Wing rib composite laminate, bidirectional fatigue strength ≥ 1200MPa (10⁶ cycles), reducing the risk of cracks caused by flutter

The curved transition area is enhanced, with good flexibility (bending radius ≤ 5mm), avoiding stress concentration cracking, and the scratch resistance level is ≥ 3H

Tie rod type unidirectional force bearing component, tensile strength ≥3000MPa, 70% lighter than steel tie rod, suitable for landing gear retraction system, reducing material redundancy by 15%

Seat back cushioning layer (thickness 5-10mm), vibration absorption efficiency ≥40%, reducing collision damage to passengers; surface wear resistance >50,000 times

Wet spray molding of complex curved surfaces (such as nose radome), uniform fiber dispersion, 30% higher mold filling rate, reduced manual layering errors, rapid molding of tail trailing edge, random distribution of short fibers to enhance impact toughness, 25% higher anti-delamination ability than hand lay-up process

Circuit insulation bracket, resistivity ≥10¹³Ω・cm, high voltage breakdown resistance (≥20kV/mm), aviation lubricant erosion resistance, toilet partition reinforcement, detergent (such as sodium hypochlorite) corrosion resistance, strength retention rate ≥90% after 1000 hours of immersion, surface wear-resistant coating reinforcement (such as polyurethane base), hardness up to Shaw D75, ice crystal impact resistance >1000 times without damage

After compounding with epoxy resin, the bending strength is ≥200MPa, the temperature resistance is 180℃, which can meet the structural stability during emergency evacuation, and the tensile strength is ≥800MPa at 200℃

The pipe insulation layer is fixed, with a temperature resistance of -60℃~+150℃, and a viscosity retention rate of ≥90% (1000 hours aging), which simplifies the pipe wrapping process.