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.


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    Title :

    NO TITLE SPECIFIED


    Additional title:

    AUCUN TITRE SPECIFIE


    Contributors:

    Publication date :

    2020-12-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



    NO TITLE SPECIFIED

    CHANG CHE-WEI / YANG CHENG-KAI / CHANG CHUAN-CHIH | European Patent Office | 2023

    Free access

    NO TITLE SPECIFIED

    SOETEMANS DEVAN ANTHONY / SCHMIDT QUINN MATHEW | European Patent Office | 2021

    Free access

    Maintainability Specified

    Losee, John E. | SAE Technical Papers | 1964


    SAFETY - Not otherwise specified

    Online Contents | 2001


    SAFETY - Not otherwise Specified

    Online Contents | 2001