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 ingestion propulsion


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

    Erscheinungsdatum :

    28.04.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    ASSEMBLY FOR AIRCRAFT COMPRISING ENGINES WITH BOUNDARY LAYER PROPULSION BY INJECTION

    NEGULESCU CAMIL / ROGERO JEAN-MICHEL / FAURE RENAUD | Europäisches Patentamt | 2017

    Freier Zugriff

    Boundary Layer Ingestion Propulsion Benefit for Transport Aircraft

    Hall, David K. / Huang, Arthur C. / Uranga, Alejandra et al. | AIAA | 2017



    Conceptual Analysis of Boundary Layer Ingestion towards Aircraft Propulsion Integration

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


    Benefits of Boundary Layer Ingestion Propulsion

    Sabo, Kevin M. / Drela, Mark | AIAA | 2015