A method for supplying air to an engine of an aircraft via an air supply system of the aircraft. A dynamic air intake vent of the system can be closed by a closure member that is movable between a closed position and an open position. A static air intake vent is equipped with a filter medium. During flight, the method comprises an unfiltered operating mode that comprises the following steps: positioning of the closure member in the open position, and, during a phase of forward travel of the aircraft, dynamic intake of a flow of air, then transfer of a first portion of the flow of air to the engine and a second portion of the flow of air to the filter medium in order to clean the filter medium.


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    Titel :

    SYSTEME ET PROCEDE DE FILTRATION D'AIR À MEDIA FILTRANT AUTONETTOYANT POUR UN MOTEUR D'UN AERONEF


    Weitere Titelangaben:

    SYSTEM AND METHOD FOR FILTERING AIR WITH A SELF-CLEANING FILTERING MEDIUM FOR AN ENGINE OF AN AIRCRAFT
    SYSTEM UND VERFAHREN ZUR LUFTFILTERUNG MIT SELBSTREINIGENDEN FILTERMEDIEN FÜR EINEN LUFTFAHRZEUGMOTOR


    Beteiligte:
    FAYARD BENOÎT (Autor:in)

    Erscheinungsdatum :

    28.02.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT





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