In one example embodiment, a strut (14) for mounting a jet engine (10) to a wing (12) of an aircraft includes a plurality of engine mounts (312, 316) and a space frame truss (600) supported from the wing (12) and comprising front and aft portions, the front portion (602) being coupled to and supporting the engine mounts (312, 316), the aft portion (604) extending upwardly and rearwardly from an aft end of the front portion (602). By removing the aft end of the strut (14) from the core exhaust zone (20) of the engine (10), substantial reductions in the weight and drag of the strut (14), 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


    Weitere Titelangaben:

    STRAHLTRIEBWERKSMONTAGESTREBEN MIT VERBESSERTER LEISTUNG
    PYLÔNES HAUTES PERFORMANCES DE FIXATION DE RÉACTEUR


    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) / PARMINDER SINGH (Autor:in) / HARPAL NAIMISHKUMAR (Autor:in) / NA ANDREW Y (Autor:in)

    Erscheinungsdatum :

    2019-06-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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