A method (500) of modeling and integrating engine installation deltas includes receiving (502) flight data related to an aircraft that includes an engine installed therein. The flight data includes values of an engine parameter. The method also includes determining (504) values of a measured installation delta for the engine based, at least in part, on the flight data. The method also includes determining (506) values of a measured power parameter for the engine based, at least in part, on the flight data. The method also includes generating (510) a mathematical model of a plurality of installation deltas for the engine as a function of the engine parameter, where the plurality of installation deltas include the measured installation delta and an unmeasured installation delta. The method also includes validating (512) the mathematical model based, at least in part, on the values of the measured installation delta. The method also includes generating (516) a performance profile of the engine.


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    Title :

    MODELING AND INTEGRATING AIRCRAFT ENGINE INSTALLATION DELTAS


    Additional title:

    MODELLIERUNG UND INTEGRATION VON FLUGTRIEBWERKINSTALLATIONSDELTAS
    MODÉLISATION ET INTÉGRATION DE DELTAS D'INSTALLATION DE MOTEUR D'AÉRONEF


    Contributors:

    Publication date :

    2022-06-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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    SIEMSEN MARK ALLEN / TJANDRA ALBERTUS MULJADI | European Patent Office | 2022

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