This system (36) for controlling an aircraft thrust reversal means comprises a reverse idle control means (38), a first detection means (31) configured to detect, when the reverse idle control is active, a condition for activation of the thrust reversal means, and an actuation means (52) configured to activate the thrust reversal means when the first detection means (31) detects a condition for activation of the thrust reversal means.It further comprises a second detection means (42, 44, 46, 48, 49) configured to detect a condition for activation of the reverse idle control, the control means (38) being configured to activate the reverse idle control when the second detection means (42, 44, 46, 48, 49) detects a condition for activating the reverse idle control.
SYSTEM FOR CONTROLLING AN AIRCRAFT THRUST REVERSAL MEANS
2022-12-29
Patent
Electronic Resource
English
Method for controlling an aircraft propeller system during thrust reversal
European Patent Office | 2017
|Method For Controlling An Aircraft Propeller System During Thrust Reversal
European Patent Office | 2016
|Method for controlling an aircraft propeller system during thrust reversal
European Patent Office | 2019
|System for controlling braking of aircraft equipped with thrust reversal system
European Patent Office | 2021
|Thrust reversal for jet aircraft
Engineering Index Backfile | 1959
|