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Tribodiagnostics of aviation reduction gears according to the stages of the surface fatigue wear for its units

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Abstract

One method for the early examination of the aviation reduction gear’s state is to predict the rates of process of surface fatigue wear according to the type of fatigue wear particles, which appear in friction units. We perform this investigation based on example of the main reduction gear of the helicopter and reduction gears of the KSA type of MIG-29K/KUB aircraft during their bench testing.

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References

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Authors and Affiliations

  1. Baranov Central Institute of Aviation Motors, Moscow, 111116, Russia

    L. A. Shabalinskaya, V. V. Golovanov, E. S. Bubnova & A. O. Melnikov

  2. AO “KLIMOV”, St. Petersburg, 194100, Russia

    A. V. Grigorev & E. S. Prodanov

Authors
  1. L. A. Shabalinskaya
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  2. V. V. Golovanov
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  3. E. S. Bubnova
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  4. A. O. Melnikov
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  5. A. V. Grigorev
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  6. E. S. Prodanov
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Corresponding author

Correspondence to L. A. Shabalinskaya.

Additional information

Original Russian Text © L.A. Shabalinskaya, V.V. Golovanov, E.S. Bubnova, A.O. Melnikov, A.V. Grigorev, E.S. Prodanov, 2017, published in Trenie i Iznos, 2017, Vol. 38, No. 4, pp. 341–346.

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Shabalinskaya, L.A., Golovanov, V.V., Bubnova, E.S. et al. Tribodiagnostics of aviation reduction gears according to the stages of the surface fatigue wear for its units. J. Frict. Wear 38, 297–301 (2017). https://doi.org/10.3103/S1068366617040122

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  • DOI: https://doi.org/10.3103/S1068366617040122

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