There is provided a system and a method for operating a multi-engine rotorcraft. When the rotorcraft is cruising in an asymmetric operating regime (AOR) at least one engine is an active engine and is operated in an active mode to provide motive power to the rotorcraft and at least one second engine is a standby engine and is operated in a standby mode to provide substantially no motive power to the rotorcraft, at least one of a power level of the at least one second engine is increased and at least one variable geometry mechanism of the at least one second engine is moved to shed any ice accumulation on the at least one second engine.
NO TITLE SPECIFIED
AUCUN TITRE SPECIFIE
2020-12-17
Patent
Electronic Resource
English
SAE Technical Papers | 1964
|SAFETY - Not otherwise specified
Online Contents | 2001
SAFETY - Not otherwise Specified
Online Contents | 2001