Patent ID: 9650994
Date: 2017-05-16
CPC Classifications: F02K

Claim:
1. An apparatus, comprising: a first flight computer; a second flight computer; a first controller to communicate with the first flight computer and the second flight computer; a first electric motor to communicate with the first controller; a second controller to communicate with the first flight computer and the second flight computer; a second electric motor to communicate with the second controller; and an aircraft thrust reverser operatively coupled to the first electric motor and the second electric motor, each of the first controller and the second controller to receive a first command from the first flight computer and a second command from the second flight computer, the first controller to control the first electric motor based on the first command and the second command, the second controller to control the second electric motor based on the first command and the second command, the first electric motor and the second electric motor to synchronously move the aircraft thrust reverser.