Influence of cooling rate during the heat treatment process on the precipitates and ductility behavior of inconel 718 superalloy fabricated by selective laser melting
IN718 superalloy by elective laser melting (SLM) has shown great application prospects in the aerospace engine key parts. Different phases are precipitated during the SLM forming process. Although the Laves phase could be dissolved in dendrites by heat treatment, the specific evolution of the second...
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Veröffentlicht in: | Materials science & engineering. A, Structural materials : properties, microstructure and processing Structural materials : properties, microstructure and processing, 2024-06, Vol.902, p.146603, Article 146603 |
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Sprache: | eng |
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Zusammenfassung: | IN718 superalloy by elective laser melting (SLM) has shown great application prospects in the aerospace engine key parts. Different phases are precipitated during the SLM forming process. Although the Laves phase could be dissolved in dendrites by heat treatment, the specific evolution of the second phase particles is still unclear. In this work, the influences of solution and aging heat treatment, as well as cooling rate on the precipitates and ductility behavior of IN718 superalloy fabricated by SLM were systematically investigated. The medium temperature (980 °C) solution treatment regimes included three different colling rates and the control group only underwent aging treatment were studied. The results indicated that high temperature solid solution treatment effectively improved compositional segregation and significantly enhanced homogeneity of microstructure. The reduce of cooling rate at 980 °C was beneficial to the extension time and increased the number of δ phase precipitation. An appropriate number of δ phase improves the notch sensitivity and nails grain boundaries. In addition, the complex dislocations and second phase particles retards the migration of slip dislocations during ductility deformation process, which enhances the strength of SLM-ed IN718. The yield strength of specimens increases from 680 MPa to 1205 MPa. The microhardness is greatly improved as compared with as-deposited IN718, and the highest microhardness reaches 485 HV. The results provide a technical support and reference for formulating the heat treatment schedule of IN718 prepared by SLM.
•The designed heat treatment is carried out on SLM fabricated IN718 by changing the cooling rate of solution treatment.•δ precipitation increases significantly with decreasing the cooling rate from 8 °C/min to 4 °C/min of solution treatment.•The IN718 by SLM after HT-1 presents an excellent match of high σYS (1130 MPa), σUTS (1356 MPa), and microhardness (485 HV).•IN718 is ductile fracture as long as after the solution treatment and aging treatment. |
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ISSN: | 0921-5093 1873-4936 |
DOI: | 10.1016/j.msea.2024.146603 |