Carbon fiber rotor blades
Application scenario: Lightweight and high-strength propeller, suitable for low-altitude aircraft.
Technical highlights:
• For the first time, a composite material hot-pressing blade was developed, replacing the lightweight sandwich structure design of injection-molded blades and the rapid cooling and heating molding process. This resulted in a shorter molding cycle, higher efficiency, and a paint-free appearance.
For the first time, an uninterrupted automated production line was adopted for large-scale mass production, and a precisely designed lay-up structure was employed to achieve a low-cost and high-strength carbon fiber propeller structure.