The purpose of this paper is to propose specific power and efficiency as the key performance parameters for a turboelectric aircraft power system and investigate their impact on the overall aircraft. Key functional requirements are identified that impact the power system design. Breguet range equations for a base aircraft and a turboelectric aircraft are found. The benefits and costs that may result from the turboelectric system are enumerated. A break-even analysis is conducted to find the minimum allowable electric drive specific power and efficiency that can preserve the range, initial weight, operating empty weight, and payload weight of the base aircraft.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Turboelectric Aircraft Drive Key Performance Parameters and Functional Requirements


    Beteiligte:

    Kongress:

    AIAA Propulsion & Energy 2015 ; 2015 ; Orlando, FL, United States


    Erscheinungsdatum :

    2015-07-27


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Turboelectric Aircraft Drive Key Performance Parameters and Functional Requirements

    Jansen, Ralph / Brown, Gerald V. / Felder, James L. et al. | AIAA | 2015


    Turboelectric Aircraft Drive Key Performance Parameters and Functional Requirements

    Jansen R. / Brown G. V. / Felder J. L. et al. | NTIS | 2015


    Turboelectric Aircraft Drive Key Performance Parameters and Functional Requirements

    Jansen, Ralph / Brown, Gerald V. / Felder, James L. et al. | NTRS | 2015


    Turboelectric Aircraft Drive Key Performance Parameters and Functional Requirements

    Jansen, Ralph H. / Brown, Gerald V. / Felder, James L. et al. | NTRS | 2016


    Turboelectric Aircraft Drive Key Performance Parameters and Functional Requirements (AIAA 2015-3890)

    Jansen, Ralph / Brown, Gerald V. / Felder, James L. et al. | British Library Conference Proceedings | 2015