A thrust control assembly (10) includes a balk application arrangement which provides, in response to a received balk command to prohibit command of thrust in a balk direction, a balk force on a rotatable thrust lever (12) acting to oppose an attempt by the pilot to move the lever (129 in a direction so as to command or increase thrust in the balk direction. The balk application arrangement controls an auto-throttle actuator (20) to provide the balk force on the thrust lever (12).
THRUST CONTROL ASSEMBLY
SCHUBREGELUNGSANORDNUNG
ENSEMBLE DE COMMANDE DE POUSSÉE
2021-11-03
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |