Systems and methods for integrating Boundary Layer Ingestion (BLI) apparatus into an aircraft (1). The longerons (34) in the aft fuselage (18) may be extended to support an aft propulsor (20). The aft propulsor may be a turbofan or turboelectric propulsion system (46). An upper longeron (34a) may support a tail section (14) of an aircraft. The aft fuselage skin (22) is contoured to permit boundary layer airflow to enter an intake fan (24) of the aft propulsor.


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    Titel :

    Boundary layer ingestion integration into aft fuselage


    Beteiligte:
    CONTI ANGELINA M (Autor:in) / HARVEY PATRICK G (Autor:in) / MISTRY KRUNAL B (Autor:in) / RINK KIMBERLY A (Autor:in) / ROTHAUPT TED K (Autor:in)

    Erscheinungsdatum :

    2020-01-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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