Concept of monitoring for thermostressed state and service life of aircraft gas turbine engine blades |
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| Authors: | G G Kulikov V A Trushin A I Abdulnagimov A A Ganeev |
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| 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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