Detailed Description
VTOL drones consume extra energy during vertical takeoff; heavy aluminum structure greatly limits flight range. Our dry carbon plate uses tailored asymmetric layup to match directional load on VTOL airframe, porosity <0.8%. CNC edges are sealed to stop water absorption. Cyclic fatigue test verifies stable property under repeated takeoff & landing vibration. Batch mechanical property sampling ensures consistency. As export factory, we support small batch prototype and mass serial production.
Specification
| Item | Parameter |
|---|---|
| Material | T700 prepreg dry carbon autoclave |
| Weave | 3K twill custom layup |
| Thickness | 1.8mm / custom |
| Process | CNC cut, edge sealing |
| Porosity | <0.8% |
| Tolerance | ±0.1mm |
| Surface | Matte |
FAQ
Q1: Can you produce carbon ribs for VTOL wing?
A1: Yes, we can CNC machine complex rib cutouts according to your aerodynamic structure drawings.
Q2: What is your typical lead time for VTOL prototype?
A2: 7–12 working days for prototype samples after drawing confirmation.
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