The mission capability of some gas turbine powered vehicles can be greatly enhanced by the application of regeneration to the engine thermodynamic cycle. The application of regeneration to aircraft propulsion presents many unique design problems to the designer as a result of the need for very lightweight components and high performance. The many design parameters that must be evaluated, and the many tradeoff studies that must be accomplished to arrive at the best regenerator and gas turbine design are discussed. Also, the results of a series of studies are presented to graphically portray the fuel economy which results from the use of regenerative engines.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Improved Mission Capability and Economy via Regeneration


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    1965 International Automotive Engineering Congress and Exposition ; 1965



    Erscheinungsdatum :

    01.02.1965




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Improved mission capability and economy via regeneration

    Redmond, W.A. / Beam, Jr., P.E. | Engineering Index Backfile | 1965


    An Example of Improved Mission Capability through Date Fusion

    Bernhardt, M. / Royal Aeronautical Society | British Library Conference Proceedings | 1994


    Dynamic Mission Capability Analysis

    I. E. Marvin / H. P. Durand | NTIS | 1964


    Space Shuttle mission extension capability

    Fraser, W. M., Jr. | NTRS | 1984


    Mali mission matures sentinel capability

    Osborne, Tony | Online Contents | 2013