An integrated propulsion system comprising at least two gas turbine engines, at least one fan, and a transmission assembly coupling the at least two gas turbine engines to the at least one fan wherein the at least two gas turbine engines are disposed within a main body of an airframe comprising the main body and a pair of wings, and wherein the number of gas turbine engines is greater than the number of fans.


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    Titel :

    INTEGRATED AIRCRAFT PROPULSION SYSTEM


    Beteiligte:
    RICE EDWARD C (Autor:in) / KELLER RICHARD K (Autor:in) / BRYAN WILLIAM B (Autor:in)

    Erscheinungsdatum :

    2018-10-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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