Patent · US Active

Landing gear control system

US10343769B2 · kind B2 · utility

0Cited by
15References
12Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 27, 2016
Grant dateJul 9, 2019
Priority date
Expiry dateOct 31, 2036

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T74/20618
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A landing gear control lever system including a lever assembly, a locking assembly, and a switch assembly is disclosed herein. The locking assembly is connected to the lever assembly. The locking assembly has a rotary actuator and a Scotch yoke member operably connected to a portion of the rotary actuator such that rotation of the rotary actuator causes linear movement of the Scotch yoke member. The locking assembly can further include a locking arm operably coupled to the Scotch yoke member and moveable between locked and unlocked positions upon rotation of the rotary actuator.

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