New approaches based on the Euler methodology and CFD-technologies for designing complex jet systems
UDC: 622.276
DOI: -
Authors:
VORONOVA VICTORIA V.
1,
GRYAZNOVA INNA V.
1,
BONDARENKO ANTON V.
1
1 National University of Oil and Gas “Gubkin University”, Moscow, Russian Federation
Keywords: Euler methodology, CFD technology, jet systems, modeling, thrust vector
Annotation:
The article presents the results of scientific research in the field of jet systems. Scientific approaches are proposed and corresponding technical solutions are patented for the creation of new ejection systems based on a controlled all-aspect nozzle, with the ability to high-speed deflection of the thrust vector (velocity vector) in any direction within a full geometric sphere. The research results are recommended to be implemented in the creation of energy-efficient multi-mode technical systems in the field of compressor, pump and turbine technologies for various areas of the economy, as well as in the creation of new digital computerized control systems using ejection devices and systems. Individual results of the work can be used in the creation of promising unmanned vehicles operating on land, under water or in the air.
Bibliography:
1. Sazonov Yu.A. Metodologiya konstruirovaniya nasosnyh ustanovok // Trudy Rossijskogo gosudarstvennogo universiteta nefti i gaza imeni I.M. Gubkina. – 2010. – № 2 (259). – S. 94–100.
2. Razrabotka perspektivnyh tekhnologij s primeneniem ezhektornyh sistem i setchatyh turbin / Yu.A. Sazonov, M.A. Mohov, I.V. Gryaznova [i dr.] // Trudy Rossijskogo gosudarstvennogo universiteta nefti i gaza imeni I.M. Gubkina. –2020. – № 4 (301). – S. 49–60.
3. Development and Prototyping of Jet Systems for Advanced Turbomachinery with Mesh Rotor / Y.A. Sazonov, M.A. Mokhov, I.V. Gryaznova [et al.] // Emerging Science Journal. – 2021. – Vol. 5, № 5. – R. 775–801. – DOI: 10.28991/esj-2021-01311
4. Designing Mesh Turbomachinery with the Development of Euler’s Ideas and Investigating Flow Distribution Characteristics / Y.A. Sazonov, M.A. Mokhov, I.V. Gryaznova [et al.] // Civil Engineering Journal (C.E.J). – 2022. – Vol. 8, № 11. – P. 2598–2627. – DOI: 10.28991/CEJ-2022-08-11-017
5. Sazonov Yu.A. Osnovy rascheta i konstruirovaniya nasosno-ezhektornyh ustanovok. – M.: GUP Izd-vo “Neft’ i gaz” RGU nefti i gaza imeni I.M. Gubkina, 2012. – 305 s. – URL: https://www.gubkin.ru/faculty/mechanical_engineering/chairs_and_departments/machines_and_equipment/Sazonov_Yu.A._Osnovy_rascheta_i_konstr-niya_nas.-ezhekt._ustanovok.pdf
6. Raskin N.M. Voprosy tekhniki u Ejlera // Leonard Ejler. Sbornik statej v chest’ 250-letiya so dnya rozhdeniya, predstavlennyh Akademii nauk SSSR / pod red. M.A. Lavrent’eva, A.P. Yushkevicha, A.T. Gruggor’yana. – M.: Izdatel’stvo Akademii nauk SSSR, 1958. – S. 499–556.
7. Voronov Yu.P. Forsajt kak instrument / pod red. V.I. Suslova. – Novosibirsk: IEOPP SO RAN, 2010. – 212 s.
8. Ackeret (Zurich) J. Untersuchung einer nach den Eulerschen Vorschlagen (1754) Gebauten Wasserturbine // Schweizerische Bauzeitung. – 1944. – Bd. 123, № 1. – URL: https://arxiv.org/ftp/barxiv/papers/2108/2108.12048.pdf
9. Kuznecov V.E. Adaptivnoe upravlenie elektrogidravlicheskimi privodami rulevyh aviacionnyh kompleksov: avtoref. dis. … d-ra tekh. nauk. – SPb: FGAOUVO Sankt-Peterburgskij gosudarstvennyj elektrotekhnicheskij universitet LETI im. V.I. Ul'yanova (Lenina), 2017. – 32 s. – URL: https://etu.ru/assets/files/nauka/dissertacii/2017/Kuznecov/Avtoreferat-Kuznecova-VE.pdf
10. Taherinezhad M., Ramirez-Serrano A. An Enhanced Incremental Nonlinear Dynamic Inversion Control Strategy for Advanced Unmanned Aircraft Systems // Aerospace. – 2023. – № 10. – 843 p. – URL: https://doi.org/10.3390/aerospace10100843
11. Numerical Investigation on the Effect of Section Width on the Performance of Air Ejector with Rectangular Section / Y. Zhang, J. Dong, S. Song [et al.] // Entropy. – 2023. – № 25. – 179 p. – URL: https://doi.org/10.3390/e25010179
12. Performance Analysis of Transcritical CO2 Quasi-Secondary Compression Cycle with Ejector Based on Pinch Point / J. Yang, X. Zhang, L. Wang [et al.] // Designs. – 2023. – № 7. – 89 p. – URL: https://doi.org/10.3390/designs7040089
13. Prediction of Performance and Geometrical Parameters of Single-Phase Ejectors Using Artificial Neural Networks / M. Bencharif, S. Croquer, Y. Fang [et al.] // Thermo. – 2023. – № 3. – R. 1–20. – URL: https://doi.org/10.3390/thermo3010001
14. Numerical Study on Flow and Noise Characteristics of High-Temperature and High-Pressure Steam Ejector / J. Zhang, Y. Liu, Y. Guo [et al.] // Energies. – 2023. – № 16. – P. 41–58. – URL: https://doi.org/10.3390/en16104158
15. Optimum Efficiency of a Steam Ejector for Fire Suppression Based on the Variable Mixing Section Diameter / Y. Han, X. Wang, A. Li [et al.] // Entropy. – 2022. – № 24. – R.1625. – URL: https://doi.org/10.3390/e24111625
16. US Patent № 3,064,878. Method and apparatus for high performance evacuation system. – URL: https://www.freepatentsonline.com/3064878.pdf
17. Efficiency Optimization of an Annular-Nozzle Air Ejector under the Influence of Structural and Operating Parameters / I.A. Lysak, G.V. Lysak, Konyukhov [et al.] // Mathematics. – 2023. – № 11. – R. 3039. – URL: https://doi.org/10.3390/math11143039
18. Computational Fluid Dynamics (CFD) Simulation of Mesh Jet Devices for Promising Energy-Saving Technologies / Y.A. Sazonov, M.A. Mokhov, I.V. Gryaznova [et al.] // Civil Engineering Journal (C.E.J). – 2022. – Vol. 8, № 12. – P. 2749–2767. – DOI: 10.28991/CEJ-2022-08-12-06
19. Patent na izobretenie RF № 2 778 961. Strujnaya nasosnaya ustanovka / Yu.A. Sazonov, M.A. Mohov, H.A. Tumanyan, M.A. Frankov, V.V. Voronova, N.N. Balaka; zayavka № 2021136705, 13.12.2021; opubl. 29.08.2022, Byul. № 25. – URL: https://www1.fips.ru/ofpstorage/Doc/IZPM/RUNWC1/000/000/002/778/961/%D0%98%D0%97-02778961-00001/document.pdf
20. Prototyping mesh turbine with the jet control system / Yu.A. Sazonov, M.A. Mokhov, Kh.A. Tumanyan [et al.] // Periódico Tchê Química. – 2020. – Vol. 17, № 36. – P. 1160–1175. – URL: http://www.deboni.he.com.br/Periodico36.pdf