There is provided a method and system for operating a turboprop engine of an aircraft. When a resulting value for Ng is between at least one upper limit and at least one lower limit, the output power is governed as a function of the target power. When the resulting value for Ng is on or outside of the at least one upper limit and the at least one lower limit, the output power is governed as a function of the maximum Ng and the minimum Ng.
SYSTEM AND METHOD FOR OPERATING A TURBOPROP ENGINE
SYSTEME ET METHODE D`EXPLOITATION D`UN TURBOPROPULSEUR
2021-01-26
Patent
Electronic Resource
English