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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    Titel :

    NO TITLE SPECIFIED


    Weitere Titelangaben:

    AUCUN TITRE SPECIFIE


    Beteiligte:

    Erscheinungsdatum :

    2020-12-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    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 | Europäisches Patentamt | 2023

    Freier Zugriff

    NO TITLE SPECIFIED

    SOETEMANS DEVAN ANTHONY / SCHMIDT QUINN MATHEW | Europäisches Patentamt | 2021

    Freier Zugriff

    Maintainability Specified

    Losee, John E. | SAE Technical Papers | 1964


    SAFETY - Not otherwise specified

    Online Contents | 2001


    SAFETY - Not otherwise Specified

    Online Contents | 2001