A system for enhancing the thrust produced by an aircraft propulsion element having a propulsion fluid outlet includes a shroud element having an inlet, an outlet and a diffusing section positioned between the shroud element inlet and shroud element outlet. The shroud element is coupled to the aircraft such that the diffusing section is positioned directly downstream of the propulsion fluid outlet. At least one actuator is operable to rotate the shroud element about a first transverse axis of the shroud element and a second transverse axis of the shroud element.


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    Titel :

    Gimballed Augmentation Shroud


    Beteiligte:
    EVULET ANDREI (Autor:in)

    Erscheinungsdatum :

    2019-01-17


    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



    GIMBALLED AUGMENTATION SHROUD

    EVULET ANDREI | Europäisches Patentamt | 2019

    Freier Zugriff

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    Servidia, Pablo A. | Elsevier | 2009