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Materials Science in Additive Manufacturing                  Additive manufacturing of NASA HR-1 angled walls



            from A-286 and JBK-75 alloys. NASA HR-1 was designed   The  LP-DED  process  has  some  limitations,  such
            to  improve  strength  and corrosion resistance while   as geometric build angles, variations in thickness and
            offering superior weldability compared to A-286 and JBK-  surface texture, and the potential for process defects.  It
                                                                                                          1,9
            75. The alloy’s chemical modifications include an increased   has been shown that walls with angles >30° begin to fail
            nickel and molybdenum content to mitigate solidification   during deposition, whereas failure occurs at angles above
            fractures. In addition, the tungsten content was increased   45° in laser powder bed fusion.  In addition, varying the
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            to enhance the solution hardening treatment and reduce   orientation of the build can lead to different degrees of
            the formation of the acicular η-Ni Ti phase. Furthermore,   anisotropic characteristics in the AM microstructure.  To
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            titanium and aluminum levels were also elevated to   optimize the LP-DED process, the build parameters must
            promote the formation of spherical γ’ precipitates, thereby   be  adjusted during printing to strike a  balance  between
            improving the alloy’s strength. The chromium and   build deposition rates and geometric resolutions. Key
            vanadium volume fractions were maintained to ensure   parameters include laser power  and spot size, powder
            that NASA HR-1 retains the high corrosion resistance   flow  rate,  gas  flow  rate,  travel  speed,  layer  height,  and
            characteristic of A-286 and JBK-75 alloys. 1,2     hatching.   High  laser  power  is  particularly  important
                                                                      1,13
              The alloy NASA HR-1 is used in aerospace components,   for alloys like NASA HR-1, as it has a high melting point
            particularly in liquid rocket engines. These components, such   and high thermal conductivity that enables rapid heat
                                                                        2
            as regeneratively cooled nozzles, are designed to withstand   dissipation.  Consequently, laser power levels between
            extreme conditions, including high temperatures, high   1,200 W and 3,000 W are essential for effectively additively
            cyclic pressures, and hydrogen-rich environments, which   manufacturing this alloy using LP-DED. Increased laser
            render materials susceptible to hydrogen embrittlement. 1,3-5    power  may  produce  deeper  melt  pools,  allowing  higher
            Conventionally, regeneratively cooled nozzles were   deposition rates and thus, enhancing raw material
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            produced using vacuum induction melting and vacuum   utilization efficiency.  It is also crucial to maintain a
            arc remelting, followed by hot or cold rolling to fabricate   balance between these parameters, as they can alter the
            individual parts that are subsequently assembled into   thermodynamics  during  solidification,  which,  in  turn,
            the final engine components. This conventional process   affects the microstructure and mechanical properties
            is expensive and time-consuming. In  contrast, additive   of the alloy. 1,10,11  The primary objective of this study is to
            manufacturing (AM) processes, such as laser powder direct   assess the impact of different laser power settings and build
            energy deposition (LP-DED), are being explored as viable   angles on the microstructure and mechanical properties
            alternatives due to their potential to reduce production costs   of walls following heat treatment. The variables used in
            and facilitate the fabrication of large-scale components with   this study were selected based on previous research that
            complex features.  In addition, AM is considered more   demonstrated variations in performance when using
                          4,6
            sustainable than traditional manufacturing processes, such   1,070 W and 2,620 W before any heat treatment. This study
            as casting and powder metallurgy, which have low efficiency   evaluated the effectiveness of heat treatment in achieving
            in terms of material utilization and energy consumption.    a homogeneous microstructure across all angled walls. In
                                                         7,8
            At present, AM is employed across different industries,   addition, mechanical properties such as microhardness,
            including aerospace, oil and gas, industrial, power, and   tensile strength, and low cycle fatigue (LCF) were compared
            energy, to create new components and repair damaged   to evaluate different manufacturing parameters for angled
            parts.  DED  is  capable  of  producing  parts  from  a  range   walls in component fabrication.
            of high-performance materials, such as stainless steel,   2. Materials and methods
            titanium, nickel, cobalt, and aluminum-based alloys.  For
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            instance, Inconel 718 has been manufactured using the   Angled  walls  with  a  thickness  of  13  mm  were  built
            same technology and has shown an ultimate tensile strength   using rotary-atomized NASA HR-1 powder supplied by
            (UTS) of 711 MPa and a yield strength (YS) of 464 MPa   Homogenized Metals Inc. (HMI; USA) in a boxed-shaped
            after heat treatment.  These mechanical properties can be   structure, employing  two different  sets  of parameters,
                            10
            achieved by designing a suitable heat treatment process   1,070  W and 2,620 W. This geometry was chosen to
            that facilitates the creation of the desired microstructure.   facilitate the formation of desired build angles. The layer
            The LP-DED process involves creating a melt pool using a   height, travel speed, and powder feed rate are shown in
            laser while simultaneously feeding metal powder into the   Table 1. These parameters were modified to create the
            melt pool; this powder melts and solidifies during cooling.   desired build angle and laser power settings. The walls were
            In addition, the use of an inert gas is essential to prevent   deposited at angles of 0°, 20°, and 30° relative to the build
            any contamination between layers during the deposition   direction, as shown in Figure 1. The walls were heat treated
            process. 11                                        in the following order: Stress relief, homogenization,


            Volume 4 Issue 1 (2025)                         2                              doi: 10.36922/msam.8069
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