Patent · US Active

Multistage landing gear actuator with slip-clutch assembly

US12344203B2 · kind B2 · utility

0Cited by
6References
19Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 14, 2020
Grant dateJul 1, 2025
Priority date
Expiry dateFeb 16, 2042

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF16H2063/3093
  • WIPO fieldMechanical elements
  • WIPO sectorMechanical engineering

Abstract

A landing gear system including a landing gear actuator assembly arranged to selectably provide an increased torque output to a cross-shaft adaptor rotationally coupled to a cross-shaft of a trailer landing gear assembly. A rotational engagement mechanism is arranged to, in response to a remote signal, shift a rotational engagement mechanism to selectably couple the cross-shaft adaptor with a light gear set or selectably couple the cross-shaft adaptor with a heavy gear set. The landing gear actuator includes a slip-clutch assembly to dampen, reduce, or eliminate rotational shock caused when retracting or extending the legs of the landing gear system.

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