The aeronautics industry has been challenged on many fronts to increase efficiency, reduce emissions, and decrease dependency on carbon-based fuels. The NASA Aeronautics Research Mission Directorate has identified a suite of investments to meet long term research demands beyond the purview of commercial investment. Electrification of aviation propulsion through turboelectric or hybrid electric propulsion is one of many exciting research areas which has the potential to revolutionize the aviation industry. This paper will provide an overview of the turboelectric and hybrid electric technologies being developed under NASAs Advanced Air Transportation Technology (AATT) Project, and how these technologies can impact vehicle design. An overview will be presented of vehicle system studies and the electric drive system assumptions for successful turboelectric and hybrid electric propulsion in single aisle size commercial aircraft. Key performance parameters for electric drive system technologies will be reviewed, and the technical investment made in materials, electric machines, power electronics, and integrated power systems will be discussed. Finally, power components for a single aisle turboelectric aircraft with an electrically driven tail cone thruster and a hybrid electric nine passenger aircraft with a range extender will be parametrically sized.


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    Titel :

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


    Beteiligte:
    Jansen, Ralph H. (Autor:in) / Bowman, Cheryl (Autor:in) / Jankovsky, Amy (Autor:in)

    Kongress:

    AIAA Aviation 2016 Conference ; 2016 ; Washington, DC, United States


    Erscheinungsdatum :

    2016-06-13


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch





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

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


    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 (AIAA 2016-3766)

    Jansen, Ralph / Bowman, Cheryl / Jankovsky, Amy | British Library Conference Proceedings | 2016


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

    HIMMELMANN RICHARD A | Europäisches Patentamt | 2018

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