发明名称 ROTOR HUB FOR USE WITH HIGH-INERTIA BLADES
摘要 <p>A rotor hub has a yoke with radial arms allowing flapping of connected blades about a flap axis. A grip is rigidly attached to each blade, and a lead-lag bearing connects each grip to one of the arms, the bearing defining a lead-lag axis outboard of the flap axis. Each arm has a pair of straps located on opposite sides of the rotor plane for transferring centrifugal force from the blades to the central portion of the yoke. A pair of lead-lag dampers is provided for each grip, the dampers of each pair being located on opposite sides of the rotor plane and connecting an inboard end portion of the grip to the adjacent strap. In-plane motion of a blade causes rotation of the attached grip about the lead-lag axis, causing opposite motion of an inboard end portion of the grip. The dampers act to oppose rotation of the grip.</p>
申请公布号 EP2686239(B1) 申请公布日期 2015.08.12
申请号 EP20110868662 申请日期 2011.06.29
申请人 BELL HELICOPTER TEXTRON INC. 发明人 STAMPS, FRANK, B.;TISDALE, PATRICK, R.;YUCE, MITHAL
分类号 B64C27/37 主分类号 B64C27/37
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