There are described methods and systems for providing an autothrottle mode in a propeller-driven aircraft. A thrust change is obtained corresponding to a difference between an actual thrust and a desired thrust for an engine (110). When greater than a pre-determined threshold, a setting change to one or more control input(s) (201) of the engine (110) is determined. One or more commands is output to cause the setting change of the control input(s) (201).
AUTOTHROTTLE CONTROL FOR TURBOPROP ENGINES
AUTODROSSELSTEUERUNG FÜR TURBOPROPTRIEBWERKE
COMMANDE D'AUTO-ÉTRANGLEMENT POUR TURBOPROPULSEURS
2025-06-11
Patent
Electronic Resource
English