Research of strength parameters and dynamic characteristics of rotor parts of a promising small sized GTE

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Abstract

The presented work demonstrates a study devoted to assessing the strength characteristics of the rotor elements of a promising small-sized gas turbine engine. The main feature is that the analysis of the stress-strain state of the engine rotor is carried out taking into account vibrations and resonant frequencies. In turn, the assessment of the dynamic characteristics of the rotor elements was carried out taking into account the conditions of their mutual contact. The research materials presented in this article will serve for further iterations of engine design.

About the authors

Dmitriy V. Evdokimov

Samara National Research University; JSC «Aviaagregat»

Author for correspondence.
Email: dmitry.evd.ssau@gmail.com

Candidate of Science (Engineering), Associate Professor of the Department of Engine Production Technologies, Associate Professor of Strength of Materials Department, Senior Researcher of Research laboratory NIL-207; Leading Engineer of JSC «Aviaagregat»

Russian Federation, Samara

Evgeniy P. Filinov

Samara National Research University

Email: filinov@ssau.ru

Candidate of Science (Engineering), Associate Professor of the Department of Theory of Aircraft Engines named after V.P. Lukachev, Senior Researcher of Research laboratory  NIL-207, Senior Researcher of «Advanced Aerospace Engineering School», с.н.с. KB-203 (Engine Engineering Design Bureau of Samara University)

Russian Federation, Samara

Dmitriy L. Skuratov

Samara National Research University

Email: dmitry.evd.ssau@gmail.com

Doctor of Science (Engineering), Professor

Russian Federation, Samara

Yaroslav A. Ostapyuk

Samara National Research University

Email: dmitry.evd.ssau@gmail.com

Researcher of NIL-207, Senior Lecturer of the Department of Aircraft Engine Theory named after V. P. Lukachev, Researcher of KB-203

Russian Federation, Samara

References

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  2. Antonyuk, V. E. (2005), "Dynamic stabilization of disk-type parts", Strengthening technologies and coatings, no. 7, pp. 24-29. (in Russian).
  3. Antonyuk, V. E. (2005), "Technological possibilities for increasing the accuracy of manufacturing disks and shafts", Mechanical engineering technology, no. 6, pp. 43-48. (in Russian).
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  5. Shevchenko, V. P., Vlasov, O. I. and Kairov, V. A. (2013), "Experimental study of natural vibrations of structurally inhomogeneous cylindrical shells", News of NTUU "KPI". Machine-building series, no. 2 (68), pp. 122-127. (in Russian).
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  7. Kay, G. and Lesuer, D. (2003), Failure Modeling of Titanium 6Al-4V and Aluminum 2024-T3 With the Johnson-Cook Material Model: research report (conclusion), Lawrence Livermore National Laboratory, National Technical Information Service (NTIS), Virginia, 17 p.
  8. Dorogoy, A and Rittel, D. (2005), "Numerical Validation of the Shear Compression Specimen. Part I: Quasi-static Large Strain Testing", Experimental mechanics, vol. 45, no. 2, pp. 167-177.
  9. Dorogoy, A and Rittel, D. (2005), "Numerical Validation of the Shear Compression Specimen. Part II: Dynamic Large Strain Testing", Experimental mechanics, vol. 45, no. 2. pp. 178-185.
  10. Baturin, O.V., Lyu, Ch., Sun, P. and Han, K. (2022), "Educational Optimization Software for Axial Compressor Flow Path Design", 2022 IEEE 5th International Conference on Electronics Technology (ICET 2022), pp. 381-385.
  11. Ananyev, I. V. and Timofeev, P. G. (1965), Vibrations of elastic systems in aircraft structures and their damping, Mashinostroenie [Mechanical Engineering], Moscow, 526 p. (in Russian).

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Copyright (c) 2024 Evdokimov D.V., Filinov E.P., Skuratov D.L., Ostapyuk Y.A.

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Journal of Dynamics and Vibroacoustics

ISSN 2409-4579 (Online)

Publisher and Founder: Samara National Research University, 34, Moskovskoye shosse, Samara, 443086, Russian Federation.

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Editor-in-chief:  Academician of the RAS
E. V. Shakhmatov 

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Address for correspondence: 34, Moskovskoye shosse, Samara, 443086, Russian Federation, Samara National Research University (room 324, building 14)

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