A system (20) is provided for an aircraft. This aircraft system (20) includes an aircraft powerplant (22), a powerplant sensor system (26), an environment sensor system (28) and a monitoring system (30). The aircraft powerplant (22) includes a heat engine (34). The powerplant sensor system (26) is configured to provide engine data indicative of one or more operating parameters of the heat engine (34). The environment sensor system (28) is configured to provide environment data indicative of one or more environmental parameters of an environment in which the heat engine (34) is operating. The monitoring system (30) is configured to determine formation of a contrail and quantify an impact of the contrail when formed based on the engine data and the environment data.


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    Titel :

    AIRCRAFT CONTRAIL MONITORING AND TARGETED MITIGATION


    Weitere Titelangaben:

    FLUGZEUGKONDENSWAREÜBERWACHUNG UND GEZIELTE ABSCHWÄCHUNG
    SURVEILLANCE DE TRAÎNÉE DE CONDENSATION D'AÉRONEF ET ATTÉNUATION CIBLÉE


    Beteiligte:

    Erscheinungsdatum :

    18.06.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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