A system is provided for an aircraft. This aircraft system includes an aircraft powerplant, a powerplant sensor system, an environment sensor system and a monitoring system. The aircraft powerplant includes a heat engine. The powerplant sensor system is configured to provide engine data indicative of one or more operating parameters of the heat engine. The environment sensor system is configured to provide environment data indicative of one or more environmental parameters of an environment in which the heat engine is operating. The monitoring system 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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT CONTRAIL MONITORING AND TARGETED MITIGATION


    Beteiligte:

    Erscheinungsdatum :

    2024-02-15


    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



    AIRCRAFT CONTRAIL MONITORING AND TARGETED MITIGATION

    STRATTON RUSSELL | Europäisches Patentamt | 2024

    Freier Zugriff

    AIRCRAFT CONTRAIL MONITORING AND TARGETED MITIGATION

    STRATTON RUSSELL | Europäisches Patentamt | 2024

    Freier Zugriff

    Contrail Mitigation Through 3D Aircraft Trajectory Optimization

    Hartjes, Sander / Hendriks, Thijs / Visser, Dries | AIAA | 2016


    Aircraft contrail detection

    GARRETT TIMOTHY MARK | Europäisches Patentamt | 2016

    Freier Zugriff

    The contrail mitigation potential of aircraft formation flight scenarios

    Unterstraßer, Simon | Deutsches Zentrum für Luft- und Raumfahrt (DLR) | 2020

    Freier Zugriff