Patent · US Active

Pilot control system with adjustable pedals

US9764830B2 · kind B2 · utility

5Cited by
29References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJan 8, 2013
Grant dateSep 19, 2017
Priority date
Expiry dateNov 9, 2035

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T74/20528
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

According to one embodiment, a method of adjusting an aircraft pedal assembly includes providing a pedal linkage coupled between a pedal and an attachment assembly situated proximate to an aircraft instrument panel. A brake cylinder is provided coupled between the pedal and the attachment assembly. The pedal linkage is rotated in response to an adjustment input. The pedal linkage is maintained approximately parallel to the brake cylinder during rotation of the pedal linkage.

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