A boundary layer ingestion engine (120, 300, 400) includes a gas generator (130, 310) and a turbine fluidly connected to the gas generator (130, 310). A fan (330, 406) is mechanically linked to the turbine (140, 320) via a shaft (322) such that rotation of the turbine (140, 320) is translated to the fan (330, 406). A boundary layer ingestion inlet (122, 342, 404) is aligned with an expected boundary layer, such that the boundary layer ingestion inlet (122, 342, 404) is configured to ingest fluid from a boundary layer during operation of the boundary layer ingestion engine (120, 300, 400).


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    Title :

    BOUNDARY LAYER EXCITATION AFT FAN GAS TURBINE ENGINE


    Additional title:

    AFT-FAN-GASTURBINE ZUR GRENZSCHICHTANREGUNG
    TURBINE À GAZ À SOUFFLANTE ARRIÈRE POUR EXCITATION DE COUCHE LIMITE


    Contributors:

    Publication date :

    2021-10-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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