The possibility of improving aircraft range, payload, and endurance through application of regenerative cycle engines is examined in this paper. Emphasis is placed on the reduction in propulsion system weight realizable for first and second generation aircraft of the future. Propulsion system characteristics of future regenerative and nonregenerative turboshaft, turboprop, and turbofan engines is estimated and discussed.


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    Titel :

    Application of Regenerative Engines to Current and Future Aircraft


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Mehwald, G. (Autor:in) / Sallee, G. P. (Autor:in)

    Kongress:

    1965 International Automotive Engineering Congress and Exposition ; 1965



    Erscheinungsdatum :

    01.02.1965




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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    Future development of aircraft engines

    Schwab, R. R. / Deutschen Verband fur Schweisstechnik | British Library Conference Proceedings | 1993


    Aircraft Engines and the Future

    Emerald Group Publishing | 1930



    Regenerative System for Turboprop Engines

    Agrawal, Rishabh / Singh, Deepanshu / Subbarao, PMV | AIAA | 2017