3.1 Mechanism of hot cracking
The formation of hot cracking we discussed in this paper is determined by two factors: the temperature and the strain rate.
1) The yield strength decreases with the increase of the temperature. There are a lot of dislocations in the material and a large number of them gather to form the Cottrell atmosphere. On the micro-level, the yield strength is the force that dislocations overcome the pinning of the Cottrell atmosphere's surroundings. With the increase of the temperature, the pinning effect of the Cottrell atmosphere on the dislocations is weakened and the force required for the dislocations' slip is also reduced. On the macro level, it is manifested as a decrease in the yield strength of the material;
2) The yield strength increases with the strain rates. The time responded to the strains decreases when the strain rates rise. It causes work hardening and more external stress will be applied to the whole material for completing the whole forming process. On the macro level, it is manifested as an increase in the yield strength of the material.
3.2 Points prone to cracks
According to the mechanism of cracks' formation mentioned above, cracks are easy to occur in the high temperature region or in the low strain rate region. From the simulation results of DEFORM-3D, P1 is located in the area with the highest temperature as shown in Fig. 9 (a) and P2 is located in the area with the lowest equivalent strain rates from 4.32×10-5 to 0.053, as shown in Fig. 9 (b). Two representative characteristic points P1 and P2 are selected on the deformed body after the ultra-high temperature forging process. If P1 and P2 do not crack during the upsetting [19-21] and the whole workpiece will not crack. In the traditional forging process, the temperature differences in the deforming body after the upsetting are small, as shown in Fig. 9 (c) . The differences of the equivalent strain rate are also very small with the lowest equivalent strain rates from 6.33×10-4 to 0.0358, as shown in Fig. 9 (d).
When the temperature and the equivalent strain rate are known, the maximum principal stress can evaluate the possibility of cracks in the forging process. The workpiece is prone to cracks in the place where the maximum principal stress is large. So in the traditional forging process only one representative point P1 is selected, as shown in Fig. 9 (c). P1 is located in the area with the highest maximum principal stress. In the same way, if no cracks occur at P1, the entire workpiece will not crack.
3.3 Hot cracking prediction method
In the ultra-high temperature forging process, the temperature is 1430℃ and the equivalent strain is 0.42 at P1 where the strain rate is 0.02 s-1. According to the calculation results of JMatPro®, the maximum stress Assab 718 can bear is 9.55 MPa, as shown in Fig. 10 (a). It is larger than the maximum principal stress of 9.27 MPa obtained by the finite element simulation, so there is no crack at P1. When the temperature is 1200℃ at P2, the deformation strain rate is 0.001 s-1 and the equivalent strain is 0.02. According to the JMatPro®, the maximum stress the material can bear is 16.25 MPa, as shown in Fig. 10 (b). It is larger than the maximum principal stress of 15.14 MPa obtained by the finite element simulation, so there is no crack at P2. In the traditional forging process, the temperature of P1 is 1200℃ and the equivalent strain becomes 0.02 where the strain rate is 0.01 s-1. According to JMatPro®, the maximum stress that Assab 718 plastic mold steel can bear is 17.41 MPa, as shown in Fig. 10 (c). It is less than the maximum principal stress of 21 MPa obtained by the finite element simulation. Therefore it is easy to crack at P1 during the traditional forging process. In the production process, the reduction speed should be reasonably controlled to increase the strain rate.
3.1 Mechanism of hot cracking
The formation of hot cracking we discussed in this paper is determined by two factors: the temperature and the strain rate.
1) The yield strength decreases with the increase of the temperature. There are a lot of dislocations in the material and a large number of them gather to form the Cottrell atmosphere. On the micro-level, the yield strength is the force that dislocations overcome the pinning of the Cottrell atmosphere's surroundings. With the increase of the temperature, the pinning effect of the Cottrell atmosphere on the dislocations is weakened and the force required for the dislocations' slip is also reduced. On the macro level, it is manifested as a decrease in the yield strength of the material;
2) The yield strength increases with the strain rates. The time responded to the strains decreases when the strain rates rise. It causes work hardening and more external stress will be applied to the whole material for completing the whole forming process. On the macro level, it is manifested as an increase in the yield strength of the material.
3.2 Points prone to cracks
According to the mechanism of cracks' formation mentioned above, cracks are easy to occur in the high temperature region or in the low strain rate region. From the simulation results of DEFORM-3D, P1 is located in the area with the highest temperature as shown in Fig. 9 (a) and P2 is located in the area with the lowest equivalent strain rates from 4.32×10-5 to 0.053, as shown in Fig. 9 (b). Two representative characteristic points P1 and P2 are selected on the deformed body after the ultra-high temperature forging process. If P1 and P2 do not crack during the upsetting [19-21] and the whole workpiece will not crack. In the traditional forging process, the temperature differences in the deforming body after the upsetting are small, as shown in Fig. 9 (c) . The differences of the equivalent strain rate are also very small with the lowest equivalent strain rates from 6.33×10-4 to 0.0358, as shown in Fig. 9 (d).
When the temperature and the equivalent strain rate are known, the maximum principal stress can evaluate the possibility of cracks in the forging process. The workpiece is prone to cracks in the place where the maximum principal stress is large. So in the traditional forging process only one representative point P1 is selected, as shown in Fig. 9 (c). P1 is located in the area with the highest maximum principal stress. In the same way, if no cracks occur at P1, the entire workpiece will not crack.
3.3 Hot cracking prediction method
In the ultra-high temperature forging process, the temperature is 1430℃ and the equivalent strain is 0.42 at P1 where the strain rate is 0.02 s-1. According to the calculation results of JMatPro®, the maximum stress Assab 718 can bear is 9.55 MPa, as shown in Fig. 10 (a). It is larger than the maximum principal stress of 9.27 MPa obtained by the finite element simulation, so there is no crack at P1. When the temperature is 1200℃ at P2, the deformation strain rate is 0.001 s-1 and the equivalent strain is 0.02. According to the JMatPro®, the maximum stress the material can bear is 16.25 MPa, as shown in Fig. 10 (b). It is larger than the maximum principal stress of 15.14 MPa obtained by the finite element simulation, so there is no crack at P2. In the traditional forging process, the temperature of P1 is 1200℃ and the equivalent strain becomes 0.02 where the strain rate is 0.01 s-1. According to JMatPro®, the maximum stress that Assab 718 plastic mold steel can bear is 17.41 MPa, as shown in Fig. 10 (c). It is less than the maximum principal stress of 21 MPa obtained by the finite element simulation. Therefore it is easy to crack at P1 during the traditional forging process. In the production process, the reduction speed should be reasonably controlled to increase the strain rate.