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Materials Science in Additive Manufacturing                        Multi-material Ti6Al4V-B4C through L-DED



            must be examined. Additive manufacturing (AM) has   and compression testing. These tests were performed to
            many benefits over traditional manufacturing, including   evaluate whether a radial structure of two Ti alloys would
            the ease of constructing multi-material structures.  These   exhibit synergistic behavior, potentially surpassing the
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            multi-material structures facilitate the study of different   performance of the control Ti alloy.
            arrangements of multiple alloys within a single structure.
            Structures manufactured with different alloys have been   2. Materials and methods
            used for various applications, such as coating hard materials   2.1. Processing of Ti64 and Ti64-B4C radial
            onto soft but ductile ones to improve wear resistance   composite (RC) structures
            and thin layers of high thermally conductive materials
            onto poor conductors to increase the high-temperature   Samples were printed using a FormAlloy (Spring Valley,
            applications of an alloy.  Thus, different structure designs   CA, USA) five-axis DED AM system. The Ti6Al4V (Ti64)
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            were investigated to further improve an alloy’s mechanical   powder was purchased from AP&C (GE Additive, USA),
            properties. Radial bimetallic structures have demonstrated   and non-spherical-B C (B4C) powder (particle size: 15
                                                                                4
            the  potential  to  enhance  the mechanical  properties  of  a   – 45  µm) was attained from Reade Advanced Materials
            cylinder. 11,12  This has led to the development of an annular   (USA). The build chamber was maintained at an O  level of
                                                                                                       2
            toolpath for manufacturing the cylinders used in this study.   <20 ppm during the print in an argon-filled environment.
            The control and first treated samples were monolithic in   The powders were sieved to ensure that the powders had
            design, using the control alloy and composite; the second   a particle size between 15 µm and 63 µm. Although DED
            treated sample was constructed using both the control   systems prefer a coarser powder particle size of 45 – 150 µm,
            and composite, with the core consisting of the control and   the printing parameters were optimized to accommodate
            composite shell. This could potentially increase the service   finer powder particle size. The radial shape was designed,
            life  of  components  made  from  Ti6Al4V,  which  requires   and the corresponding G-code was written to print.
            high temperature and wear resistance. Coating the exterior   Figure 1A displays an example of the toolpath for six sample
            with the composite could enhance these properties without   layers. Nominal dimensions are oversized to avoid rough
            compromising the excellent properties of Ti6Al4V.  exterior and uneven surfaces after machining. The radial
                                                               toolpath requires different scan speeds of the laser head for
              Alloys of Ti and boron carbide (B4C) have been studied   the annular sections of the cylinders. The scan speed for
            for high-temperature and wear applications due to the   the Ti64 varied from 1000 to 1200 mm/min, while the scan
            increased formation of TiC and TiB within the matrix,   speed for Ti6Al4V + 5wt.% B4C (Ti64-B4C) varied from
            leading to improvements in the properties mentioned   400 to 600 mm/min. The Ti64-B4C powders were mixed
            above. 13-16  Both TiC and TiB form around the particle due   and ball-milled for 30  min to achieve a homogeneous
            to local concentrations of boron and carbon exceeding   mixture.  Three  sets  of  samples  were  printed:  monolithic
            the required levels for formation within the matrix. Thus,   Ti64, monolithic Ti64-B4C, and a RC cylinder comprising
            the particles become bonded to the matrix, forming a   a Ti64 core and Ti64-B4C cylindrical shell, with one
            metal matrix composite (MMC). Manufacturing these   example displayed in Figure 1B. With the different types
            MMCs requires extensive parameter optimization for   of samples and treatments, to simplify the terminology,
            successful production. 14,17  With AM, these optimizations   the monolithic Ti64 samples will be referred to as Ti64,
            can be achieved more rapidly compared to conventional   the monolithic Ti64-B4C samples as Ti64-B4C, and the
            manufacturing methods.  This benefit facilitates the easier   RC samples as RC. The layer height for both monolithic
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            production of MMCs when utilizing directed energy   types (Ti64 and Ti64-B4C) was 0.295 mm, while that of RC
            deposition (DED)-based AM.                         was 0.21 mm. The laser power used for Ti64 and Ti64-B4C
              Previous studies have used various AM types, including   cylinders were 320 and 350 W, respectively, while that of RC
            powder-based DED to wire arc DED, 12,19  to develop multi-  samples used both laser powers depending on the section
            material structures through alloying composites, and   of the sample. With FormAlloy, the powder feeders, seen
                                           ,
            bimetallics. 12,19,20  However, these studies did not focus   in Figure 1E, use a feed rate of rotations per minute (RPM)
            on radial bimetallic structures involving MMCs. Herein,   to determine the rate at which the powder is delivered to
            cylinders were produced using powder-based DED to   the deposition head of the printer. For all sample types, a
            additively manufacture a control and two treated samples.   feed rate of 0.26 RPM was used. With monolithic samples,
            After the fabrication of the cylinders, they were subjected   the carrier gas flow rate used was 8 L/min, and the shield
            to various tests, including X-ray diffraction (XRD) for   gas flow rate was 12 L/min. For RC samples, the powder
            phase analysis of the control and treated samples, energy   feeders’ carrier gas flow rate was 6 L/min, and the shield
            dispersive spectroscopy (EDS), Vickers microhardness,   gas flow rate was 15 L/min.


            Volume 3 Issue 3 (2024)                         2                              doi: 10.36922/msam.3571
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