The report presents the results of dynamic load tests performed on a turbine powered helicopter transmission which incorporates a roller gear drive unit as the main reduction stage. The primary purpose of this program was to conduct a 200-hour endurance test at 100% design speed and at a load spectrum equivalent to military helicopter usage. (Modified author abstract)


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    Title :

    3000-HP Roller Gear Transmission Development Program. Volume IV. Laboratory Bench Test


    Contributors:
    G. F. Gardner (author) / R. E. Haven (author)

    Publication date :

    1974


    Size :

    454 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English