TY - JOUR
TI - Thermal simulation model of aero-engine blade material forging simulation
AU - Dai Huaren
AU - Chen Zhe
AU - Guo Wei
AU - Wang Ju
JN - Thermal Science
PY - 2021
VL - 25
IS - 4
SP - 3169
EP - 3177
PT - Article
AB - During the high temperature forging process, the thermal parameters such as  the temperature field and strain field in the blank have an important  influence on the crack damage and micro-structure in the forging. We use the  rigid viscoelastic finite element method to carry out the forging process of  a heavy aero-engine blade the finite element numerical simulation was  carried out to obtain the temperature field, strain field and forging load  change law in the forging process with time, and on this basis, combined  with the crack damage and repair mechanism and the re­crystallization  structure evolution law, an optimization was proposed. The forging process  plan. That is, the pre-forging is performed on the basis of the tolerance of  the final forging dimension under pressure of 4 mm, the pre-forging  temperature is 1160°C, and the final forging temperature is 1120°C. The  actual forging process test verifies the feasibility of the process plan,  which is the engineering of this process the application lays the  scientific foundation.