Patent · US Active

Thrust reverser actuator systems

US9650994B2 · kind B2 · utility

1Cited by
4References
19Claims
0Family size

Assignee

Inventor

Key dates

Filing dateJul 30, 2014
Grant dateMay 16, 2017
Priority date
Expiry dateMay 21, 2035

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF02K1/766
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

Thrust reverser actuator systems are disclosed herein. An example apparatus disclosed herein includes a first controller to communicate with a first flight computer and a second flight computer of an aircraft. The example apparatus also includes a second controller to communicate with the first flight computer and the second flight computer. The example apparatus further includes a thrust reverser and a first electrical actuator coupled to the thrust reverser. The first electrical actuator is to be communicatively coupled to the first controller and the second controller. The example apparatus also includes a second electrical actuator coupled to the thrust reverser. The second electrical actuator is to be communicatively coupled to the second controller. The first electrical actuator and the second electrical actuator are to synchronously actuate the thrust reverser.

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