Why Polycarbonate Injection Molding Parts Crack: Solving Internal Stress in Injection Molding

Every cracked PC injection molding part is a small murder mystery. The victim: a crystal-clear enclosure that passed every inspection. The scene: your customer’s warehouse, eleven days after delivery. The weapon is almost always the same — stored internal stress, meeting the wrong chemical or the wrong load at the wrong moment.
This article is the autopsy report: six suspects, the forensic toolkit that identifies them, and the prevention protocol we run at Ulite on every polycarbonate injection molding program.
⚗️ The Physics in 90 Seconds — Stress + Agent = Crack
Polycarbonate is tough — until it isn’t. Residual (internal) stress gets locked in during molding by three mechanisms: flow/orientation stress (high shear near gates), thermal stress (uneven or too-fast cooling), and assembly stress (screws, press-fits, inserts). Alone, it may sit silently for weeks. Add a chemical agent — solvent wipes, plasticizers, alkalis, even alcohol — and you get environmental stress cracking (ESC): crazing and cracking far below the material’s normal strength.
The equation to remember: Crack = Locked-in Stress × Chemical/Load Trigger. Remove either factor and the crack never starts.
🕵️ The Six Suspects — Exhibit Cards
EXHIBIT A · Moisture & Hydrolysis
Evidence: Silver streaks/splay, brittle parts, char-free brittleness, MFR shift.
Root cause: PC is hygroscopic; undried resin hydrolyzes in the barrel — water literally cuts the polymer chains, dropping impact strength.
Fix: Desiccant-dry 4 h @ 120 °C, dew point ≤ −40 °C, moisture < 0.02%; verify with a moisture analyzer, not a timer.
Prevention: Dryer dew-point alarms + logged moisture per lot.
EXHIBIT B · Process Stress (Shear & Cooling)
Evidence: Stress fringes near gates under a polariscope; warpage; cracks radiating from the gate.
Root cause: Too-fast injection (high shear orientation), mold temperature too low (PC wants 80–110 °C), unbalanced cooling, over-packing.
Fix: Raise mold temp into spec, slow first-stage speed, decouple packing (scientific molding), balance cooling to ±2 °C.
Prevention: Polariscope audit on first articles + periodic pulls.
EXHIBIT C · Design Stress Concentrators
Evidence: Cracks always at the same sharp corner, wall transition, or boss.
Root cause: Sharp internal radii (<0.4 mm), abrupt wall changes, and metal inserts (steel/brass shrinks differently than PC → hoop stress).
Fix: Internal radii ≥ 0.5–0.8 × wall; uniform walls; pre-heat inserts (~80 °C), reduce interference, add relief.
Prevention: DFM radius map before cutting steel — the cheapest crack fix costs $0 in steel.
EXHIBIT D · Environmental Stress Cracking (ESC)
Evidence: Fine crazing after shipping/storage/cleaning; cracks where a gasket, label adhesive, or wipe touched.
Root cause: Aromatics/chlorinated solvents, ketones, strong alkalis, ammonia cleaners, plasticizers, alcohol wipes on stressed parts, thread-lockers.
Fix: Chemical audit of every touch-point (cleaner, gasket, carton liner, ink, adhesive); switch to ESC-safe agents; lower assembly stress.
Prevention: Solvent craze test as a release audit.
EXHIBIT E · Degradation & Regrind Abuse
Evidence: MFR up 20–30%+ vs virgin; impact strength down; yellow tint.
Root cause: Over-long residence, overheated melt, or regrind > 15–20% re-cooking the polymer.
Fix: Cap regrind (≤10–15% structural, 0% optical/medical); incoming MFR check; right-size the barrel.
Prevention: Lot-level regrind log + MFR trend chart.
EXHIBIT F · Ejection & Assembly Stress
Evidence: Cracks at ejector pins; cracks appearing only after screws are torqued.
Root cause: Parts sticking (low draft, rough cavities) → high ejection force; over-torqued screws adding hoop stress on top of molded-in stress.
Fix: Draft ≥1–1.5°, polish, ejector speed profile, more/larger pins; written torque specs + boss radii.
Prevention: Torque validation on the assembly line, not in the field.
🔬 The Forensic Toolkit — How We Identify the Suspect
| Tool | What It Reveals | One-Liner |
| Polariscope | Locked-in stress map (color fringes) | See stress before it becomes a crack. |
| Solvent craze test | ESC susceptibility / stress level | A seconds-long dip exposes high-stress zones. |
| MFR comparison | Degradation / regrind abuse | MFR drift = cooked polymer. |
| Moisture analyzer | Drying adequacy | Trust grams of water, not dryer timers. |
| Cross-section microscopy | Brittle vs ductile fracture, weld quality | The fracture face confesses. |
| Annealing oven trial | Confirms stress-driven cracking | If annealed twins don’t crack — stress did it. |
🛡️ The Ulite Prevention Protocol (Spec Sheet)
| # | Spec |
| 1 | Dry: 120 °C × 3–4 h, dew point ≤ −40 °C, moisture < 0.02%, logged per lot. |
| 2 | Melt: 280–310 °C, residence < 10 min, full purge on color/lot change. |
| 3 | Mold temp: 80–110 °C (higher end for clear/structural); cooling balanced ±2 °C. |
| 4 | Process: moderate fill speed, decoupled packing, scientific molding window documented. |
| 5 | Design DFM: internal radii ≥0.5–0.8×wall; uniform walls; draft ≥1°; insert pre-heat. |
| 6 | Anneal: 120–125 °C, ~1–2 h for ≤3 mm walls (scale with thickness), slow oven cool. |
| 7 | Regrind: ≤10–15% structural, 0% optical/medical; incoming MFR trend. |
| 8 | QC release: polariscope first-article + periodic; solvent craze audit; torque validation; ESC chemical audit of packaging & assembly touch-points. |
🧭 Crack Pattern → Suspect → Fix (Field Matrix)
| Crack Pattern | Prime Suspect | First Fix |
| Radiating from gate | B shear/orientation | Slower fill, bigger gate, hotter mold |
| At weld/knit line | B + weak knit | Hotter melt/mold, vent, move gate |
| Around metal insert | C + F | Pre-heat insert, radius, anneal, torque spec |
| Fine crazing after storage | D ESC | Chemical audit, liner, ESC-safe wipe |
| Splay + brittle | A moisture | Fix dryer, verify <0.02% |
| At ejector pins | F ejection | Draft, polish, ejection profile |
| Only after screws torqued | F + D | Torque spec, boss radius, ESC-safe locker |
🗂 Case Files — Six Cracks, Solved
| Case | Symptom | Culprit | Verdict / Result |
| CF-1 | Clear lens crazed after IPA wipe | D + B | Mold 70→100 °C, anneal, ESC-safe wipe → 0 field failures |
| CF-2 | Enclosure split at brass inserts, −20 °C transit | C + F | Insert pre-heat 80 °C, radius 0.4→1.2 mm, anneal → passed |
| CF-3 | Medical housing cracked after quat wipes | D | Wipe change + boss radii + polariscope release audit → 0 escapes |
| CF-4 | Brittle batch + splay | A | Dryer dew point −18→−42 °C; moisture 0.06→0.015% |
| CF-5 | Impact −40%, MFR +35% | E | Regrind 25%→10% cap + incoming MFR check |
| CF-6 | Cracks at pin marks, sticking | F | Draft 0.5°→1.5°, cavity polish, ejector profile → solved |
❓ FAQ (Snippet-Optimized)
Q1: Why does polycarbonate crack after molding?
Locked-in internal stress (from shear, fast/uneven cooling, or design sharp corners) combines with a trigger — a chemical (ESC), a load, or a temperature swing — and crazing/cracking follows, sometimes weeks later.
Q2: What mold temperature prevents PC stress?
80–110 °C; the higher end for clear or structural parts — low mold temp is the #1 process cause of residual stress.
Q3: How do you dry polycarbonate properly?
Desiccant dryer, 120 °C for 3–4 h, dew point ≤ −40 °C, moisture below 0.02% — verified with a moisture analyzer.
Q4: Does annealing really fix internal stress?
Yes — 120–125 °C for 1–2 h (scale with wall) with slow cooling relaxes orientation stress; we verify with a polariscope before/after.
Q5: Which chemicals crack polycarbonate?
Aromatics/chlorinated solvents, ketones, strong alkalis, ammonia cleaners, plasticizers, thread-lockers — and alcohol wipes on stressed parts.
Further Reading: Secondary Operations Guide (annealing station)↗ · Custom Plastic Molding Cost Calculator↗
🎯 CTA — Contact The Ulite Team
Cracking PC Injection Molding parts right now? Ship us 5 samples + your resin grade. Within 72 hours Ulite returns a free crack autopsy report: polariscope stress map, moisture/MFR data, suspect ranked, and a written fix spec. Ulite — your one-stop custom plastic molder.
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