This ARP applies to turbine engines that are to be used in helicopters. It provides the engine designer guide lines in achieving a satisfactory turbine engine drive shaft connection. ARP721 has been reaffirmed to comply with the SAE Five-Year Review policy.


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    Title :

    Turbine Drive Shaft Connection


    Publication date :

    2023-01-20



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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