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 Aircraft Eng v 33 n 385 Mar 1961 p 67)


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    Title :

    Turboprops for light aircraft


    Additional title:

    Oil Engine Gas Turbine


    Published in:

    Publication date :

    1961


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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