OUR CARBON FIBER PROPS ADVANTAGES

Optimized moment of inertia
The prop shape was designed based on power dissipation, thrust, efficiency and moment inertia of a propeller, especially for the especial condition of multirotor aircrafts. Smaller tip area and bigger root area, it helped to get the optimized moment of inertia while remain the equal thrust output, so that the responsive speed could be more sensitive.
Optimized Load Distribution
Through simulation and analyses, the tip load was decreased without the loss of thrust by a multi optimization method, which is helpful to save structure weight. The values for propeller beta were optimized to match thrust demand at different rotation rate.
High efficient structure
To meet a more powerful, rigid, and lighter structure, it adopts high
modulus carbon fiber material with balsa wood core.