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Electromechanical drive for rotary mechanisms in spacecraft

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Russian Engineering Research Aims and scope

Abstract

It has been shown the advantages of electromechanical drive of angular rotation with torque ac converter-fed motor, epicyclic gear, and with cylinder-conic engagement in comparison with existing drives of the same intention. The block diagram of the drive and of reductor engagement, and also some recommendations of how to calculate it are presented.

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References

  1. Lopatin, B.A., Lopatin, D.B., and Kazartsev, D.N., Planetary Gear with Cylindrical-Conical Coupling, Mezhotraslevaya nauch.-prakt. konf. Snezhinsk i nauka (Interdisciplinary Conference on Science in Snezhinsk), Snezhinsk: SFTI, pp. 100, 101.

  2. Tsukanov, O.N. and Poluektov, E.A., Analysis of Cylindrical-Conical Gear Transmissions in Generalized Coordinates, Izv. Vyssh. Uchebn. Zaved., 2007, no. 9, pp. 10–12.

  3. Lopatin, B.A., Tsukanov, O.N., and Kalashnikov, D.B., Software for Calculation and Design of Cylindrical-Conical Couplings for Planetary Gear Systems, Komp. Uchebn. Programmy Innovats., 2007, no. 12, p. 183.

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Authors and Affiliations

  1. South Ural State University, Zlatoust, Russia

    O. N. Tsukanov, D. B. Lopatin & E. A. Poluektov

Authors
  1. O. N. Tsukanov
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  2. D. B. Lopatin
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  3. E. A. Poluektov
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Additional information

Original Russian Text © O.N. Tsukanov, D.B. Lopatin, E.A. Poluektov, 2009, published in Vestnik Mashinostroeniya, 2009, No. 2, pp. 14–16.

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Tsukanov, O.N., Lopatin, D.B. & Poluektov, E.A. Electromechanical drive for rotary mechanisms in spacecraft. Russ. Engin. Res. 29, 116–118 (2009). https://doi.org/10.3103/S1068798X09020026

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  • DOI: https://doi.org/10.3103/S1068798X09020026

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