Fabrication of thin-wall components using the laser powder bed fusion(LPBF)additive manufacturing(AM)technology was investigated for two“hard-to-weld”high gamma prime Ni-based superalloys RENé65(R65)and REN...Fabrication of thin-wall components using the laser powder bed fusion(LPBF)additive manufacturing(AM)technology was investigated for two“hard-to-weld”high gamma prime Ni-based superalloys RENé65(R65)and RENé108(R108).Simple block parts with wall thicknesses of 0.25 mm,1.00 mm,and5.00 mm are printed using a bidirectional laser scanning strategy without layer-wise rotation.Parts with walls thinner than 5 mm fail before reaching the designated build height.Results indicate that reduction of limiting build height(LBH)corresponds to the reduction of part thickness and is unaffected by alloy composition.On the contrary,the number of internal micro-cracks along columnar grain boundaries in the build direction(BD)increases with part thickness and is significantly higher in R108 than R65.These findings suggest that reduced LBH in parts with thinner walls is not caused by internal micro-crack formation.Fractography and finite element analysis(FEA)of the in-process thermal stresses show that the LBH trend is not explained by the conventional cracking mechanism.Simulations suggest that part thickness affects stress distribution leading to more substantial distortion and consequent failure to add layers for continued fabrication of thinner parts.展开更多
基金supported by the Natural Sciences and Engineering Research Council of Canada(NSERC)(No.CRDPJ 533406-18)
文摘Fabrication of thin-wall components using the laser powder bed fusion(LPBF)additive manufacturing(AM)technology was investigated for two“hard-to-weld”high gamma prime Ni-based superalloys RENé65(R65)and RENé108(R108).Simple block parts with wall thicknesses of 0.25 mm,1.00 mm,and5.00 mm are printed using a bidirectional laser scanning strategy without layer-wise rotation.Parts with walls thinner than 5 mm fail before reaching the designated build height.Results indicate that reduction of limiting build height(LBH)corresponds to the reduction of part thickness and is unaffected by alloy composition.On the contrary,the number of internal micro-cracks along columnar grain boundaries in the build direction(BD)increases with part thickness and is significantly higher in R108 than R65.These findings suggest that reduced LBH in parts with thinner walls is not caused by internal micro-crack formation.Fractography and finite element analysis(FEA)of the in-process thermal stresses show that the LBH trend is not explained by the conventional cracking mechanism.Simulations suggest that part thickness affects stress distribution leading to more substantial distortion and consequent failure to add layers for continued fabrication of thinner parts.
