Hot die forging process optimization of superalloy IN718 turbine disc using processing map and finite element method

被引:26
|
作者
Zhang, H. Y. [1 ]
Zhang, S. H. [1 ]
Li, Z. X. [2 ]
Cheng, M. [1 ]
机构
[1] Chinese Acad Sci, Inst Met Res, Shenyang 110016, Liaoning, Peoples R China
[2] Beijing Inst Aeronaut Mat, Beijing, Peoples R China
关键词
superalloy IN718; turbine disc; processing map; finite element method; microstructure simulation; HIGH-TEMPERATURE DEFORMATION; METADYNAMIC RECRYSTALLIZATION; MICROSTRUCTURAL EVOLUTION; FLOW BEHAVIOR; INCONEL-718; WORKING; SIMULATION; IN-718;
D O I
10.1243/09544054JEM1571
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The deformation constitutive equation and the microstructure models in terms of critical strain, dynamic recrystallization, and grain growth for superalloy IN718 have been established based on the isothermal compression tests. Non-isothermal upsetting experiments have been carried out to refine and validate the microstructure evolution models. A processing map has been generated using the flow stress data obtained from the isothermal compressing tests. According to the processing map, the Optimum hot working parameters for superalloy IN718 have been obtained. The effect of process parameters on the microstructure development during the hot die forging of IN718 turbine disc have been investigated through Coupling the microstructure evolution prediction system developed with a commercial FE software, MSC.Superform. To design the hot die forging of IN718 turbine disc, a uniform Function Of microstructure has been proposed as the goal function. On the basis of simulation results, the optimum hot die forging parameters have been obtained.
引用
收藏
页码:103 / 110
页数:8
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