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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    Title :

    Assembly for aircraft comprising engines with boundary layer ingestion propulsion


    Contributors:

    Publication date :

    2020-04-28


    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 / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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    NEGULESCU CAMIL / ROGERO JEAN-MICHEL / FAURE RENAUD | European Patent Office | 2017

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    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