MOQ: | 200㎡ |
Price: | $14.37-$19.01(㎡) |
Standard Packaging: | Palletize |
Delivery Period: | 3-7 work days |
Payment Method: | T/T |
Supply Capacity: | 500000KGS/month |
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.
Carbon fibers (e.g., T700, T800) are produced via pyrolysis of polyacrylonitrile (PAN) precursors, achieving high tensile strength and stiffness.
Fibers pass through a resin bath or film-coating system to achieve uniform resin saturation (30-40% resin content).
Partial curing at 80 -120°C creates a tacky, tack-free state for easy handling and storage.
Multiple prepreg layers are stacked and aligned using automated cutting and placement systems.
Heat and pressure (120-180°C, 0.5-2.0 MPa) in autoclaves ensure full resin curing and void elimination.
Store at -18 °C to halt curing; thaw for 24 hours at room temperature before use.
Wear PPE (gloves, respirators) to avoid fiber irritation and inhalation hazards.
Maintain strict temperature and pressure controls to prevent warping or void formation.
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.
MOQ: | 200㎡ |
Price: | $14.37-$19.01(㎡) |
Standard Packaging: | Palletize |
Delivery Period: | 3-7 work days |
Payment Method: | T/T |
Supply Capacity: | 500000KGS/month |
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.
Carbon fibers (e.g., T700, T800) are produced via pyrolysis of polyacrylonitrile (PAN) precursors, achieving high tensile strength and stiffness.
Fibers pass through a resin bath or film-coating system to achieve uniform resin saturation (30-40% resin content).
Partial curing at 80 -120°C creates a tacky, tack-free state for easy handling and storage.
Multiple prepreg layers are stacked and aligned using automated cutting and placement systems.
Heat and pressure (120-180°C, 0.5-2.0 MPa) in autoclaves ensure full resin curing and void elimination.
Store at -18 °C to halt curing; thaw for 24 hours at room temperature before use.
Wear PPE (gloves, respirators) to avoid fiber irritation and inhalation hazards.
Maintain strict temperature and pressure controls to prevent warping or void formation.
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.