Disclosed is a system for generating power for an aircraft. The system includes a boundary layer ingestion propulser that includes a propulsion fan configured to receive torsional energy from a boundary layer airstream, and a motor generator in operable communication with the propulsion fan and configured to generate power in response to rotation of the propulsion fan.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    EMERGENCY POWER GENERATION VIA ELECTRICALLY DRIVEN TAIL CONE BOUNDARY LAYER INGESTION THRUSTER


    Beteiligte:

    Erscheinungsdatum :

    2018-09-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



    EMERGENCY POWER GENERATION VIA ELECTRICALLY DRIVEN TAIL CONE BOUNDARY LAYER INGESTION THRUSTER

    HIMMELMANN RICHARD A | Europäisches Patentamt | 2018

    Freier Zugriff

    VARIABLE SPEED AC BUS POWERED TAIL CONE BOUNDARY LAYER INGESTION THRUSTER

    HIMMELMANN RICHARD A | Europäisches Patentamt | 2018

    Freier Zugriff


    Sizing Power Components of an Electrically Driven Tail Cone Thruster and a Range Extender

    Jansen, Ralph / Bowman, Cheryl / Jankovsky, Amy | AIAA | 2016


    Sizing Power Components of an Electrically Driven Tail Cone Thruster and a Range Extender

    Jansen, Ralph H. / Bowman, Cheryl / Jankovsky, Amy | NTRS | 2016