Patent · US Active

Actuator for use in aircraft

US10859036B2 · kind B2 · utility

1Cited by
6References
13Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 25, 2018
Grant dateDec 8, 2020
Priority date
Expiry dateJan 19, 2039

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2270/64
  • WIPO fieldMechanical elements
  • WIPO sectorMechanical engineering

Abstract

There is provided an actuator for an aircraft thrust reverser, comprising a first member, a second member movable relative to the first member, a third member movable relative to the first member and the second member, and a lock system configured to selectively lock the second member to the third member in a first stage of actuation, and the first member to the second member in a second, separate stage of actuation.

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