Abstract A concept of monitoring for material properties with residual life estimation of rotor blades for gas turbine engines is proposed. The structure of on-board control and conditionmonitoring system based on the intelligent pyrometer module with the algorithm for calculating the residual life of turbine rotor blades is described.


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    Title :

    Concept of monitoring for thermostressed state and service life of aircraft gas turbine engine blades


    Contributors:

    Published in:

    Publication date :

    2016-01-01


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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