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

  • Aircraft and Rocket Engine Design and Development
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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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Authors and Affiliations

  1. Ufa State Aviation Technical University, ul. Karla Marksa 12, Ufa, 450000, Bashkortostan, Russia

    G. G. Kulikov, V. A. Trushin, A. I. Abdulnagimov & A. A. Ganeev

Authors
  1. G. G. Kulikov
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  2. V. A. Trushin
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  3. A. I. Abdulnagimov
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  4. A. A. Ganeev
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Corresponding author

Correspondence to G. G. Kulikov.

Additional information

Original Russian Text © G.G. Kulikov, V.A. Trushin, A.I. Abdulnagimov, A.A. Ganeev, 2016, published in Izvestiya VUZ, Aviatsionnaya Tekhnika, 2016, No. 1, pp. 71-76.

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Kulikov, G.G., Trushin, V.A., Abdulnagimov, A.I. et al. Concept of monitoring for thermostressed state and service life of aircraft gas turbine engine blades. Russ. Aeronaut. 59, 77–83 (2016). https://doi.org/10.3103/S1068799816010128

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  • DOI: https://doi.org/10.3103/S1068799816010128

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