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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    Titel :

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


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    01.06.2011


    Format / Umfang :

    4 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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