Phase Transformation and Mechanical Behavior of Laser Powder Bed Fusion (LPBF) Manufactured Co-28Cr-6Mo

dc.contributor.authorWaite, Lucy Rebekah Aien
dc.contributor.committeechairFu, Yaoen
dc.contributor.committeememberAcar, Pinaren
dc.contributor.committeememberPhilen, Michael Keithen
dc.contributor.departmentAerospace and Ocean Engineeringen
dc.date.accessioned2025-06-05T08:02:07Zen
dc.date.available2025-06-05T08:02:07Zen
dc.date.issued2025-06-04en
dc.description.abstractThis thesis analyzes how laser powder bed fusion (LPBF) additive manufacturing print settings affect the phase transformation properties, tensile mechanical properties, microstructure, and fracture behavior of Co-28Cr-6Mo. Four different LPBF print settings were analyzed and compared in this study, with varying laser powers, scan speeds, and hatch spacings. It was found that for the phase transformation properties, Co-28Cr-6Mo's phase transformation rate from a metastable γ-phase face-centered-cubic (FCC) structure to ϵ-phase hexagonal-close packed (HCP) structure varies in speed and sensitivity to phase transformation aging temperature depending on the print setting. Phase transition time reached a minimum for all the samples at around a Tp = 850 or 860◦C. The 250W-400mm/s-100μm sample transformed at the fastest rates with the most sensitivity of these rates to aging temperature, while the 350W-800mm/s-125μm sample was one of the slowest to transform at the peak transformation temperature, but also least sensitive to changes in the aging temperature. For tensile behaviors, the print settings affected the ultimate strengths and elongations at fracture, leading to the 250W-400mm/s-100μm outperforming the other sets when mostly FCC, and 350W-800mm/s-125μm outperforming the others after the phase transformation. As the phase composition transformed from the as-built γ-phase FCC structure to the ϵ-phase HCP structure, samples became more brittle, but also had much higher resulting ultimate strengths. Analysis of the microstructure of these samples revealed that the massive phase transformation occurring in LPBF Co-28Cr-6Mo had lamellar structures of HCP forming within the FCC matrix, and that grain size decreased while orientation preference slightly increased in the samples as HCP percent increased within the phase composition of Co-28Cr-6Mo. Common fracture features were also identified for the varying phase compositions and print settings, which found that cleavage fracture structures and a surface dimpling texture were the most common features identifiable within the fracture surfaces. Varying the print settings and temperature at which samples were tensile tested modified which structures were most present in the fracture, allowing for correlation to be made between the testing conditions used, tensile properties analyzed, and the resulting features present on the sample.en
dc.description.abstractgeneralThis thesis analyzes how laser powder bed fusion (LPBF), which is an additive manufacturing process for metals, and the settings input to the LPBF machine affect the properties of a high-temperature and corrosion-resistant cobalt-based material used in aerospace and biomedical prosthetic applications. This material, made up of approximately 28% chromium, 6% molybdenum, and the rest made up of a cobalt base, is shortened to Co-28Cr-6Mo or CoCrMo. CoCrMo, which is typically crystalline in nature, has its atoms arranged in a crystal structure called face-centered-cubic (FCC) after being printed on the LPBF. When heated up to and held constant at temperatures between around 700-900◦C, CoCrMo undergoes a solid-to-solid phase transformation from the FCC crystal structure, to a new structure called hexagonal-close-packed (HCP) over the course of 2 hours to several days of what is called an aging heat treatment. These transformation times vary greatly with respect to the temperature at which CoCrMo is aged and the various internal properties of the CoCrMo sample being heat-treated. CoCrMo can exist as 100% FCC, 100% HCP, or some mixed phase composition of FCC and HCP as well (such as 50% FCC and 50% HCP), depending on the amount of time CoCrMo is aged. This paper analyzes how the different settings on the LPBF and different phase compositions of CoCrMo affect the material's strength, internal structure, and mechanisms for fracture and breakage due to an applied force. This thesis finds that the phase transformation typically occurs the fastest when samples are aged at what is defined as the peak rate temperature, which is around 850 or 860◦C for CoCrMo, and also finds that different LPBF print settings lead to shorter or faster times for the phase to reach 100% HCP from FCC. Additionally, print settings can affect the sensitivity of a CoCrMo sample to the aging temperature as well, leading to some samples transitioning much slower when the aging temperature deviates from this peak rate temperature, while some samples are more consistent with their transition rates, even with variations in aging temperature. CoCrMo also had varying strength to tensile forces depending on the print settings and phase composition as well, leading to the material having more brittle or ductile behavior depending on these settings and phase. As the phase transforms to be dominantly HCP, samples can resist higher forces before breaking, but also become more brittle. These different settings and phase compositions lead to variations in how the material behaves on a micro-scale and nano-scale as well, and can be analyzed using electron microscopy and electron backscatter diffraction to look at properties on the 1-100μm scales. These small-scale properties can give insight into the root causes of the variations in material strength and phase transformation behaviors. These small-scale properties were also found to vary depending on the print settings analyzed in this thesis, leading to a greater understanding of how different LPBF print settings and aging heat treatments can affect the resulting properties of components made from CoCrMo.en
dc.description.degreeMaster of Scienceen
dc.format.mediumETDen
dc.identifier.othervt_gsexam:44101en
dc.identifier.urihttps://hdl.handle.net/10919/135064en
dc.language.isoenen
dc.publisherVirginia Techen
dc.rightsIn Copyrighten
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/en
dc.subjectCo-28Cr-6Moen
dc.subjectSuperalloysen
dc.subjectLPBFen
dc.subjectLaser Powder Bed Fusionen
dc.subjectMechanical Propertiesen
dc.subjectMicrostructureen
dc.titlePhase Transformation and Mechanical Behavior of Laser Powder Bed Fusion (LPBF) Manufactured Co-28Cr-6Moen
dc.typeThesisen
thesis.degree.disciplineAerospace Engineeringen
thesis.degree.grantorVirginia Polytechnic Institute and State Universityen
thesis.degree.levelmastersen
thesis.degree.nameMaster of Scienceen

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