The aeronautics industry has been challenged on many fronts to increase efficiency, reduce emissions, and decrease dependency on carbon-based fuels. This paper provides an overview of the turboelectric and hybrid electric technologies being developed under NASA's Advanced Air Transportation Technology (AATT) Project and discusses how these technologies can impact vehicle design. The discussion includes an overview of key hybrid electric studies and technology investments, the approach to making informed investment decisions based on key performance parameters and mission studies, and the power system architectures for two candidate aircraft. Finally, the power components for a single-aisle turboelectric aircraft with an electrically driven tail cone thruster and for a hybrid-electric nine-passenger aircraft with a range extender are parametrically sized, and the sensitivity of these components to key parameters is presented.


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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 ; 2016 ; Washington, DC, United States


    Erscheinungsdatum :

    2016-06-13


    Medientyp :

    Aufsatz (Konferenz)


    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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