Systems and methods for integrating Boundary Layer Ingestion (BLI) apparatus into an aircraft (1) are disclosed. 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.


    Access

    Download


    Export, share and cite



    Title :

    BOUNDARY LAYER INGESTION INTEGRATION


    Contributors:

    Publication date :

    2018-06-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



    Boundary layer ingestion integration into aft fuselage

    CONTI ANGELINA M / HARVEY PATRICK G / MISTRY KRUNAL B et al. | European Patent Office | 2020

    Free access

    Boundary layer ingestion duct

    ROLT ANDREW | European Patent Office | 2017

    Free access

    Conceptual Analysis of Boundary Layer Ingestion towards Aircraft Propulsion Integration

    Lv, P. / Rao, A.G. | British Library Conference Proceedings | 2013


    Boundary layer ingestion fan system

    GOODHAND MARTIN N | European Patent Office | 2022

    Free access

    Boundary layer ingestion fan system

    GOODHAND MARTIN N | European Patent Office | 2022

    Free access