Compression mold shrinkage can change the size, flatness, and fit of BMC and SMC parts after molding. The problem often starts with the compound, mold temperature, or fiber direction, but it appears later as a dimensional inspection failure.
Designers must control BMC molding, SMC compression molding, and the thermoset molding process from the first design review.
A mold cavity that matches the target part size at room temperature may produce an undersized part after cooling.
This article explains how to predict shrinkage, size the cavity, select process settings, and inspect molded parts. It also shows why a stable compression mold design matters for repeatable production.
BMC and SMC parts usually shrink between about 0.1 percent and 0.4 percent in the main flow direction, but the actual value depends on the compound, fiber orientation, mold temperature, pressure, cure time, geometry, and post-mold cooling. A reliable compression mold uses supplier shrinkage data, a controlled mold temperature, uniform wall thickness, correct charge placement, and a measured mold trial. For a 100.00 mm feature, a 0.20 percent shrinkage allowance requires a cavity size of about 100.20 mm before final process correction.
Compression mold shrinkage is the reduction in part dimensions between molding and a defined inspection condition. Thermoset compounds do not behave like simple liquid plastics. BMC and SMC contain resin, fillers, glass fibers, additives, and curing agents. Each material changes volume during heating, flow, curing, and cooling.
During molding, the resin heats and cures inside the cavity. The compound may expand while it reaches the mold temperature. After cure, it cools to room temperature and contracts. The final dimension is the result of both effects.
Glass fibers reduce shrinkage along their length. They can also create different shrinkage across the flow direction. This difference is called anisotropic shrinkage. It can cause warpage, corner movement, and hole position changes.
Mineral fillers generally reduce resin shrinkage. A high glass fiber content may lower shrinkage in one direction but increase dimensional differences in another direction. BMC often has a short fiber structure. SMC uses longer fiber strands and may show stronger orientation effects in large or thin parts.
Thick areas retain heat longer than thin areas. A rib, boss, or mounting pad can cool at a different rate from the main wall. This creates local shrinkage and stress. Uneven cooling is a common cause of sink marks and warpage.
The values below are engineering starting points. They are not a replacement for the compound supplier's data sheet or a mold trial.
| Material or condition | Typical linear shrinkage range | Main dimensional risk | Recommended design action |
|---|---|---|---|
| BMC with mineral filler | 0.10% to 0.25% | Local variation around ribs and inserts | Use measured cavity compensation and balanced cooling |
| BMC with higher glass content | 0.10% to 0.30% | Directional shrinkage and fiber marks | Check both flow and cross-flow dimensions |
| SMC with standard glass reinforcement | 0.15% to 0.40% | Warpage in large panels | Control charge layout, pressure, and mold temperature |
| Low-profile or low-shrink SMC | 0.05% to 0.20% | Variation between compound lots | Confirm the supplier's shrinkage and cure data |
For example, a 250.00 mm SMC panel with 0.30 percent shrinkage may finish about 0.75 mm smaller in one direction. A 100.00 mm BMC feature with 0.15 percent shrinkage may finish about 0.15 mm smaller.
The basic cavity compensation formula is:
Cavity dimension = target part dimension / (1 - shrinkage rate)
For a 100.00 mm target and 0.20 percent shrinkage:
100.00 / (1 - 0.002) = 100.20 mm approximately
This calculation is a starting point. The final mold size should also consider mold steel temperature, measurement temperature, machine pressure, and process capability.
| Factor | BMC | SMC |
|---|---|---|
| Material form | Bulk charge with short fibers | Sheet charge with longer glass fibers |
| Common use | Electrical housings, brackets, appliance parts | Automotive panels, covers, structural housings |
| Fiber orientation | Usually more uniform in small parts | More sensitive to sheet placement and flow direction |
| Typical risk | Local dimensional change near bosses | Panel warpage and uneven edge shrinkage |
| Charge control | Control weight, shape, and location | Control sheet size, stacking, and coverage |
| Best process control | Stable preheating and cavity filling | Stable charge layout and balanced flow |
Ask for the compound grade, filler percentage, glass fiber content, recommended mold temperature, cure time, density, and shrinkage range. Record the direction used for each value. A single shrinkage number is not enough for a large SMC panel.
Measure the part at a controlled temperature. ISO 2577 provides a common framework for shrinkage testing of thermosetting plastics. ASTM D955 is also used to measure molding shrinkage. The inspection report should state the time after molding and the part temperature.
Use separate compensation values for length, width, and height when the material is anisotropic. Do not apply one value to every axis if the part has strong fiber orientation.
Keep walls as uniform as the design allows. A practical target for many compression molded housings is a wall variation within plus or minus 10 percent of the nominal thickness. Larger changes can create different cooling rates.
Use enough draft to release the cured part without high ejection force. Many thermoset parts use about 0.5 to 2 degrees of draft, depending on surface texture, depth, and compound. Deep textured surfaces may need more.
Metal inserts can cool faster than the compound. This may create local shrinkage or stress. Use controlled insert temperature when possible, and inspect hole location with a coordinate measuring machine.
The cavity must remain stable at the molding temperature. A mold operating at 150 to 180 degrees C can expand by several tenths of a millimeter over a large length. The mold design should consider steel grade, thermal expansion, support, guide accuracy, and heating layout.
Use multiple temperature zones when the mold is large. A useful process target is a cavity temperature difference of no more than plus or minus 3 degrees C across the active molding area. Infrared checks and embedded thermocouples can confirm the result.
The following flow helps reduce dimensional variation from material preparation to final inspection.
Temperature affects cure speed, flow, pressure history, and final dimensions. A mold that is 10 degrees C colder in one area may produce a different cure state and different shrinkage. Record the actual temperature at several cavity points, not only the controller setting.
Pressure helps the compound fill the cavity and reduces voids. Excessive pressure can move inserts, increase flash, or change fiber orientation. Use the material supplier's range and verify the result with part weight, void inspection, and dimensional data.
Short cure time may leave the part under-cured. The part can continue to change size after ejection. Excessive cure time can increase cycle cost and may increase thermal exposure. Use differential scanning calorimetry, when required, to compare the cure state of trial parts.
A charge weight error of 1 percent can affect flash, filling, and local thickness. Use a calibrated scale with a resolution of at least 1 gram for small BMC charges. For larger SMC charges, record the sheet mass and coverage area for every trial batch.
Do not compare one part measured at 25 degrees C with another part measured immediately after ejection. Use the same conditioning time for every sample. A practical validation plan may measure parts at 2 hours, 24 hours, and 72 hours after molding to identify post-mold dimensional movement.
A good inspection plan links each critical dimension to a measurement method and acceptance limit.
| Inspection item | Suggested method | Useful process metric |
|---|---|---|
| Overall length and width | Caliper, height gauge, or CMM | Record average, range, and standard deviation |
| Flatness | Granite table and height gauge or CMM | Report maximum deviation over the full surface |
| Hole position | Coordinate measuring machine | Check true position against the drawing tolerance |
| Part weight | Calibrated digital scale | Control batch variation within the approved range |
| Void content | Cut section, microscopy, or computed tomography | Compare void size and distribution by location |
| Flammability | UL 94 when required by the application | Verify the specified rating for the selected material |
| Water absorption | ASTM D570 when required | Check possible dimensional change after conditioning |
One part that passes inspection does not prove process stability. For a production validation study, measure at least 30 consecutive parts after the process reaches steady state. Calculate the average, standard deviation, and range for each critical dimension.
A common starting target is a process capability index of Cpk 1.33 or higher for critical dimensions. The required value depends on the customer and product risk. If the Cpk is low, first check material batch variation, mold temperature balance, charge placement, and measurement repeatability.
| Problem | Likely cause | Corrective action |
|---|---|---|
| Part is smaller in every direction | Compensation value is too low or cure and cooling conditions changed | Confirm the actual shrinkage rate and update the cavity data |
| One direction is smaller than the other | Fiber orientation or charge placement | Measure flow and cross-flow dimensions separately |
| Panel is bowed | Uneven wall thickness or mold temperature | Balance thickness, heating zones, and cooling support |
| Hole position moves after molding | Insert movement or local thermal stress | Improve insert location control and review local geometry |
| Part has sink marks | Thick section, low pressure, or uneven cure | Reduce section thickness and improve charge and pressure control |
| Dimension changes after 24 hours | Incomplete cure or post-mold cooling movement | Review cure time and compare conditioned measurements |
| Flash varies between cycles | Charge weight, mold gap, or pressure variation | Control charge mass and inspect mold shutoff surfaces |
A controlled trial is more reliable than changing several settings at once. The following plan can support a new BMC or SMC compression mold.
Assume a target length of 300.00 mm. The first trial uses a 0.25 percent allowance. The calculated cavity length is approximately 300.75 mm. If the measured average part length is 299.55 mm, the actual shrinkage is about 0.40 percent.
The next trial should not simply add material to the charge. Review the material batch, mold temperature, cure time, and measurement condition first. If those values are stable, the cavity may need a controlled dimensional correction.
SET MOLD can be included in a project review from part design through production approval. The key work is not only cutting the steel. It also includes shrinkage analysis, mold temperature planning, insert control, trial measurement, and process correction.
A useful project record should include the following data:
For production launch, a quantified implementation plan can use one design review, one mold flow and shrinkage review, two controlled mold trials, a 30-piece capability run, and a final inspection report. The exact number of trials depends on part complexity, customer requirements, and the size of the dimensional risk.
Not always. Many BMC grades show lower or more uniform shrinkage because of their filler and short fiber structure. However, a high-glass BMC can still have directional shrinkage. The compound grade and process conditions are more important than the material name alone.
A common starting range is 0.1 percent to 0.4 percent. Use the supplier's measured data when available. Apply separate values when the part has strong fiber direction or a large flat surface.
No. It can be controlled and compensated, but resin curing and cooling still change the part size. Stable material batches, mold temperature, charge placement, pressure, cure time, and inspection conditions reduce variation.
Measure parts after a defined conditioning period. Immediate measurement may include thermal expansion and handling distortion. Record the time and temperature for every dimensional report.
Start with uniform wall thickness, balanced charge coverage, even mold heating, correct cure time, and flat cooling support. Also measure shrinkage in both principal directions.
Compression mold shrinkage is a design and process issue, not only a final inspection issue. BMC and SMC parts can show different dimensional changes because of resin cure, filler content, glass fiber orientation, wall thickness, mold temperature, charge placement, and cooling.
Use supplier data as the starting point. Calculate cavity compensation by direction. Control the thermoset compression molding process with recorded temperature, pressure, cure time, and charge weight. Confirm the result with standards-based testing and at least 30 consecutive parts for capability analysis when the application requires it.
When these controls are included in the compression mold design and trial plan, manufacturers can reduce rework, improve part fit, and achieve more stable production dimensions.
Sep 29, 2026
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