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Modeling of Compression Molding Problems using PASSAGE®/COMPRESSION Software
  • Thin - walled geometries
  • Hele - Shaw or Barone - Caulk model for flow
  • Thermoplastics or thermosets
  • Filling and heat transfer coupled
  • Post-fill curing
  • Fiber orientations
Modeling of Injection Molding Problems
  • Thin - walled geometries
  • Hele - Shaw model for flow
  • Filling and heat transfer coupled
  • Thermoplastics or thermosets
  • Packing and curing
  • Mold cooling
  • Fiber orientations
General Capabilities
  • Injection or compression mold flow analysis
  • Newtonian and non-Newtonian fluids
  • Isothermal and non-isothermal
  • Coupled flow and energy equations
  • Multiple gates and inserts
  • Prediction of frozen and molten layer interfaces during filling
  • Fiber orientations
  • Shrinkage and warpage analysis of parts due to cooling
  • Analysis of packing and curing (cooling) stages
  • Stress analysis of parts under external static and dynamic loads
Different Levels of Modeling
  • Isothermal filling analysis
  • Non-isothermal filling analysis
  • Packing and curing (non-isothermal)
  • Mold cooling or heating
  • Fiber orientation analysis
  • Warpage analysis
  • DT due to filling, packing and curing
  • DT due to uneven mold cooling or heating
  • Shrinkage indices
Factors Affecting Warpage
  • Uneven shrinkage due to filling and packing
  • Nonuniform temperature distribution due to mold cooling or heating
  • Anisotropic and non-homogeneous material properties due to orientations of fibers
3-D Transient Heat Transfer
  • Coupled with fluid flow
  • Frozen layer prediction
  • Fiber orientations and warpage
  • Layered finite element model across the cavity thickness
Fiber Orientation - Injection Molding
From Velocity Field:
  • Shear Layer - fibers to flow
  • Core Layer - fibers to flow or determined from orientation tensor calculations
For Stress Analysis:
  • Layered composite model
  • Locally orthotropic layers
Determine Mechanical Properties from Halpin - Tsai Equations
Fiber Orientation - Compression Molding (SMC)
Procedure:
  • Determine velocity field over time
  • Find fiber orientation from solving orientation tensor equations
  • Determine mechanical properties from:
    - Squeeze flow test correlations, or Halpin - Tsai equations
  • Determine Thermal Properties from:
    - Squeeze flow test correlations, or Schapery's equations
  • Perform Warpage and Stress Analysis
PASSAGE®/COMPRESSION Design and Analysis Procedure
  1. Construct finite element mesh of part geometry.
  2. Define process conditions.
  3. Perform a non-isothermal filling analysis.
  4. If necessary, modify conditions and repeat steps 1 through 3 until favorable filling conditions are reached.
  5. Perform a fiber-orientation analysis to determine fiber orientation through the layers.
  6. Using fiber orientation information, construct a laminated composite shell model for stress analysis:
    - Analyze part under initial thermal strains to determine warpage.
    - Analyze part (warped geometry) under external loads for structural integrity.
If necessary, modify the conditions and repeat steps 1 through 6 or 5 through 6 until a satisfactory design is obtained.
Features of PASSAGE®/COMPRESSION Software
  • Injection and compression molding processes.
  • Newtonian and non-Newtonian fluids.
  • Additional material models can be incorporated.
  • An accurate and efficient layered finite element model for thermal energy equation in thin-walled geometries.
  • Accurate prediction of solid-fluid interfaces
  • Multiple gates and inserts.
  • Analysis of packing (shrinkage) and curing after mold-filling.
  • Prediction of fiber orientations.
  • Has built-in pre- and post-processors.
  • Can interface with other preprocessors.
  • Readily adaptable to specialized applications:
  • - Injection molding
    - In-mold coating
    - Structural RIM

An Injection Molding Analysis - (Air-Conditioning System Evaporator Plate)
Geometry:
  • Received part drawings
  • Imported into 3D-CAD environment
  • Generated finite element mesh
  • Received mold drawings
  • Imported into 3D-CAD environment
  • Generated finite element mesh
Filling Analysis:
  • Part fill pattern is obtained
Mold Cooling Analysis:
  • Temperature variation over part surfaces is obtained
Warpage Analysis:
  • Deformed geometry of part is obtained
Filling Analysis
  • Melt front history
  • Pressure and temperature results
  • - Grid size : 1200 grid points
    - Run time (CPU) : 4 hours on workstation

Process Conditions
Part
  • Material: 20% Talc Filled Polypropylene
  • Mold Temp: 80°F
  • Melt Temp: 450°F
  • Fill Time: 2 sec
  • Flow Rate: 242 cm3/sec
  • Coef. Conduction: 1.94 x 104 cm2 K)
  • Specific Heat: 2.264 x 107 K)
  • Mass Density: 0.862 gm/cm3
  • Cooling Cycle: 60 sec 
Mold
  • Material: Steel
  • Coef. Conduction: 3.63 x 106 cm2 K)
Mold Cooling Analysis
  • Description of transient temperature variation in mold and over part surfaces
  • Cooling channels modeled
  • Interaction effects of filling included
    - Grid size : 23,000 grid points
    - Run time (CPU) : 20 minutes on a workstation
A Cycle-Averaged Mold Heating/Cooling Analysis
  • Accounts for transient temperature effects over part surfaces
Steps
  • Perform a non-isothermal filling analysis under fixed mold temperatures
  • Continue solving heat transfer equation until ejection (cycle) time
  • Determine final bulk temperature distribution in part
  • Calculate amount of heat removed or added during cycle
  • Perform a heat transfer analysis of mold to determine cycle averaged temperature distribution in mold and part surfaces
  • Use obtained temperature distributions for warpage predictions of part
Warpage Analysis
  • Displacement of part due to warpage:
    - Grid size : 1200 grid points
    - Run time (CPU) : 10 minutes on a workstation
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