Epoxy Tooling System (Low CTE, High-Temperature Composite Mold)
Key Features
- Low CTE (25-35 µm/m/°C) for dimensional stability during autoclave cycles
- High Tg (180-220°C) for 180°C autoclave service
- Surface finish reproduction <0.5 µm Ra for Class A surface tools
- Operational life >500 autoclave cycles
- Compatible with hand lay-up, vacuum bagging, and spray application
Epoxy Tooling System is a specialized high-performance epoxy resin system designed for fabricating composite molds (tools) used in aerospace and automotive autoclave curing of composite parts at temperatures up to 180-200°C. The system is engineered for minimum coefficient of thermal expansion (CTE 25-35 µm/m/°C, approaching carbon fiber composite values) and high Tg (180-220°C) to maintain dimensional stability during repeated autoclave cure cycles.
The low CTE is achieved through combination of multi-functional epoxy components (epoxy novolac content) and high-modulus filler systems (aluminum trihydrate, silica, or hollow glass microspheres depending on application). The system is formulated for hand lay-up, vacuum bagging, and spray application over master models (Ureol foam, aluminum, fiberglass) to build up tool laminate sections.
Tool performance requirements include: surface finish reproduction <0.5 µm Ra (for Class A automotive surface tools), dimensional accuracy within ±0.1mm over the tool surface, autoclave pressure resistance up to 7 bar, and operational life of >500 autoclave cycles. Post-cure protocol for maximum dimensional stability requires staged cure from 60°C to 200°C with controlled heating rates to minimize residual thermal stress. Applications: aerospace autoclave carbon fiber molds, automotive press-forming tools, wind blade molds, and high-temperature test fixtures.
Specifications
| Parameter | Value |
|---|---|
| CTE (25-200°C) | 25-35 µm/m/°C |
| Max Autoclave Cycles | >500 |
| Tg (post-cure 180-200°C) | 180-220°C |
| Surface Finish Reproduction | <0.5 µm Ra |
| Autoclave Service Temperature | Up to 180-200°C |
| System Viscosity (mixed, 25°C) | 1,000-5,000 mPa·s (paste/liquid) |
Applications
FAQ
Unidirectional CFRP (0° lay-up) has CTE ≈ 0 µm/m/°C in the fiber direction and ~25-30 µm/m/°C transverse. Quasi-isotropic CFRP laminates ([0/±45/90]s) have CTE ≈ 2-4 µm/m/°C in-plane. A pure epoxy tooling system has CTE ~55-65 µm/m/°C — too high, causing significant thermal mismatch and residual stress during autoclave cure. Filled epoxy tooling systems with 30-50% wt mineral filler reduce CTE to 25-40 µm/m/°C, significantly reducing thermal mismatch. CFRP tooling prepregs (carbon fiber/epoxy tooling prepreg) achieve CTE ~2-4 µm/m/°C matching the part, but at higher cost. For critical dimensional tolerance parts (±0.1mm), CFRP tooling prepregs are recommended; for general structural parts (±0.5mm), filled epoxy tooling systems are adequate and significantly more economical.
Direct Contact
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