Email this article 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://ogarev-online.ru/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
- Pokazeev, V. P. (2002), Tekhnicheskoe obsluzhivanie gidrosistemy samoleta TU-154: Metodicheskie ukaza-niya k prakticheskoy rabote [Maintenance of the hydraulic system of the TU-154 aircraft: Guidelines for practical work], Samarsk. gos. aerokos. univ-t., Samara. (in Russian)
- Samolet Il-76TD: instruktsiya po tekhnicheskoy ekspluatatsii ch. III gl. 33. Gidravlicheskaya sistema [Aircraft Il-76TD: technical operation manual, part III, chapter 33. Hydraulic system] (1978), KB Il'yushina, Moscow. (in Russian)
- Krivoy, S. G., Panin, S. A., Kubasov, A. V. and Pimenov, A. V. (2012), Gidravlicheskaya sistema samoleta №2010147306/11 [Aircraft hydraulic system №2010147306/11], Zakrytoe aktsionernoe obshchestvo «Grazhdanskie samolety Sukhogo», Ministerstvo promyshlennosti i torgovli Rossiyskoy Federatsii (2012),: declared 22.11.2010: published 10.07.2012, RU 2 455 197 C1. (in Russian)
- Polyakov, N. A., Solov'eva, A. A. and Tselishchev, V. A. (2021), “Concept of development of power transmission units in the hydraulic system of a civil aircraft”, Vestnik PNIPU. Aerospace engineering, №67, pp. 5-15. doi: 10.15593/2224-9982/2021.67.01. (in Russian)
- Proportional Directional Control Valves A01_Cat2500.indd, ddp, 04/19 A47 (2018), Parker Hannifin Corporation Hydraulic Valve Division Elyria, Ohio, USA A Technical Information Series D*1FB.
- Vickers® Constant Pressure Reversible Power Transfer Unit (2013), Part Number 971600 Model MPHV3-115-1C.
- Kuderko, D. A., Polyakov, N. A., Frolov, G. K. and Tselishchev, V. A. (2024), “High-speed power transmission unit with hydromechanical regulation”, Vestnik PNIPU. Aerospace engineering, №76, pp. 30–40. doi: 10.15593/2224-9982/2024.76.03. (in Russian)
- Kuderko, D. A., Polyakov, N. A., Frolov, G. K. and Tselishchev, V. A. (2023), “Correction of the operation of the emergency hydraulic drive for releasing the aircraft landing gear”, Vestnik PNIPU. Aerospace engineering, №74, pp.51–62. doi: 10.15593/2224-9982/2023.74.05. (in Russian)
- Kuderko, D. A., Polyakov, N. A. and Tselishchev, V. A. (2023), “Constant power regulator of a volumetric hydraulic machine in a power transmission unit of a civil aircraft”, Vestnik USATU, vol. 27, №3 (101), pp. 3-13. (in Russian)
- Konstantinov, S. Yu., Kuderko, D. A., Mukminov, D. F., Polyakov, N. A. and Tselishchev, V. A. (2024), Blok peredachi moshchnosti gidravlicheskoy sistemy samoleta №2023116704 [Aircraft hydraulic power transmission unit №2023116704], Federal'noe gosudarstvennoe byudzhetnoe obrazovatel'noe uchrezhdenie vysshego obrazovaniya «Ufimskiy universitet nauki i tekhnologiy», filed 06/26/2023, published 02/06/2024, RU 2 812 955 C1. (in Russian)
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