1. ELARTU — Інституційний репозитарій ТНТУ імені Івана Пулюя
  2. Вісник ТНТУ
  3. 2026
  4. Вісник ТНТУ, 2026, № 2 (122)
Please use this identifier to cite or link to this item: http://elartu.tntu.edu.ua/handle/lib/54172

Full metadata record
DC FieldValueLanguage
dc.contributor.authorBoiko, Ihor
dc.date.accessioned2026-10-13T08:48:20Z-
dc.date.available2026-10-13T08:48:20Z-
dc.date.created2026-05-26
dc.date.issued2026-05-26
dc.date.submitted2026-02-25 |
dc.identifier.citationBoiko I. Modal analysis of aircraft engine blisks / Ihor Boiko // Scientific Journal of TNTU. — Tern. : TNTU, 2026. — Vol 122. — No 2. — P. 43–53.
dc.identifier.issn2522-4433
dc.identifier.urihttp://elartu.tntu.edu.ua/handle/lib/54172-
dc.description.abstractThe article deals with the actual problem of ensuring the vibrational reliability of aircraft engine blisks by conducting modal analysis, which makes it possible to determine natural vibration frequencies and modes. The localization of vibrations, increased resonance stresses and threat of disk destruction have been subjected to analysis due to heterogeneous geometric configuration of blades caused by machining errors and operational wear. The paper presents a comparative analysis of experimental natural vibration frequencies and mathematical modeling by the finite element method (FEM) using a specialized software demonstrating high convergence of results. Particular attention is paid to evaluating the effectiveness of various technological refinements for both compressor centrifugal impellers and axial stages. These modifications include trimming the leading edge and tailoring the profile thickness into several distinct shapes. The primary objective of these adjustments is to shift the natural vibration frequencies beyond the engine's resonance operational range. The study covers the analysis of the influence of centrifugal forces, which increase the dynamic stiffness of the structure, aerodynamic loads, as well as the temperature factor, which significantly reduces frequencies due to changes in the material's elasticity moduli under high-temperature operation. To evaluate resonance conditions, Campbell diagrams are used, which make it possible to graphically determine the intersection points of natural frequencies with excitation harmonics from the engine's structural elements. The practical part is based on the analysis of the dynamic characteristics of the AI-450MS, D-36, and PZL-10W engine components to confirm the possibility of avoiding resonance zones through structural modifications. Additionally, the role of harmonic analysis is considered, which, unlike modal analysis, makes it possible to take into account the system damping and determine the amplitude-frequency characteristics of the blade under influence of specific exciting forces.
dc.format.extent43-53
dc.language.isoen
dc.publisherТНТУ
dc.publisherTNTU
dc.relation.ispartofВісник Тернопільського національного технічного університету, 2 (122), 2026
dc.relation.ispartofScientific Journal of the Ternopil National Technical University, 2 (122), 2026
dc.relation.urihttps://doi.org/10.3390/coatings7070103
dc.relation.urihttps://doi.org/10.2514/1.16345
dc.relation.urihttps://doi.org/10.1016/j.jsv.2025.119607
dc.relation.urihttps://doi.org/10.1115/1.4037863
dc.relation.urihttps://doi.org/10.1007/978-3-319-67988-4_122
dc.relation.urihttps://doi.org/10.30931/jetas.452857
dc.relation.urihttps://doi.org/10.1063/5.0113223
dc.relation.urihttps://doi.org/10.20998/2078-9130.2024.2.314978
dc.relation.urihttps://doi.org/10.1109/PAEP49887.2020.9240781
dc.relation.urihttps://doi.org/10.1088/1757-899X/531/1/012080
dc.relation.urihttps://doi.org/10.33108/visnyk_tntu2023.04.032
dc.relation.urihttps://doi.org/10.21595/jve.2016.16776
dc.relation.urihttps://doi.org/10.3390/ma15238391?urlappend=%3Futm_source%3Dresearchgate.net%26utm_medium%3Darticle
dc.relation.urihttps://doi.org/10.1007/978-3-031-61415-6_34
dc.subjectnatural vibration frequency
dc.subjectblisk
dc.subjectcentrifugal impeller
dc.subjectmodal analysis
dc.subjectfinite element method
dc.subjectCampbell diagram
dc.titleModal analysis of aircraft engine blisks
dc.typeArticle
dc.rights.holder© Тернопільський національний технічний університет імені Івана Пулюя, 2026
dc.coverage.placenameТернопіль
dc.coverage.placenameTernopil
dc.format.pages11
dc.relation.referencesen1. Kumar B. V. R. R. (2013) A review on blisk technology, Int. J. Innov. Res. Sci. Eng. Technol, 2, pp. 1353–1358.
dc.relation.referencesen2. Gao F., Sun W., (2017) Reduced-order modeling for and vibration characteristics analysis of a hard-coated mistuned blisk. Coatings, 7 (12), pp. 1–18. https://doi.org/10.3390/coatings7070103.
dc.relation.referencesen3.Castanier M. P., Pierre C. (2006) Modeling and analysis of mistuned bladed disk vibration: Status and emerging directions. J. Propul. Power, 22 (2), pp. 384–396. https://doi.org/10.2514/1.16345.
dc.relation.referencesen4.Li H., Yang X., Zhang J. (2025) Vibration characteristics of integrally mistuned turbine blisks with hard-coating and bladed multi-packet shrouds. J. Sound Vib, 596, 118742. https://doi.org/10.1016/j.jsv.2025.119607.
dc.relation.referencesen5. Klauke T., Kühhorn A., Beirow B. (2007) Blade mistuning induced blisk vibration, in: Proc. 1st CEAS Eur. Air Space Conf., Berlin, pp. 317–327.
dc.relation.referencesen6. Li J., (2007). Experimental investigation of mistuned bladed disks system vibration, Ph.D. thesis, University of Michigan.
dc.relation.referencesen7. Zang C., Tan Y., Petrov E. P. (2018) Analysis of Forced Response for Bladed Disks Mistuned by Material Anisotropy Orientation Scatters. J. Eng. Gas Turbines Power, 140 (2), 022503, https://doi.org/10.1115/1.4037863.
dc.relation.referencesen8. Berger R., Häfele J., Hofmeister B., Rolfes R. (2018) Blend repair shape optimization for damaged compressor blisks, in: J. Schumacher, J. Sienz (Eds.), Advances in Structural and Multidisciplinary Optimization, Springer, Cham, 1631–1642. https://doi.org/10.1007/978-3-319-67988-4_122.
dc.relation.referencesen9. Efe-Ononeme O. E., Ikpe A. E., Ariavie G. O. (2018) Modal analysis of conventional gas turbine blade materials (Udimet 500 and IN738) for industrial applications. J. Eng. Technol. Appl. Sci, 3 (2), pp. 119–133. https://doi.org/10.30931/jetas.452857.
dc.relation.referencesen10. Umamaheswararao L., Mallikarjunarao K. (2014) Design and analysis of a gas turbine blade by using FEM. Int. J. Latest Trends Eng. Technol, 3 (4), pp. 63–69. https://doi.org/10.1063/5.0113223.
dc.relation.referencesen11. Martynenko V. H. (2024) Metody modeliuvannia dynamichnoi povedinky, vyznachennia mitsnosti ta otsinky konstruktsiinoi stiikosti kompozytsiinykh lopatok rotornykh mashyn. Visnyk NTU “KhPI”. Ser. Dyn. Mitsnist Mashyn, 2, pp. 3–15. https://doi.org/10.20998/2078-9130.2024.2.314978. (In Ukrainian).
dc.relation.referencesen12. Babenko O. M. (2021). Modeliuvannia rezonansnykh kharakterystyk znoshenykh robochykh lopatok osovoho kompresora HTD, Ph.D. thesis, National University Zaporizhzhia Politechnic, 2021. (In Ukrainian).
dc.relation.referencesen13.Martynenko G., Martynenko V., (2020). Rotor dynamics modeling for compressor and generator of the energy gas turbine unit with active magnetic bearings in operating modes, in: 2020 IEEE 25th Int. Conf. Probl. Autom. Electr. Drive Theory Pract. (PAEP), 2020, pp. 1–6. https://doi.org/10.1109/PAEP49887.2020.9240781.
dc.relation.referencesen14. Wang H. B., Zhang W., Yao M. H., Zhang M. M. (2019) Modal analysis of the coupled vibration in an aero-turbine compressor blisk considering both aerodynamic and centrifugal load. IOP Conf. Ser.: Mater. Sci. Eng, 531, pp. 1–11. https://doi.org/10.1088/1757-899X/531/1/012080.
dc.relation.referencesen15. Lavrenko I., Sydora T., Sushchenko M. (2023) Determination of dynamic characteristics of the centrifuge shaft. Sci. J. TNTU, 4, pp. 32–40. https://doi.org/10.33108/visnyk_tntu2023.04.032.
dc.relation.referencesen16.Wang D., Luo G., Wang F. (2015) Vibration characteristics analysis of a centrifugal impeller. Vibroengineering PROCEDIA 5, pp. 287–291. https://doi.org/10.21595/jve.2016.16776.
dc.relation.referencesen17. Bednarz A., Puchala K., Salacinski M., Hutsaylyuk V. (2022) Numerical investigation of the influence of aerodynamic loads on the resonant frequency of a compressor blade made of EI-961 alloy. Materials, 15 (23), pp. 1–12. https://doi.org/10.3390/ma15238391?urlappend=%3Futm_source%3Dresearchgate.net%26utm_medium%3Darticle.
dc.relation.referencesen18. Nemanezhyn Y., Lvov G., Torba Y. (2024). A research on the influence of anisotropic characteristics of single-crystal gas turbine blades on their durability, in: Advanced Manufacturing Processes VI, Lecture Notes in Mechanical Engineering, Springer, Cham, 2024, pp. 325–334. https://doi.org/10.1007/978-3-031-61415-6_34.
dc.identifier.doihttps://doi.org/10.35784/ visnyk_tntu2026.02.043
dc.contributor.affiliationZhytomyr Polytechnic State University, Zhytomyr, Ukraine
dc.citation.journalTitleВісник Тернопільського національного технічного університету
dc.citation.volume122
dc.citation.issue2
dc.citation.spage43
dc.citation.epage53
dc.identifier.citation2015Boiko I. Modal analysis of aircraft engine blisks // Scientific Journal of TNTU, Ternopil. 2026. Vol 122. No 2. P. 43–53.
dc.identifier.citationenAPABoiko, I. (2026). Modal analysis of aircraft engine blisks. Scientific Journal of the Ternopil National Technical University, 122(2), 43-53. TNTU..
dc.identifier.citationenCHICAGOBoiko I. (2026) Modal analysis of aircraft engine blisks. Scientific Journal of the Ternopil National Technical University (Tern.), vol. 122, no 2, pp. 43-53.
Appears in Collections:Вісник ТНТУ, 2026, № 2 (122)

Files in This Item:
File Description SizeFormat 
TNTUSJ_2026v122n2_Boiko_I-Modal_analysis_of_aircraft_43-53.pdf4,27 MBAdobe PDFView/Open
TNTUSJ_2026v122n2_Boiko_I-Modal_analysis_of_aircraft_43-53__COVER.png1,11 MBimage/pngView/Open
Show simple item record


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.