A method includes receiving image data from a camera 162 coupled to an air intake system of a gas turbine engine. The image data corresponds to an air passage of the air intake system. The method also includes comparing the received image data to reference image data of the air intake system 164. The method also includes generating an icing notification 168 based at least in part on the comparison when a difference between the received image data and reference image data is greater than an icing threshold.


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    Titel :

    IMAGING ASSISTED GAS TURBINE ANTI-ICING SYSTEM


    Weitere Titelangaben:

    BILDGESTÜTZTES GASTURBINENENTEISUNGSSYSTEM
    SYSTÈME ANTIGIVRAGE DE TURBINE À GAZ ASSISTÉE PAR IMAGERIE


    Beteiligte:

    Erscheinungsdatum :

    04.11.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / 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



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