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