In one example, a strut for mounting a jet engine to a wing of an aircraft includes a plurality of engine mounts and a space frame truss supported from the wing and including front and aft portions, the front portion being coupled to and supporting the engine mounts, the aft portion extending upwardly and rearwardly from an aft end of the front portion. By removing the aft end of the strut from the core exhaust zone of the engine, substantial reductions in the weight and drag of the strut, and a corresponding increase in the specific fuel consumption of the associated aircraft may be achieved.


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    Titel :

    ENHANCED PERFORMANCE JET ENGINE MOUNTING STRUTS


    Beteiligte:
    NAKHJAVANI OMID B (Autor:in) / WILLIE ROBERT H (Autor:in) / PARK PAUL S (Autor:in) / HEIDARI MOHAMMAD ALI (Autor:in) / HEBERT LEONARD J (Autor:in) / STEFANOVIC MILAN (Autor:in) / SINGH PARMINDER (Autor:in) / HARPAL NAIMISHKUMAR B (Autor:in) / NA ANDREW Y (Autor:in)

    Erscheinungsdatum :

    2018-06-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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