Herein provided are methods and systems for controlling operation of a first propeller (120) of an aircraft, the first propeller (120) associated with a first engine (110), the aircraft further comprising a second propeller (170) associated with a second engine (160). A first requested engine power for the first engine (110) is obtained. A second requested engine power for the second engine (160) is obtained. The first propeller (120) is synchronized with the second propeller (170) by setting a first propeller command for the first propeller (120) based on the first and second requested engine power, and the first propeller command is sent for the first propeller (120).
SINGLE LEVER CONTROL IN TWIN TURBOPROPELLER AIRCRAFT
EINHEBELSTEUERUNG IN FLUGZEUG MIT ZWEI TURBOPROPELLERN
COMMANDE À LEVIER UNIQUE DANS UN AÉRONEF À DOUBLE TURBOPROPULSEUR
2018-08-29
Patent
Electronic Resource
English
SINGLE LEVER POWERPLANT CONTROL ON TWIN TURBOPROPELLER AIRCRAFT
European Patent Office | 2018
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