hot forming introduction
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Hot Forming Introduction
2014.6.16
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Thermal thick shells for the tools (TSHELL=1)
Thermal gravity loading simulation
Thermal press hardening simulation
Default friction coefficient for hot forming (0.46)
Initial temperatures for both blanks and tools
Support of *DEFINE_TABLE_3D for *MAT_106/*MAT_244
Thermal time step for hot forming
New features
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Basic unit system
All the units will be converted to basic unit [ton, mm , s, N] in the input deck.
Unit in the GUI
Commonly used unit is provided in the GUI, user does not need to convertthem to the basic unit system manually in the hot forming setup.
Unit system
!"## $%&'() *+,% -./0% 1/%##2/% 3./4 ./ 6&%/'7 8%+(7 69"#:0
,.;292#
!"# $$ % & '() & $$ !"#+$$,- '()
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Hot forming process
./)01!2 3")41#5 6"! 7"/$1#5 (/8%% 9)/48#1#5
Full processes of hot forming in eta/Dynaform 5.9.2
Thestagesofgravity loading andpress hardening areoptional.
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Thermal thick shells for the tools
Thermal thick shells
*CONTROL_SHELLTSHELL=1
*CONTROL_CONTACTITHOFF=1
The heat transfer from blank to the tools is proportional to the temperaturegradient of the contact partners.
The thermal thick shells give us higher accuracy for longer contact times.This is necessary for the gravity phase and slow tool velocity.
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Thermal thick shells for the tools
Thermal thick shells
The artificial thickness can be calculated from the thermal effusivity
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Thermal gravity loading simulation
Since the blank material is very soft at high temperatures, the bending
of the blank during the insertion might be significant. This could affect
the initial blank position before the press hardening process.
The material properties change significantly with the temperature.
During the insertion of the hot blank into the press, some areas of theblank get in contact with the tools, some do not. In those areas where
contact occurs, the temperature of the blank decreases significantly dueto the cooling of the tools. Thus, the initial temperature distribution in the
blank before the forming stage is NOT uniform.
Thermal gravity loading
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FrictionSince there is no lubricant in hot forming, the friction is very high, the
default friction coefficient is 0.46. The user can change this if necessary.
Thermal friction
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Supports *DEFINE_TABLE_3D for stress/strain
Support of *DEFINE_TABLE_3D
Temperature
Strain rate
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Thermal time stepThermal time step is higher than the mechanical time step with dynamic
explicit time integration:
Thermal time step
TMAX = !"#$$% '(%$)*#+,
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Hot Formingis a separate module.
GUI of hot forming
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The tools of gravity/hardening arereferred to as the tools of forming.
GUI of hot forming
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Blank material definition: Structural
Thermal
Blank sheet material definition
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Select the material type anddefine the parameters of the
material.
Structural material
MAT106*MAT_ELASTIC_VISCOPLASTIC_THERMAL
MAT244*MAT_UHS_STEEL
Thermal material
1. *MAT_THERMAL_ISOTROPIC
2. *MAT_THERMAL_ORTHOTROPIC
3. *MAT_THERMAL_ISOTROPIC_TD
4.
*MAT_THERMAL_ORTHOTROPIC_TD5.
*MAT_THERMAL_ISOTROPIC_PHASE
_CHANGE
6. *MAT_THERMAL_ISOTROPIC_TD_LC
Blank sheet material definition
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Select the material type anddefine the parameters of the
material.
Structural material
MAT20 *MAT_RIGID
Tool structural material is definedautomatically.
Thermal material
1. *MAT_THERMAL_ISOTROPIC
2.
*MAT_THERMAL_ORTHOTROPIC
3.
*MAT_THERMAL_ISOTROPIC_TD
4. *MAT_THERMAL_ORTHOTROPIC_TD
5.
*MAT_THERMAL_ISOTROPIC_PHASE_CHANGE
6.
*MAT_THERMAL_ISOTROPIC_TD_LC
Tool material definition
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Setup the contact parameters foreach tool.
Contact parameters
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Setup the initial temperature foreach tool.
Used for all tools All tools have
the same initial temperature.
Initial temperature for tools
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The initial temperature of theblank is defined in the boundary
of the 1ststage.
The temperature information file
*.new_temp_ic.inc will be
included.
User can select Celsius(C)or
Kelvin(K) as the unit of
temperature.
Boundary condition
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User can modify the default parameters for hot forming in default config.
Configuration for hot forming