To meet requirements for turboprop engines T.P./60 and T.P./90, suitable for club, executive and agricultural aircraft, were developed by Rover Gas Turbines Ltd; two engines are similar featuring single shaft turbine propeller engine with single stage centrifugal compressor, one combustion chamber, single stage turbine and shaft power outlet through reduction gear to propeller; propeller blade roots are retained by ball thrust bearings and pitch movements synchronized by bevel gears. (see also Oil Engine and Gas Turbine v 29 n 332 June 1961 p 74)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Turboprops for light aircraft


    Weitere Titelangaben:

    Aircraft Eng


    Erschienen in:

    Erscheinungsdatum :

    1961


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Turboprops for Light Aircraft

    Emerald Group Publishing | 1961


    Turboprops for light aircraft

    Engineering Index Backfile | 1961


    Tradewind turboprops

    Withee, W.W. | Engineering Index Backfile | 1955



    REGIONALS: JETS v TURBOPROPS

    Duffy, Paul | Online Contents | 1995