
Air Propeller for UAVs - 2 Blades, 100mm Diameter for Optimal Thrust
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FOB, CIF & EXW terms available
Description
A blade propulsor driven by an engine and designed to produce the thrust required in the air to propel an unmanned aircraft.Number of blades: 2 Diameter x Nominal propeller pitch, in: 40x16; 40x13.1; 36x11.5; 34x13.6; 34x11.5; 32x12.8; 32x11; 30x12; 30x10.5; 30x10; 29x9.5; 29x8.7; 28x9.2; 28x8.4; 27x8.8; 27x8.1; 26.1x8.7; 26x8.7; 26x8.7; 26x8.5; 26x7.8; 24x7.8; 24x7,2; 22x7,4; 22x7,2; 22x6,6; 21x6,3; 20x6,5; 20x6; 19x5,7; 18x7,2; 18x6,1; 18x5,9; 17x5,8; 16x5,4; 15x5; 14x4,8; 13x4,4; 12x4; 16x10; 16x12; 17x10; 17x14; 21x16.According to the inclination of the blades (the propeller creates thrust forward, in the direction of flight), the propeller is airborne: - Left (CCW - counterclockwise rotation); - Right (CW- clockwise rotation). Propeller pitch: fixed. Material: - Carbon (PU-Satin4H/4), Saw-timber-1-beech GOST 2695-83.
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