Patent · US Active

Yoke and bearing fitting assembly for rotors

US8360727B2 · kind B2 · utility

9Cited by
4References
15Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJan 19, 2009
Grant dateJan 29, 2013
Priority date
Expiry dateJan 19, 2029

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C27/32
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A yoke and bearing fitting assembly for a multi-blade aircraft rotor is disclosed. The assembly has a yoke having arms extending generally radially from a central portion of the yoke, the arms each having opposing surfaces. An aperture is formed in each arm and extends between the surfaces. A bearing fitting has a body configured for insertion into the aperture of the yoke and has two rims protruding from a periphery of the body, the body also having a bearing mount adapted for mounting a pitch change bearing assembly to the yoke. Each rim abuts one of the surfaces of the associated yoke arm when the bearing fitting is installed within the aperture, so as to create clamping forces between the rims and the arm and the arm. The bearing fitting transmits forces from the pitch bearing assembly into the yoke.

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