Patent · US Active

Support assembly

US8757543B2 · kind B2 · utility

1Cited by
3References
21Claims
0Family size

Assignee

Inventor

Key dates

Filing dateJul 14, 2010
Grant dateJun 24, 2014
Priority date
Expiry dateFeb 26, 2032

Classification

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

Abstract

A support assembly for guiding a flap on an aircraft wing during deployment of the flap. The assembly includes an arcuate guide track mountable to an aircraft wing and defining a two-dimensional path, a carriage mounted on the guide track so as to slide along the track during flap deployment, a part-spherical bearing, and a shaft having one end attachable to a flap and the opposite end coupled to the carriage via said part-spherical bearing. The shaft is free to pivot relative to the carriage about a center of the part-spherical bearing in all directions, as the carriage slides along the track.

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