Patent · US Active

Control lever assembly for controlling an aircraft system

US12049298B2 · kind B2 · utility

0Cited by
3References
16Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 13, 2022
Grant dateJul 30, 2024
Priority date
Expiry dateSep 13, 2042

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG05G25/04
  • WIPO fieldMechanical elements
  • WIPO sectorMechanical engineering

Abstract

A control lever assembly for controlling an aircraft system. The lever includes: a housing having an outer side and an aperture defined by a rim; and a control lever extending through the aperture and movable in the aperture; the control lever having an outer cover member arranged to slide over the outer side of the housing and cover the rim throughout the range of movement of the control lever.

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