A method of suppressing contrails 4a emitted by a propulsion system 3 of an aircraft 1. A first fuel composition is fed into the propulsion system for a predetermined period of time in a step a. The expiry of the predetermined period of time is detected with a timer 18 in a step b. Upon expiry of the predetermined period of time, a second fuel composition is fed into the propulsion system in a step c. The second fuel composition is more prone to cause contrails than the first fuel composition. Contrails generated by the propulsion system are detected as the second fuel composition is fed into the propulsion system. If a contrail is detected, the steps a-c are repeated.


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    Titel :

    Contrail suppression


    Beteiligte:
    MARTIN LEE (Autor:in) / ANTHONY DENNISS (Autor:in) / MATTHEW STUTTARD (Autor:in) / MARTIN AGNEW (Autor:in)

    Erscheinungsdatum :

    23.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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