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Theory of an annular corrugated damper in the vibrator precession motion

  • Aircraft and Rocket Engine Design and Development
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Abstract

The theory for calculating elastodamping characteristics of multilayer corrugated dampers being used in the rotor supports of aircraft gas turbine engines (GTEs), turbo-pump assemblies of rocket engines as well as in different articles of machine building industry is presented.

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References

  1. Chegodayev, D.E. and Ponomarev, Yu.K, Dempfirovanie (Damping), Samara: SGAU, 1997.

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  2. Tsyrlin, A.L., Dinamika rotorov dvoyakoi zhestkosti (Dynamics of Double-Stiffened Rotors), Nauka: Moscow, 1972.

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Authors and Affiliations

  1. Samara State Aerospace University, Samara, Russia

    A. I. Belousov, Yu. K. Ponomarev, Yu. N. Pronichev & D. G. Krypaev

Authors
  1. A. I. Belousov
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  2. Yu. K. Ponomarev
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  3. Yu. N. Pronichev
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  4. D. G. Krypaev
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Additional information

Original Russian Text © A.I. Belousov, Yu.K. Ponomarev, Yu.I. Pronichev, D.G. Krypaev, 2009, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2009, No. 2, pp. 46–49.

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Belousov, A.I., Ponomarev, Y.K., Pronichev, Y.N. et al. Theory of an annular corrugated damper in the vibrator precession motion. Russ. Aeronaut. 52, 201–207 (2009). https://doi.org/10.3103/S1068799809020111

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  • DOI: https://doi.org/10.3103/S1068799809020111

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