furnace at 50°C for approximately 12 h.

Prior to printing the samples for material characterization, a set of L-PBF process parameters resulting in dense parts needed to be determined experimentally. A parameter space was studied where the laser power, scanning speed and hatch distance were limited to 150-225 W, 575-975 mm/s and 80-120 µm, respectively. The parameter space was narrowed down by limiting the volumetric energy density to 70-130 J/mm3, and the final design consisted of 27 different parameter combinations. The printed samples were prepared for optical microscopy analysis using standard metallographic practices. The porosity of the samples was measured using image analysis based on thresholded binary images. The optimal process parameter set used for manufacturing the characterization samples was power = 200W, scanning speed = 775 mm/s and hatch spacing = 80 µm. The different sample types printed for material characterization were the following: 10 × 10 × 10 mm³ cubes for microstructural analysis, 90 × 10 × 10 mm³ bars and ring samples (outer diameter = 60 mm, inner diameter = 50 mm, height = 5 mm) for magnetic measurements and flat tensile test specimens (30 mm gage length, 5 mm thickness, 99.6 mm overall length) for mechanical testing. All of the samples were oriented horizontally on the build platform. The samples were cut from the platform using electrical discharge machining.

Desirable magnetic properties for Fe-Co alloys are achieved with suitable heat treatments, where the optimal heat treatment procedure depends on the alloy composition as well as the initial microstructure. The different heat treatment procedures done in this study are presented in Table I. The samples were placed inside a pipe furnace (Ar-4 per cent H2 atmosphere), which was then heated to the target temperature at a rate of 200°C/h. In the pre-anneal and normalizing heat treatments, the samples were allowed to cool down within the furnace. For the primary anneal, a cooling rate of 100°C/h was used until reaching 500°C, after which the samples were let to cool down to room temperature in the furnace.

The 10 × 10 × 10 mm³ samples were cut, polished and etched prior to analysis of the microstructure and chemical composition. The chemical composition of the gas atomized powder and a printed sample were measured using a panalytical axios max X-ray fluorescence (XRF) spectrometer equipped with Rh anode. The microstructure was analyzed using optical microscopy (OM) and an SEM equipped with electron diffraction spectrometer (EDS). The resistivity measurements were done as follows: a current (2 A) was directed to the 90 × 10 × 10 mm³ bar samples, which were placed between copper plates, and the conductivity was measured between two pins that were placed on the sample surface and separated by a distance of 4.7 mm. Each sample was measured four times for a total duration of 15 min, and the polarization of the current was alternated during measurements. Measurements of the magnetic properties were outsourced from a third party where AC measurements with sinusoidal supply and quasi-static DC measurements were carried out. The bar samples were used only for the quasi-static DC measurements to analyze the properties at high excitation, i.e. with high external magnetic field strength up to 50 kA/m. The ring samples were then used for quasi-static characterization of the samples at lower excitation, maximum 10 kA/m as well as for the AC measurements at 10 and 50 Hz and with different magnetic flux densities. The purpose of these AC measurements was to study the losses of the 3D printed samples. The tensile tests were carried out at room temperature using an Instron universal testing machine (model 1185), where three samples were tested in as-built condition and three for each of the heat treatments (Table I). The tensile tests were carried out in accordance to the ISO 6892-1 2016 standard. The elongation after fracture was measured by placing the two pieces of a fractured test specimen together, and measuring the new length as compared to markings with a 25 mm spacing made on the samples prior to testing.

3. Results and discussion

3.1 Porosity analysis

The 3D printed samples attached to the build platform and one of the polished cross-sections used for porosity analysis are shown in Figure 2. The measured average porosity for four samples was 0.07 per cent (Table II). The optimized process parameters led to high density, which is important in high-performance components because defects such as pores can hinder the movement of magnetic domains, thus weakening the magnetic properties. Most of the pores are small, with a diameter of 10-20 µm, and are likely induced by gas trapped inside the molten powder (Zhang et al., 2017).

3.2 Chemical composition

The chemical composition of the gas-atomized powder and a printed sample in as-built condition were measured using semi-quantitative XRF analysis (Table III), which has a detection limit of 0.01 per cent for elements from fluorine to uranium. Carbon and oxygen contents were not measured for the samples. The measured composition of the powder is close to the nominal composition, except for cobalt, which is below 49 wt%. The printed sample shows a higher vanadium and lower cobalt content compared to the powder.

3.3 Resistivity

The measured resistivities of the 3D printed samples were 49.4 and 48.8 µOhm × cm (Table IV). The resistivities of commercial Fe-49Co-2V alloy strips were measured as 44.6 and 46.0 µOhm×cm. The resistivity of Fe-Co-V alloys is considerably higher compared to binary Fe-Co (≤ 7 µOhm × cm) (Sundar and Deevi, 2005), which is beneficial in reducing eddy current losses. The resistivity of the material printed in this study was approximately 10 per cent higher compared to the commercial alloy, which is mainly a result of the difference in chemical compositions.

3.4 Microstructure

The microstructure and grain morphology were studied using OM and SEM. OM images of the etched sample cross-sections (Figure 3) revealed that microstructure varies greatly between heat treatments. The sample in as-built condition [Figure 3(a)] has a fine grain structure, where the solidified grains are oriented toward the center of the solidified melt track. Heat treatment, HT1, at 820°C for 4 h [Figure 3(b)] led to a bimodal grain structure consisting of very small and large grains, indicating that abnormal grain growth took place during the heat treatment. The small grains have a diameter of only a few micrometers, whereas the largest grains have a diameter of over 200 µm. HT2, which consisted of a pre-anneal at 700°C followed by 10 h anneal at 820°C [Figure 3(c)], resulted in an equiaxed grain structure with relatively large grain size. A normalizing heat treatment was done in HT3 to homogenize the microstructure prior to the primary heat treatment at 820°C for 10 h. This heat treatment resulted in a similar bimodal grain structure as HT1 [Figure 3(d)] except for a smaller fraction of large grains. The bimodal grain structure observed in HT1 and HT3 samples indicate that part of the grain boundaries became pinned, inhibiting the grain growth, whereas some grain boundaries were able to grow significantly. Different phenomena can cause abnormal grain growth, one being grain boundary pinning caused by the presence of second phase particles (Holm et al., 2015). Bimodal grain size distribution was also observed in heat-treated Fe-Co-V sample produced by additive manufacturing process previously (Kustas et al., 2018), where second phase particle pinning was named as a likely cause.

The temperature of the normalizing heat treatment is high enough to relieve the internal stresses but possibly not high enough for full homogenization to take place. Compared to the HT2 samples that were pre-annealed at lower 700°C temperature, only partial grain growth took place in the HT3 samples despite being exposed to identical heat treatment at 820°C. This implies that some of the grain boundaries were pinned by second phase particles during the anneal. The printed alloy contains 0.06 wt% niobium as an alloying element, which is used in commercial alloys to suppress grain growth to improve mechanical properties (Sundar and Deevi, 2005). Niobium acts as a carbide former in steels, but it has been shown to form carbonitrides with 0.06 wt% Nb additions and intermetallic Laves phase with 0.3 wt% Nb additions in Fe-Co alloys (Shang et al., 2000). The Laves phase forms along grain boundaries, restricting grain growth (Ackermann et al., 1970). The printed samples were analyzed with SEM/EDS to study the precipitates in more detail. Most of the second phase γ2 precipitates have a diameter of approximately 100 nm and are distributed relatively homogeneously in the as-built samples, as shown in Figure 4. In the heat treated sample (HT1), niobium-rich precipitates were observed in the matrix as well as at the grain boundaries. The reason behind the abnormal grain growth could be that the second phase particles precipitate unevenly in the grain boundaries, pinning their movement during heat treatment. A comprehensive explanation of the effect of heat treatment temperature on the grain structure evolution would require more extensive studies and is considered an important topic for future research.

3.5 Magnetic properties

The measured quasi-static DC magnetic properties are presented in Table V. The samples in as-built condition have relatively low saturation magnetization (Bmax) and magnetic permeability (µmax) but high coercivity (HcJ). The poor magnetic performance of the as-built sample results from the presence of internal stresses, small grain size and presumably low degree of order resulting from the high cooling rates, characteristic of the L-PBF process. Heat treatments improved the magnetic properties of all samples, and the improvement was most significant for HT2. The very low coercivity and high permeability show that the HT2 led to magnetic saturation at very low external field strength. The large grain size of the HT2 sample means that there are fewer boundaries inhibiting the movement of magnetic domains. A homogenous microstructure with large grain size reduces the magnetic coercivity and improves permeability (Sourmail, 2005). The J-H curves that represent the intrinsic demagnetization, i.e. magnetic polarization of the samples, are presented in Figure 5. The quasi-static and low-frequency B-H hysteresis loops from the AC measurements at 10 and 50 Hz, where Bmax=1.5T, are shown for all of the samples in Figure 6. The 3D printed samples have higher losses compared to the laminated sample, as was expected for solid material. The laminated samples were heat-treated according to the supplier recommendation (HT1), and it is obvious that the magnetic properties for the 3D printed samples with the same heat treatment differ greatly. The alloy compositions were not identical, which affects the optimal heat treatment procedure. It is however not clear why the HT2 heat treatment led to a vastly different microstructure compared to HT3. Due to the relatively high magnetic losses in the 3D-printed material, it would be very important to increase the resistivity of the material for increased commercial viability.

3.6 Mechanical properties

The mechanical properties of the Fe-Co-V tensile test specimens, including the 0.2 per cent yield strength (Rp0.2), tensile strength (Rm) and elongation after fracture (A) are presented in Figure 7(a) and the stress-strain curves, in Figure 7(b). Some of the samples fractured outside of the constant cross-section area and for those cases, the result is omitted. The stress-strain curves show the strain from the extensometer and do not represent the actual elongation of the tensile test specimen. The actual elongation was measured from the fractured samples as described earlier, resulting in a relatively high uncertainty in the results. The as-built samples have a fine grain structure inhibiting the mobility of dislocations, and presumably, they predominantly consist the disordered phase structure that results in high strength. After heat treatment, the strength of the samples decreases significantly and the elongation after fracture drops from 4 per cent to approximately 2 per cent. Despite the low elongation, the vanadium addition improves ductility, compared to the binary Fe-Co alloys manufactured by L-PBF that were extremely brittle, with heat-treated samples fracturing before the 0.2 offset yield point (Lindroos et al., 2017). The mechanical properties of the printed samples are slightly better compared to the heat-treated standard commercial Fe-Co-V alloy with a similar composition that was used as a reference in Figure 7(a) (VACUUMSCHMELZE, 2016). The advantage of the L-PBF process is that there is no need for cold work after printing, meaning that the ductility is not as critical as with traditional manufacturing of thin sheets.

4. General remarks on the results

Grain growth and the subsequent grain size coarsening significantly affect magnetic domain mobility and is, therefore, a key factor in obtaining good magnetic properties for the soft magnetic Fe-Co-V alloy in this study. The structure-sensitive magnetic properties, e.g. coercivity and permeability, however, also depend on precipitate distribution and size, internal stresses, state of order, texture, imposed external stress and test temperature (Sundar and Deevi, 2005). During SEM analysis, precipitates containing Niobium were observed at the grain boundaries. These precipitates could have acted as pinning sites for grain boundaries during heat treatment resulting in bimodal grain structure. Some of the grain boundaries had greater mobility and were able to grow during heat treatment. The second phase γ2 precipitates do not directly contribute to the strength of the material but increase ductility as well as the strength indirectly by inhibiting grain growth during annealing (Sourmail, 2005). The γ2 precipitates act as a pinning site for magnetic domains, which is important to consider when choosing the heat treatment, as obtaining good magnetic properties is a balance between grain size, number and size of precipitates and the order parameter. The state of order has an effect on the yield stress of Fe-Co-V, which is higher in the disordered state, but a high state of order is still preferred as it decreases the coercivity (Sundar and Deevi, 2005). The ordering parameter was not studied in this paper.

As is evident from the AC magnetic hysteresis loops, the losses are substantial for the printed samples. The electrical resistivity of the material should be increased considerably to make the 3D printed components practical in commercial applications. The electrical resistivity can be increased by modifying the alloy composition, but this has some obvious drawbacks, such as diminishing magnetic properties. Increase in electrical resistivity could also be achieved by modifying the component geometry and microstructure by taking advantage of the layer-by-layer nature of the L-PBF process and the ability to control the movement of the heat source. Controlling the microstructure by changing the process parameters is a challenging task, as the main laser parameters, i.e. power, scanning speed and hatch distance, directly influence the geometry and heat-flow properties of the moving melt pool (Gong et al., 2014; Gunenthiram et al., 2017). Scanning pattern determines how the heat is distributed during the build, which in turn affects the thermal history and solidification kinetics of previous layers (Sames et al., 2016). During the build process, the consecutive heating and cooling cycles result in segregation of alloying elements and formation of precipitates. These in turn have can an effect on the recrystallization and grain growth kinetics during heat treatments. Exploration of the full potential of the L-PBF technology for manufacturing soft magnetic components would require extensive studies on the microstructure evolution with different process parameters such as scanning pattern, laser parameters and heat treatments. In this study, the laser parameters were optimized with the goal of minimizing the porosity in printed samples, and thus the effect of process parameters on the microstructure formation was out of the scope of this study.

5. Conclusions

The parts printed in this study varied greatly in microstructure and magnetic properties. The HT2 heat treatment with low-temperature pre-anneal done prior to the final anneal at 820°C for 10 h led to the best magnetic performance and a uniform distribution of relatively large grains. A normalizing heat treatment done prior to the final anneal (HT3) led to a bimodal grain size distribution and hence suboptimal magnetic properties. Similar results were obtained with 4 h annealing at 820°C. The grain growth and subsequent grain size significantly affect magnetic domain mobility and are therefore of key importance in obtaining good magnetic properties for soft magnetic alloys. The heat treatments are crucial in changing the microstructure and hence the magnetic properties of the 3D printed alloys. Based on the results of this study, more experimental work is required for gaining a better understanding of the phenomena behind the microstructure evolution. The L-PBF technology shows promise as a manufacturing technology for small-series production of components with high geometrical complexity. This, combined with the possibility to influence the microstructure by altering the L-PBF process parameters and the use of proper heat treatments, could enable manufacturing of components with superior magnetic performance.


Particle morphology of the gas atomized and sieved Fe-Co-V powder (left) and the measured particle size distribution (right)

Figure 1

Particle morphology of the gas atomized and sieved Fe-Co-V powder (left) and the measured particle size distribution (right)

3D printed Fe-Co-V samples (left), a cross-section image used for porosity analysis (right)

Figure 2

3D printed Fe-Co-V samples (left), a cross-section image used for porosity analysis (right)

OM images of polished and etched Fe-Co-V samples

Figure 3

OM images of polished and etched Fe-Co-V samples

SEM images of 3d printed Fe-Co-V samples showing the solidified structure in the as-built sample (left) and the grain boundary precipitates in the heat treated sample containing Niobium

Figure 4

SEM images of 3d printed Fe-Co-V samples showing the solidified structure in the as-built sample (left) and the grain boundary precipitates in the heat treated sample containing Niobium

J-H curves of the Fe-Co-V samples obtained from DC-measurements

Figure 5

J-H curves of the Fe-Co-V samples obtained from DC-measurements

DC quasi static and low frequency AC magnetic hysteresis loops for 3D printed and laminated Fe-Co-V samples

Figure 6

DC quasi static and low frequency AC magnetic hysteresis loops for 3D printed and laminated Fe-Co-V samples

Mechanical properties of Fe-Co-V tensile test specimens

Figure 7

Mechanical properties of Fe-Co-V tensile test specimens

Fe-49Co-2V heat treatment procedures

heat treatment Pre-anneal Normalizing Primary anneal
Heat treatment 1 (HT1) 820°C/4 h
Heat treatment 2 (HT2) 700°C/2 h 820°C/10 h
Heat treatment 3 (HT3) 950°C/0.5 h 820°C/10 h

Measured porosities of 3D printed samples

Measurement As-built HT1 HT2 HT3 Average
Measurement area (mm2) 98 97 97 97 97
Porosity (%) 0.07 0.06 0.05 0.07 0.07

Chemical composition of gas atomized powder and 3D printed Fe-Co-V sample, measured using X-Ray fluorescence spectrometer. Values in wt%

Sample Si V Mn Fe Co Ni Ga Nb
Powder 0.04 2.2 0.07 49.1 48.4 0.08 0.02 0.06
Printed, as-built* 2.6 0.12 49.4 47.8 0.06

*The sample was measured using a 6 mm mask, increasing the measurement uncertainty

Measured electrical resistivities of 3D printed and laminated Fe-Co-V samples

Sample Sample condition Test current (A) Area (mm²) Resistivity (µOhm × cm) Estimated uncertainty (%) Electrical conductivity IACSa% Temperature (°C) Humidity (%)
3D printed Fe-49Co-2V HT1 2 100.35 49.4 2 3.5 23.62 37.3
HT2 2 100.40 48.8 2 3.5 23.62 37.4
Commercial As-built 0.1 3.66 44.6 3 3.9 23.1 36.1
Commercial HT1 0.1 3.65 46.0 3 3.7 23.1 36.1

aInternational Annealed Copper Standard (resistivity of commercially available copper = 0.15328 Ohm×m at 20°C); bstandardized commercial Fe-49Co-2V alloy (ASTM A801-09 Alloy type 1)

Magnetic properties of Fe-Co-V samples from quasi-static DC measurements

Sample type Heat treatment Br (T) HcB (A/m) HcJ (A/m) µmax (−) H(µmax) (A/m) Hmax (kA/m) Jmax (T) Bmax (T)
Bar As-built 0.90 1344 1345 307 1930 55.20 2.10 2.17
Ring 0.88 1287 1288 322 1754 9.30 1.56 1.57
Bar HT1 1.59 73 73 9156 72 56.00 2.22 2.29
Ring 1.56 493 493 1922 125 9.38 2.16 2.18
Bar HT2 1.51 52 52 17000 47 55.80 2.21 2.28
Ring 1.31 47 47 13000 60 9.09 2.22 2.23
Bar HT3 1.36 527 527 1421 737 56.80 2.23 2.30
Ring 1.43 144 144 4463 99 10.10 2.14 2.16
Commercial Fe-Co-V (bar)* As-built 0.39 85 85 2204 170 57.10 2.15 2.23
Commercial Fe-Co-V (ring)* 0.39 104 104 1811 152 9.78 2.17 2.18
Commercial Fe-Co-V (bar)* HT1 0.51 59 59 4300 272 57.10 2.16 2.24
Commercial Fe-Co-V (ring)* 1.26 40 40 12000 53 9.75 2.22 2.23

*Laminated samples made from commercial Fe-Co-V sheet material (ASTM A801-09 Alloy type 1)


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The authors gratefully acknowledge the financial support from Academy of Finland (funding decisions 289338 and 306236).

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Tuomas Riipinen can be contacted at: