Occurrence of nonlinear effects in the suspension of floating gyroscope

Authors

  • Виктория Николаевна Мельник National Technical University of Ukraine “Kyiv Polytechnic Institute”, Avenue Victories, 37, Kyiv, Ukraine, 03056, Ukraine https://orcid.org/0000-0002-0004-7218
  • Владимир Владимирович Карачун National Technical University of Ukraine “Kyiv Polytechnic Institute”, Avenue Victories, 37, Kyiv, Ukraine, 03056, Ukraine
  • Галина Владимировна Бойко National Technical University of Ukraine “Kyiv Polytechnic Institute”, Avenue Victories, 37, Kyiv, Ukraine, 03056, Ukraine https://orcid.org/0000-0003-4011-8110

DOI:

https://doi.org/10.15587/2312-8372.2015.41465

Keywords:

float gyroscope, nonlinear effects, resonance overlap, design models

Abstract

It is built the refined model of the elastic interaction of penetrating acoustic radiation with float gyroscope to detect non-linear effects of resonant type in the suspension at the operational use of the gyroscope.

It is investigated the cylindrical shell part of device case, computational model of which is built in the form of elastic compliance shell with acoustic impedance.

The regularity of elastic radial displacements of the material of device body in the radial direction is determined and its acoustic permeability in a hypersonic flight is defined. The conditions for the appearance of "acoustic transparency" of the case in the event of resonance overlap are outlined.

An application area in suborbital and atmospheric hypersonic technology at forming initiation of the resonance overlap in the suspension of gyroscope, leading to the onset of the "acoustic transparency" of the body.

The obtained results can serve as the basis of decision-making in the selection of design models of investigated effects from the perspective of pending outline of wave size in hypersonic flight operating conditions and ensuring the appropriate choice of impedance of the body material.

Author Biographies

Виктория Николаевна Мельник, National Technical University of Ukraine “Kyiv Polytechnic Institute”, Avenue Victories, 37, Kyiv, Ukraine, 03056

Doctor of Engineering, Professor, Head of Department

Department of Bioengineering and Engineering

Владимир Владимирович Карачун, National Technical University of Ukraine “Kyiv Polytechnic Institute”, Avenue Victories, 37, Kyiv, Ukraine, 03056

Doctor of Engineering, Professor

Department of Bioengineering and Engineering 

Галина Владимировна Бойко, National Technical University of Ukraine “Kyiv Polytechnic Institute”, Avenue Victories, 37, Kyiv, Ukraine, 03056

Graduate student

Department of Bioengineering and Engineering

References

  1. Ishlinskij, A. Y. (1976). Orientation, gyroscopes and inertial navigation. Moscow, USSR: Nauka, 672.
  2. Feodosyev, V. I., Sinyarev, G. B. (1969). Introduction to rocket technology. Moscow, USSR: Defense Publishing, 506.
  3. Wrigley, W., Hollister, W., Denhardt, W. (1972). The theory, design and testing of gyroscopes. Translated from English. Moscow, USSR: Mir, 416.
  4. Mel'nick, V. N., Karachun, V. V. (2013). Hypersonic technology and some navigation problems. Kyiv, Ukraine: Kornіychuk, 152.
  5. Boyko, G. (2013). Linearly elastic suspension of the float gyroscope in the acoustic field. Technology Audit And Production Reserves, 6(1(14)), 7-10. Available: http://journals.uran.ua/tarp/article/view/19534
  6. Boiko, G. V. (2013). Additional error of floating gyroscope under flight manual. Proceedings of the All-Ukrainian scientific-practical conference of young scientists “Problems of navigation and motion control”. Kyiv: NAU, 85.
  7. Shybetskyy, V. U. (2013). Euler inertial forces in noninertional coordinates of float gyroscope suspension. VIII International scientific and practical. conf. “Science and innovation -2013”. Poland, Przemysl, 90-92.
  8. Kosova, V. P. (2012). Supersonic flight and gyro error float. Proceedings of the International Scientific Conference «Achievement of high school – 2012», Vol. 26. Technology. Sofia: "Byal GRAD-BG" LTD, 30-32.
  9. Karachun, V., Mel’nick, V. (2010). Wave tasks of inertial navigation. Eastern-European Journal Of Enterprise Technologies, 6(3(48)), 16-20. Available: http://journals.uran.ua/eejet/article/view/3238
  10. Karachun, V. V., Mel’nik, V. N. (2012, July). Influence of diffraction effects on the inertial sensors of a gyroscopically stabilized platform: three-dimensional problem. International Applied Mechanics, Vol. 48, № 4, 458–464. doi:10.1007/s10778-012-0533-y
  11. Karachun, V. V., Mel’nik, V. N. (2012, November). Elastic stress state of a floating-type suspension in the acoustic field. Deviation of the spin axis. Strength of Materials, Vol. 44, № 6, 668–677. doi:10.1007/s11223-012-9421-2

Downloads

Published

2015-04-02

How to Cite

Мельник, В. Н., Карачун, В. В., & Бойко, Г. В. (2015). Occurrence of nonlinear effects in the suspension of floating gyroscope. Technology Audit and Production Reserves, 2(3(22), 30–33. https://doi.org/10.15587/2312-8372.2015.41465

Issue

Vol. 2 No. 3(22) (2015): Systems and control processes

Section

Systems and Control Processes: Original Research

License

Copyright (c) 2016 Виктория Николаевна Мельник, Владимир Владимирович Карачун, Галина Владимировна Бойко

Creative Commons License

This work is licensed under a Creative Commons Attribution 4.0 International License.

The consolidation and conditions for the transfer of copyright (identification of authorship) is carried out in the License Agreement. In particular, the authors reserve the right to the authorship of their manuscript and transfer the first publication of this work to the journal under the terms of the Creative Commons CC BY license. At the same time, they have the right to conclude on their own additional agreements concerning the non-exclusive distribution of the work in the form in which it was published by this journal, but provided that the link to the first publication of the article in this journal is preserved.