Patent · US Active

Device for controlling the pitch of fan blades of a turboprop

US8985954B2 · kind B2 · utility

7Cited by
8References
10Claims
0Family size

Assignee

Inventors

Key dates

Filing dateApr 19, 2010
Grant dateMar 24, 2015
Priority date
Expiry dateJun 14, 2032

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A device for controlling pitch of fan blades of a turboprop including at least one set of adjustable-pitch fan blades secured to rotate with a rotary ring mechanically connected to a turbine rotor, each blade of the set being coupled for pitch adjustment to a synchronization ring. The device includes a rolling bearing including an inner cage slidably mounted on a turbine casing and connected to the rod of an actuator, and an outer cage that is mechanically connected to the synchronization ring by a plurality of connection arms connected to the actuator rod and hinge-mounted on the synchronization ring such that actuating the actuator causes the synchronization ring to move in turning about the longitudinal axis.

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