PSI - Issue 14
Manojakumar Chimmat et al. / Procedia Structural Integrity 14 (2019) 746–757 Author name / Structural Integrity Procedia 00 (2018) 000 – 000
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4. Conclusions
Residual stresses in the DMLS CoCrMo and SS316L were evaluated and studied in the as printed and heat treated condition using the Sin 2 technique, for two geometries. Both the alloys were produced with a dense structure with little or no porosity (0.043% in CoCrMo and 0.038% in SS316L). The layer by layer structure of the as printed CoCrMo is seen to undergo partial recrystallization at 1050 °C followed by a completely recrystallized microstructure at 1150 °C . The residual stresses correlate with the microstructure evolution by measuring a tensile stress of 250 MPa and a showing a compressive behaviour with a similar magnitude (of 300 MPa), between the as printed and grit blasted conditions, in the CoCrMo samples. Upon heat treatment, a sinusoidal residual stress behaviour was noted, going from tensile (950 C) to compressive (1050 C) to a completely stress relieved state at 1150 C. The residual stress response was similar for both the geometries. Between the CoCrMo and SS316L, the optimized process parameters for a dense part indicated a residual stress that seemed to relate to the material yield strength, with the SS316L measuring only half (127 MPa) that of CoCrMo in the as printed condition. Overall, the role of processing parameters in influencing the residual stress and hence in distortion or defect free DMLS materials is brought out via this study. Acknowledgements This study was done during the internship tenure of Manojakumar Chimmat at the Repair Development Center (RDC), GE Power, Bangalore, India as part of his M.Tech thesis. The authors are thankful to the global RDC management for their sponsorship of the projects. INTECH, DMLS, is acknowledged for the DMLS samples provided for this study. References Basak, A., and Das, S. (2016) . “Epitaxy and Microstructure Evolution in Metal Additive Manufacturing.” Annu. Rev. Mater. Res. , 46(1), 125 – 149. Bawane, K. K., Srinivasan, D., and Banerjee, D. (2018). “Microstructural Evolution and Mechanical Properties of Direct Metal Laser-Sintered (D MLS) CoCrMo After Heat Treatment.” Metall. Mater. Trans. A . Bi, G., Sun, C. N., Chen, H. chi, Ng, F. L., and Ma, C. C. K. (2014). “Microstructure and tensile properties of superalloy IN 100 fabricated by micro- laser aided additive manufacturing.” Mater. Des. , 60, 401 – 408. FRARENDI. (2018). “Gas turbines first stage nozzles.”
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