2018
DOI: 10.1016/j.jallcom.2018.01.029
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Hot workability and microstructure evolution of the nickel-based superalloy Inconel 718 produced by laser metal deposition

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Cited by 78 publications
(16 citation statements)
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“…A reduction of porosity was obtained by high deformation rates and a high degree of deformation, which also leads to higher fatigue strength. Previous work of Bambach and Sizova [10] focused on the forming of AM-preforms made of Ti6Al4V and Inconel 718 [11]. A good formability of both materials was observed in the 3D printed state, with lower activation energy for hot forming.…”
Section: Introductionmentioning
confidence: 95%
“…A reduction of porosity was obtained by high deformation rates and a high degree of deformation, which also leads to higher fatigue strength. Previous work of Bambach and Sizova [10] focused on the forming of AM-preforms made of Ti6Al4V and Inconel 718 [11]. A good formability of both materials was observed in the 3D printed state, with lower activation energy for hot forming.…”
Section: Introductionmentioning
confidence: 95%
“…Graphite flakes were added between the end face of sample and anvil to reduce friction. The softening effect caused by thermal effect during deformation can be calculated by formula ∆ = − , where Q is an activation energy, R is the gas constant (8.314 J/(mol•K), ΔT is measured by thermocouple, and n, α are material parameters, which are later presented in Equation (7). There is one sample for each experimental condition, and only one sample is added when the experimental results are obviously abnormal.…”
Section: Specimen Preparationmentioning
confidence: 99%
“…It is concluded that NRA has limited effect on that of the accuracy SCAM model. This is because each of the test data was also used when TLRM and NRA were used to solve the four parameters in Equation (7). Therefore, the NRA had less influence on the SCAM results than it did on the J-C model.…”
Section: Evaluation Of the Phenomenological Modelsmentioning
confidence: 99%
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“…The use of superalloys is particularly dominant in aerospace engines and various industrial gas turbines. [1][2][3][4][5][6] However, the working conditions of Ni-Cr-Fe superalloys that have a working temperature of 800 C or higher are extremely demanding. The amount of water vapor in the exhaust gas reaches 20%, which accelerates the corrosion of the material; in addition, high-frequency cyclic stress results in fatigue damage and eventually material breakage.…”
Section: Introductionmentioning
confidence: 99%