Energy mathematical model of an aircraft power transfer unit
- Authors: Konstantinov S.Y.1, Kuderko D.A.2, Polyakov N.A.2, Tselishchev V.A.1
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Affiliations:
- Ufa University of Science and Technology
- Holding «Technodinamika»
- Issue: Vol 11, No 1 (2025): 30.04.2025
- Pages: 51-61
- Section: Articles
- URL: https://journals.rcsi.science/2409-4579/article/view/312372
- DOI: https://doi.org/10.18287/2409-4579-2025-11-1-51-61
- ID: 312372
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Abstract
The article proposes an energy mathematical model of an aircraft power transmission unit, as well as the results of experimental studies of a model power transmission unit at the “Diagnostics and Identification of Hydraulic Systems” stand of the Department of Applied Fluid Mechanics of the Federal State Budgetary Educational Institution of Higher Education UUNiT. The proposed mathematical model was verified with experiment, showing good consistency and sufficient reliability. The energy model of the data transmission unit is compared with existing and evaluated predictions for its application.
Keywords
About the authors
Sergey Y. Konstantinov
Ufa University of Science and Technology
Author for correspondence.
Email: konstserge@mail.ru
Candidate of Science(Engineering), Associate Professor of the Department of the Applied Hydromechanics
Russian Federation, UfaDmitriy A. Kuderko
Holding «Technodinamika»
Email: dm_kuderko@mail.ru
Candidate of Science(Engineering), Director of Design Center,
JSC “Technodinamika”
Nikolay A. Polyakov
Holding «Technodinamika»
Email: polyakovna@tdhc.ru
Deputy Director of Design Center, JSC “Technodinamika”
Russian Federation, MoscowVladimir A. Tselishchev
Ufa University of Science and Technology
Email: pgl.ugatu@mail.ru
Doctor of Science(Engineering), Professor, Head of the Department
of the Applied Hydromechanics
References
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