Patent · US Active

Landing gear locking device

US12054241B2 · kind B2 · utility

0Cited by
4References
11Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 21, 2021
Grant dateAug 6, 2024
Priority date
Expiry dateAug 9, 2041

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C25/22
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A locking device locks a landing gear mounted in rotation on an aircraft and includes a deployment hydraulic jack including a first chamber connected to a first hydraulic supply and a second chamber connected to a second hydraulic supply. The locking device includes a hydraulic actuator connected to a rotary distributor. The rotary distributor includes a coupling operationally connecting the rotary distributor to a strut of the landing gear, a first supply port fluidly connected to the first hydraulic supply, and a first outlet port fluidly connected to the hydraulic actuator.

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