There a few NASA funded electric and hybrid electric projects from different NASA Centers, including the NASA Armstrong Flight Research Center (AFRC) (Edwards, California). Each project identifies a specific technology gap that is currently inhibiting the growth and proliferation of relevant technologies in commercial aviation. This paper describes the design and development of a turbo-electric distributed propulsion (TeDP) hardware-in-the-loop (HIL) simulation bench, which is a test bed for discovering turbo-electric control, distributed electric control, power management control, and integration competencies while providing risk mitigation for future turbo-electric flying demonstrators.


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    Title :

    Design and Development of a 200-kW Turbo-Electric Distributed Propulsion Testbed


    Contributors:

    Publication date :

    2017-01-31


    Type of media :

    Article/Chapter (Book)


    Type of material :

    No indication


    Language :

    English




    Design and Development of a 200-kW Turbo-Electric Distributed Propulsion Testbed

    Papathakis, Kurt V. / Kloesel, Kurt J. / Lin, Yohan et al. | NTRS | 2016



    Design and Development of a 200-kW Turbo-Electric Distributed Propulsion Testbed

    K. V. Papathakis / K. J. Kloesel / Y. Lin et al. | NTIS | 2016


    Design and Development of a 200-kw Turbo-Electric Distributed Propulsion Testbed

    K. V. Papathakis / K. J. Kloesel / Y. Lin et al. | NTIS | 2016


    Design and Development of a 200-kw Turbo-Electric Distributed Propulsion Testbed

    Papathakis, Kurt V. / Kloesel, Kurt J. / Lin, Yohan et al. | NTRS | 2016