Product overview
The T-MOTOR VZ45×18 is a carbon fiber propeller supplied as a two-piece pair for UAV VTOL propulsion. Its stated maximum thrust is up to 60kg, while each blade weighs 285g. The physical construction combines prepreg molding with a PMI foam core to provide a lightweight, high-strength structure with low porosity. The blade architecture also supports load distribution and structural redundancy for heavy-duty operation, with reduced inertia intended to improve response and control under flight loads.
Its integration role is in VTOL propulsion systems, including large-scale logistics UAV applications. The aerodynamic design combines a special airfoil and blade tip geometry intended to improve lift and reduce vortex drag, with high lift during takeoff and low drag during cruise. During transition, the propeller is designed to resist complex airflow interference and reduce thrust fluctuation. Blade deformation and vibration control address high-speed operation. The supplied product is a propeller pair, and its warranty runs for 12 months from purchase with valid proof required.
Specifications
| Specification | Value & conditions |
|---|---|
| Product | T-MOTOR VZ45×18 Carbon Fiber VTOL Propeller |
| Supplied quantity | 2PCS/PAIR |
| Maximum thrust | Up to 60kg |
| Weight | 285gPer blade. |
| Material and construction | Carbon fiber propeller with prepreg molding and PMI foam core; high strength, low porosity and lightweight structure. |
| Load resistance and response | Withstands high RPM loads and flight stress; reduced inertia supports faster response and better control.High RPM loads and flight stress. |
| Deformation and vibration | Designed to minimize blade deformation and vibration.High-speed operation. |
| Flight-phase characteristics | High lift during takeoff and low drag during cruise, supporting efficiency and endurance.Takeoff and cruise in large-scale logistics UAV applications. |
| Transition airflow behavior | Designed to resist complex airflow interference, reduce thrust fluctuation and improve stability.VTOL transition phases. |
| Structural characteristics | Enhanced load distribution and structural redundancy.Heavy-duty operation. |
| Aerodynamic design | Special airfoil and blade tip design intended to improve lift and reduce vortex drag. |
| Warranty | 12 months from date of purchase.Valid proof of purchase required. |
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