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Hardware-in-the-loop testing technology for integrated control and condition monitoring systems of aircraft gas turbine engines

  • Aircraft and Rocket Engine Design and Development
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Abstract

Hardware-in-the-loop testing technology for automatic control, condition monitoring and diagnostics systems of gas turbine engines is described. The technology proposed makes it possible to simulate combinations and chains of unexpected and gradual failures of engines, transducers and actuators.

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References

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Authors and Affiliations

  1. Ufa State Aviation Technical University, Ufa, Russia

    G. G. Kulikov, V. Yu. Ar’kov & A. I. Abdulnagimov

Authors
  1. G. G. Kulikov
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  2. V. Yu. Ar’kov
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  3. A. I. Abdulnagimov
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Additional information

Original Russian Text ©. G.G. Kulikov, V.Yu. Ar’kov, A.I. Abdulnagimov, 2008, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2008, No. 1, pp. 37–40.

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Kulikov, G.G., Ar’kov, V.Y. & Abdulnagimov, A.I. Hardware-in-the-loop testing technology for integrated control and condition monitoring systems of aircraft gas turbine engines. Russ. Aeronaut. 51, 47–52 (2008). https://doi.org/10.3103/S106879980801008X

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  • DOI: https://doi.org/10.3103/S106879980801008X

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