Patent · US Active

Rotor hub for use with high-inertia blades

US8444382B2 · kind B2 · utility

12Cited by
6References
16Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 29, 2011
Grant dateMay 21, 2013
Priority date
Expiry dateJun 29, 2031

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C27/35
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

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.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.