Brazing Tungsten/Tantalum/RAFM Steel Joint for DEMO by Fully Reduced Activation Brazing Alloy 48Ti-48Zr-4Be

: To create a DEMO reactor, it is necessary to develop high-quality technology to join tungsten with reduced-activation ferritic-martensitic (RAFM) steel (Rusfer, Eurofer, CLF-1, etc.). Difﬁculties arise in their direct connection due to the large difference in the coefﬁcient of thermal expansion (CTE). To suppress the difference of CTE, intermediate interlayers are usually used, such as vanadium or tantalum, and brazing is a prospective technology to conduct the joining. The vast majority of works represent copper-or nickel-based brazing alloys, but their applicability is under signiﬁcant discussion due to their activation properties. That is why, in this work, fully reduced activation 48Ti-48Zr-4Be wt.% brazing alloy was used. The following joint was made: Rusfer steel/48Ti-48Zr-4Be/Ta/48Ti-48Zr-4Be/W. The brazing was successfully carried out under a mode providing thermal heat treatment of Rusfer. Through EDS and EBSD analysis, the microstructure of the joint was determined. Shear strength of the as-joined composition was measured as 127 ± 20 MPa. The joint endured 200 thermocycles in the temperature range between 300–600 ◦ C, but the ﬁllet regions degraded.


Introduction
The DEMO fusion reactor is the next step towards an industrial thermonuclear power plant; projects of DEMO have been developed worldwide [1][2][3][4].DEMO will focus on the production of electricity.It must demonstrate technological stability, safe power generation and reliable plant maintenance.When designing such a plant, it is necessary to take into account not only the physical requirements, but also the technical and technological constraints.Operating parameters in DEMO will be tougher than for ITER, so tungsten will be the Plasma Facing Material (PFM) for the First Wall, and Reduced Activation Ferritic Martensitic (RAFM) steel, such as Rusfer [5] or Eurofer [6], will be the construction material.Because of this fact, one urgent issue should be solved before construction-the production of a strong joint between tungsten and steel.However, direct connection is tough to achieve because of the big difference in coefficients of thermal expansion (CTE): (10.5-12.3)× 10 −6 K −1 for steel and (4.3-6.0)× 10 −6 K −1 for tungsten.A significant difference causes large residual stresses during cooling, and as a result can lead to the destruction of the joint [7,8].Usually, intermediate layers are used to suppress a mismatch of CTE [9].In DEMO, in order to relieve these stresses, it is proposed to use Nb [10], V [11], Ti [12], Cu [13], and Ta [14].
Nevertheless, it is necessary to select a reliable manufacturing technology.Several methods have been proposed: brazing with powder alloys [15], galvanic layers [16] and amorphous foils [17], or solid-state technologies for diffusion bonding [12,18,19].Brazing Metals 2021, 11, 1417 2 of 15 is considered to be the most reliable technology, because it does not cause creep of the materials which are to be joined, and the cost is lower compared with hot isostatic pressing et al.According to ITER experience, it is also important to use a technology which allows local repair of damaged components during production [20].However, until now no fully reduced activation brazing alloy has been used, or the strength of the joint was low [21].Instead, scientists use nickel [17,22,23] or copper [11,[24][25][26] brazing alloys, although these materials do not fully satisfy the requirement of reduced activation.To solve this problem, we are attempting to use a fully reduced activation composition, 48Ti-48Zr-4Be wt.%.This alloy has already been successfully used when brazing a self-passivating tungsten alloy [27].
Another advantage of brazing is the possibility of carrying out a simultaneous production process and the heat treatment of the materials to be joined.If a RAFM steel is used in a heat-treated state, a high joining temperature leads to α-γ transition during joining, so the steel is not martensitic anymore [28].This means that the joining temperature is limited to 500 • C, because the properties of heat-treated RAFM steels significantly decrease after heating above 500 • C [29,30].Not to spoil the steels' microstructure during the joining process, brazing should be carried out simultaneously with the heat treatment of the steels.
In addition, it is very important to study mechanical strength, the exact microstructure of the brazed joints, and its changes under working conditions to assess the influence of the technological process, and the composition of the intermediate layers and filler alloys.The information obtained will be useful for the further optimization of the technology.All in all, a good joint for DEMO satisfies the requirement of reduced activation, can withstand heat loads and thermocycling during operation, and the manufacturing process does not spoil the microstructure of the materials to be joined.

Materials
In this work the following materials were used:
We manufactured the following joint: Rusfer/TiZr4Be/Ta/TiZr4Be/W.STEMET brazing alloys are widely used in the nuclear, air and automotive industries [32][33][34][35][36]. TiZr4Be alloy has a good glass forming ability (GFA) produced by melt spinning [37], and a high GFA makes it possible to produce flexible foil by this spinning technology.The alloy has an amorphous state with a limited crystalline phase.The liquidus temperature of the alloy is close to 840 • C. The brazing alloy has been investigated in detail elsewhere [38].
Figure 1 shows the schematic view of the specimens in mm, for microstructural observation (a) and for shear tests (b).

Methods
We carried out brazing in a vacuum furnace (p < 10 −5 mmHg).The specimens were fixed by a 200 g load that corresponded to 0.4 MPa.The gap between the base materials corresponded to the thickness of the brazing alloy.We used the brazing mode to arrive at thermal heat treatment of the steel: 1100 • C, 1 h + 720 • C 3 h [39], heating rate (Vh) for the first step 40      C/min (we present the graph of the mode in [9]).This means that we carried out brazing simultaneously to the heat treatment of the steel.

Methods
We carried out brazing in a vacuum furnace (p < 10 −5 mmHg).The specimens wer fixed by a 200 g load that corresponded to 0.4 MPa.The gap between the base materia corresponded to the thickness of the brazing alloy.We used the brazing mode to arrive a thermal heat treatment of the steel: 1100 °C, 1 h + 720 °C 3 h [39], heating rate (Vh) for th first step 40 °C/min, cooling rate (Vc) 20 °C/min, for the second step Vh = 20 °C/min, Vc 10 °C/min (we present the graph of the mode in [9]).This means that we carried out braz ing simultaneously to the heat treatment of the steel.
The microstructure was investigated on the cross-sections of the brazed samples b MTI MM500T metallographic microscope (MTI Corporation, USA) and JEOL JSM-6610L scanning electron microscope (SEM) with energy dispersive spectroscopy (EDS) INCA X ACT (Jeol, Japan).Electron beam scattered diffraction (EBSD) analysis and ultra-high res olution photos were obtained by means of SEM TESCAN CLARA (Tescan, The Czec Republic) equipped with EBSD Oxford Instruments Nordlys Nano and EDS Oxford In struments Ultim MAX 100 (Oxford Instruments, UK).
The specimens were prepared using a common metallographic procedure.For meta lographic microscopy the samples were etched with 20% HNO3 + 20% HF + 60% glycero solution, and the etching time was 1-3 s to identify the structure of the brazed seam an 20-30 s to identify the steel's microstructure.Before EBSD analysis, the samples wer etched with Technoorg Linda SEMPrep2 (Technoorg, Hungary).
Microhardness HV0.1 (load 0.9807 Н, holding time 15 s) in the cross section of a braze seam was measured by Vickers FM-800 (Future-Tech, Japan) equipment.Shear strengt was measured by a Quasar50 (Galdabini, Switzerland) universal testing machine with mm/min crosshead speed.The scheme of the shear test used is presented elsewhere [40 We chose the shear test to ensure that the joint will fail throughout a seam.If the tensil test had been chosen, a failure could have occurred in the tungsten, because of its brittle ness.
Thermocycling tests are very important while developing brazing processes, becaus phase transformation or a joint degradation can occur [41,42].In this work we carried ou the thermocycling test in an evacuated quartz ampoule with dynamic vacuum of p = 10 mmHg; to suppress oxygen concentration, titanium getter was also inserted into th ampoule.Samples were inserted into the ampoule and a thermocouple was as close as th samples.Previously we carried out thermocycling with cooling down by water [8,11] tha was used to make express comparison of joints, but in this work we decided to carry ou thermocycling closer to operating conditions.RAFM steel working temperature is limite to 550 °C, so we decided to heat up the joint to 600 °C, as the joints' temperature can b higher.The ampoule was heated up in a tube furnace, and after achieving 600 °C th The microstructure was investigated on the cross-sections of the brazed samples by MTI MM500T metallographic microscope (MTI Corporation, USA) and JEOL JSM-6610LV scanning electron microscope (SEM) with energy dispersive spectroscopy (EDS) INCA X-ACT (Jeol, Japan).Electron beam scattered diffraction (EBSD) analysis and ultrahigh resolution photos were obtained by means of SEM TESCAN CLARA (Tescan, The Czech Republic) equipped with EBSD Oxford Instruments Nordlys Nano and EDS Oxford Instruments Ultim MAX 100 (Oxford Instruments, UK).
The specimens were prepared using a common metallographic procedure.For metallographic microscopy the samples were etched with 20% HNO 3 + 20% HF + 60% glycerol solution, and the etching time was 1-3 s to identify the structure of the brazed seam and 20-30 s to identify the steel's microstructure.Before EBSD analysis, the samples were etched with Technoorg Linda SEMPrep2 (Technoorg, Hungary).
Microhardness HV 0.1 (load 0.9807 H, holding time 15 s) in the cross section of a brazed seam was measured by Vickers FM-800 (Future-Tech, Japan) equipment.Shear strength was measured by a Quasar50 (Galdabini, Switzerland) universal testing machine with 1 mm/min crosshead speed.The scheme of the shear test used is presented elsewhere [40].We chose the shear test to ensure that the joint will fail throughout a seam.If the tensile test had been chosen, a failure could have occurred in the tungsten, because of its brittleness.
Thermocycling tests are very important while developing brazing processes, because phase transformation or a joint degradation can occur [41,42].In this work we carried out the thermocycling test in an evacuated quartz ampoule with dynamic vacuum of p = 10 −2 mmHg; to suppress oxygen concentration, titanium getter was also inserted into the ampoule.Samples were inserted into the ampoule and a thermocouple was as close as the samples.Previously we carried out thermocycling with cooling down by water [8,11] that was used to make express comparison of joints, but in this work we decided to carry out thermocycling closer to operating conditions.RAFM steel working temperature is limited to 550 • C, so we decided to heat up the joint to 600 • C, as the joints' temperature can be higher.The ampoule was heated up in a tube furnace, and after achieving 600 • C the ampule was pulled out the furnace.Cooling lasted until 300 • C. We chose 300 • C to be close to water coolant temperature.During shut down, the First Wall will be cooled down to the coolant temperature [43].Figure 2 shows the schematic image of the thermocycling regime.Four samples were subjected to the test, and integrity of the samples was observed every 50 cycles.
In Section 3.2.2.we conducted Fenite Elemental Analysis (FEA) of a specimen to optimize its geometry for further investigation.We calculated brazed joints W/Ta/Rusfer by means of FEA in ANSYS Workbench 18.2.The mechanical and physical properties of the materials, such as Young's modulus (E), Poisson's ratio (ν), yield strength (σ 0.2 ), tangent modulus (σ tan ), stress-strain curves, and coefficient of thermal expansion (α), were taken from [8,44].Figure 3 shows the resulting dimensions of the joints.ampule was pulled out the furnace.Cooling lasted until 300 °C.We chose 300 °C to be close to water coolant temperature.During shut down, the First Wall will be cooled down to the coolant temperature [43].Figure 2 shows the schematic image of the thermocycling regime.Four samples were subjected to the test, and integrity of the samples was observed every 50 cycles.In Section 3.2.2.we conducted Fenite Elemental Analysis (FEA) of a specimen to optimize its geometry for further investigation.We calculated brazed joints W/Ta/Rusfer by means of FEA in ANSYS Workbench 18.2.The mechanical and physical properties of the materials, such as Young's modulus (E), Poisson's ratio (), yield strength ( .), tangent modulus ( ), stress-strain curves, and coefficient of thermal expansion (), were taken from [8,44].Figure 3 shows the resulting dimensions of the joints.regime.Four samples were subjected to the test, and integrity of the samples was observed every 50 cycles.In Section 3.2.2.we conducted Fenite Elemental Analysis (FEA) of a specimen to optimize its geometry for further investigation.We calculated brazed joints W/Ta/Rusfer by means of FEA in ANSYS Workbench 18.2.The mechanical and physical properties of the materials, such as Young's modulus (E), Poisson's ratio (), yield strength ( .), tangent modulus ( ), stress-strain curves, and coefficient of thermal expansion (), were taken from [8,44].Figure 3 shows the resulting dimensions of the joints.We modeled the process of cooling the assemblies from a joining temperature of 1100 °C to room temperature of 22 °C.Figure 5 shows the boundary conditions for modeling.We modeled the process of cooling the assemblies from a joining temperature of 1100 • C to room temperature of 22 • C. Figure 5 shows the boundary conditions for modeling.We modeled the process of cooling the assemblies from a joining temperature of 1100 °C to room temperature of 22 °C.Figure 5 shows the boundary conditions for modeling.

Microstructural Analysis
Figure 6 shows the micrograph of the whole as-joined sample.We obtained the image in the area close to the fillet region of the sample.No cracks or pores were observed.Rusfer/Ta seam can be divided into the following zones: (1) martensite grains, (2) ferritic grains, (3) interaction zone with sharp phases, (4) interaction zone with elongated grains, (5) pure tantalum.Formation of the ferritic zone was also observed in [15,27,45].The thickness of the layer increases closer to the fillet, because in Figure 6, a 50 μm ferritic layer formed, but in the central zone of a sample [27], this was 20 μm.In this work (Section 3.2), we present optical images of the central area of the joint, and the thickness is also close to 20-30 μm in different samples.This means that the ferritic layer is thinner while brazing with TiZr4Be compared with Cu-based brazing alloys, where the scientists observed 200 μm [11] and ≈300 μm [46].We divided the Ta/W seam into the following zones: (1) pure tantalum, (2) mechanical mixture, (3) thick dark layer, (4) pure tungsten.A thin grain boundary depletion of pure W is observed close to the Ta/TiZr4Be/W brazed seam, marked with an arrow in Figure 6.

Microstructural Analysis
Figure 6 shows the micrograph of the whole as-joined sample.We obtained the image in the area close to the fillet region of the sample.No cracks or pores were observed.Rusfer/Ta seam can be divided into the following zones: (1) martensite grains, (2) ferritic grains, (3) interaction zone with sharp phases, (4) interaction zone with elongated grains, (5) pure tantalum.Formation of the ferritic zone was also observed in [15,27,45].The thickness of the layer increases closer to the fillet, because in Figure 6, a 50 µm ferritic layer formed, but in the central zone of a sample [27], this was 20 µm.In this work (Section 3.2), we present optical images of the central area of the joint, and the thickness is also close to 20-30 µm in different samples.This means that the ferritic layer is thinner while brazing with TiZr4Be compared with Cu-based brazing alloys, where the scientists observed 200 µm [11] and ≈300 µm [46].We divided the Ta/W seam into the following zones: (1) pure tantalum, (2) mechanical mixture, (3) thick dark layer, (4) pure tungsten.A thin grain boundary depletion of pure W is observed close to the Ta/TiZr4Be/W brazed seam, marked with an arrow in Figure 6.We used EBSD and EDS analyzes to investigate the seams more prec Rusfer/TiZr4Be/Ta seams' analysis is presented in Figure 7: a-backscattered electro age, b-EBSD phase map, c-EDS maps.Because EDS analysis fails to reliably deter the concentration of light elements (Be, B, H), we do not present Be distribution.By analysis we determined that the Rusfer/TiZr4Be/Ta seam consists of bcc-Fe, ZrC, T ZrFe2 and bcc-Ta phases.The same microstructure was observed in [27], but no acc investigation was made there.A ZrC phase formed in the Fe-bcc/ZrFe2 interface, n ther appearance of it was observed, and the thickness of the phase varied between μm.Ta2Be in the form of sharp needles formed within ZrFe2.Its amount varies in the which can be related to the different gaps between base materials during brazing ZrFe2 phase itself also dissolves Ti, Cr, Ta.We presented further quantitative analy this article (Section 3.2).Elongated grains after ZrFe2 are bcc-Ta phases.According to maps, strong interaction among the brazing alloy, steel and tantalum occurred.Iron fully distributed within the interaction layer as well as titanium and zirconium.In We used EBSD and EDS analyzes to investigate the seams more precisely.Rusfer/TiZr4Be/Ta seams' analysis is presented in Figure 7: a-backscattered electron image, b-EBSD phase map, c-EDS maps.Because EDS analysis fails to reliably determine the concentration of light elements (Be, B, H), we do not present Be distribution.By EBSD analysis we determined that the Rusfer/TiZr4Be/Ta seam consists of bcc-Fe, ZrC, Ta 2 Be, ZrFe 2 and bcc-Ta phases.The same microstructure was observed in [27], but no accurate investigation was made there.A ZrC phase formed in the Fe-bcc/ZrFe 2 interface, no further appearance of it was observed, and the thickness of the phase varied between 2-10 µm.Ta 2 Be in the form of sharp needles formed within ZrFe 2 .Its amount varies in the seam, which can be related to the different gaps between base materials during brazing.The ZrFe 2 phase itself also dissolves Ti, Cr, Ta.We presented further quantitative analysis in this article (Section 3.2).Elongated grains after ZrFe 2 are bcc-Ta phases.According to EDS maps, strong interaction among the brazing alloy, steel and tantalum occurred.Iron was fully distributed within the interaction layer as well as titanium and zirconium.In addition, tantalum was distributed within the interaction layer.
Rusfer/TiZr4Be/Ta seams' analysis is presented in Figure 7: a-backscattered electron age, b-EBSD phase map, c-EDS maps.Because EDS analysis fails to reliably determ the concentration of light elements (Be, B, H), we do not present Be distribution.By EB analysis we determined that the Rusfer/TiZr4Be/Ta seam consists of bcc-Fe, ZrC, Ta2 ZrFe2 and bcc-Ta phases.The same microstructure was observed in [27], but no accur investigation was made there.A ZrC phase formed in the Fe-bcc/ZrFe2 interface, no f ther appearance of it was observed, and the thickness of the phase varied between 2 μm.Ta2Be in the form of sharp needles formed within ZrFe2.Its amount varies in the sea which can be related to the different gaps between base materials during brazing.T ZrFe2 phase itself also dissolves Ti, Cr, Ta.We presented further quantitative analysi this article (Section 3.2).Elongated grains after ZrFe2 are bcc-Ta phases.According to E maps, strong interaction among the brazing alloy, steel and tantalum occurred.Iron w fully distributed within the interaction layer as well as titanium and zirconium.In ad tion, tantalum was distributed within the interaction layer.Figure 8 shows the Ta/W seams' analysis: a-backscattered electron image, b-EB phase map, c-g-EDS maps.By EBSD analysis we determined that the Ta/TiZr4Be seam consists of bcc-Ta, Ta2Be, tetragonal-Ta (β-Ta), a solid solution based on bcc-Ti, a ZrC.Formation of ZrC can be related to the mixing of the melts between Rusfer/Ta a Ta/W seams throughout a fillet region [27] that occurs due to high wettability of the br ing alloy.The same morphology of the Ta2Be phase was observed while brazing Ta Figure 8 shows the Ta/W seams' analysis: a-backscattered electron image, b-EBSD phase map, c-g-EDS maps.By EBSD analysis we determined that the Ta/TiZr4Be/W seam consists of bcc-Ta, Ta 2 Be, tetragonal-Ta (β-Ta), a solid solution based on bcc-Ti, and ZrC.Formation of ZrC can be related to the mixing of the melts between Rusfer/Ta and Ta/W seams throughout a fillet region [27] that occurs due to high wettability of the brazing alloy.The same morphology of the Ta 2 Be phase was observed while brazing Ta to boron-nitride [38].Ta and W dissolved in the brazing alloy melt, which is required for a firm brazed joint.The bcc-Ti based layer dissolved Zr, Ta, and W, which also confirms good interaction.A magnified image of this zone is presented in Figure 9; the image was taken by ultra-high resolution SEM regime.Approximate position of the image is shown in Figure 8a.
Fine bright grains and few dendrites formed on the background of bcc-Ti.By EBSD analysis the grains were seen to be bcc-Ta.We obtained the clear image of the Kukuchi lines only while scanning a phase larger than 0.5 µm.This fine microstructure was likely to be formed during cooling the joint from 1100 • C because of Ti-Ta decay according to the phase diagram [47].We did not observe such fine grained microstructure while brazing the W-Cr-Y alloy [27].

Mechanical Characterization
This section presents the results of mechanical tests that included shear tests, thermocycling tests and microhardness measurements.

Shear Strength Tests
We measured the shear strength only for as-joined samples.Figure 10a shows the stress-displacement curves of the tested samples.All samples failed along the Rusfer/TiZr4Be/Ta seam.Average shear strength is 127 ± 20 MPa.The lowest shear strength is 80 MPa, whereas the highest is 190 MPa.The test scheme should be improved, because the relative error of 15% is believed to be high.We calculated earlier that a minimum required shear strength for W/steel joint in Water Cooled Lithium Lead blanket is 180 MPa [21], though some attempts can be made to improve the strength of the joint.Figure 10b shows the SEM image in secondary electrons of Rusfer/TiZr4Be/Ta seam after the shear test.The failure occurred throughout the Ta 2 Be phase.Existence of Ta 2 Be phase profiles on the failure surface (pointed with arrows in Figure 10b) and a crack propagated through Ta 2 Be support this assumption.Hence, the dense of this phase should be reduced to improve the shear strength.This can be made by reduction of the brazing alloy melt while using thinner foil.The Ta/TiZr4Be/W seam remained unbroken after the test; hence, it is not necessary to prevent interaction of the melts from Rusfer and W to prevent ZrC phase formation.
Metals 2021, 11, x FOR PEER REVIEW 7 o boron-nitride [38].Ta and W dissolved in the brazing alloy melt, which is required fo firm brazed joint.The bcc-Ti based layer dissolved Zr, Ta, and W, which also confir good interaction.A magnified image of this zone is presented in Figure 9; the image w taken by ultra-high resolution SEM regime.Approximate position of the image is sho in Figure 8a.Fine bright grains and few dendrites formed on the background of bcc-Ti.By EB analysis the grains were seen to be bcc-Ta.We obtained the clear image of the Kuku lines only while scanning a phase larger than 0.5 μm.This fine microstructure was lik to be formed during cooling the joint from 1100 °C because of Ti-Ta decay according boron-nitride [38].Ta and W dissolved in the brazing alloy melt, which is required for a firm brazed joint.The bcc-Ti based layer dissolved Zr, Ta, and W, which also confirms good interaction.A magnified image of this zone is presented in Figure 9; the image was taken by ultra-high resolution SEM regime.Approximate position of the image is shown in Figure 8a.Fine bright grains and few dendrites formed on the background of bcc-Ti.By EBSD analysis the grains were seen to be bcc-Ta.We obtained the clear image of the Kukuchi lines only while scanning a phase larger than 0.5 μm.This fine microstructure was likely to be formed during cooling the joint from 1100 °C because of Ti-Ta decay according to profiles on the failure surface (pointed with arrows in Figure 10b) and a crack propagated through Ta2Be support this assumption.Hence, the dense of this phase should be reduced to improve the shear strength.This can be made by reduction of the brazing alloy melt while using thinner foil.The Ta/TiZr4Be/W seam remained unbroken after the test; hence, it is not necessary to prevent interaction of the melts from Rusfer and W to prevent ZrC phase formation.

Thermocycling
We subjected four different samples to different numbers of thermocycles: as-joined, 50, 100, and 200.Degradation of the joint accumulated in the fillet region and mostly between tungsten and tantalum which is shown in Figure 11.Some cracks and detachments are observed.

Thermocycling
We subjected four different samples to different numbers of thermocycles: as-joined, 50, 100, and 200.Degradation of the joint accumulated in the fillet region and mostly between tungsten and tantalum which is shown in Figure 11.Some cracks and detachments are observed.The geometry of a sample is likely to influence the resistance against thermocycli We calculated that the stress in the fillet region could be reduced by using a tantal interlayer the same width as the tungsten and steel.Figure 12 shows the results of the F calculations.Maximum equivalent von Mises stress is located in the tungsten layer n the edge of the W/Ta contact region in both cases.Its value is 858 MPa when all th The geometry of a sample is likely to influence the resistance against thermocycling.We calculated that the stress in the fillet region could be reduced by using a tantalum interlayer the same width as the tungsten and steel.Figure 12 shows the results of the FEA calculations.Maximum equivalent von Mises stress is located in the tungsten layer near the edge of the W/Ta contact region in both cases.Its value is 858 MPa when all three layers have the same width and 1348 MPa when the tantalum layer wider.This means that the geometry with tantalum of the same width as tungsten and steel reduces the stress by 40%.The geometry of a sample is likely to influence the resistance against thermocycling.We calculated that the stress in the fillet region could be reduced by using a tantalum interlayer the same width as the tungsten and steel.Figure 12 shows the results of the FEA calculations.Maximum equivalent von Mises stress is located in the tungsten layer near the edge of the W/Ta contact region in both cases.Its value is 858 MPa when all three layers have the same width and 1348 MPa when the tantalum layer is wider.This means that the geometry with tantalum of the same width as tungsten and steel reduces the stress by 40%.Magnified and etched images with microhardness profiles are presented further.Figure 13 shows Rusfer/TiZr4Be/Ta seam.Microhardness in the layer 1 is ≈300 HV 0.1 which corresponds to thermo-treated Rusfer [48], even when thermocycling microhardness does not decrease, though the temperature higher than 550 • C negatively affects the RAFM steel's microstructure.After the thermocycling, loss of martensite structure in layer 1 occurred.The scope of this work was aimed at brazing rather than at the steels' microstructure, so we did not pay close attention to the steel.
Microhardness of ferritic grains in zone 2 is close to 170 HV 0.1 in all cases from as-joined to 200 thermo-cycled sample.No further growth of ferritic grains occurred.Ferritization and further carbide formation can be expected if the operation temperature exceeds 700 • C, because the ferritic layer forms during diffusion bonding at a temperature higher than 700 • C [45].
Interaction layer 3 is quite hard: microhardness almost reaches 800 HV 0.1 and does not decrease after thermocycling.Microhardness of the layer 4 lies between the third and fifth layer.Pure tantalum characterized with 100 HV 0.1 and did not harden after 200 thermocycles, hence no further dissolution of other components was observed.
Figure 14 shows the microstructure of the Ta/TiZr4Be/W brazed joint with the microhardness profiles.The thickness of the seam did not vary from sample to sample as was seen in the Rusfer/TiZr4Be/Ta joint.The microhardness of tantalum in layer 1 is obviously the same as in the Rusfer/TiZr4Be/Ta seam.The mechanical mixture of Ti-based solid solution with Ta 2 Be phase is close to 700 HV 0.1 , which should be related to the beryllide phase, because the third layer is softer and more characterized by 300-600 HV 0.1 .This spread of values can be related to the complex microstructure of this layer, as presented in Figure 6.The microhardness of pure tungsten is ≈420 HV 0.1 .The microhardness in this joint is higher than for the joints with vanadium interlayer and amorphous Cu-based brazing alloy, where the microhardness in the interaction zone lies in the range between 100-400 HV 0.1 [40].Thermocycling did not lead to any change in the microhardness qualitative and quantitative profile.
Magnified and etched images with microhardness profiles are presented further.Figure 13 shows Rusfer/TiZr4Be/Ta seam.Microhardness in the layer 1 is ≈300 HV0.1 which corresponds to thermo-treated Rusfer [48], even when thermocycling microhardness does not decrease, though the temperature higher than 550 °C negatively affects the RAFM steel's microstructure.After thermocycling, loss of martensite structure in layer 1 occurred.The scope of this work was aimed at brazing rather than at the steels' microstructure, so we did not pay close attention to the steel.Microhardness of ferritic grains in zone 2 is close to 170 HV0.1 in all cases from asjoined to 200 thermo-cycled sample.No further growth of ferritic grains occurred.Ferritization and further carbide formation can be expected if the operation temperature exceeds 700 °C, because the ferritic layer forms during diffusion bonding at a temperature higher than 700 °C [45].
Interaction layer 3 is quite hard: microhardness almost reaches 800 HV0.1 and does not decrease after thermocycling.Microhardness of the layer 4 lies between the third and fifth layer.Pure tantalum characterized with 100 HV0.1 and did not harden after 200 thermocycles, hence no further dissolution of other components was observed.
Figure 14 shows the microstructure of the Ta/TiZr4Be/W brazed joint with the microhardness profiles.The thickness of the seam did not vary from sample to sample as was seen in the Rusfer/TiZr4Be/Ta joint.The microhardness of tantalum in layer 1 is obviously the same as in the Rusfer/TiZr4Be/Ta seam.The mechanical mixture of Ti-based solid solution with Ta2Be phase is close to 700 HV0.1, which should be related to the beryllide phase, because the third layer is softer and more characterized by 300-600 HV0.1.This spread of values can be related to the complex microstructure of this layer, as presented in Figure 6.The microhardness of pure tungsten is ≈420 HV0.1.The microhardness in this joint is higher than for the joints with vanadium interlayer and amorphous Cu-based brazing alloy, where the microhardness in the interaction zone lies in the range between 100-400 HV0.1 [40].Thermocycling did not lead to any change in the microhardness qualitative and quantitative profile.Comparing with Rusfer/V/W joints obtained using Cu-Ti [11] and Cu-Ge [40] rapidly solidified into foil brazing alloys, microhardness values in the Rusfer/TiZrBe/Ta/TiZrBe/W joint were higher.
We carried out EDS analysis of the phases forming the seams to check if the thermocycling affects the phase composition.SEM images of the as-joined and 200 thermo-cycled seams are presented in Figure 15 (Rusfer/Ta) and Figure 16 (Ta/W).Table 1 presents the quantitative analysis of the points.Comparing with Rusfer/V/W joints obtained using Cu-Ti [11] and Cu-Ge [40] rapidly solidified into foil brazing alloys, microhardness values in the Rusfer/TiZrBe/Ta/TiZrBe/W joint were higher.
We carried out EDS analysis of the phases forming the seams to check if the thermocycling affects the phase composition.SEM images of as-joined and 200 thermo-cycled seams are presented in Figure 15 (Rusfer/Ta) and Figure 16 (Ta/W).Table 1 presents the quantitative analysis of the points.Figure 15a shows the as-joined Rusfer/Ta seam (Figure 15b) after 200 thermocy The compositions of 2-6 points are an average number collected from at least three m urements, and the composition of the 1 point is a measurement by a square zone, outl in Figure 15.Composition of the steel (point 1) did not change after thermocycling, h   Figure 15a shows the as-joined Rusfer/Ta seam (Figure 15b) after 200 therm Figure 15a shows the as-joined Rusfer/Ta seam (Figure 15b) after 200 thermocycles.The compositions of 2-6 points are an average number collected from at least three measurements, and the composition of the 1 point is a measurement by a square zone, outlined in Figure 15.Composition of the steel (point 1) did not change after thermocycling, hence no further diffusion from the seam observed.The ZrC phase (point 2) differs mostly with Si, which could have been dissolved from the steel.Compared with the as-joined composition of the Ta 2 Be phase (point 3), Zr and Cr start to dissolute more in the needles.The ZrFe 2 (point 4) phase also dissolves Ti, Ta and Cr.It is hard to conclude whether the compositions differ because of thermocycling, or because of local heterogeneity.The same occurs for the fifth and the sixth points, because on EDS maps (Figure 7) the contrast of the components varies.
Figure 16a shows the as-joined Ta/TiZr4B/W seam, and Figure 16b after 200 thermocycles.The compositions of 1-6 points are an average number collected from at least three measurements.Point 1 is pure Ta for both samples.In this seam we can confidently claim that no further erosion of Ta was observed during 200 thermocycles, because the thickness and morphology of layer 2 are the same.Tantalum in point 2 dissolved a different amount of Ti, which corresponds with the Ta-Ti [47] phase diagram, but did not dissolve Zr.Ta and Ti have mutual solubility, whereas Ta-Zr only form a mechanical mixture at low temperatures [49].The Ta 2 Be phase (point 3) remained the same in its morphology and composition after 200 thermocycles, as as the Ti-based solid solution (point 4).The β-Ta (point 5) has a slightly different composition in the as-joined and 200 thermo-cycled samples, but still based on the tantalum solid solution.Pure tungsten (point 6) remained pure after thermocycling.
Therefore, the morphology and composition of the brazed joint did not change after 200 thermocycles in a range between 300-600 • C.
Shear strength of the as-joined composition is 127 ± 20 MPa.Failure occurs along Rusfer/Ta seam throughout the Ta 2 Be phase.
Thermocycling tests were carried out in a vacuum in the temperature range between 300-600 • C (V heating = 5 • C/min, V cooling = 2 • C/min).After thermocycling, neither morphology nor composition of the phases in the seams changed, no did microhardness.Degradation of samples occurred in the fillet region, but the samples remained integrated after 200 thermocycles.Stresses in the fillet region can be reduced by using tantalum of the same width as the tungsten and steel.
TiZr4Be brazing alloy seems to be prospective in the DEMO application; however, further improvement of the Rusfer/TiZr4Be/Ta seam is needed.This can be processed with a reduction of the Ta 2 Be phase.

Figure 1 .
Figure 1.Schematic view of a brazed specimen (dimensions in mm): (a) the sample for microstructural observation; (b) the shear test sample.

Figure 1 .
Figure 1.Schematic view of a brazed specimen (dimensions in mm): (a) the sample for microstructural observation; (b) the shear test sample.

Figure 3 .
Figure 3.The dimensions of the first (a) and second (b) brazed joints for thermocycling tests.

Figure 4
Figure4shows the generated mesh .The element size in the tantalum layer and near both contact regions is 0.01 mm.The element size in the tungsten and Rusfer layers is 0.05 mm.

Figure 3 .
Figure 3.The dimensions of the first (a) and second (b) brazed joints for thermocycling tests.

Figure 4
Figure4shows the generated mesh .The element size in the tantalum layer and near both contact regions is 0.01 mm.The element size in the tungsten and Rusfer layers is 0.05 mm.

Figure 3 .
Figure 3.The dimensions of the first (a) and second (b) brazed joints for thermocycling tests.

Figure 4 Figure 4 .
Figure 4 shows the generated mesh.The element size in the tantalum layer and near both contact regions is 0.01 mm.The element size in the tungsten and Rusfer layers is 0.05 mm.Metals 2021, 11, x FOR PEER REVIEW 5 of 16

Figure 4 .
Figure 4.The mesh of the first (a) and second (b) models.Only the right halves of the symmetric assemblies are depicted.

Figure 4 .
Figure 4.The mesh of the first (a) and second (b) models.Only the right halves of the symmetric assemblies are depicted.

Figure 5 .
Figure 5.The boundary conditions for the first (a) and second (b) FEA models.

Figure 5 .
Figure 5.The boundary conditions for the first (a) and second (b) FEA models.
Metals 2021, 11, x FOR PEER REVIEW

Figure 9 .
Figure 9. Magnified image of the zone outlined by the rectangle in Figure 8a in the Ta/TiZr4Be/W seam.

Figure 12 .
Figure 12.Contour plots of the equivalent von Mises stress distributions after cooling the first (a) and second (b) assemblies.Only the right halves of the symmetric assemblies are depicted.Figure 12. Contour plots of the equivalent von Mises stress distributions after cooling the first (a) and second (b) assemblies.Only the right halves of the symmetric assemblies are depicted.

Figure 12 .
Figure 12.Contour plots of the equivalent von Mises stress distributions after cooling the first (a) and second (b) assemblies.Only the right halves of the symmetric assemblies are depicted.Figure 12. Contour plots of the equivalent von Mises stress distributions after cooling the first (a) and second (b) assemblies.Only the right halves of the symmetric assemblies are depicted.