Continuing interest in fuel efficient Prop-Fan propulsion has highlighted the need for a large horsepower advanced technology turboprop engine. The initial application could be in a 100-150 passenger short/medium range aircraft. An engine concept which could provide from 9000 to 25000 SHP for commercial and military applications, and which could be available for introduction to service by 1990, is described. Results of engineering studies which support the preliminary design of the power unit and the approach being taken to defining the reduction gear are presented. Key technology issues related specifically to the propulsion system are identified. (Wassmann)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Turboprop engine propulsion for the 1990's


    Weitere Titelangaben:

    Propellerturbinentriebwerk fuer die neunziger Jahre


    Beteiligte:
    Reynolds, C.N. (Autor:in) / Banach, H.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1981


    Format / Umfang :

    8 Seiten, 12 Bilder, 2 Tabellen, 5 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Turboprop engine propulsion for the 1990's

    BANACH, H. J. / REYNOLDS, C. N. | AIAA | 1984


    Turboprop engine propulsion for the 1990's

    BANACH, H. / REYNOLDS, C. | AIAA | 1981



    Commuter Turboprop Propulsion Technology

    Hirschkron, R. / Warren, R.E. | SAE Technical Papers | 1980


    POWERED TURBOPROP ENGINE

    CARROUSET PIERRE / CARROUSET NICOLE / CARROUSET GABRIELLE | Europäisches Patentamt | 2017

    Freier Zugriff