Patent · US Active

Compact rotorcraft dual-element spherical elastomeric centrifugal-force bearing assembly

US8926281B2 · kind B2 · utility

12Cited by
5References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateFeb 21, 2012
Grant dateJan 6, 2015
Priority date
Expiry dateJul 7, 2033

Classification

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

Abstract

A rotary system includes a retention member and a flexible yoke having an opening forming a bridge. The rotary system is further provided with two bearing assemblies, a first bearing assembly extending through the opening of the yoke and configured to secure a rotor blade to the retention member and a second bearing assembly extending through the opening of the flexible yoke and configured to secure the rotor blade to the bridge. The second bearing element includes a bearing element having a first surface forming a spherical contouring and an opposing integral second surface forming a conical contouring.

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