Lightweight Epoxy Carbon Fiber Cloth Sheets Carbon Fiber Woven Fabric With Thermal Stability
Carbon Fiber Prepreg is a high-performance composite material combining carbon fibers with a thermosetting resin matrix (typically epoxy). Prepreg undergoes a controlled partial curing process (B-staging), resulting in a tacky, ready-to-use material that eliminates manual resin application. This ensures consistent fiber-resin ratios, superior mechanical properties, and reduced waste.
- Exceptional Strength-to-Weight Ratio: Delivers 5-7× higher strength than steel at 1/4 the weight.
- Uniform Resin Distribution: Automated processes guarantee precise fiber alignment and resin saturation.
- Thermal Stability: Operates effectively up to 300 °C without significant degradation.
- Corrosion Resistance: Impervious to acids, alkalis, and moisture, ideal for harsh environments.
- Customizability: Adjustable fiber orientation (0°, ±45°, 90°) and resin systems (epoxy, phenolic) to meet specific performance needs.
- Fiber Preparation:
Carbon fibers (e.g., T700, T800) are produced via pyrolysis of polyacrylonitrile (PAN) precursors, achieving high tensile strength and stiffness.
- Resin Impregnation:
Fibers pass through a resin bath or film-coating system to achieve uniform resin saturation (30-40% resin content).
- B-Staging:
Partial curing at 80 -120°C creates a tacky, tack-free state for easy handling and storage.
- Layer Consolidation:
Multiple prepreg layers are stacked and aligned using automated cutting and placement systems.
- Curing:
Heat and pressure (120-180°C, 0.5-2.0 MPa) in autoclaves ensure full resin curing and void elimination.
- Storage:
Store at -18 °C to halt curing; thaw for 24 hours at room temperature before use.
- Handling:
Wear PPE (gloves, respirators) to avoid fiber irritation and inhalation hazards.
- Curing Parameters:
Maintain strict temperature and pressure controls to prevent warping or void formation.
- Surface Preparation:
Clean molds with release agents (e.g., PVA wax) to ensure part release.
| Parameter | Details |
|---|---|
| Material | PAN-based carbon fiber + epoxy resin |
| Fiber Type | T700/T800 (Standard/High Modulus) |
| Resin System | Epoxy, phenolic, or cyanate ester |
| Weight | 160-500 g/m² |
| Thickness | 0.05-0.3 mm |
| Tensile Strength | 3,000-5,000 MPa |
| Elastic Modulus | 70-200 GPa |
| Compressive Strength | 1,500-3,000 MPa |
| Operating Temp | -60°C to +300°C |
| Certifications | ISO 9001, REACH, RoHS |
Aircraft Components: Fuselage panels, wings, and engine mounts. Prepreg's lightweight rigidity enhances fuel efficiency and payload capacity.
Performance Vehicles: High-strength chassis, suspension arms, and Formula 1 body panels.
Turbine Blades: Reinforces leading edges to withstand high wind loads and fatigue cycles.
Bicycle Frames: Lightweight yet durable frames for racing bikes.
Tennis Rackets: Optimized stiffness-to-weight ratios for power and control.
Robotics & Drones: Structural components requiring high strength-to-weight ratios.
Prosthetics & Implants: Biocompatible, corrosion-resistant materials for load-bearing applications.
Boat Hulls & Offshore Structures: Resists saltwater corrosion and wave-induced stress.

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