Yan An-ru, Yang Tian-tian, Wang Yan-ling etc. Forming process and high-temperature mechanical properties of variable energy laser selective melting manufacturing IN718 superalloy[J]. Editorial Office of Optics and Precision Engineering, 2015,23(6): 1695-1704
Yan An-ru, Yang Tian-tian, Wang Yan-ling etc. Forming process and high-temperature mechanical properties of variable energy laser selective melting manufacturing IN718 superalloy[J]. Editorial Office of Optics and Precision Engineering, 2015,23(6): 1695-1704 DOI: 10.3788/OPE.20152306.1695.
Forming process and high-temperature mechanical properties of variable energy laser selective melting manufacturing IN718 superalloy
Selective laser melting manufacturing IN718 powder with changed laser energy densities was researched. The part to be machined was divided into a core and a contour
and the selective laser melting manufacturing was performed by changing the laser energy density. Firstly
a numerical model of sintering in melting pool was set up
the influencing factors of changed laser energy densities on the densification of the part were obtained by changing laser energy densities
and the microstructure features of the formed part were observed. Then
by increasing scanning for the contour and changing the laser energy densities
the effect law of changed laser energy densities on the surface quality of the part was also obtained. Finally
the heat treatment processing was optimized and the high-temperature tensile strength and high temperature lasting time properties of the part were improved to obtain the perfect surface quality. The results indicate when the linear laser energy density is 300 J/m
the optimal densification level of formed part is as high as 98.9%. In this condition
the typical microstructures of the formed part are dendrite and equiaxial crystals along the deposition direction and are equiaxial crystal along the inside layer. Using the core + contour scanning way
the optimal surface quality of the part is obtained in laser energy densities of 100 J/m with the roughness of 3.1 μm. The optimal high temperature performance of the formed part is realized by solution + double aging combination in 1 065 ℃
in which the high temperature tensile strength is 1 356 MPa and the high temperature lasting time is 34 h. Results show that the IN718 nickel-based super alloy manufactured by selective laser melting can satisfy the demands of complex aerospace parts for the densfication level
good forming quality and high-temperature mechanical properties.
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