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Advanced designs of elastic damper supports for aircraft engine rotors

  • Aircraft and Rocket Engine Design and Development
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Abstract

This paper examines the advanced designs of elastic damper supports for aircraft engine rotors. A design of a compound elastic damper support and the method of calculating the adjustable hydrodynamic damper are proposed.

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References

  1. Belousov, A.I. Balyakin, V.B., and Novikov, D.K., Teoriya i proektirovanie gidrodinamicheskikh dempferov opor rotorov (Theory and Design of Hydrodynamic Dampers for Rotor Supports), Samara: Izd. SNTs RAN, 2002.

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  2. Balyakin, V.B., Zhil’nikov E.P., Samsonov V.N., et al., Teoriya i proektirovanie opor rotorov aviatsionnykh GTD (Theory and Design of Aircraft GTE Rotor Supports), Samara: Izd. SGAU, 2007.

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  3. Balyakin, V.B., Zhil’nikov, E.B., Makarchuk, V.V., Kozhin, A.O., and Murashkin, V.V., RU Patent 2400655, Byul. Izobr., 2010, no. 27.

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Correspondence to V. B. Balyakin.

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Original Russian Text © V.B. Balyakin, 2015, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2015, No. 1, pp. 35–38.

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Balyakin, V.B. Advanced designs of elastic damper supports for aircraft engine rotors. Russ. Aeronaut. 58, 42–47 (2015). https://doi.org/10.3103/S1068799815010079

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  • DOI: https://doi.org/10.3103/S1068799815010079

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