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Single-blade propeller : ウィキペディア英語版 | Single-blade propeller A single-blade propeller may be used on aircraft to generate thrust. Normally propellers are multiblades but the simplicity of a single-blade propeller fits well on motorized gliders, because it permits the design of a smaller aperture of the glider fuselage for retraction of the powerplant. The counterbalanced teetering mono-blade propeller generates fewer vibrations than conventional multiblade configurations. Single-blade propellers are also more efficient, as the blade passes through clean air, where in multi-blade propellers, each blade passes through turbulent air from the previous blade. Single-blade propeller drawing. Single-blade propeller and glider drawing. == Patents ==
* (US Patent 2742095 Mechanism for balancing single blade aircraft rotor ) * (US Patent 6619585 Helicopter single-blade rotor ) * (US Patent 5971322 ) - Propeller propulsion unit for aircraft in general
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