Patent · US Active

Joint for tiltrotor hubs

US7867096B2 · kind B2 · utility

2Cited by
12References
17Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 7, 2005
Grant dateJan 11, 2011
Priority date
Expiry dateOct 9, 2026

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF16D3/78
  • WIPO fieldMechanical elements
  • WIPO sectorMechanical engineering

Abstract

A joint is configured for use with a rotary-wing aircraft having at least one engine. A driver is coupled to an output shaft of the engine, the driver being rotatable about an axis. A yoke is at least partially rotatable relative to the driver about a first center of rotation, the center of rotation being located on the axis. A plurality of upright links couple the yoke to the driver, each link being translatable relative to the yoke, the driver, or both. Each link is also rotatable relative to the yoke, the driver, or both, about a second center of rotation.

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