In order to further benefit from the principle of boundary layer ingestion by engines of an aircraft assembly, the rear portion of the fuselage of this aircraft assembly includes a front portion which splits up into at least two distinct rear portions, spaced apart from each other, and each integrating the rotary ring of the receiver of one of the engines.


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    Titel :

    ASSEMBLY FOR AIRCRAFT COMPRISING ENGINES WITH BOUNDARY LAYER PROPULSION BY INJECTION


    Beteiligte:
    NEGULESCU CAMIL (Autor:in) / ROGERO JEAN-MICHEL (Autor:in) / FAURE RENAUD (Autor:in)

    Erscheinungsdatum :

    21.12.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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