Patent · US Active

Actuation system for a lift assisting device and lined track rollers used therein

US10023302B2 · kind B2 · utility

1Cited by
73References
11Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 19, 2012
Grant dateJul 17, 2018
Priority date
Expiry dateDec 3, 2034

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/40
  • WIPO fieldMechanical elements
  • WIPO sectorMechanical engineering

Abstract

An actuation system for deploying and retracting a lift assisting device of a leading edge of a wing of an aircraft including a track pivotally coupled to the lift assisting device. The track has first and second outer surfaces and side surfaces. The actuation system includes a shaft rotationally coupled within the wing of the aircraft and operable, in response to flight control signals, to deploy or retract the lift assisting device. The actuation system includes an actuator for actuating the lift assisting device, coupled to the shaft, between a retracted position to a deployed position along an arcuate path. The actuation system includes a plurality of track roller bearings rotatably contacting the first and second outer surfaces of the track to guide the track along the arcuate path. The plurality of track roller bearings includes one or more lined track roller assembly.

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