发明授权
US09528375B2 Non-uniform blade distribution for rotary wing aircraft 有权
旋翼飞机的不均匀叶片分布

Non-uniform blade distribution for rotary wing aircraft
摘要:
A translational thrust system for a rotary wing aircraft is provided including a propeller system. The propeller system includes more than one pair of propeller blades extending radially outward from a rotatable propeller hub. Each pair of propeller blades includes a first propeller blade and a second propeller blade arranged diametrically opposite one another about a circumference of the propeller hub. Each pair of propeller blades is arranged at an angle to an adjacent pair of propeller blades such that the angle is less than is the pairs of propeller blades were uniformly distributed around the circumference of the propeller hub.
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