Epoxy Tooling System (Low CTE, High-Temperature Composite Mold)

CAS 25068-38-6In StockSample available

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

ParameterValue
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 TemperatureUp to 180-200°C
System Viscosity (mixed, 25°C)1,000-5,000 mPa·s (paste/liquid)

Applications

Aerospace autoclave carbon fiber composite moldsAutomotive Class A surface press-forming toolsWind turbine blade molds (large-scale infusion molds)High-temperature test fixtures and jigsMaster model encapsulation for tooling duplication

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.

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