Abstract Influence of the free air temperature during aircraft takeoff and engine operating time upon the cyclic life of an aircraft GTE turbine disk made from the heat-resistance deformable nickel-base alloy is analyzed and the variation of engine operating parameters in the process of service is taken into account.


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    Title :

    Variation of aircraft GTE turbine disks cyclic life depending on operational factors


    Contributors:

    Published in:

    Publication date :

    2011-06-01


    Size :

    4 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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