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Metals, Volume 14, Issue 3 (March 2024) – 117 articles

Cover Story (view full-size image): A gradient nanostructured surface layer was successfully fabricated on the TC4 Titanium alloy via USP technology. The surface microhardness was elevated from 330 HV to 438 HV with a penetrating depth of around 900 μm after USP. EBSD characterization results confirmed the presence of high-density grain boundaries and dislocation density within the gradient structure within the region of 0–200 μm. TEM characterization indicated a substantial amount of nanograin with an average size of 74.58 nm. The surface strengthening effect was predicted. The calculated maximum residual stress reached 973 MPa after multi-ball impact. The impact behavior of the shots was studied. View this paper
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11 pages, 3266 KiB  
Article
Mechanical Properties of a Structural Component Processed in High-Pressure Die Casting (HPDC) with a Non-Heat-Treated Aluminum Alloy
by David Servando Cantú-Fernández, José Jaime Taha-Tijerina, Alejandro González, Pablo Guajardo Hernández and Brian Quinn
Metals 2024, 14(3), 369; https://doi.org/10.3390/met14030369 - 21 Mar 2024
Cited by 1 | Viewed by 1839
Abstract
This industrial research focuses on the implementation and development of a productive process for an automotive structural component (Shock tower) manufactured by a high-pressure die casting (HPDC) process made of aluminum alloy AuralTM-5. This aluminum alloy has been considered in diverse [...] Read more.
This industrial research focuses on the implementation and development of a productive process for an automotive structural component (Shock tower) manufactured by a high-pressure die casting (HPDC) process made of aluminum alloy AuralTM-5. This aluminum alloy has been considered in diverse automotive and aerospace components that do not require heat treatment due to its mechanical properties as cast material (F temper). On the other hand, AuralTM-5 has been designed for processing as HPDC because it is an alloy with good fluidity, making it ideal for large castings with thin-wall thicknesses, like safety structural components such as rails, supports, rocker panels, suspension crossmembers, and shock towers. The mechanical properties that were evaluated for the evaluated components were yield strength, ultimate tensile strength, and elongation. Eight samples were taken from different areas of each produced shock tower for evaluating and verifying the homogeneity of each casting. The samples were evaluated from the first hours after they were manufactured by casting until eight weeks after being produced. This was performed to understand the behavior of the alloy during its natural aging process. Two groups of samples were obtained. One set of components was heat-treated by a water quench process after the castings’ extraction and the other set of components was not quenched. Results demonstrated that both sets of components, quenched and not quenched, achieved the expected values for the AuralTM-5 of yield strength ≥ 110 MPa, ultimate tensile strength ≥ 240 MPa, and elongation ≥ 8%. Additionally, this is very important for industry since by not treating the structural components by quenching, there are savings in terms of infrastructure and energy consumption, together with benefits in the environmental aspect by avoiding CO2 emissions and being sustainable. Full article
(This article belongs to the Section Metal Casting, Forming and Heat Treatment)
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<p>Model of the <span class="html-italic">shock tower</span> component.</p>
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<p>Specification of the specimens that were taken from the shock tower (units in mm).</p>
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<p>Schematic of the Shock tower component showing the position where the tensile coupons were obtained and areas for evaluations.</p>
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<p>Mechanical properties of elongation with and without quenching.</p>
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<p>Mechanical properties of yield strength with and without quenching.</p>
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<p>Mechanical properties of tensile strength with and without quenching.</p>
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<p>Examples of porosity in samples tested for mechanical properties.</p>
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<p>Shock towers were analyzed by X-ray technique, showing no porosity or internal defects.</p>
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<p>Results of blister test, none of the casting had an air trap.</p>
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20 pages, 11267 KiB  
Article
The Angular Velocity as a Function of the Radius in Molten Ga75In25 Alloy Stirred Using a Rotation Magnetic Field
by András Roósz, Arnold Rónaföldi, Mária Svéda and Zsolt Veres
Metals 2024, 14(3), 368; https://doi.org/10.3390/met14030368 - 21 Mar 2024
Viewed by 959
Abstract
The simulation of the solidification of alloys (like steel or aluminium alloys), which is carried out by using the melt flow induced by a rotation magnetic field (RMF), needs the correct angular velocity vs. the radius function of the melt. Because it is [...] Read more.
The simulation of the solidification of alloys (like steel or aluminium alloys), which is carried out by using the melt flow induced by a rotation magnetic field (RMF), needs the correct angular velocity vs. the radius function of the melt. Because it is impossible to directly obtain information about the melt flow from industrial casting, this information can only be obtained from well-monitored experiments using low-melting-point metals or alloys (e.g., Hg, Ga, GaIn, and GaInSn). In this work, we first summarized the measuring methods that are suitable for determining this function and analysed their advantages and disadvantages. All of them disturb, to some degree, the melt flow, except for the Pressure Compensation Method (PCM); therefore, this method was used in the experiments. Closed TEFLON crucibles with a 60 mm length and 12.5 mm radius and Ga75wt%In25wt% alloy was used. The angular velocity (ω) was calculated from the compensation pressure measured at r = 5, 7.5, 10, and 12.5 mm in the 0–90 mT range of magnetic induction, B. Based on the ω(B, r) dataset, a suitable ω(B, r) function was determined for the simulation. Full article
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Figure 1
<p>A sketch of the free surface of the rotating melt if h &gt;&gt; R (the aspect ratio is higher than 6).</p>
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<p>Glass ampulla (a) and glass “turbine” (b), “shaft + turbine blade” (b and c), and complete measuring unit (d)</p>
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<p>Picture of process of determining Rpm of molten gallium.</p>
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<p>A sketch of the measuring possibilities with the turbine blade in a bigger crucible; 1: inductor; 2: turbine blades in 3 different positions of the crucible.</p>
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<p>Sketch of turbine (version B); 1: inductor, 2: turbine blades, 3: shaft of turbine blades, 4: glass crucible, 5: fixing wheel, 6: crucible cover.</p>
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<p>Sketch of facility using conductive anemometer with its own magnetic field; 1: inductor, 2: permanent magnet, 3: ceramic tube, 4: nano-voltmeter, 5: crucible.</p>
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<p>Developing the melt level difference, Δh, in the gauges connected to the closed crucible. The melt levels before (<b>A</b>) and after (<b>B</b>) the switch on the inductor; 1: closed crucible, 2: inductors, a and b: the two gauges connected to the closed crucible, L is the height and R is the crucible’s radius.</p>
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<p>1: Closed crucible; 2: inductors; a and b: the two gauges connected to the closed crucible; c: manometer.</p>
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<p>Compensation of melt levels by p<sub>comp</sub> pressure in gauges. 1: Closed crucible; 2: inductors; a and b: the two gauges connected to the closed crucible.</p>
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<p>A sketch of the new type of crucibles. The “a” gauge is at the centre of the crucible, the “b1” gauge is in three different positions, and the “b2” gauge is at the wall of the crucible.</p>
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<p>Four crucibles with 2 mm diameter holes. The distances from the axis are (<b>a</b>) 5 mm, (<b>b</b>) 7.5 mm, (<b>c</b>) 10 mm, and (<b>d</b>) 12.5 mm. The black and yellow arrows show the holes.</p>
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<p>A sketch of the two measuring methods. (<b>a</b>) The measuring hole is across the crucible’s cover; (<b>b</b>) the measuring hole is at the crucible’s wall.</p>
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<p>A comparison of the angular velocity measured using the two methods.</p>
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<p>The measured p<sub>comp</sub> is a function of magnetic induction.</p>
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<p>(<b>a</b>) The measured azimuthal and (<b>b</b>) angular velocities as functions of magnetic induction.</p>
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<p>(<b>a</b>) The measured azimuthal and (<b>b</b>) angular velocities as functions of the radius.</p>
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<p>Graphical calculation of the stationary angular velocity (ω(st)) at two different radiuses.</p>
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<p>(<b>a</b>) The calculated ω(st) vs. the radius; (<b>b</b>) a comparison of the measured and calculated ω(st) values.</p>
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<p>(<b>a</b>) Y as a function of magnetic induction (B) at five different radiuses (r); (<b>b</b>) f(r) as a function of r.</p>
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<p>(<b>a</b>) The calculated angular velocity as a function of the radius at five magnetic inductions. (<b>b</b>) The calculated azimuthal velocity as a function of the radius at five magnetic inductions.</p>
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<p>Comparison of measured and calculated angular velocities.</p>
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<p>(<b>a</b>) The calculated angular velocity as a function of a wide range of magnetic inductions at five radiuses. (<b>b</b>) The calculated azimuthal velocity as a function of a wide range of magnetic inductions at five radiuses.</p>
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23 pages, 15689 KiB  
Article
Steel Sheet Deformation in Clinch-Riveting Joining Process
by Waldemar Witkowski, Jacek Mucha and Łukasz Boda
Metals 2024, 14(3), 367; https://doi.org/10.3390/met14030367 - 21 Mar 2024
Cited by 1 | Viewed by 1088
Abstract
This paper presents the deformation of a joined sheet after the clinch riveting process. The DX51D steel sheet with zinc coating was used. The samples to be joined with clinch riveting technology had a thickness of 1 ± 0.05 mm and 1.5 ± [...] Read more.
This paper presents the deformation of a joined sheet after the clinch riveting process. The DX51D steel sheet with zinc coating was used. The samples to be joined with clinch riveting technology had a thickness of 1 ± 0.05 mm and 1.5 ± 0.1 mm. The sheet deformation was measured before and after the joining process. The rivet was pressed in the sheets with the same dimension between the rivet axis and three sheet edges: 20, 30, and 40 mm. For fixed segments of the die, from the rivet side close to the rivet, the sheet deformation was greater than that of the area with movable segments. The movement of the die’s sliding element caused more sheet material to flow in the space between the fixed part of the die and movable segments. Hence, the sheet deformation in these places was smaller than for the die’s fixed element—the sheet material was less compressed. For sheet thickness values of 1.5 mm and a width value of 20 mm, the bulk of the sheet was observed. For a sheet width of 20 mm, it was observed that the deformation of the upper and lower sheets in the area of the rivet was greater than for sheet width values of 30 or 40 mm. Full article
(This article belongs to the Special Issue New Technology of Welding/Joining of Metallic Materials)
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<p>Example of the clinch joint formed close to the sheets edge: (<b>a</b>) aluminum alloy sheets; (<b>b</b>) thin stainless steel sheet and thick carbon steel sheet.</p>
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<p>The characteristics of sheet deformation in clinch riveting process (<b>a</b>) before joining, (<b>b</b>) after punch retract, and (<b>c</b>) after die retract.</p>
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<p>The C-frame stand for forming CR joints: (<b>a</b>) C-frame machine; (<b>b</b>) cross-section of the punch system with rivet feeder.</p>
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<p>The basic forming tools used in clinch riveting technology: (<b>a</b>) die, (<b>b</b>) punch system, and (<b>c</b>) rivet.</p>
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<p>The force–displacement diagram of clinch riveting process.</p>
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<p>The sample and measuring area dimensions: (<b>a</b>) before joining; (<b>b</b>) after joining.</p>
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<p>The scheme of the measurements: (<b>a</b>) position of the movable segments of the die; (<b>b</b>) radius dimensions; (<b>c</b>) angles for joint cross-sections.</p>
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<p>The measurement stand with 3D ATOS Capsule scanner.</p>
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<p>The summary of the performed measurement series, with a specification of one shot as comprising 2 photos.</p>
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<p>The measurement coordinate system (<b>a</b>) and elements used for determining and positioning axis system (<b>b</b>).</p>
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<p>The force–displacement diagrams of clinch riveting process for one sample combination (seven samples, <span class="html-italic">b</span> = 20 mm, <span class="html-italic">t</span> = 1 mm)—diagrams move by each other at a distance of 0.5 mm.</p>
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<p>The comparison of the force–displacement diagrams of clinch riveting process.</p>
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<p>The comparison of joint interlocks (<span class="html-italic">α</span> = 90°): (<b>a</b>) 20 mm × 1 mm, (<b>b</b>) 20 mm × 1.5 mm, (<b>c</b>) 30 mm × 1 mm, (<b>d</b>) 30 mm × 1.5 mm, (<b>e</b>) 40 mm × 1 mm, and (<b>f</b>) 40 mm × 1.5 mm.</p>
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<p>The results of the sheet deviation before joining.</p>
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<p>Sample of the mesh grid (<b>a</b>) and the measurement mesh defects close to the punch–sheet contact area (<b>b</b>) points 1–5 are the places where light reflections occurred.</p>
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<p>Samples of the sheet deformations with clinch-rivet joints for sheet width <span class="html-italic">b</span> and thickness <span class="html-italic">t</span>: (<b>a</b>) 20 mm × 1 mm, (<b>b</b>) 20 mm × 1.5 mm, (<b>c</b>) 30 mm × 1 mm, (<b>d</b>) 30 mm × 1.5 mm, (<b>e</b>) 40 mm × 1 mm, and (<b>f</b>) 40 mm × 1.5 mm.</p>
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<p>Samples of the sheet deformations with clinch-rivet joints for sheet width <span class="html-italic">b</span> and thickness <span class="html-italic">t</span>: (<b>a</b>) 20 mm × 1 mm, (<b>b</b>) 20 mm × 1.5 mm, (<b>c</b>) 30 mm × 1 mm, (<b>d</b>) 30 mm × 1.5 mm, (<b>e</b>) 40 mm × 1 mm, and (<b>f</b>) 40 mm × 1.5 mm.</p>
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<p>The scheme of the sheet material flow in CR joining process.</p>
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<p>Example of sheet deformation in a clinch-rivet joint (sheet thickness <span class="html-italic">t</span> = 1.5 mm, sheet width <span class="html-italic">b</span> = 20 mm): (<b>a</b>) real view from the die side; (<b>b</b>) view from punch side of the joint CAD model.</p>
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<p>Profiles of the sheets: (<b>a</b>) <span class="html-italic">α</span> = 0° and <span class="html-italic">α</span> = 180°; (<b>b</b>) α = 45° and <span class="html-italic">α</span> = 225°; (<b>c</b>) <span class="html-italic">α</span> = 90° and <span class="html-italic">α</span> = 270°.</p>
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<p>Profiles of the sheets: (<b>a</b>) <span class="html-italic">α</span> = 0° and <span class="html-italic">α</span> = 180°; (<b>b</b>) α = 45° and <span class="html-italic">α</span> = 225°; (<b>c</b>) <span class="html-italic">α</span> = 90° and <span class="html-italic">α</span> = 270°.</p>
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<p>Profiles of the sheet with 1.5 mm thickness (<span class="html-italic">α</span> = 45°): (<b>a</b>) half of the cross-section, (<b>b</b>) 10× zoom in y axis of A area.</p>
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<p>Profiles of the sheet with 1.0 mm thickness (<span class="html-italic">α</span> = 45°): (<b>a</b>) half of the cross-section; (<b>b</b>) 10× zoom in y axis of A area.</p>
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<p>Profiles of the sheet with 20 mm width and angles <span class="html-italic">α</span> = 45° and <span class="html-italic">α</span> = 225° (sheet thickness 1.5 mm—green line and 1 mm—red line).</p>
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<p>Profiles of the sheet with 20 mm width (<span class="html-italic">α</span> = 0°—green line and <span class="html-italic">α</span> = 45°—red line).</p>
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12 pages, 3777 KiB  
Article
MgAl Oxide Coatings Modified with CeO2 Particles Formed by Plasma Electrolytic Oxidation of AZ31 Magnesium Alloy: Photoluminescent and Photocatalytic Properties
by Stevan Stojadinović and Nenad Radić
Metals 2024, 14(3), 366; https://doi.org/10.3390/met14030366 - 21 Mar 2024
Cited by 1 | Viewed by 1074
Abstract
MgAl oxide coatings composed of MgO and MgAl2O4 phases were doped with CeO2 particles via plasma electrolytic oxidation (PEO) of AZ31 magnesium alloy in a 5 g/L NaAlO2 water solution. Subsequently, particles of CeO2 up to 8 [...] Read more.
MgAl oxide coatings composed of MgO and MgAl2O4 phases were doped with CeO2 particles via plasma electrolytic oxidation (PEO) of AZ31 magnesium alloy in a 5 g/L NaAlO2 water solution. Subsequently, particles of CeO2 up to 8 g/L were added. Extensive investigations were conducted to examine the morphology, the chemical and phase compositions, and, most importantly, the photoluminescent (PL) properties and photocatalytic activity (PA) during the photodegradation of methyl orange. The number of CeO2 particles incorporated into MgAl oxide coatings depends on the concentration of CeO2 particles in the aluminate electrolyte. However, the CeO2 particles do not significantly affect the thickness, phase structure, or surface morphology of the coatings. The PL emission spectrum of MgAl oxide coatings is divided into two bands: one in the 350–600 nm range related to structural defects in MgO, and another much more intense band in the 600–775 nm range attributed to the F+ centres in MgAl2O4. The incorporated CeO2 particles do not have a significant effect on the PL intensity of the band in the red spectral region, but the PL intensity of the first band increases with the concentration of CeO2 particles. The PA of MgAl/CeO2 oxide coatings is higher than that of pure MgAl oxide coatings. The MgAl/CeO2 oxide coating developed in aluminate electrolyte with a concentration of 2 g/L CeO2 particles exhibited the highest PA. The MgAl/CeO2 oxide coatings remained chemically and physically stable across multiple cycles, indicating their potential for applications. Full article
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<p>Voltage–time curves during anodization in 5 g/L NaAlO<sub>2</sub> without and with 8 g/L of CeO<sub>2</sub> particles.</p>
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<p>(<b>a</b>) Top view and (<b>b</b>) cross-section micrographs of coatings formed in 5 g/L NaAlO<sub>2</sub> by adding CeO<sub>2</sub> particles in concentrations of (<b>i</b>) 0 g/L; (<b>ii</b>) 1 g/L; (<b>iii</b>) 2 g/L; (<b>iv</b>) 4 g/L; (<b>v</b>) 8 g/L.</p>
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<p>(<b>a</b>) XRD patterns and (<b>b</b>) Raman spectra of coatings formed in 5 g/L NaAlO<sub>2</sub> with varying concentrations of CeO<sub>2</sub> particles.</p>
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<p>PL excitation and emission spectra of MgO/MgAl<sub>2</sub>O<sub>4</sub> coatings: (<b>a</b>) λ<sub>ex</sub> = 265 nm, λ<sub>em</sub> = 720 nm; (<b>b</b>) λ<sub>ex</sub> = 340 nm, λ<sub>em</sub> = 410 nm.</p>
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<p>PL spectra of MgO/MgAl<sub>2</sub>O<sub>4</sub>/CeO<sub>2</sub> coatings formed in 5 g/L NaAlO<sub>2</sub> with varying concentrations of CeO<sub>2</sub> particles: (<b>a</b>) emission spectra excited at 265 nm; (<b>b</b>) emission spectra excited at 340 nm; (<b>c</b>) excitation spectra monitored at 720 nm; (<b>d</b>) excitation spectra monitored at 410 nm; (<b>e</b>) excitation spectra monitored at 520 nm.</p>
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<p>(<b>a</b>) PA and (<b>b</b>) first-order kinetic plots of coatings formed in 5 g/L NaAlO<sub>2</sub> with varying concentrations of CeO<sub>2</sub> particles.</p>
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<p>DRS spectra of CeO<sub>2</sub> particles and coatings formed in 5 g/L NaAlO<sub>2</sub> with varying concentrations of CeO<sub>2</sub> particles added.</p>
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<p>(<b>a</b>) MO photodegradation recycling experiment; (<b>b</b>) SEM micrographs before and after 10 cycles; and (<b>c</b>) XRD patterns before and after 10 cycles of a coating formed in 5 g/L NaAlO<sub>2</sub> + 2 g/L CeO<sub>2</sub>.</p>
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11 pages, 4481 KiB  
Article
Effect of Coiling Temperature on Microstructure and Properties of Ferritic-Bainitic Dual-Phase Steels
by Zhengrong Li, Feng Zhou, Jinhai Liu, Lei Liu, Chuangwei Wang and Zhengzhi Zhao
Metals 2024, 14(3), 365; https://doi.org/10.3390/met14030365 - 21 Mar 2024
Viewed by 1074
Abstract
In this study, a 780 MPa grade ferritic-bainitic dual-phase steel with excellent matching of strength-plasticity and formability was developed using thermomechanical control processing. Optical microscopy, Scanning electron microscopy, and Electron Backscatter Diffraction techniques were used to characterize the microstructure comprehensively, and the effects [...] Read more.
In this study, a 780 MPa grade ferritic-bainitic dual-phase steel with excellent matching of strength-plasticity and formability was developed using thermomechanical control processing. Optical microscopy, Scanning electron microscopy, and Electron Backscatter Diffraction techniques were used to characterize the microstructure comprehensively, and the effects of coiling temperature on the microstructure, the strength-plasticity, and hole-expansion ratio of the test steels were thoroughly investigated. The results showed that the test steel had an excellent combination of ferrite and bainite at the coiling temperature of 520 °C, 23.7 and 76.3%, respectively, with a hole expansion ratio of 58.5 ± 2.8%. The uniformity of the microstructure was the key to obtaining a high expansion ratio in ferrite-bainite dual-phase steels. The test steels formed granular bainite at low-temperature coiling, while polygonal ferrite was promoted at high-temperature coiling. The effect of coiling temperature on grain size is small. Dislocations were redistributed during high-temperature coiling, resulting in a decrease in dislocation density. The higher elongation and hole expansion rate at higher coiling temperatures were attributed to increased polygonal ferrite content, reduced grain size, and enhanced TRIP effect. When coiling at low temperatures, the agglomeration of polygonal ferrite or granular bainite tends to result in a non-uniform distribution of the soft and hard phases of the matrix. At the same time, the strong texture parallel to the rolling direction has a significant difference in plasticity in different directions, leading to non-uniform deformation, which is liable to stress concentration, causing crack nucleation and extension in the hole expanding process, thus reducing the hole expansion performance. Full article
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<p>Schematic diagram of the TMCP for test steel.</p>
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<p>Tensile specimen machining schematic.</p>
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<p>Schematic diagrams of the punching and hole-expanding test.</p>
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<p>Optical microstructure of test steel at coiling temperatures 480 °C and 520 °C. (<b>a</b>) CT of 480 °C; (<b>b</b>) CT of 520 °C.</p>
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<p>SEM micrographs of test steel at coiling temperatures of 480 °C and 520 °C: (<b>a</b>,<b>c</b>) are SEM micrographs at coiling temperatures of 480 °C and 520 °C, respectively; (<b>b</b>,<b>d</b>) are the local magnification of the rectangle region marked by the white line in (<b>a</b>,<b>c</b>), respectively.</p>
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<p>GOS, GNDdensity, and IPF maps of test steels at coiling temperatures of 480 °C and 520 °C. (<b>a1</b>–<b>a3</b>) 480 °C; (<b>b1</b>–<b>b3</b>) 520 °C; (<b>a1</b>,<b>b1</b>) are GOS maps, (<b>a2</b>,<b>b2</b>) are GND density maps, (<b>a3</b>,<b>b3</b>) are IPF maps.</p>
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<p>The fine structure of PF and granular bainite in region I. (<b>a</b>) IPF map; (<b>b</b>) GOS map; (<b>c</b>) GND density map.</p>
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<p>BCC and FCC crystal structures of test steels at coiling temperatures of 480 °C and 520 °C. (<b>a</b>) 480 °C; (<b>b</b>) 520 °C; red represents BCC crystal structure and green represents FCC crystal structure.</p>
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13 pages, 7906 KiB  
Article
The Study on Corrosion Resistance of Ti-6Al-4V ELI Alloy with Varying Surface Roughness in Hydrofluoric Acid Solution
by Han Wang, Quanshi Cheng, Zhuo Chang, Kedi Wang, Xuemin Gao and Xueling Fan
Metals 2024, 14(3), 364; https://doi.org/10.3390/met14030364 - 20 Mar 2024
Viewed by 1134
Abstract
The corrosion resistance of titanium alloy poses a crucial challenge, significantly affecting its prospect for service and application. The present study aimed to investigate the corrosion resistance of Ti-6Al-4V ELI alloys with varying surface roughness in hydrofluoric acid solution, in order to assess [...] Read more.
The corrosion resistance of titanium alloy poses a crucial challenge, significantly affecting its prospect for service and application. The present study aimed to investigate the corrosion resistance of Ti-6Al-4V ELI alloys with varying surface roughness in hydrofluoric acid solution, in order to assess the influence of roughness on their corrosion resistance performance. The weight loss percentage, surface morphology evolution, and roughness variation of Ti-6Al-4V ELI alloys before and after exposure to hydrofluoric acid corrosion were characterized. While the weight loss and weight loss percentage of the Ti-6Al-4V ELI alloy increased with prolonged corrosion, the overall weight loss rate decreased. The accumulation of TiF3 phases and depletion of the Ti-6Al-4V ELI matrix mutually led to the alterations of the surface roughness. Due to the inability to prevent fluoride ions from contacting with the Ti-6Al-4V ELI alloy, continuous corrosion occurred in hydrofluoric acid. Based on these experimental results and analysis, the corrosion mechanism of the Ti-6Al-4V ELI alloy corroded by hydrofluoric acid solution was elucidated. Furthermore, an analysis was conducted to explore the influence of corrosion time on mechanical properties by analyzing the decay in compressive properties of the Ti-6Al-4V ELI titanium alloy after hydrofluoric acid corrosion treatment. The bearing capacity of the Ti-6Al-4V ELI alloy deteriorated over the corrosion time. Full article
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<p>The illustration of the corrosion experiment and specimens of Ti-6Al-4V ELI alloy with different surface roughness.</p>
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<p>(<b>a</b>) Weight loss, (<b>b</b>) weight loss percentage, and (<b>c</b>) weight loss rate of specimens with different surface states at various HF solution corrosion times.</p>
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<p>The surface roughness indexes (<b>a</b>) <span class="html-italic">Sa</span> and (<b>b</b>) <span class="html-italic">Sq</span> of Ti-6Al-4V ELI alloy before and after corrosion.</p>
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<p>The surface morphology of Ti-6Al-4V ELI alloy before and after corrosion observed by WLI.</p>
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<p>The XRD pattern of the Ti-6Al-4V ELI alloy specimens before and after HF solution corrosion.</p>
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<p>The surface microstructure and morphology of Ti-6Al-4V ELI alloy specimens before and after corrosion observed by SEM.</p>
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<p>The surface microstructure and morphology of Ti-6Al-4V ELI alloy specimens before and after corrosion observed by AFM.</p>
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<p>The depiction of corrosion mechanism of Ti-6Al-4V ELI alloy when exposed to an HF solution.</p>
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<p>(<b>a</b>) The compression force–displacement curves and (<b>b</b>) the stress–strain curves of Ti-6Al-4V ELI alloy before and after corrosion.</p>
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<p>(<b>a</b>) The quasi-static compression processes and (<b>b</b>) the specimen diameter variation of Ti-6Al-4V ELI alloy before and after corrosion.</p>
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17 pages, 7347 KiB  
Article
Effects of Different CaO/Al2O3 Ratios on the Phase Composition and Desulfurization Ability of CaO-Based Desulfurizers in Hot Metal
by Jyun-Ming Shen, Chi-Ming Lin, Yu-En Chang, Hui-Jan Lin and Weite Wu
Metals 2024, 14(3), 363; https://doi.org/10.3390/met14030363 - 20 Mar 2024
Viewed by 1038
Abstract
In response to the development of low-carbon smelting technology, reducing the use of fluor-containing materials in desulfurizers is an important research topic. The development of new-generation KR (Kambara Reactor) desulfurizers is shifting towards a higher Al2O3 content rather than CaF [...] Read more.
In response to the development of low-carbon smelting technology, reducing the use of fluor-containing materials in desulfurizers is an important research topic. The development of new-generation KR (Kambara Reactor) desulfurizers is shifting towards a higher Al2O3 content rather than CaF2, yet there is currently an absence of thorough and comprehensive mechanisms for desulfurization. Consequently, this research provides an extensive comparison using a specially constructed small-scale KR desulfurization hot model test, alongside FactSage simulation and SEM analysis (of desulfurization process). The findings indicate that at 1400 °C, for the desulfurization of molten iron, the capacity for desulfurization initially increases and then diminishes as the Al2O3 content in the KR desulfurizer rises. With Al2O3 content in the desulfurizer below 22 wt.%, the phase composition predominantly consists of C3A, employing a solid(slag)–liquid(metal) diffusion method for desulfurization. The optimal desulfurization capacity (Ls: 64.1) is observed when the Al2O3 content is 15 wt.%, attributed to the simultaneous presence of CaO particle precipitation and C3A. However, as the Al2O3 content reaches 20 wt.%, all the oversaturated CaO integrates into C3A, leading to a reduction in Ls from 64.1 to 10.7, thereby diminishing the desulfurization capacity by approximately sixfold. When Al2O3 exceeds 22 wt.%, the phase composition transitions from the C3A to C12A7 phase, and the desulfurization approach shifts from solid(slag)–liquid(metal) to liquid(slag)–liquid(metal) diffusion, with Ls decreasing to 23.4. This reduction is due to C12A7’s lower sulfur capacity compared to C3A and the absence of saturated CaO particle precipitation. Therefore, for Al2O3 to effectively replace fluorite in KR desulfurizers, a higher presence of C3A phases and CaO particle precipitation are essential. The desulfurizer must contain over 65 wt.% CaO and maintain Al2O3 levels at 10~16.2 wt.%. Full article
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<p>Schematic diagram of the KR mechanical mixing equipment.</p>
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<p>XRD analysis results of desulfurizer.</p>
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<p>FactSage (<b>a</b>) and Thermo-Calc (<b>b</b>) simulation of the phase composition of A30 at different temperatures.</p>
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<p>Comparison of the appearance of desulfurization slag at different reaction times at 1400 °C.</p>
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<p>(<b>a</b>) Comparison of the sulfur content in the hot metal of desulfurizers. (<b>b</b>) Sulfur distribution ratio and desulfurization of each group.</p>
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<p>SEM images of A15 (<b>a</b>) and A30 (<b>b</b>) desulfurization slags.</p>
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<p>SEM images of the A15 desulfurizer: (<b>a</b>) unreacted zone; (<b>b</b>) reacted zone.</p>
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<p>SEM images of the A30 desulfurizer: (<b>a</b>) unreacted zone; (<b>b</b>) reacted zone.</p>
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<p>FactSage phase fractionation simulation and the relationship between the sulfur partition ratio.</p>
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<p>SEM images of the A15 desulfurizer reaction zone.</p>
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<p>Effect of composition on desulfurization speed.</p>
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<p>Schematic diagram of the calcium aluminate desulfurization method: (<b>a</b>) Al<sub>2</sub>O<sub>3</sub> &lt; 22 wt.%; (<b>b</b>) Al<sub>2</sub>O<sub>3</sub> &gt; 22 wt.%.</p>
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<p>A15 Comparison of reaction zone thickness at different times: (<b>a</b>) 10 min; (<b>b</b>) 30 min.</p>
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<p>A schematic diagram of KR desulfurization, which is divided into three steps. (The first is the concentration of oxygen ions in the desulfurizer, the second is the replacement of sulfur ions at the slag–steel interface, and the third is the ability of the desulfurizer to store sulfur.)</p>
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11 pages, 10641 KiB  
Article
Morphological Evolution of Single-Core Multi-Strand Wires during Ultrasonic Metal Welding
by Andreas Gester, Dmitrii Ozherelkov and Guntram Wagner
Metals 2024, 14(3), 362; https://doi.org/10.3390/met14030362 - 20 Mar 2024
Viewed by 1015
Abstract
Ultrasonic metal welding (USMW) finds widespread utilization in automotive industries, where it is used for connecting the wire harness of the vehicle, consisting of stranded wires, to the terminals. However, the behavior of the strands during the compaction process is still understudied and [...] Read more.
Ultrasonic metal welding (USMW) finds widespread utilization in automotive industries, where it is used for connecting the wire harness of the vehicle, consisting of stranded wires, to the terminals. However, the behavior of the strands during the compaction process is still understudied and often overlooked. Therefore, this work focuses on the investigation of the wire compaction behavior from a morphological point of view. A newly developed method for investigating cross-sections of such joints is introduced, facilitating area quantification of the strands for a microscale examination of compaction variations for every single strand as a function of welding time. It is shown that the deformation in the wire is not homogenous throughout the wire cross-section; instead, the formation of distinct zones is observed. Three distinct regimes dominating the welding process were observed: (i) linear reduction in nugget height with primary compaction of the nugget and sealing of the interstitial spaces between the strands for weld times from 0 s up to 1.3 s; (ii) accelerated loss of nugget height due to strong plastic deformation of the strands for weld times between 1.3 s and 1.7 s; and (iii) comprehensive welding of the individual strands and strong loss of nugget height. Furthermore, it was demonstrated that the deformation of the wire during the USMW process originates in the coupling area of the horn and the wire and not in the interface of the wire and the terminal. Therefore, it can be assumed that the temperature of the interface between the horn and the wire must be significantly higher than that of the interface between the wire and the terminal. The presented approach and new insights into the behavior of ultrasonically welded joints of stranded wires and terminals provide guidance for improving the welding process. Full article
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<p>Distinct morphological zones in the weld nugget according to Bergman et al. (adapted from Ref. [<a href="#B37-metals-14-00362" class="html-bibr">37</a>]).</p>
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<p>Light microscopic images of cross-sections of joints welded with (<b>a</b>) 100 ms; (<b>b</b>) 500 ms; (<b>c</b>) 1000 ms; (<b>d</b>) 1500 ms; and (<b>e</b>) 2000 ms.</p>
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<p>Average compaction and average nugget height as a function of welding time.</p>
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<p>Wire strand area for distinct welding times for (<b>a</b>) 100 ms; (<b>b</b>) 300 ms; (<b>c</b>) 500 ms; (<b>d</b>) 700 ms; (<b>e</b>) 900 ms; (<b>f</b>) 1100 ms; (<b>g</b>) 1300 ms; (<b>h</b>) 1500 ms; (<b>i</b>) 1700 ms; (<b>j</b>) 1900 ms; (<b>k</b>) legend.</p>
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<p>Wire strand distribution for (<b>a</b>) a welding time of 500 ms; and (<b>b</b>) all investigated welding times.</p>
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2 pages, 148 KiB  
Correction
Correction: Gargalis et al. A Comparative Investigation of Duplex and Super Duplex Stainless Steels Processed through Laser Powder Bed Fusion. Metals 2023, 13, 1897
by Leonidas Gargalis, Leonidas Karavias, Joachim S. Graff, Spyros Diplas, Elias P. Koumoulos and Evangelia K. Karaxi
Metals 2024, 14(3), 361; https://doi.org/10.3390/met14030361 - 20 Mar 2024
Viewed by 758
Abstract
In the original publication [...] Full article
17 pages, 5100 KiB  
Article
Cu2−xS and Cu2−xSe Alloys: Investigating the Influence of Ag, Zn, and Ni Doping on Structure and Transport Behavior
by Andrzej Mikuła, Tomasz Kurek, Miłosz Kożusznik and Paweł Nieroda
Metals 2024, 14(3), 360; https://doi.org/10.3390/met14030360 - 20 Mar 2024
Cited by 1 | Viewed by 1003
Abstract
Cu2−xS and Cu2−xSe (0 ≤ x ≤ 0.2) alloys stand out as highly promising materials for thermoelectric applications, owing to the phonon–liquid electron–crystal (PLEC) convention. In this study, we undertake a comprehensive investigation to reassess the synthesis [...] Read more.
Cu2−xS and Cu2−xSe (0 ≤ x ≤ 0.2) alloys stand out as highly promising materials for thermoelectric applications, owing to the phonon–liquid electron–crystal (PLEC) convention. In this study, we undertake a comprehensive investigation to reassess the synthesis conditions, with a focus on achieving pure-phased systems through a direct reaction between elements at elevated temperatures. Simultaneously, we present experimental evidence showcasing the feasibility of doping these systems with Ag, Ni, and Zn. The study demonstrates that obtaining single-phased systems requires multi-step processes, and the dissolution of chosen impurities appears doubtful, as evidenced by numerous foreign phase segregations. Additionally, it is revealed that the partial dissolution of individual impurities deteriorates the operational parameters of these chalcogenides. For the optimal Cu1.97S composition, it reduces the thermoelectric figure-of-merit ZT from 1.5 to approximately 1.0, 0.65, and 0.85 for Ag-, Ni-, and Zn-doped systems, respectively, while marginally improving their stability. For metal-like Cu1.8Se, the ZT parameter remains at a low level, ranging between 0.09 and 0.15, showing slight destabilization during subsequent operating cycles. The article concludes with an in-depth analysis of the basic thermoelectric performance exhibited by these doped systems, contributing valuable insights into the potential enhancements and applications of Cu2−xS and Cu2−xSe alloys in the field of thermoelectric materials. Full article
(This article belongs to the Special Issue Nano-Metallic Materials for New Energy)
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<p>XRD diffraction patterns of copper(I) sulfides obtained by high-temperature reaction between elements and slow-cooled to RT from 1273 K or 1073 K: (<b>a</b>) Cu<sub>1.97</sub>S, (<b>b</b>) Cu<sub>2</sub>S.</p>
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<p>XRD diffraction patterns of copper(I) selenides obtained by high-temperature reaction between elements and slow-cooled or quenched to RT: (<b>a</b>) Cu<sub>2</sub>Se, (<b>b</b>) C<sub>1.8</sub>Se.</p>
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<p>Rietveld analysis of sintered pellets: (<b>a</b>) Cu<sub>1.97</sub>S; (<b>b</b>) Cu<sub>1.8</sub>Se.</p>
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<p>The comparison of powder and sintered pellet XRD diffraction patterns of Cu<sub>1.96</sub>M<sub>0.01</sub>S (M = Ag, Ni, Zn).</p>
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<p>The comparison of powder and sintered pellet XRD diffraction patterns of Cu<sub>1.79</sub>M<sub>0.01</sub>Se (M = Ag, Ni, Zn).</p>
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<p>Thermal conductivity of undoped and doped copper chalcogenides as a function of temperature: Cu<sub>1.97</sub>S (<b>a</b>); Cu<sub>1.8</sub>Se (<b>b</b>).</p>
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<p>Seebeck coefficient as a function of temperature for copper(I) sulfide systems.</p>
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<p>Seebeck coefficient as a function of temperature for copper(I) selenide systems.</p>
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<p>Electrical conductivity as a function of temperature for copper(I) sulfide systems.</p>
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<p>Electrical conductivity as a function of temperature for copper(I) selenide systems.</p>
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<p>Thermoelectric figure of merit parameter ZT as a function of temperature for copper(I) sulfide systems.</p>
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<p>Thermoelectric figure of merit parameter ZT as a function of temperature for copper(I) selenide systems.</p>
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19 pages, 8387 KiB  
Article
Mechanism of Crystallographic Orientation and Texture Evolution of Ti60 Alloy during Plane Strain Compression
by Yi Dai, Yunteng Xiao, Weidong Zeng, Runchen Jia and Weiju Jia
Metals 2024, 14(3), 359; https://doi.org/10.3390/met14030359 - 20 Mar 2024
Viewed by 966
Abstract
The crystallographic orientation and texture evolution mechanism of equiaxed Ti60 alloy plates were investigated in this study through plane strain compression tests. The EBSD analysis revealed that the received plate contained two characteristic textures that were perpendicular to each other, i.e., c-axis//TD (Component [...] Read more.
The crystallographic orientation and texture evolution mechanism of equiaxed Ti60 alloy plates were investigated in this study through plane strain compression tests. The EBSD analysis revealed that the received plate contained two characteristic textures that were perpendicular to each other, i.e., c-axis//TD (Component 1) and c-axis//RD (Component 2), with the latter being caused by the change in direction of the TD texture that was generated during the previous unidirectional rolling process into an RD direction in the cross-rolling process. The results demonstrated that, with increasing the deformation temperature from 930 °C to 960 °C and 990 °C, the intensity of the c-axis//TD texture (Component 1) initially rose to a peak value of 5.07, which then—subsequently—decreased significantly to 2.96 at 960 °C and 3.11 at 990 °C. Conversely, the intensity of the c-axis//RD texture (Component 2) remained relatively unchanged. These texture changes were correlated with slip system activity and the spheroidization of the primary alpha phase. For the c-axis//TD texture, the initial intensity of the texture components during compression at lower temperatures could be attributed to the incomplete dynamic spheroidization process of the α phase, which leads to the reinforcement of the c-axis//TD due to prismatic slip. As the deformation temperature increased, the dynamic spheroidization process became more prominent, thereby leading to a significant reduction in the intensity of the c-axis//TD texture. In contrast, the c-axis//RD texture exhibited difficulty in activating the prismatic slip and basal slip; in addition, it also encountered resistance to dynamic spheroidization, thus resulting in negligible changes in the texture intensity. Full article
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<p>Schematic diagram of the unidirectional, cross-rolling process and plane strain compression.</p>
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<p>Schematic diagram of the compression process, as well as of the SEM and EBSD observation areas.</p>
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<p>SEM microstructural images under different conditions: (<b>a</b>) original; (<b>b</b>) 930 °C; (<b>c</b>) 960 °C; (<b>d</b>) 990 °C; and (<b>e</b>) new grain boundaries at a higher magnification.</p>
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<p>The inverse pole figure, KAM figure, and pole figure maps of the microstructures under different conditions: (<b>a</b>) the initial temperature; (<b>b</b>) 930 °C; (<b>c</b>) 960 °C; and (<b>d</b>) 990 °C.</p>
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<p>Inverse pole figure map of the (<b>a</b>) primary α-phase αp; (<b>b</b>) secondary α-phase αs; KAM maps of (<b>c</b>) primary α-phase αp; and (<b>d</b>) secondary α-phase αs.</p>
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<p>Pole figure maps of both the original and compression microstructures: original pole figure map of (<b>a</b>) the primary α-phase α<sub>p</sub> and (<b>b</b>) secondary α-phase α<sub>s</sub>. A 930 °C pole figure map of (<b>c</b>) the primary α-phase α<sub>p</sub>; (<b>d</b>) secondary α-phase α<sub>s</sub>; and (<b>e</b>) the primary α-phase under different compression temperatures at the initial temperature, 930 °C, 960 °C, and 990 °C.</p>
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<p>(<b>a</b>) Percentages of the texture components under different compression temperatures: the initial temperature, 930 °C, 960 °C, and 990 °C. PF maps of the ideal texture component: (<b>b</b>) the &lt;0001&gt;//TD texture and (<b>c</b>) the &lt;0001&gt;//RD texture.</p>
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<p>Inverse pole figure maps of the primary α-phase αp of (<b>a</b>) the initial temperature and (<b>b</b>) 930 °C. KAM maps of the primary α-phase αp of (<b>c</b>) the initial temperature and (<b>d</b>) 930 °C.</p>
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<p>(<b>a</b>) Inverse pole figure map of 930 °C; (<b>b</b>) KAM map of 930 °C; and (<b>c</b>) the characteristic Grain A and Grain B.</p>
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<p>The characteristic grains from the two typical texture components in the original microstructure: (<b>a</b>) grain orientation spread map of Component 1 and (<b>c</b>) of Component 2, as well as the (<b>b</b>) the KAM maps of Component 1 and (<b>d</b>) of Component 2.</p>
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<p>The first typical grain diagram of dynamic spheroidization: (<b>a</b>) grain orientation; (<b>b</b>) the GOS map; and (<b>c</b>) the KAM map.</p>
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<p>The second typical grain diagram of dynamic spheroidization: (<b>a</b>) grain orientation; (<b>b</b>) the GOS map; and (<b>c</b>) the KAM map.</p>
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<p>The third typical grain diagram of dynamic spheroidization: (<b>a</b>) grain orientation; (<b>b</b>) the GOS map; and (<b>c</b>) the KAM map.</p>
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8 pages, 5342 KiB  
Communication
Metallurgical Method of Determining Heat Transfer Coefficient in Simulations of Twin-Roll Casting
by Min-Seok Kim and Jiwon Kim
Metals 2024, 14(3), 358; https://doi.org/10.3390/met14030358 - 20 Mar 2024
Cited by 3 | Viewed by 1031
Abstract
We herein suggest a metallurgical method using pure aluminum with no freezing temperature range to derive appropriate roll/melt interfacial heat transfer coefficients in simulation of twin-roll casting process. This method is inspired by the concept that the position of the kiss points where [...] Read more.
We herein suggest a metallurgical method using pure aluminum with no freezing temperature range to derive appropriate roll/melt interfacial heat transfer coefficients in simulation of twin-roll casting process. This method is inspired by the concept that the position of the kiss points where two solidifying shells encounter and the roll nip coincides under the condition where the roll load becomes zero as the roll rotation speed decreases. The conditions where the roll load becomes zero under various melt supply temperature conditions in the actual TRC process are found experimentally. These conditions are then applied to simulation models to derive heat transfer coefficient values. When comparing these values with those derived previously from the empirical relation for roll rotation speed and heat transfer coefficient, the conclusion is drawn that the deviation was reasonably low, around 10%. Full article
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<p>Schematic diagram of twin-roll casting process.</p>
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<p>(<b>a</b>) Appearance of pure Al strip fabricated by TRC process, and (<b>b</b>) anodized grain structure of the longitudinal cross-section of the strip.</p>
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<p>Variation in roll load under various roll rotation speeds and melt supply temperatures.</p>
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<p>The influence of the roll/melt interfacial HTC on solidification behavior in TRC process, (<b>a</b>) 4.2 m/min and (<b>b</b>) 3.1 m/min.</p>
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<p>Relationship between the roll/melt interfacial HTC and the position of the kiss point (distance from the roll nip to the kiss point).</p>
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11 pages, 3104 KiB  
Article
A Study on the Aging Behavior of Nitrided W18Cr4V Steel in High-Temperature Sodium
by Xiaogang Fu, Na Liang, Wei Zhang, Liu Tao, Bo Qin, Zhangshun Ruan, Bin Long and Shasha Lv
Metals 2024, 14(3), 357; https://doi.org/10.3390/met14030357 - 19 Mar 2024
Viewed by 862
Abstract
The loading and unloading elevators are the primary equipment in the refueling system, used for transferring fuel assemblies in the sodium-cooled fast reactors. The guideway friction pairs are the critical components of these elevators in the refueling system. With the excellent hardness and [...] Read more.
The loading and unloading elevators are the primary equipment in the refueling system, used for transferring fuel assemblies in the sodium-cooled fast reactors. The guideway friction pairs are the critical components of these elevators in the refueling system. With the excellent hardness and wear resistance in air, nitrided W18Cr4V steel is a promising material for the guideway friction pairs. In order to assess the feasibility of using nitrided W18Cr4V steel, it is essential to understand the aging behavior of nitrided W18Cr4V steel in high-temperature sodium. Aging tests were conducted on nitrided W18Cr4V steel in sodium and in argon environments at various temperatures for different exposure times. The results showed that the nitrogen atoms in the nitrided layer exhibited bidirectional diffusion behavior in the sodium or argon environment at 540 °C. Compared to the argon environment, cracks formed within the nitrided layer and the diffusion of nitrogen into the sodium was accelerated in the nitrided layer. As a significant number of nitrogen atoms had diffused into the sodium, there was little difference in the hardness between nitrided W18Cr4V steel and non-nitrided W18Cr4V steel after long-term exposure to 540 °C sodium. Full article
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<p>The characterization results of W18Cr4V steel before and after the ion nitriding process: (<b>a</b>) The microstructure of W18Cr4V steel before ion nitriding process, (<b>b</b>) The XRD result of W18Cr4V steel before and after ion nitriding process.</p>
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<p>The microhardness test results of nitrided W18Cr4V steel after 200 h aging in sodium and argon at 540 °C.</p>
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<p>The results of the microhardness examinations of nitrided W18Cr4V steel before and after aging tests: (<b>a</b>) aging in sodium at 540 °C for 200 h and 500 h, (<b>b</b>) aging in argon at 540 °C for 200 h and 500 h.</p>
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<p>The SEM results of nitrided W18Cr4V steel after 200 h aging in sodium and argon at 540 °C: (<b>a</b>) aging in sodium, (<b>b</b>) aging in argon.</p>
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<p>The XRD patterns of nitrided W18Cr4V steel before and after aging in sodium and argon environments at 540 °C for 200 h and 500 h.</p>
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<p>The results of accelerated tests conducted on nitrided W18Cr4V steel and non-nitrided W18Cr4V steel in a sodium environment at a temperature of 700 °C.</p>
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12 pages, 2801 KiB  
Article
Movement Strategy Influences on the Characteristics of Low-Carbon Steel Generated by the Lamination Object Manufacturing Method
by Tran Le Hong Ngoc, Ha Thi Xuan Chi, Pham Son Minh, Van-Thuc Nguyen and Tran Minh The Uyen
Metals 2024, 14(3), 356; https://doi.org/10.3390/met14030356 - 19 Mar 2024
Viewed by 992
Abstract
This paper investigates the effects of heating movement techniques on the properties of low-carbon steel samples that are 3D printed using S20C lamination object manufacturing (LOM). A Tungsten iner gas (TIG) machine and a computer numerical control (CNC) machine were used together to [...] Read more.
This paper investigates the effects of heating movement techniques on the properties of low-carbon steel samples that are 3D printed using S20C lamination object manufacturing (LOM). A Tungsten iner gas (TIG) machine and a computer numerical control (CNC) machine were used together to join the steel sheet. The LOM samples were created with a straight-profile, short-profile, cross-profile, and curved-profile. The results indicate that the majority of the samples had a grain size number of 7–9. The samples exhibited an isotropy grain shape. The LOM samples exhibited dimples, which suggests ductility fractures. Pore flaws showed up in the microstructure of the cross-profile and short-profile samples during the LOM process. The samples with curved- and straight-profiles had a better microstructure. In comparison to samples with a short profile and a cross-profile, the samples with a straight-profile and a curved-profile had a superior combination of ultimate tensile strengths (UTSs) and elongation value. The straight- and curved-profiles’ greater elongation and tensile strength can be attributed to their improved microstructure and finer grain size. A straight-profile sample with an elongation value of 25.6% and a UTS value of 430 MPa was the ideal LOM sample. Conversely, the weakest sample was the LOM sample with a cross-profile, which had an elongation value of 10.8% and a UTS value of 332.5 MPa. This research could provide further information about the LOM method and the best straight-profile movement strategy. A suitable TIG gun movement strategy could produce a good LOM sample with a good microstructure, tensile strength, and ductility. Further research should incorporate more movement strategies and techniques that completely prevent the formation of pore defects. Full article
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<p>The LOM movement strategies and samples: (<b>a</b>) straight-profile, (<b>b</b>) short-profile, (<b>c</b>) cross-profile, (<b>d</b>) curved-profile, (<b>e</b>) steel lamination, (<b>f</b>) ASTM E8/E8M-13 standards sample, and (<b>g</b>) tensile test samples after wire EDM cutting.</p>
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<p>The LOM equipment and sample position: (<b>a</b>) CNC machine with TIG gun, (<b>b</b>) LOM process, and (<b>c</b>) tensile test sample position.</p>
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<p>Microstructure of LOM samples with different movement strategies: (<b>a</b>) straight-profile, (<b>b</b>) short-profile, (<b>c</b>) cross-profile, and (<b>d</b>) curved-profile.</p>
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<p>Grain size number distribution following ASTM E112-10 grain size number standard of the LOM samples with different movement strategies: (<b>a</b>) straight-profile, (<b>b</b>) short-profile, (<b>c</b>) cross-profile, and (<b>d</b>) curved-profile.</p>
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<p>SEM microstructure of LOM samples of fracture surface after tensile test with different movement strategies: (<b>a</b>) straight-profile, (<b>b</b>) short-profile, (<b>c</b>) cross-profile, and (<b>d</b>) curved-profile.</p>
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<p>Stress–strain diagrams of LOM samples of fracture surface after tensile test with different movement strategies: (<b>a</b>) straight-profile, (<b>b</b>) short-profile, (<b>c</b>) cross-profile, and (<b>d</b>) curved-profile.</p>
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<p>Average tensile strength of LOM samples of fracture surface after tensile test with different movement strategies.</p>
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<p>Average elongation of LOM samples of fracture surface after the tensile test at different movement strategies.</p>
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20 pages, 4215 KiB  
Article
Surface Residual Stress Release Behavior of Shot-Peened Springs
by Chenxi Shao, Decheng Wang, Yong Zang and Peng Cheng
Metals 2024, 14(3), 355; https://doi.org/10.3390/met14030355 - 19 Mar 2024
Viewed by 1043
Abstract
Shot peening is the primary method used to improve the fatigue life of springs. In this study, we aimed to quantify the reduction in residual stresses in the shot-peened layer by considering factors such as surface roughness, cyclic loading, and the helix angle, [...] Read more.
Shot peening is the primary method used to improve the fatigue life of springs. In this study, we aimed to quantify the reduction in residual stresses in the shot-peened layer by considering factors such as surface roughness, cyclic loading, and the helix angle, based on the spring’s periodic variation and curvature characteristics. We developed an equivalent replacement algorithm to address the challenge of characterizing the dynamic accumulation and attenuation of residual stresses under cyclic multiaxial stresses. This algorithm accurately modeled the dynamic attenuation of residual stresses and was incorporated into the spring life prediction model. Experimental validation demonstrated the high accuracy of the model for predicting fatigue life. Full article
(This article belongs to the Section Metal Failure Analysis)
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<p>Analysis of spring structural characteristics and cross-sectional stress.</p>
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<p>Spring fatigue machine, indicating the loading and fixed sections.</p>
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<p>DSP microstructure of the sample surface in the initial state and after fatigue testing (<span class="html-italic">d</span> = 4.0 mm, <span class="html-italic">C</span> = 7).</p>
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<p>DSP sample under different cyclic loading ratios, nominal stress amplitudes, cycle times (<span class="html-italic">d</span> = 4.0 mm, <span class="html-italic">C</span> = 7, DSP, inner coil), and distribution of residual stress along the depth direction.</p>
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<p>Relaxation law of maximum residual stress on the surface of the inner coil under different cycle conditions (<span class="html-italic">d</span> = 4.0 mm, <span class="html-italic">C</span> = 4, DSP, inner coil).</p>
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<p>Attenuation law for residual stress on the spring surface at different positions along the circumferential direction (<span class="html-italic">d</span> = 4.0 mm, <span class="html-italic">C</span> = 4, DSP, <span class="html-italic">r</span> = 0.2, 1200 MPa).</p>
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<p>Residual stress attenuation with different spring indexes on the inner coil (<span class="html-italic">d</span> = 4.0 mm, DSP, <span class="html-italic">r</span> = 0.2, 1200 MPa).</p>
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<p>Comparative analysis with actual test results on the residual stress relaxation behavior.</p>
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<p>Comparison of mean life and life standard deviation between two surface conditions at different stress levels (<span class="html-italic">C</span> = 4).</p>
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<p>Comparison of fatigue life differences in shot-peened springs with different spring indexes.</p>
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<p>Two-time error band test chart for SLP and DLP.</p>
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14 pages, 37796 KiB  
Article
Microgrid-Patterned Ni Foams as Current Collectors for Ultrafast Energy Storage Devices
by Un-Tae Kim, Myeong-Hun Jo and Hyo-Jin Ahn
Metals 2024, 14(3), 354; https://doi.org/10.3390/met14030354 - 19 Mar 2024
Cited by 1 | Viewed by 979
Abstract
Current research is focused on developing active materials through surface functionalization, porosity, composites, and doping for ultrafast electric double layer capacitors (EDLCs). In this study, deviating from existing strategies focused on active materials, we designed tunable 3D microgrid-patterned (MP) surface morphologies on Ni [...] Read more.
Current research is focused on developing active materials through surface functionalization, porosity, composites, and doping for ultrafast electric double layer capacitors (EDLCs). In this study, deviating from existing strategies focused on active materials, we designed tunable 3D microgrid-patterned (MP) surface morphologies on Ni foams used as current collectors using SUS meshes as rigid stamps during roll pressing. The surface geometries of the MP-Ni foams were controlled to standard mesh scales of 24, 40, and 60 (denoted as 24MP-Ni, 40MP-Ni, and 60MP-Ni, respectively). The three MP-Ni samples with different microgrid sizes presented different surface geometries, such as root-mean-square roughness (Rrms), skewness roughness (Rsk), and width/depth scales of the microgrid patterns. Consequently, 40MP-Ni demonstrated an optimized surface geometry with high Rrms (35.4 μm) and Rsk (−0.19) values, which facilitated deep slurry infiltration and increased its contact area with the active material. Surface optimization of the MP-Ni enabled ultrafast and reversible charge transport kinetics owing to its relaxed electron transfer resistance and robust adhesion to the active material compared with bare Ni foam. EDLC electrodes with 40MP-Ni achieved an ultrafast-rate capability (96.0 F/g at 20 A/g) and ultrafast longevity (101.9% capacity retention after 5000 cycles at 5 A/g) without specific modification of active material. Full article
(This article belongs to the Special Issue Metallic Nanostructured Materials and Thin Films)
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<p>(<b>a</b>) Schematic illustration of the microgrid-patterning of Ni foams using SUS meshes of different mesh sizes: (<b>b</b>) 24 mesh, (<b>c</b>) 40 mesh, and (<b>d</b>) 60 mesh. Photographs of the resultant Ni foams: (<b>e</b>) bare Ni, (<b>f</b>) 24MP-Ni, (<b>g</b>) 40MP-Ni, and (<b>h</b>) 60MP-Ni.</p>
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<p>3D micro-topography images of the Ni foams fabricated by the microgrid patterning method: (<b>a</b>) bare Ni, (<b>b</b>) 24MP-Ni, (<b>c</b>) 40MP-Ni, and (<b>d</b>) 60MP-Ni. (<b>e</b>–<b>h</b>) Top-view surface roughness images of Ni foams and (<b>i</b>–<b>l</b>) the corresponding line roughness profiles: (<b>e</b>,<b>i</b>) bare Ni, (<b>f</b>,<b>j</b>) 24MP-Ni, (<b>g</b>,<b>k</b>) 40MP-Ni, and (<b>h</b>,<b>l</b>) 60MP-Ni.</p>
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<p>(<b>a</b>) Surface geometry parameters (i.e., the width, depth, root-mean-square roughness (R<sub>rms</sub>), and skewness roughness (R<sub>sk</sub>) of the Ni foams. (<b>b</b>) Illustration of the infiltration of the surfaces of Ni foams with a highly negative R<sub>sk</sub> and slightly negative R<sub>sk</sub>.</p>
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<p>(<b>a</b>) Raman spectrum and (<b>b</b>) nitrogen adsorption/desorption curves of YP50F. XRD patterns of the (<b>c</b>) Ni foam samples and (<b>d</b>) YP50F/Ni electrodes. OM images of the Ni foams: (<b>e</b>) bare Ni, (<b>f</b>) 24MP-Ni, (<b>g</b>) 40MP-Ni, and (<b>h</b>) 60MP-Ni.</p>
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<p>Galvanostatic charge–discharge curves of the Ni foam-based electrodes at different current densities: (<b>a</b>) YP50F/bare Ni, (<b>b</b>) YP50F/24MP-Ni, (<b>c</b>) YP50F/40MP-Ni, and (<b>d</b>) YP50F/60MP-Ni.</p>
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<p>(<b>a</b>) Specific capacitance and CE plots according to the current density in the range of 0.2–20 A/g for all EDLC electrodes. (<b>b</b>) CV profiles of the Ni foam-based electrodes in the potential range of 0–1.0 V. (<b>c</b>) Capacitance retention and high-rate capability plots according to cycle number and current density, respectively. (<b>d</b>) Specific capacitance and (<b>e</b>) capacitance retention plots for 5000 charge/discharge cycles at 5.0 A/g. (<b>f</b>) Energy density vs. power density plots of the Ni foam EDLC electrodes prepared in this study and some previously reported EDLC electrodes [<a href="#B24-metals-14-00354" class="html-bibr">24</a>,<a href="#B25-metals-14-00354" class="html-bibr">25</a>,<a href="#B26-metals-14-00354" class="html-bibr">26</a>].</p>
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<p>(<b>a</b>) EIS profiles and (<b>b</b>) enlarged EIS views for the EDLC electrodes. (<b>c</b>) Schematic illustration of interfacial charge transport with cross-sectional views for all EDLC electrodes.</p>
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<p>(<b>a</b>) Photographs of symmetric EDLC electrodes in the straight and bent states, and (<b>b</b>,<b>c</b>) gravimetric charge–discharge curves obtained at 0.2, 5, and 10 A/g for (<b>b</b>) bare Ni and (<b>c</b>) 40MP-Ni EDLC electrodes. (<b>d</b>) Specific capacitance plots according to the current density in the range of 0.2 to 10 A/g for bare Ni and 40MP-Ni EDLC electrodes.</p>
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15 pages, 16225 KiB  
Article
The Influence of Yttrium Content and Ceramic Crucible Materials on Desulfurization during Vacuum Induction Melting of DD5 Superalloys
by Fuwei Wang, Ying Cheng, Shoubin Zhang, Rui Zhang, Yanyun Sun, Kai Guan, Huarui Zhang and Hu Zhang
Metals 2024, 14(3), 353; https://doi.org/10.3390/met14030353 - 19 Mar 2024
Viewed by 1116
Abstract
In this study, the effect of adding different contents of yttrium (Y) during vacuum induction melting in Al2O3 and Y2O3 crucibles on the purification of DD5 alloys was investigated. The results show that the Y2O [...] Read more.
In this study, the effect of adding different contents of yttrium (Y) during vacuum induction melting in Al2O3 and Y2O3 crucibles on the purification of DD5 alloys was investigated. The results show that the Y2O3 crucible exhibited great crucible stability and an excellent desulfurization effect when melting a Y-containing DD5 alloy. The S content of the alloy was reduced from 5.03 ppm to 1.36 ppm with the addition of 0.50 wt.% Y. Element Y combined with free S in the melt to form the YS phase, which was removed from the condensate shell and slag during the vacuum induction melting (VIM) process. Meanwhile, when the alloy was melted in the Y2O3 crucible with 0.50 wt.% Y addition, there was a reduction in S content from 2.77 ppm to 1.36 ppm compared to the Al2O3 crucible. Additionally, the loss of Y decreased from 0.12 wt.% to 0.05 wt.%. Full article
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<p>S content in samples with different Y additions in different crucibles: (<b>a</b>) Al<sub>2</sub>O<sub>3</sub> crucible, (<b>b</b>) Y<sub>2</sub>O<sub>3</sub> crucible.</p>
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<p>Microstructures of DD5 alloys with different Y contents: (<b>a</b>) M00, (<b>b</b>) Y005, (<b>c</b>) Y015, (<b>d</b>) Y05, (<b>e</b>) Y15, (<b>f</b>) Y40, (<b>g</b>) Al05, (<b>h</b>) Al15, (<b>i</b>) Al40.</p>
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<p>Analysis of the internal phases of the alloy: (<b>a</b>) alloys melted in Al<sub>2</sub>O<sub>3</sub> crucible, (<b>b</b>) alloys melted in Y<sub>2</sub>O<sub>3</sub> crucible.</p>
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<p>Interfacial morphology between the Al<sub>2</sub>O<sub>3</sub> crucible and the Al05 sample: (<b>a</b>) low-magnification SEM image, (<b>b</b>) high-magnification SEM image. Element distribution of (<b>c</b>) Y, (<b>d</b>) Al, (<b>e</b>) Cr, (<b>f</b>) Ni, (<b>g</b>) Co, and (<b>h</b>) O.</p>
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<p>Micromorphology of the inner surface of Al<sub>2</sub>O<sub>3</sub> crucible for melting Al05: (<b>a</b>) SEM image. Element distribution of (<b>b</b>) Ni, (<b>c</b>) Y, (<b>d</b>) Al, (<b>e</b>) Cr, and (<b>f</b>) O.</p>
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<p>Interfacial morphology between the Y<sub>2</sub>O<sub>3</sub> crucible and the Y05 sample: (<b>a</b>) low-magnification SEM image, (<b>b</b>) high-magnification SEM image. Element distribution of (<b>c</b>) Y, (<b>d</b>) Ni, and (<b>e</b>) O.</p>
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<p>Micromorphology of the condensation shell on the surface of Al<sub>2</sub>O<sub>3</sub> crucible in the Al05 sample: (<b>a</b>) SEM image. (<b>b</b>) EDS results for subfigure (<b>a</b>). Element distribution of (<b>c</b>) Y, (<b>d</b>) Cr, (<b>e</b>) Al, and (<b>f</b>) Ni.</p>
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<p>Micromorphology of the condensation shell on the surface of Y<sub>2</sub>O<sub>3</sub> crucible in the Y05 sample: (<b>a</b>) SEM image, (<b>b</b>) EDS results for subfigure (<b>a</b>). Element distribution of (<b>c</b>) Y and (<b>d</b>) Ni.</p>
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<p>XRD analysis of condensation shell on the surface of ceramic crucible: (<b>a</b>) Al05 sample, (<b>b</b>) Y05 sample.</p>
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<p>Micromorphology of Al<sub>2</sub>O<sub>3</sub> crucible and Y<sub>2</sub>O<sub>3</sub> crucible slag: (<b>a</b>,<b>c</b>) SEM image of Al05 sample. (<b>b</b>,<b>d</b>) SEM image of Y05 sample.</p>
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<p>XRD analysis of slag: (<b>a</b>) Al05 sample, (<b>b</b>) Y05 sample.</p>
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<p>S content in alloys, slags, and condensate shells bonded to the inner surface of Y<sub>2</sub>O<sub>3</sub> or Al<sub>2</sub>O<sub>3</sub> crucible of Y05 and Al05 samples.</p>
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<p>Interface reaction diagram of Y-containing alloy with different crucibles: (<b>a</b>) Al<sub>2</sub>O<sub>3</sub> crucible, (<b>b</b>) Y<sub>2</sub>O<sub>3</sub> crucible.</p>
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14 pages, 7950 KiB  
Article
Mechanical Properties and Fracture Toughness Prediction of Ductile Cast Iron under Thermomechanical Treatment
by Mohammed Y. Abdellah, Hamzah Alharthi, Rami Alfattani, Dhia K. Suker, H. M. Abu El-Ainin, Ahmed F. Mohamed, Mohamed K. Hassan and Ahmed H. Backar
Metals 2024, 14(3), 352; https://doi.org/10.3390/met14030352 - 19 Mar 2024
Cited by 1 | Viewed by 1449
Abstract
Temperature has a great influence on the mechanical properties of ductile cast iron or nodular cast iron. A thermomechanical treatment was carried out at various elevated temperatures of 450 °C, 750 °C and 850 °C using a universal testing machine with a tub [...] Read more.
Temperature has a great influence on the mechanical properties of ductile cast iron or nodular cast iron. A thermomechanical treatment was carried out at various elevated temperatures of 450 °C, 750 °C and 850 °C using a universal testing machine with a tub furnace. Specimens were held at these temperatures for 20 min to ensure a homogeneous temperature distribution along the entire length of the specimen, before a tensile load was applied. Specimens were deformed to various levels of uniform strain (0%, 25%, 50%, 75%, and 100%). These degrees of deformation were measured with a dial gauge attached to a movable cross plate. Three strain rates were used for each specimen and temperature: 1.8×104 s1, 9×104 s1 and 4.5×103 s1. A simple analytical model was extracted based on the CT tensile test geometry and yield stress and a 0.2% offset strain to measure the fracture toughness (JIC). To validate the analytical model, an extended finite element method (XFEM) was implemented for specimens tested at different temperatures, with a strain rate of 1.8×104 s1. The model was then extended to include the tested specimens at other strain rates. The results show that increasing strain rates and temperature, especially at 850 °C, increased the ductility of the cast iron and thus its formability. The largest percentage strains were 1 and 1.5 at a temperature of 750 °C and a strain rate of 1.8×104 s1 and 9×104 s1, respectively, and reached their maximum value of 1.7 and 2.2% at 850 °C and a strain rate of 9×104 s1 and 4.5×103 s1, respectively. In addition, the simple and fast analytical model is useful in selecting materials for determining the fracture toughness (JIC) at various elevated temperatures and different strain rates. Full article
(This article belongs to the Special Issue Thermomechanical Treatment of Metals and Alloys—Second Edition)
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<p>Standard circular dog bone tensile specimen for thermomechanical treatment (dim. mm).</p>
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<p>Finite element domain (<b>a</b>) with dimension (in mm); (<b>b</b>) mesh domain.</p>
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<p>Relation variation with different temperatures at <math display="inline"><semantics> <mrow> <mn>1.8</mn> <mo>×</mo> <msup> <mrow> <mn>10</mn> </mrow> <mrow> <mo>−</mo> <mn>4</mn> </mrow> </msup> <mo> </mo> <msup> <mrow> <mi mathvariant="normal">s</mi> </mrow> <mrow> <mo>−</mo> <mn>1</mn> </mrow> </msup> </mrow> </semantics></math> strain rate: (<b>a</b>) stress and strain; (<b>b</b>) plastic stress and plastic strain.</p>
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<p>Relation variation with different temperatures at <math display="inline"><semantics> <mrow> <mn>9</mn> <mo>×</mo> <msup> <mrow> <mn>10</mn> </mrow> <mrow> <mo>−</mo> <mn>4</mn> </mrow> </msup> <mo> </mo> <msup> <mrow> <mi mathvariant="normal">s</mi> </mrow> <mrow> <mo>−</mo> <mn>1</mn> </mrow> </msup> </mrow> </semantics></math> strain rate: (<b>a</b>) stress verse strain; (<b>b</b>) plastic stress verse plastic strain.</p>
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<p>Relation variation with different temperatures at <math display="inline"><semantics> <mrow> <mn>4.5</mn> <mo>×</mo> <msup> <mrow> <mn>10</mn> </mrow> <mrow> <mo>−</mo> <mn>3</mn> </mrow> </msup> <mo> </mo> <msup> <mrow> <mi mathvariant="normal">s</mi> </mrow> <mrow> <mo>−</mo> <mn>1</mn> </mrow> </msup> </mrow> </semantics></math> strain rate: (<b>a</b>) stress verse strain; (<b>b</b>) plastic stress verse plastic strain.</p>
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<p>Average nonmilled tensile strength relation with the absolute thermomechanical temperature.</p>
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<p>SEM macrograph at room temperature (<b>a</b>) (25 °C), (<b>b</b>) 450 °C, (<b>c</b>) 750 °C, and (<b>d</b>) 850 °C.</p>
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<p>Strain rate variation with true strain through tensile test.</p>
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<p>Average strength as a power function of strain rate.</p>
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<p>Different finite element model validation with experimental data.</p>
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13 pages, 70513 KiB  
Article
Coaxial Electrospinning of CoS1.097@C Core–Shell Fibers Anode Material for High-Performance Sodium-Ion Batteries
by Hongming Chen, Yan Li and Dan Zhou
Metals 2024, 14(3), 351; https://doi.org/10.3390/met14030351 - 19 Mar 2024
Viewed by 997
Abstract
As an important component that affects the storage performance of sodium-ion batteries (SIBs), novel anode materials still need to be well explored. Herein, CoS1.097@C core–shell fibers as anode material were designed via coaxial electrospinning, stabilization, and carbonization. Specially, CoS1.097 powders [...] Read more.
As an important component that affects the storage performance of sodium-ion batteries (SIBs), novel anode materials still need to be well explored. Herein, CoS1.097@C core–shell fibers as anode material were designed via coaxial electrospinning, stabilization, and carbonization. Specially, CoS1.097 powders are distributed in the inner shell of carbon fibers, and sufficient pore spaces are present among themselves. The unique encapsulation structure, porous characteristics, and one-dimensional conductive carbon shell can enable the CoS1.097@C core–shell fibers’ high initial specific capacity, excellent rate capability, and long cycle life. The initial charge and discharge capacities of the electrode at 50 mA g−1 are 386.0 and 830.9 mAh g−1, respectively. After 2000 cycles at 500 mA g−1, the discharge capacity is 216.3 mAh g−1. Even at 3000 mA g−1, the rate capacity can be maintained at 83.3 mAh g−1. Full article
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<p>Schematic illustrations of the coaxial electrospinning process of the CoS<sub>1.097</sub>@C core—shell fibers.</p>
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<p>(<b>a</b>) XRD patterns, (<b>b</b>) Raman spectra, and (<b>c</b>) TG curve of the CoS<sub>1.097</sub>@C core—shell fibers.</p>
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<p>XPS spectrum of the CoS<sub>1.097</sub>@C core—shell fibers. (<b>a</b>) Full XPS spectrum, (<b>b</b>) high-resolution C 1s spectrum, (<b>c</b>) high-resolution S 2p spectrum, (<b>d</b>) high-resolution Co 2p spectrum, (<b>e</b>) high-resolution N 1s spectrum, and (<b>f</b>) high-resolution O 1s spectrum.</p>
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<p>SEM images of the CoS<sub>1.097</sub>@C core—shell fibers under different magnification times.</p>
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<p>TEM images of the CoS<sub>1.097</sub>@C core—shell fibers under different magnification times.</p>
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<p>Pore structure characteristics of the CoS<sub>1.097</sub>@C core—shell fibers: (<b>a</b>) N<sub>2</sub> adsorption–desorption isotherms, (<b>b</b>) pore size distribution curve.</p>
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<p>(<b>a</b>) CV curves of the CoS<sub>1.097</sub>@C core—shell fibers under the scan rate of 0.1 mV s<sup>−1</sup>; (<b>b</b>) galvanostatic charge–discharge profiles of the CoS<sub>1.097</sub>@C core—shell fibers under 50 mA g<sup>−1</sup>; (<b>c</b>) cycling performance of the CoS<sub>1.097</sub>@C core—shell fibers and CoS<sub>1.097</sub> powders under 50 mA g<sup>−1</sup>; (<b>d</b>) rate performance of the CoS<sub>1.097</sub>@C core—shell fibers under various current densities; (<b>e</b>) long-term cycling performance of the CoS<sub>1.097</sub>@C core—shell fibers under 500 mA g<sup>−1</sup>.</p>
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<p>EIS curves of the electrode of CoS<sub>1.097</sub>@C core—shell fibers before and after cycling.</p>
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<p>SEM image of the cycled electrode of CoS<sub>1.097</sub>@C core—shell fibers.</p>
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14 pages, 10053 KiB  
Article
Effect Mechanism of α-Ferrite Sustained Precipitation on High-Temperature Properties in Continuous Casting for Peritectic Steel
by Songyuan Ai, Yifan Li, Mujun Long, Haohao Zhang, Dengfu Chen, Huamei Duan, Danbin Jia and Bingzhi Ren
Metals 2024, 14(3), 350; https://doi.org/10.3390/met14030350 - 18 Mar 2024
Cited by 1 | Viewed by 995
Abstract
Exploring the mechanism of the α-ferrite precipitation process on high-temperature properties plays an important guiding role in avoiding slab cracks and effectively regulating quality. In this work, in situ observation of the α-ferrite sustained precipitation behavior for peritectic steel during the austenitic [...] Read more.
Exploring the mechanism of the α-ferrite precipitation process on high-temperature properties plays an important guiding role in avoiding slab cracks and effectively regulating quality. In this work, in situ observation of the α-ferrite sustained precipitation behavior for peritectic steel during the austenitic phase transition process has been investigated using high-temperature confocal scanning laser microscopy. Meanwhile, the high-temperature evolution of the phase fractions during the phase transition process was quantitatively analyzed based on the high-temperature expansion experiment using the peak separation method. Furthermore, the high-temperature properties variations of the casting slab during the α-ferrite sustained precipitation process were investigated with the Gleeble thermomechanical simulator. The results show that the film-like ferrite precipitated along the austenite grain boundaries at the initial stage of phase transition, then needle-like ferrite initiates rapid precipitation on film-like ferrite when the average thickness reaches 15~20 μm. Hot ductility reached a minimum at the ferrite phase fraction fα = 10~15%, while high-temperature properties returned to a higher level after fα > 40~45%. The appearance of a considerable amount of needle-like ferrite and grain refinement effectively improves the high-temperature properties with the α-ferrite precipitation process advances. Full article
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<p>Schematic diagram of the position and dimension for experimental specimens: (<b>a</b>) Position of specimen processing; (<b>b</b>) specimen dimensions for the high-temperature experiment.</p>
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<p>Diagram of the experimental scheme: (<b>a</b>) In situ observation and high-temperature expansion analysis; (<b>b</b>) high-temperature thermal tensile analysis.</p>
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<p>Microstructure evolution during the whole process of <span class="html-italic">α</span>-ferrite precipitation for the slab: (<b>a</b>) 819.4 °C; (<b>b</b>) 795.8 °C; (<b>c</b>) 751.3 °C; (<b>d</b>) 699.3 °C; (<b>e</b>) 650.1 °C; (<b>f</b>) 599.6 °C.</p>
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<p>High-temperature expansion behavior of the casting slab during austenite phase transition: (<b>a</b>) Dilation curve and LTEC curve; (<b>b</b>) Separation results of LTEC curve.</p>
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<p>Variations of phase fractions with temperature during austenite phase transition.</p>
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<p>Microstructure of the specimen at the completion of the high-temperature expansion test.</p>
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<p>Stress-strain curves at different temperatures during the <span class="html-italic">α</span>-ferrite precipitation process: (<b>a</b>) Engineering stress-strain curves; (<b>b</b>) true stress-strain curves.</p>
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<p>Variation of hot ductility parameters with <span class="html-italic">α</span>-ferrite precipitation process advances: (<b>a</b>) As functions of temperature; (<b>b</b>) As functions of <span class="html-italic">f<sub>α</sub></span>.</p>
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<p>Fracture morphology at typical temperatures: (<b>a</b>) 700 °C; (<b>b</b>) 750 °C; (<b>c</b>) 800 °C.</p>
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<p>Microstructure at typical temperatures: (<b>a</b>) 700 °C; (<b>b</b>) 750 °C; (<b>c</b>) 800 °C.</p>
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<p>Relationship between high-temperature strength and test temperature during austenite phase transition process.</p>
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<p>Effect mechanism of the α-ferrite precipitation process on hot ductility and high-temperature strength.</p>
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12 pages, 5237 KiB  
Article
Influence of Submerged Entry Nozzles on Fluid Flow, Slag Entrainment, and Solidification in Slab Continuous Casting
by Xingang Zhen, Shiheng Peng and Jiongming Zhang
Metals 2024, 14(3), 349; https://doi.org/10.3390/met14030349 - 18 Mar 2024
Cited by 1 | Viewed by 1133
Abstract
In this paper, the fluid flow, slag entrainment and solidification process in a slab mold were studied using physical modeling and numerical simulation. The effect of two types of submerged entry nozzles (SENs) was also studied. The results showed that the surface velocity [...] Read more.
In this paper, the fluid flow, slag entrainment and solidification process in a slab mold were studied using physical modeling and numerical simulation. The effect of two types of submerged entry nozzles (SENs) was also studied. The results showed that the surface velocity for type A SEN was larger than that using type B SEN. For type A SEN, the maximum surface velocity was 0.63 m/s and 0.56 m/s, and it was 0.20 m/s and 0.18 m/s for type B SEN. The larger shear effect on the top surface made the slag at narrow face impacted to the vicinity of 1/4 wide face, while the slag layer at the top surface was relatively stable for type B SEN. Increasing the immersion depth of SEN decreased the surface velocity and slag entrainment. For type A SEN, the thickness of the solidified shell at the narrow face of the mold outlet was thin (12.3 mm) and there was a risk of breakout. For type B SEN, the liquid steel with high temperature would flow to the meniscus and it was beneficial to the melting of the mold flux. The thickness of the solidified shell at the narrow face of the mold outlet was increased. Furthermore, the surface velocity was also increased and it was not recommended for high casting speed. Full article
(This article belongs to the Special Issue Inclusion Metallurgy (2nd Edition))
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<p>Schematic diagram of the water model.</p>
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<p>Schematic diagram of submerged entry nozzle. (<b>A</b>) Type A; (<b>B</b>) Type B.</p>
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<p>Geometric model and mesh of the mold. (<b>A</b>) Computational domain; (<b>B</b>) mesh.</p>
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<p>Flow field in the mold at different immersion depths and 1.5 m/min with type A SEN. (<b>A</b>) 120 mm; (<b>B</b>) 150 mm; (<b>C</b>) 170 mm.</p>
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<p>Flow field in the mold at different immersion depths and 1.5 m/min with type B SEN. (<b>A</b>) 120 mm; (<b>B</b>) 150 mm; (<b>C</b>) 170 mm.</p>
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<p>Flow field in the mold at different immersion depths and 1.5 m/min with type B SEN. (<b>A</b>) 120 mm; (<b>B</b>) 150 mm; (<b>C</b>) 170 mm.</p>
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<p>Velocity distribution of top surface at 1/4 wide face with different immersion depths and casting speed of 1.5 m/min. (<b>A</b>) Type A SEN; (<b>B</b>) type B SEN.</p>
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<p>Liquid level fluctuation at casting speed of 1.50 m/min. (<b>A</b>) type A SEN; (<b>b</b>) type B SEN.</p>
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<p>The proportion of liquid level fluctuation in the range of ±3 mm. (<b>A</b>) type A SEN; (<b>B</b>) type B SEN.</p>
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<p>Oil distribution at different SEN immersion depths at casting speed of 1.50 m/min. (<b>A</b>) Type A SEN; (<b>B</b>) type B SEN.</p>
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<p>Distributions of surface velocity, temperature, and shell thickness at the mold outlet at different SEN immersion depths and casting speed of 1.50 m/min. (<b>A</b>) Type A SEN; (<b>B</b>) type B SEN.</p>
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19 pages, 25574 KiB  
Article
Different Heat-Exposure Temperatures on the Microstructure and Properties of Dissimilar GH4169/IC10 Superalloy Vacuum Electron Beam Welded Joint
by Hualin Cai, Zhixuan Ma, Jiayi Zhang, Liang Qi, Jinbing Hu and Jiayi Zhou
Metals 2024, 14(3), 348; https://doi.org/10.3390/met14030348 - 18 Mar 2024
Viewed by 1029
Abstract
Vacuum electron-beam welding (EBW) was used to join the precipitation-strengthened GH4169 superalloy and a new nickel-based superalloy IC10 to fabricate the turbine blade discs. In this study, a solid solution (1050 °C/2 h for GH4169 and 1150 °C/2 h for IC10) and different [...] Read more.
Vacuum electron-beam welding (EBW) was used to join the precipitation-strengthened GH4169 superalloy and a new nickel-based superalloy IC10 to fabricate the turbine blade discs. In this study, a solid solution (1050 °C/2 h for GH4169 and 1150 °C/2 h for IC10) and different heat-exposure temperatures (650 °C, 750 °C, 950 °C and 1050 °C/200 h, respectively) were used to study the high-temperature tensile properties and microstructure evolution of welded joints; meanwhile, the formation and evolution of the second phases of the joints were analyzed. After EBW, the welded joint exhibited a typical nail morphology, and the fusion zone (FZ) consisted of columnar and cellular structures. During the solidification process of the molten pool, Mo elements are enriched in the dendrites and inter-dendrites, and that of Nb and Ti elements was enriched in the dendrites, which lead to forming a non-uniform distribution of Laves eutectic and MC carbides in the FZ. The microhardness of the FZ gradually increased during thermal exposure at 650 °C and reached 300–320 HV, and the γ′ and γ″ phases were gradually precipitated with size of about 50 nm. Meanwhile, the microhardness of the FZ decreased to 260–280 HV at 750 °C, and the higher temperature resulted in the coarsening of the γ″ phase (with a final size of about 100 nm) and the formation of the acicular δ-phase. At 950 °C and 1050 °C, the microhardness of FZ decreased sharply, reaching up to 170~190 HV and 160~180 HV, respectively. Moreover, the Laves eutectic and MC carbides are dissolved to a greater extent without the formation of γ″ and δ phases; as a result, the absent of γ″ and δ phases are attributed to the significant improvement of segregation at higher temperatures. Full article
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<p>Overall morphologies of the welded plate (<b>a</b>) top and (<b>b</b>) bottom, and (<b>c</b>) localized enlargement of the top of the welded joint.</p>
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<p>Schematic diagram of electron-beam welding and dimensions of high-temperature tensile specimen.</p>
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<p>Microhardness variations of welded joints after different heat-exposure temperatures for 200 h.</p>
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<p>High-temperature tensile properties of welded joints with different heat-exposure temperatures at 700 °C.</p>
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<p>(<b>a</b>) Overall morphology of the welded joint cross-section and (<b>b</b>) microscopic morphology of the welded joint zones.</p>
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<p>(<b>a</b>) EBSD images (for Z<sub>0</sub> direction) and inverse pole figures (IPFs) of cross-sectioned welded joint and (<b>b</b>) percentage of misorientation angle on both sides of the FZ.</p>
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<p>The SEM images of (<b>a</b>) IC10 BM, (<b>b</b>,<b>c</b>) FZ, and (<b>d</b>) GH4169 BM regions.</p>
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<p>EPMA images showing element distributions in BMs and FZ regions.</p>
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<p>TEM images showing the second phases of the welded joint (<b>a</b>) carbide and its EDX mapping, (<b>b</b>) MC-type carbide, (<b>c</b>) Laves phase.</p>
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<p>OM images of welded joints after 200 h heat exposure at different temperatures: (<b>a</b>) 650 °C, (<b>b</b>) 750 °C, (<b>c</b>) 950 °C, and (<b>d</b>) 1050 °C.</p>
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<p>EBSD images showing microstructure variations of welded joints after different heat-exposure temperatures: (<b>a</b>,<b>b</b>) 650 °C, (<b>c</b>,<b>d</b>) 750 °C, (<b>e</b>,<b>f</b>) 950 °C, and (<b>g</b>,<b>h</b>) 1050 °C.</p>
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<p>Volume fraction of the misorientation angle (°) near the FZ on both sides at different heat-exposure temperatures.</p>
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<p>TEM observations of the FZ of welded joints at 650 °C, (<b>a</b>) HAADF for Laves eutectic phase and EDX mapping, (<b>b</b>) Laves eutectic morphology, and (<b>c</b>) γ′ and γ″ phases and SAED pattern.</p>
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<p>TEM observations of the FZ of welded joints at 750 °C (<b>a</b>) HAADF for Laves eutectic phase and EDX mapping, (<b>b</b>) HAADF for carbide and δ phases, (<b>c</b>) δ and γ″ phases and SAED pattern, and (<b>d</b>) carbide.</p>
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<p>TEM observations of the FZ of welded joints at 950 °C (<b>a</b>) HAADF for carbides and its EDX mapping, (<b>b</b>) carbide morphology, (<b>c</b>) dislocation, and (<b>d</b>) SAED pattern.</p>
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<p>TEM observations of the FZ of welded joints at 1050 °C (<b>a</b>) carbide and EDX mapping, (<b>b</b>) subgrain boundary, (<b>c</b>) carbide, and (<b>d</b>) SAED pattern.</p>
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<p>The morphologies of the FZ for (<b>a</b>) as-welded heat exposures at (<b>b</b>) 650 °C, (<b>c</b>) 750 °C, (<b>d</b>) 950 °C, and (<b>e</b>) 1050 °C, respectively; (<b>f</b>) Ni-Nb-C ternary-phase diagram [<a href="#B33-metals-14-00348" class="html-bibr">33</a>].</p>
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<p>Schematic diagram of microstructure evolution of the FZ under different heat-exposure temperatures.</p>
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14 pages, 28826 KiB  
Article
Laser Remelting of Ductile Cast Iron to Achieve a Graphite-Free Surface Layer for Enabling a Manual High-Gloss Finish
by Laura Kreinest, Johannes Schüssler, Onur Özaydin, Sujith Kochuthundil Subhash, Edgar Willenborg and Andreas Bührig-Polaczek
Metals 2024, 14(3), 347; https://doi.org/10.3390/met14030347 - 18 Mar 2024
Viewed by 1105
Abstract
Laser remelting is being explored as a viable technique for obtaining a graphite-free, defect-free surface layer on cast iron EN GJS 400-15. The goal is to obtain a large remelted layer along with a low surface roughness to enable a subsequent manual high-gloss [...] Read more.
Laser remelting is being explored as a viable technique for obtaining a graphite-free, defect-free surface layer on cast iron EN GJS 400-15. The goal is to obtain a large remelted layer along with a low surface roughness to enable a subsequent manual high-gloss surface finish. The impact of the laser remelting process parameters is evaluated by using samples with three different cooling rates, resulting in different graphite microstructures. By utilizing four passes and a laser power of 300 W, the smallest roughness and largest remelting depth are achieved. The remelted layer is mostly devoid of graphite particles. Subsequent manual polishing is performed to evaluate the potential for achieving a high-gloss finish with a roughness of Sa < 0.05 µm. Laser remelting alone does not improve visual appearance or reduce roughness. However, after manual polishing, the roughness of the laser-remelted surfaces with Sa = 0.018 µm is one order of magnitude smaller than the manually polished initial state. Graphite removal during laser remelting therefore makes it possible to achieve a conventional and high-gloss polish, overcoming the previous limitations of GJS materials. Full article
(This article belongs to the Topic Laser Processing of Metallic Materials)
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<p>(<b>a</b>) Schematic representation of the three cast geometries with a gating system. (<b>b</b>) Cooling rates of the distinct geometries.</p>
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<p>Light microscopy images of metallographically prepared cross-sections of the three geometries. (<b>a</b>) Geometry Y<sub>IV</sub>. (<b>b</b>) Geometry Y<sub>II</sub>. (<b>c</b>) Cylinder geometry.</p>
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<p>Microstructure analysis for the three geometries. Standard deviation calculated from 5 measurements. (<b>a</b>) Graphite content. (<b>b</b>) Nodularity. (<b>c</b>) Nodule count.</p>
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<p>Machine used for laser remelting.</p>
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<p>Exemplary representation of the measurement of the remelting depth from a microscopic image of the etched metallographically prepared cross-section.</p>
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<p>Roughness as a function of laser power for laser-remelted test fields on the three microstructures investigated. (<b>a</b>) Number of passes n = 1. (<b>b</b>) Number of passes n = 4. With d<sub>L</sub> = 500 µm, v<sub>scan</sub> = 50 mm/s, dy = 100 µm.</p>
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<p>Light microscopy images of laser-remelted test fields on a sample of the Y<sub>IV</sub> geometry. (<b>a</b>,<b>b</b>) Number of passes n = 1. (<b>c</b>,<b>d</b>) Number of passes n = 4. P<sub>L</sub> = 300 W, d<sub>L</sub> = 500 µm, v<sub>scan</sub> = 50 mm/s, dy = 100 µm.</p>
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<p>Remelting depth as a function of laser power for laser-remelted test fields on the three microstructures investigated. (<b>a</b>) Number of passes n = 1. (<b>b</b>) Number of passes n = 4. D<sub>L</sub> = 500 µm, v<sub>scan</sub> = 50 mm/s, dy = 100 µm.</p>
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<p>Light microscopy images of metallographically prepared cross-sections of laser-remelted test fields on a sample of the Y<sub>IV</sub> geometry. The yellow circles mark graphite particles in the remelted layer. (<b>a</b>) Number of passes n = 1. (<b>b</b>) Number of passes n = 4. P<sub>L</sub> = 300 W, d<sub>L</sub> = 500 µm, v<sub>scan</sub> = 50 mm/s, dy = 100 µm.</p>
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<p>(<b>a</b>) Remelting depth and (<b>b</b>) roughness as a function of laser power for laser-remelted test fields with various numbers of passes on a sample of the cylinder geometry. P<sub>L</sub> = 300 W, d<sub>L</sub> = 500 µm, v<sub>scan</sub> = 50 mm/s, dy = 100 µm.</p>
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<p>(<b>a</b>) Light microscopy image of a metallographically prepared cross-section of a laser-remelted test field on a sample of the cylinder geometry. (<b>b</b>) Surface topography of a laser-remelted test field on a sample of the cylinder geometry. P<sub>L</sub> = 300 W, d<sub>L</sub> = 500 µm, v<sub>scan</sub> = 50 mm/s, dy = 100 µm.</p>
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<p>(<b>a</b>) SEM image and (<b>b</b>) EBSD analysis (acceleration voltage: 20.00 kV, sample tilt angle (degrees): 70.00°, hit rate: 80.31%, acquisition speed: 12.02 Hz) of a metallographically prepared cross-section of a laser-remelted test field on a sample of the cylinder geometry. P<sub>L</sub> = 300 W, d<sub>L</sub> = 500 µm, v<sub>scan</sub> = 50 mm/s, dy = 100 µm.</p>
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<p>Demonstrator sample after laser remelting and manual polishing.</p>
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<p>Surface topography of the demonstrator sample. (<b>a</b>) Manually polished initial state. (<b>b</b>) Laser-remelted and manually polished surface.</p>
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20 pages, 17699 KiB  
Article
Effect of Hydrogen on Fatigue Life and Fracture Morphologies of TRIP-Aided Martensitic Steels with Added Nitrogen
by Tomohiko Hojo, Akihiko Nagasaka, Junya Kobayashi, Yuki Shibayama and Eiji Akiyama
Metals 2024, 14(3), 346; https://doi.org/10.3390/met14030346 - 17 Mar 2024
Viewed by 1120
Abstract
The effects of hydrogen on the tensile properties, fatigue life, and tensile and fatigue fracture morphologies of nitrogen-added ultrahigh-strength transformation-induced plasticity (TRIP)-aided martensitic (TM) steels were investigated. The total elongation and number of cycles to failure (Nf) of the hydrogen-charged [...] Read more.
The effects of hydrogen on the tensile properties, fatigue life, and tensile and fatigue fracture morphologies of nitrogen-added ultrahigh-strength transformation-induced plasticity (TRIP)-aided martensitic (TM) steels were investigated. The total elongation and number of cycles to failure (Nf) of the hydrogen-charged TM steels decreased with the addition of nitrogen; in particular, adding 100 ppm of nitrogen decreased the total elongation and Nf of the TM steels. The quasi-cleavage cracking around the AlN occurred near the sample surface, which is the crack propagation region, although dimples appeared at the center of the fracture surface in the tensile samples. The initial fatigue crack initiated at the AlN precipitate or matrix/AlN interface, located at the notch root. During crack propagation, new cracks were initiated at the AlN precipitates or matrix/AlN interfaces, while quasi-cleavage crack regions were observed around the AlN precipitates. The decrease in the total elongation and Nf of the hydrogen-charged TM steel with 100 ppm of added nitrogen might be attributable to the crack initiation around the AlN precipitates formed by a large amount of hydrogen trapped at the AlN precipitates and matrix/AlN interfaces, and to the dense distribution of AlN, which promoted crack linkage. Full article
(This article belongs to the Special Issue Fatigue, Creep Behavior and Fracture Mechanics of Metals)
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<p>Heat treatment diagram of annealing and isothermal transformation treatment processes for TM steels, in which “R<sub>T</sub>” and “O.Q.” represent room temperature and quenching in oil, respectively.</p>
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<p>Dimensions of (<b>a</b>) tensile test and (<b>b</b>) fatigue test specimens [<a href="#B7-metals-14-00346" class="html-bibr">7</a>]. The unit for these specimens is mm.</p>
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<p>Arrangements of (<b>a</b>) hydrogen charging and (<b>b</b>) fatigue test with hydrogen charging.</p>
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<p>(<b>a</b>,<b>c</b>,<b>e</b>) Scanning electron micrographs and (<b>b</b>,<b>d</b>,<b>f</b>) transmission electron micrographs of (<b>a</b>,<b>b</b>) TM-A, (<b>c</b>,<b>d</b>) TM-B and (<b>e</b>,<b>f</b>) TM-C steels.</p>
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<p>(<b>a</b>,<b>c</b>,<b>e</b>) Band contrast and (<b>b</b>,<b>d</b>,<b>f</b>) phase maps of (<b>a</b>,<b>b</b>) TM-A, (<b>c</b>,<b>d</b>) TM-B and (<b>e</b>,<b>f</b>) TM-C steels.</p>
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<p>Nominal stress—strain curves of (<b>a</b>) TM-A, (<b>b</b>) TM-B and (<b>c</b>) TM-C steels without and with hydrogen.</p>
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<p>Comparisons of (<b>a</b>) tensile strength (<span class="html-italic">TS</span>) and (<b>b</b>) total elongation (<span class="html-italic">TEl</span>) of nitrogen-added TM steels without and with hydrogen.</p>
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<p>Hydrogen embrittlement susceptibility (<span class="html-italic">HES</span>) of nitrogen-added TM steels.</p>
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<p><span class="html-italic">S</span>-<span class="html-italic">N</span> curves of (<b>a</b>) TM-A, (<b>b</b>) TM-B and (<b>c</b>) TM-C steels without and with hydrogen charging [<a href="#B7-metals-14-00346" class="html-bibr">7</a>].</p>
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<p>Comparisons of (<b>a</b>) fatigue limit (<span class="html-italic">FL</span>) without hydrogen and (<b>b</b>) number of cycles to failure (<span class="html-italic">N</span><sub>f</sub>) with hydrogen charging (Δ<span class="html-italic">σ</span> = 135 MPa, <span class="html-italic">σ</span><sub>max</sub> = 300 MPa, <span class="html-italic">σ</span><sub>min</sub> = 30 MPa) [<a href="#B7-metals-14-00346" class="html-bibr">7</a>].</p>
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<p>Fracture surfaces at (<b>a</b>,<b>c</b>,<b>e</b>) the center and (<b>b</b>,<b>d</b>,<b>f</b>) near the edge of tensile-tested (<b>a</b>,<b>b</b>) TM-A, (<b>c</b>,<b>d</b>) TM-B and (<b>e</b>,<b>f</b>) TM-C steels without hydrogen charging.</p>
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<p>Fracture surfaces at (<b>a</b>,<b>c</b>,<b>e</b>) the center and (<b>b</b>,<b>d</b>,<b>f</b>) near the edge of tensile-tested (<b>a</b>,<b>b</b>) TM-A, (<b>c</b>,<b>d</b>) TM-B and (<b>e</b>,f) TM-C steels with hydrogen charging. Yellow arrows in (<b>d</b>,<b>f</b>) represent AlN or traces of AlN.</p>
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<p>(<b>a</b>) Fracture surface and (<b>b</b>) energy-dispersive X-ray spectroscopy (EDX) analysis of the precipitate on the fracture surface in TM-C steel without hydrogen charging.</p>
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<p>Fatigue specimens after fatigue tests with hydrogen charging for (<b>a</b>) TM-A, (<b>b</b>) TM-B and (<b>c</b>) TM-C steels. Yellow arrows represent the crack propagation direction.</p>
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<p>Fracture surfaces of fatigue-tested TM-A steel with hydrogen charging. (<b>a</b>) Low-magnification image, (<b>b</b>) magnified image of crack initiation region at (b) in (<b>a</b>), (<b>c</b>) magnified image of crack propagation region at (c) in (<b>a</b>), (<b>d</b>) magnified image of final fracture region at (d) in (<b>a</b>).</p>
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<p>Fracture surfaces of fatigue-tested TM-B steel with hydrogen charging. (<b>a</b>) Low-magnification image, (<b>b</b>) magnified image of crack initiation region at (b) in (<b>a</b>), (<b>c</b>) magnified image of internal crack initiation region at (c) in (<b>a</b>), (<b>d</b>) magnified image of final fracture region at (d) in (<b>a</b>). Yellow arrows in (<b>c</b>) represent AlN or trace of AlN.</p>
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<p>Fracture surfaces of fatigue-tested TM-C steel with hydrogen charging. (<b>a</b>) Low-magnification image, (<b>b</b>) magnified image of crack initiation region at (b) in (<b>a</b>), (<b>c</b>) magnified image of internal crack initiation region at (c) in (<b>a</b>), (<b>d</b>) magnified image of internal crack initiation region at (d) in (<b>a</b>). Yellow arrows in (<b>c</b>) and (<b>d</b>) represent AlN or trace of AlN.</p>
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<p>Hydrogen desorption curves of TM steels [<a href="#B4-metals-14-00346" class="html-bibr">4</a>]. <span class="html-italic">H</span><sub>D</sub> denotes diffusible hydrogen concentration.</p>
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<p>Fracture surface of internal crack initiation region at AlN or trace of AlN of fatigue-tested TM-B steel with hydrogen. Yellow arrows represent traces of AlN. The density of AlN precipitation was 680 pieces/mm<sup>2</sup>.</p>
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<p>Fracture surface of internal crack initiation region at AlN of fatigue-tested TM-C steel with hydrogen. The density of AlN precipitation was 80 pieces/mm<sup>2</sup>.</p>
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15 pages, 4891 KiB  
Article
Efficient Recovery of Lithium from Spent Lithium Ion Batteries Effluent by Solvent Extraction Using 2-Ethylhexyl Hydrogen {[Bis(2-Ethylhexyl) Amino]methyl} Phosphonate Acid
by Xiaoqin Wang, Zhulin Zhou, Xuting Si, Youcai Lu and Qingchao Liu
Metals 2024, 14(3), 345; https://doi.org/10.3390/met14030345 - 17 Mar 2024
Cited by 1 | Viewed by 1940
Abstract
In order to overcome the interface emulsification problem of TBP-FeCl3 systems and the instability of β-diketone systems in high-concentration alkaline medium, it is necessary to design and synthesize some new extractants. By introducing amino groups into a phosphorus extractant, a new 2-ethylhexyl [...] Read more.
In order to overcome the interface emulsification problem of TBP-FeCl3 systems and the instability of β-diketone systems in high-concentration alkaline medium, it is necessary to design and synthesize some new extractants. By introducing amino groups into a phosphorus extractant, a new 2-ethylhexyl hydrogen {[bis(2-ethylhexyl)amino]methyl} phosphonate acid (HA) extractant was synthesized. In this study, an efficient method of recovering lithium from the effluent of spent lithium-ion batteries (LIBs) is proposed. Experiments were conducted to assess the influential factors in lithium recovery, including the solution pH, saponification degree, extractant concentration, and phase ratio. Over 95% of lithium in the effluent was extracted into the organic phase, and nearly all lithium in the organic phase could be stripped into the aqueous phase using a 3 mol/L HCl solution. There was no significant decrease in extraction capacity after 10 cycles. The experimental results indicated that the extraction mechanism was a cation exchange process, and the extractive complex was proposed as LiA. Importantly, after three months of stable operation, the process demonstrated excellent stability and extraction efficiency, with rapid phase separation and a clear interface. This study offers an efficient, cost-effective, and environmentally friendly method for lithium extraction from the effluent of spent LIBs. Full article
(This article belongs to the Special Issue Advances in Sustainable Hydrometallurgy)
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<p>The structure of HA.</p>
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<p>General scheme of the lithium recovery process.</p>
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<p>(<b>a</b>) Effect of pH on lithium extraction, (<b>b</b>) Effect of saponification degree, (<b>c</b>) Effect of pH value on lithium extraction by saponified organic. Extraction conditions: [Li<sup>+</sup>] = 3.6 g/L, [HA] = 1 mol/L, O:A = 1:1, 25 °C, t = 30 min.</p>
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<p>Effect of extraction time on lithium extraction. Extraction conditions: [Li<sup>+</sup>] = 3.6 g/L, [HA] = 1 mol/L, pH = 8.5, saponification ratio = 70%, O:A = 1:1, 25 °C.</p>
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<p>Effect of initial concentration of HA on lithium extraction. Extraction conditions: [Li<sup>+</sup>] = 3.6 g/L, pH = 8.5, saponification ratio = 70%, O:A = 1:1, 25 °C, t = 30 min.</p>
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<p>Effect of equilibrium concentration of NaA on lithium extraction. [Li<sup>+</sup>] = 3.6 g/L, pH = 8.5, saponification ratio = 70%, O:A = 1:1, 25 °C, t = 30 min.</p>
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<p>Infrared spectra of HA (<b>a</b>), saponified organic phase NaA (<b>b</b>), extracted organic phase LiA (<b>c</b>), and regenerated organic phase HA (<b>d</b>).</p>
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<p>Effect of temperature on lithium extraction. [Li<sup>+</sup>] = 3.6 g/L, [HA] = 1 mol/L, pH = 8.5, saponification ratio = 70%, O:A = 1:1, t = 30 min.</p>
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<p>Circular regeneration properties of the extraction HA. Extraction conditions: [Li<sup>+</sup>] = 3.6 g/L, [HA] = 1 mol/L, pH = 8.5, saponification ratio = 70%, O:A = 1:1, 25 °C, t = 30 min; Stripping conditions: 2 mol/L HCl, O:A = 1:1, 25 °C, t = 30 min.</p>
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<p>Effect of phase ratio on lithium extraction. [Li<sup>+</sup>] = 3.6 g/L, [HA] = 1 mol/L, pH = 8.5, saponification ratio = 70%, 25 °C, t = 30 min.</p>
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<p>Cross-flow extraction performance. [Li<sup>+</sup>] = 3.6 g/L, [HA] = 1 mol/L, pH = 8.5, saponification ratio = 70%, O:A = 1:1, 25 °C, t = 30 min.</p>
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<p>Effect of HCl concentration on lithium stripping. Stripping conditions: O:A = 10:1, 25 °C, t = 30 min.</p>
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<p>SEM and XRD pattern of Li<sub>2</sub>CO<sub>3</sub>.</p>
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<p>Whole-process flowchart of lithium recovery from the effluent of spent LIBs.</p>
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15 pages, 15324 KiB  
Article
Improved Discharge Performance of AZ72-0.05La Alloy Anode via Refining Mg17Al12 Phase
by Junqing Guo, Bo Wang and Shizhong An
Metals 2024, 14(3), 344; https://doi.org/10.3390/met14030344 - 17 Mar 2024
Viewed by 972
Abstract
The morphology of phases in magnesium alloys is vitally important for their performance. It is found that improved discharge performance is achieved in AZ72-0.05La alloy via a refining Mg17Al12 phase by means of hot rolling. Before rolling, as-cast AZ72-0.05La alloy [...] Read more.
The morphology of phases in magnesium alloys is vitally important for their performance. It is found that improved discharge performance is achieved in AZ72-0.05La alloy via a refining Mg17Al12 phase by means of hot rolling. Before rolling, as-cast AZ72-0.05La alloy has a relatively coarse and strip-like Mg17Al12 phase. After rolling, the Mg17Al12 phase becomes much finer, showing a granulated shape. Due to the refinement of the Mg17Al12 phase, the discharge voltage and energy density of an Mg-air battery with as-rolled AZ72-0.05La alloy as the anode increases by 6% and 3% under a discharge current density of 20 mA·cm−2 in a 3.5% NaCl solution, respectively. The corrosion rate of the as-rolled AZ72-0.05La alloy is slightly larger than the as-cast AZ72-0.05La alloy, but still much lower than as-cast AZ72 alloy. The as-rolled AZ72-0.05La alloy possesses a discharge voltage of 0.74 V and an energy density of 918 mWh·g−1 under a discharge current density of 20 mA·cm−2, and a relatively low corrosion rate of 0.51 mg·cm−2·h−1, demonstrating good overall discharge performance. This work provides a method for improving the discharge performance of Mg-air batteries. Full article
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<p>Tensile specimen dimensions.</p>
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<p>(<b>a</b>) XRD patterns and (<b>b</b>) DSC heating curves of the three magnesium alloys.</p>
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<p>Metallographic photos of (<b>a</b>) as-cast AZ72 alloy, (<b>b</b>) as-cast AZ72-0.05La alloy, and (<b>c</b>) as-rolled AZ72-0.05La alloy.</p>
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<p>SEM morphologies and EDS elemental mapping. (<b>a</b>) as-cast AZ72 alloy, (<b>b</b>) as-cast AZ72-0.05La alloy, and (<b>c</b>) as-rolled AZ72-0.05La alloy.</p>
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<p>Polarization curves of three magnesium alloys in 3.5 wt.% NaCl solution.</p>
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<p>(<b>a</b>) EIS in Nyquist plots of three magnesium alloys in 3.5 wt% NaCl solution, (<b>b</b>) Equivalent circuit for fitting the EIS.</p>
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<p>Corrosion rate and hydrogen evolution rate.</p>
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<p>(<b>a</b>) Room temperature mechanical properties (<b>b</b>) Hardness performance.</p>
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<p>Discharge curves of the investigated anodes in 3.5 wt % NaCl solution at current density of: (<b>a</b>) 2.5 mA·cm<sup>−2</sup>, (<b>b</b>) 5 mA·cm<sup>−2</sup>, (<b>c</b>) 10 mA·cm<sup>−2</sup>, (<b>d</b>) 20 mA·cm<sup>−2</sup>.</p>
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<p>Discharge performance of assembled Mg-air batteries with different anodes: (<b>a</b>) Anodic efficiency, (<b>b</b>) Energy density.</p>
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<p>The surface morphologies of as-cast AZ72 (<b>a</b>,<b>d</b>), as-cast AZ72-0.05La (<b>b</b>,<b>e</b>), and as-rolled AZ72-0.05La (<b>c</b>,<b>f</b>) alloy after the removal of discharge products. The experiments were conducted in a 3.5 wt% NaCl solution for 5 h, with discharge current density of 2.5 mA·cm<sup>−2</sup> (<b>a</b>–<b>c</b>) and 20 mA·cm<sup>−2</sup> (<b>d</b>–<b>f</b>).</p>
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14 pages, 5024 KiB  
Article
The Coupled Temperature Field Model of Difficult-to-Deform Mg Alloy Foil High-Efficiency Electro-Rolling and Experimental Study
by Gengliang Liu, Jiaxuan Yang, Tianren Shan, Huaimei Li, Dianlong Wang and Lipo Yang
Metals 2024, 14(3), 343; https://doi.org/10.3390/met14030343 - 17 Mar 2024
Viewed by 908
Abstract
In response to the challenging difficult-to-deform of magnesium foils, a high-efficiency and high-precision electro-rolling temperature field coupled model is established. This model is designed to simulate the non-annealing electric rolling (NAER) process of Mg foils under conditions of high current density, rapid temperature [...] Read more.
In response to the challenging difficult-to-deform of magnesium foils, a high-efficiency and high-precision electro-rolling temperature field coupled model is established. This model is designed to simulate the non-annealing electric rolling (NAER) process of Mg foils under conditions of high current density, rapid temperature rise rates, and large temperature gradients. Firstly, a coupled temperature field difference model for the guide roller, roll, and Mg foil is established, based on the equipment for NAER and the electrification conditions. The Joule heat, distortion heat, and friction heat in the electric rolling process were precisely considered. Secondly, considering the peculiarity of the heat source and the heat transfer mechanism during NAER, the influence of the dynamic boundary conditions on the instantaneous temperature of the Mg foil was analyzed, which was closer to the actual situation. The experimental results show that the original model can accurately simulate the transient temperature change in Mg foils during NAER, and the error between the predicted value and the measured value is within 7.1%. According to the calculation of the model, the microstructure of completely recrystallized magnesium foil with a grain size of 4.61 μm and a texture strength of 11.3 can be obtained at an inlet temperature of 250 °C. Full article
(This article belongs to the Special Issue Advances in Metal Rolling Processes)
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<p>Temperature field difference model of the NAER: (<b>a</b>) temperature field model meshing; (<b>b</b>) device of the NAER.</p>
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<p>Contact resistance coefficient of the guide roller.</p>
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<p>Contact resistance measurement and fitting curve.</p>
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<p>Experimental steps of the NAER.</p>
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<p>Calculated and experimental temperature values of Mg foils during the NAER: (<b>a</b>) 1.0 mm; (<b>b</b>) 0.5 mm.</p>
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<p>Peak temperature and exit temperature–current curve of the Mg foil of the NAER temperature field simulation under different reduction rates.</p>
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<p>The temperature rises in the deformation zone of Mg foils during the NAER with different reduction rates.</p>
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<p>The temperature field calculated with Mg foils by NAER with different thicknesses: (<b>a</b>) peak temperature; (<b>b</b>) outlet temperature.</p>
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<p>The temperature rises in the deformation zone of Mg foils during the NAER with different thicknesses.</p>
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<p>The temperature measured and calculated values of Mg foils by the NAER: (<b>a</b>) the transition zone temperature field in experiment 1; (<b>b</b>) inlet and outlet temperatures of the mill in experiment 2.</p>
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<p>Microhardness–time and temperature–time curves of Mg foils of the NARE.</p>
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<p>IPF and (0001) PF for Mg foils at the mill inlet at (<b>a</b>) 25.0 A/mm<sup>2</sup>; (<b>b</b>) 28.5 A/mm<sup>2</sup>; (<b>c</b>) 32.1 A/mm<sup>2</sup>.</p>
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<p>IPF and (0001) pole figures of a grain size of less than 2 μm at the mill inlet at 25.0 A/mm<sup>2</sup>.</p>
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15 pages, 4580 KiB  
Article
The Effects of Target Thicknesses and Backing Materials on a Ti-Cu Collision Weld Interface Using Laser Impact Welding
by Mohammed Abdelmaola, Brian Thurston, Boyd Panton, Anupam Vivek and Glenn Daehn
Metals 2024, 14(3), 342; https://doi.org/10.3390/met14030342 - 16 Mar 2024
Viewed by 1130
Abstract
This study demonstrates that the thickness of the target and its backing condition have a powerful effect on the development of a wave structure in impact welds. Conventional theories and experiments related to impact welds show that the impact angle and speed of [...] Read more.
This study demonstrates that the thickness of the target and its backing condition have a powerful effect on the development of a wave structure in impact welds. Conventional theories and experiments related to impact welds show that the impact angle and speed of the flyer have a controlling influence on the development of wave structure and jetting. These results imply that control of reflected stress waves can be effectively used to optimize welding conditions and expand the range of acceptable collision angle and speed for good welding. Impact welding and laser impact welding are a class of processes that can create solid-state welds, permitting the formation of strong and tough welds without the creation of significant heat affected zones, and can avoid the gross formation of intermetallic in dissimilar metal pairs. This study examined small-scale impact using a consistent launch condition for a 127 µm commercially pure titanium flyer impacted against commercially pure copper target with thicknesses between 127 µm and 1000 µm. Steel and acrylic backing layers were placed behind the target to change wave reflection characteristics. The launch conditions produced normal collision at about 900 m/s at the weld center, with decreasing impact speed and increasing angle moving toward the outer perimeter. The target thickness had a large effect on wave morphology, with the wave amplitude increasing with target thickness in both cases, peaking when target thickness is about twice flyer thickness, and then falling. The acrylic backing showed a consistently smaller unwelded central zone, indicating that impact welding is possible at a smaller angle in that case. Strength was measured in destructive tensile testing. Failure was controlled by the breakdown of the weaker of the two base metals over all thicknesses and backings. This demonstrates that laser impact welding is a robust method for joining dissimilar metals over a range of thicknesses. Full article
(This article belongs to the Special Issue Impact Welding Technology of Metal Alloys)
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<p>Laser system and experimental chamber.</p>
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<p>Schematic of the directionality of the joint interface.</p>
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<p>The flyer velocity as a function of displacement.</p>
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<p>Various frames (<b>a</b>–<b>l</b>) captured every 2 µs by a high-speed camera following laser irradiation reveal the protrusion and the formation of cone-shaped dimples on the titanium flyer plate.</p>
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<p>Microstructures of interfacial waves at different target thicknesses in both perpendicular and parallel directions, with steel backing.</p>
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<p>Interfacial wavelength and amplitude, for different target thicknesses, in both perpendicular and parallel directions, with steel backing.</p>
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<p>The effect of different target thicknesses on the interfacial waves with steel backing in a direction perpendicular to the stand-off.</p>
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<p>Effect of different target thicknesses on the interfacial waves, with acrylic backing.</p>
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<p>Interfacial wavelength and amplitude for different target thicknesses with steel backing and acrylic backing.</p>
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<p>The impact of normalized target thickness on the wavelength relative to the literature.</p>
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<p>Interfacial waves for different target thicknesses for both steel and acrylic backing at the left side from the center of the weld.</p>
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<p>The dimensions of the non-welded zone localized at the center of the weld with steel and acrylic backing.</p>
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<p>The un-welded zone relative to the different target thicknesses with steel and acrylic backing.</p>
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<p>Lap shear-tested samples with (<b>a</b>) steel (<b>b</b>) acrylic backing.</p>
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<p>Load–displacement curves for lap shear test of welded samples with (<b>a</b>) steel (<b>b</b>) acrylic backing.</p>
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<p>Peak loads during lap shear test at different target thicknesses for steel and acrylic backing.</p>
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<p>Energy absorbed during lap shear test at different target thicknesses for steel and acrylic backing.</p>
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25 pages, 6196 KiB  
Article
Use of Electrochemical Noise for the Study of Corrosion by Passivated CUSTOM 450 and AM 350 Stainless Steels
by Facundo Almeraya-Calderon, Miguel Villegas-Tovar, Erick Maldonado-Bandala, Maria Lara-Banda, Miguel Angel Baltazar-Zamora, Griselda Santiago-Hurtado, Demetrio Nieves-Mendoza, Luis Daimir Lopez-Leon, Jesus Manuel Jaquez-Muñoz, Francisco Estupiñán-López and Citlalli Gaona-Tiburcio
Metals 2024, 14(3), 341; https://doi.org/10.3390/met14030341 - 16 Mar 2024
Cited by 4 | Viewed by 1111
Abstract
Precipitation-hardening stainless steels, like AM 350 and Custom 450, are extensively utilized in various aerospace applications. The latter steel is utilized for applications needing great strength and corrosion resistance. In contrast, the former steel has a good corrosion resistance and moderate strength. The [...] Read more.
Precipitation-hardening stainless steels, like AM 350 and Custom 450, are extensively utilized in various aerospace applications. The latter steel is utilized for applications needing great strength and corrosion resistance. In contrast, the former steel has a good corrosion resistance and moderate strength. The purpose of this study was to analyze transient frequencies in the electrochemical noise of Custom 450 and AM 350 stainless steels that had been passivated for 60 and 90 min at 25 and 49 °C using baths of citric and nitric acid and then immersed in solutions containing 1% sulfuric acid (H2SO4) and 5% sodium chloride (NaCl). The potentiodynamic polychromatic curves employed electrochemical techniques and noise (EN) based on the ASTM-G5 and G199 standards. Two methods of data analysis were applied concerning EN: the domain of frequencies (power spectral density, PSD) and the time–frequency domain (Hilbert-Huang Transform). The PHSS passivated in citric acid indicated current densities in the H2SO4 solution between 10−2 and 10−3 mA/cm2, while those in the NaCl solution were recorded around 10−4 and 10−5 mA/cm2. The citric acid functions as a passivating agent. The results of the electrochemical noise analysis show that the PHSS passivated in nitric acid displayed a greater corrosion resistance. Moreover, there is a tendency for PHSS to be passivated in nitric acid to corrode locally. Full article
(This article belongs to the Special Issue Electrochemical Analysis of Metal Corrosion)
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<p>Diagram of the passivation process of PHSSs in acid baths.</p>
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<p>OM microstructures of PHSSs. (<b>a</b>) Custom 450 and (<b>b</b>) AM 350.</p>
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<p>Potentiodynamic polarization curves for Custom 450 samples passivated in citric and nitric acids at 25 and 49 °C for 60 and 90 min: (<b>a</b>,<b>c</b>) NaCl and (<b>b</b>,<b>d</b>) H<sub>2</sub>SO<sub>4</sub> solutions.</p>
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<p>Potentiodynamic polarization curves for AM 350 samples passivated in citric and nitric acids at 25 and 49 °C for 60 and 90 min: (<b>a</b>,<b>c</b>) NaCl and (<b>b</b>,<b>d</b>) H<sub>2</sub>SO<sub>4</sub> solutions.</p>
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<p>PSDs in currents for Custom 450 passivated at 25 °C exposed to (<b>a</b>) NaCl and (<b>b</b>) H<sub>2</sub>SO<sub>4</sub> solutions and Custom 450 passivated at 49 °C exposed to (<b>c</b>) NaCl and (<b>d</b>) H<sub>2</sub>SO<sub>4</sub> solutions.</p>
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<p>PSDs in currents for AM 350 passivated at 25 °C exposed to (<b>a</b>) NaCl and (<b>b</b>) H<sub>2</sub>SO<sub>4</sub> solutions and AM 350 passivated at 49 °C minutes exposed to (<b>c</b>) NaCl and (<b>d</b>) H<sub>2</sub>SO<sub>4</sub> solutions.</p>
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<p>Z<sub>n</sub> for Custom 450 passivated at 25 °C exposed to (<b>a</b>) NaCl and (<b>b</b>) H<sub>2</sub>SO<sub>4</sub> solutions and Custom 450 passivated at 49 °C minutes exposed to (<b>c</b>) NaCl and (<b>d</b>) H<sub>2</sub>SO<sub>4</sub> solutions.</p>
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<p>Z<sub>n</sub> for AM 350 passivated at 25 °C exposed to (<b>a</b>) NaCl and (<b>b</b>) H<sub>2</sub>SO<sub>4</sub> solutions and AM 350 passivated at 49 °C minutes exposed to (<b>c</b>) NaCl and (<b>d</b>) H<sub>2</sub>SO<sub>4</sub> solutions.</p>
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<p>Hilbert spectra for Custom 450 samples passivated at 25 °C in citric acid (<b>a</b>–<b>d</b>) and nitric acid (<b>e</b>–<b>h</b>) and exposed to NaCl (<b>a</b>,<b>c</b>,<b>e</b>,<b>g</b>) and H<sub>2</sub>SO<sub>4</sub> (<b>b</b>,<b>d</b>,<b>f</b>,<b>h</b>). (<b>a</b>,<b>b</b>,<b>e</b>,<b>f</b>) were passivated for 60 min; (<b>c</b>,<b>d</b>,<b>g</b>,<b>h</b>) were passivated for 90 min.</p>
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<p>Hilbert spectra for Custom 450 samples passivated at 49 °C in citric acid (<b>a</b>–<b>d</b>) and nitric acid (<b>e</b>–<b>h</b>) and exposed to NaCl (<b>a</b>,<b>c</b>,<b>e</b>,<b>g</b>) and H<sub>2</sub>SO<sub>4</sub> (<b>b</b>,<b>d</b>,<b>f</b>,<b>h</b>). (<b>a</b>,<b>b</b>,<b>e</b>,<b>f</b>) were passivated for 60 min; (<b>c</b>,<b>d</b>,<b>g</b>,<b>h</b>) were passivated for 90 min.</p>
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<p>Hilbert spectra for AM 350 samples passivated at 25 °C in citric acid (<b>a</b>–<b>d</b>) and nitric acid (<b>e</b>–<b>h</b>) and exposed to NaCl (<b>a</b>,<b>c</b>,<b>e</b>,<b>g</b>) and H<sub>2</sub>SO<sub>4</sub> (<b>b</b>,<b>d</b>,<b>f</b>,<b>h</b>). (<b>a</b>,<b>b</b>,<b>e</b>,<b>f</b>) were passivated for 60 min; (<b>c</b>,<b>d</b>,<b>g</b>,<b>h</b>) were passivated for 90 min.</p>
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<p>Hilber spectra for AM 350 samples passivated at 49 °C in citric acid (<b>a</b>–<b>d</b>) and nitric acid (<b>e</b>–<b>h</b>) and exposed to NaCl (<b>a</b>,<b>c</b>,<b>e</b>,<b>g</b>) and H<sub>2</sub>SO<sub>4</sub> (<b>b</b>,<b>d</b>,<b>f</b>,<b>h</b>). (<b>a</b>,<b>b</b>,<b>e</b>,<b>f</b>) were passivated 60 min; (<b>c</b>,<b>d</b>,<b>g</b>,<b>h</b>) were passivated 90 min.</p>
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<p>Model diagrams of passivation processes in citric and nitric acid baths for CUSTOM 450 and AM 350 stainless steels exposed to (<b>a</b>) 5 wt.% NaCl solution and (<b>b</b>) 1 wt.% H<sub>2</sub>SO<sub>4</sub> solution.</p>
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13 pages, 3442 KiB  
Article
Effect of Deformation Degree on Microstructure and Properties of Ni-Based Alloy Forgings
by Ruifeng Dong, Jian Li, Zishuai Chen, Wei Zhang and Xing Zhou
Metals 2024, 14(3), 340; https://doi.org/10.3390/met14030340 - 15 Mar 2024
Cited by 1 | Viewed by 997
Abstract
The primary objective of this paper is to investigate the influence of deformation degree on the microstructure and properties of a Ni-based superalloy. An upsetting experiment was conducted using a free-forging hammer to achieve a deformation degree ranging from 60% to 80%. The [...] Read more.
The primary objective of this paper is to investigate the influence of deformation degree on the microstructure and properties of a Ni-based superalloy. An upsetting experiment was conducted using a free-forging hammer to achieve a deformation degree ranging from 60% to 80%. The impact of the forging deformation degree on the hardness and high-temperature erosion performance was evaluated using the Rockwell hardness tester (HRC) and high-temperature erosion tester, respectively. The experimental results indicate that as the deformation degree increased, the hardness of the forged material progressively increased while the rate of high-temperature erosion gradually decreased. In order to comprehensively study the mechanism behind the variations in forging performance, optical microscopy (OM), scanning electron microscopy (SEM), electron backscatter diffraction (EBSD), and transmission electron microscopy (TEM) were employed. The findings reveal that as the deformation degree increased, the presence of small-angle grain boundaries and an increase in grain boundary area contributed to enhanced hardness in the alloy forgings. Furthermore, it was discovered that grain boundaries with twin orientation promoted dynamic recrystallization during deformation, specifically through a discontinuous dynamic recrystallization mechanism. Additionally, the precipitated γ′ phase in the alloy exhibited particle sizes ranging from 40 to 100 nm. This particle size range resulted in a higher critical shear stress value and a more pronounced strengthening effect on the alloy. Full article
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<p>Schematic diagram of the material selection location.</p>
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<p>Microstructure of forgings of the GH4738 alloy with different degrees of deformation: (<b>a</b>) 62%; (<b>b</b>) 68%; (<b>c</b>) 72%; (<b>d</b>) 80%.</p>
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<p>γ′ phase in GH4738 alloy forgings at different deformation levels: (<b>a</b>) 62%; (<b>b</b>) 68%; (<b>c</b>) 72%; (<b>d</b>) 80%.</p>
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<p>Comparison of average grain size, γ′ phase particle size, and hardness of samples with different deformation degrees.</p>
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<p>High-temperature erosion morphology of specimens with different degrees of deformation: (<b>a</b>) 62%; (<b>b</b>) 68%; (<b>c</b>) 72%; (<b>d</b>) 80%.</p>
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<p>Effect of deformation degree on hardness and high temperature wear rate of the GH4738 alloy, cm<sup>3</sup>/Kg.</p>
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<p>EBSD diagram and distribution pattern of grain boundaries with different phase differences for GH4738 alloy. (<b>a</b>) EBSD diagram of forgings with a deformation of 80%; (<b>b</b>) the distribution of grain boundaries with orientation differences in different states of the alloy; (<b>c</b>) the distribution of &lt;2°and 2–5° orientation difference grain boundaries in different states of the alloy.</p>
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<p>Distribution of orientation angles along the direction of the straight-line segment in <a href="#metals-14-00340-f006" class="html-fig">Figure 6</a>. ((<b>a</b>,<b>b</b>) Point to origin, (<b>c</b>,<b>d</b>) point to point).</p>
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<p>EBSD diagram of GH4738 alloy forgings with 80% deformation. (<b>a</b>) Angle diagram of orientation difference between grains (&gt;15°, 5~15°, and 2~5° black line, green line, and red line are used in turn); (<b>b</b>) Σ3, Σ9 twin boundary (indicated by blue line and yellow line in turn); (<b>c</b>) dislocation density diagram between grains (increased from blue to white in turn); (<b>d</b>) distribution of recrystallized grains (indicated by blue, yellow, and red areas for complete recrystallization, substructure, and incomplete recrystallization in turn).</p>
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<p>TEM image of GH4738 alloy forgings with an 80% deformation degree.</p>
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