Carbon Fiber Plain Weave Fabric : High - Strength Composite Reinforcement For Aerospace
Carbon Fiber Plain Weave Fabric is a lightweight, high-strength composite material made by interlacing carbon fiber yarns in a simple over-under pattern. This uniform structure ensures balanced mechanical properties and exceptional durability. Key features include:
High Tensile Strength: Ranges from 3,000–5,000 MPa, ideal for structural applications requiring minimal weigh
.Lightweight: Density as low as 1.5–2.0 g/cm³, critical for aerospace and automotive industries
.Corrosion Resistance: Impervious to acids, alkalis, and solvents, making it suitable for harsh environments
.Thermal Stability: Operates effectively up to 400°C without significant degradation
.Electrical Conductivity: Non-conductive properties ensure safety in electronic and aerospace applications
.Precursor Processing:
Polyacrylonitrile (PAN) fibers are stabilized at 200–300°C and carbonized at 1,000–3,000°C to form graphite-like structures
.Yarn Formation:
Carbon filaments (5–25 µm diameter) are bundled into tows (e.g., 3K, 6K, 12K) for uniformity
.Weaving:
Tows are interlaced in a plain weave pattern (0°/90°) using automated looms to create a tight, checkerboard structure
.Surface Treatment:
Coated with sizing agents (e.g., silane) to enhance resin adhesion and UV resistance
.Quality Control:
ISO 9001-certified testing for tensile strength, thickness uniformity, and fiber alignment
.Handling:
Wear PPE (gloves, goggles) to avoid fiber irritation; use sharp tools cautiously to prevent breakage
.Resin Compatibility:
Match fabric type (e.g., standard modulus vs. high modulus) with epoxy, polyester, or vinyl ester resins
.Curing Conditions:
Maintain 120–150°C and 0.5–1.0 MPa pressure during curing to eliminate voids
.Storage:
Store in dry, ventilated areas (humidity <60%); avoid prolonged UV exposure to prevent coating degradation
. Parameter | Details |
---|---|
Material | PAN-based carbon fiber + epoxy sizing |
Density | 1.5–2.0 g/cm³ |
Weight | 200–500 g/m² |
Thickness | 0.2–0.6 mm |
Tensile Strength | 3,000–5,000 MPa |
Elastic Modulus | 70–200 GPa |
Operating Temp | -60°C to +400°C (short-term: 600°C) |
Surface Resistivity | >10¹² Ω (electrical insulation) |
Certifications | ISO 9001, REACH, RoHS |
Aircraft Components: Reinforces fuselage panels, wings, and engine mounts for lightweight durability.
Case: Boeing 787 Dreamliner uses plain weave fabric in wing structures to reduce weight by 20%
.Body Panels: Enhances strength of EV door panels and chassis components.
Case: Tesla Model S uses plain weave fabric in battery trays for crash resistance
.Turbine Blades: Reinforces leading edges to withstand high wind loads and fatigue.
Case: GE Haliade-X offshore wind turbine blades use plain weave for extended lifespan
.Boat Hulls: Corrosion-resistant alternative to steel/aluminum.
Case: Benetti superyachts employ plain weave fabric in hull laminates for 15+ years of saltwater durability
.Pressure Vessels: Reinforces FRP tanks for chemical storage.
Case: Dow Chemical’s storage tanks use plain weave-reinforced polyester for 25+ years of leak-free service
.Protective Gear: Helmets and automotive safety belts .