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Helicopter - for Russia - data - Equipment

机译:直升机-俄罗斯-数据-设备

摘要

A rotor hub system for a helicopter in which the rotor hub and pitch housing are fabricated predominately of composite material, the flap hinge, pitch hinge and lead-lag hinge contain elastomeric bearings and one step blade folding in either the forward or aft direction using the same drive system. The rotor hub includes closed loop straps which define generally opposed lugs of the flap hinge, and the pitch housing includes a pair of closed loop straps which define the lugs of the lead- lag hinge and a lug of the flap hinge. The use of composite materials as the predominant material of the rotor hub and the pitch housing results in a highly load redundant structure permitting a reduction in size and number of parts, a reduction in drag, and an increase in reliability and safety.
机译:用于直升机的旋翼轮毂系统,其中旋翼轮毂和俯仰壳体主要由复合材料制成,襟翼铰链,俯仰铰链和超前滞后铰链均包含弹性轴承和一个阶梯叶片,该叶片可使用前向或向后折叠相同的驱动系统。转子轮毂包括限定出襟翼铰链的大致相对的凸耳的闭环带,并且变桨壳体包括限定了超前滞后铰链的凸耳和襟翼铰链的凸耳的一对闭环带。使用复合材料作为转子轮毂和变桨壳体的主要材料导致了高负载冗余结构,从而允许减小零件的尺寸和数量,减少阻力以及提高可靠性和安全性。

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