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Influence of the Amplitude of Resonance Vibrations on Fatigue Life of a Compressor Blade with Simulated FOD Damage

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EN
Abstrakty
EN
This work presents the results of the numerical analyses pertaining to the influence of resonance vibration amplitude on the fatigue life of a compressor blade with a defect made by a collision with a hard object (FOD). The research object was the first stage compressor blade of the PZL-10W engine. The numerical simulation of the notch formation was performed for the tested blade. The material fatigue models (for e-N analysis), three cyclic hardening models, and two mean stress correction models were used in the numerical analyses. As a result of the numerical analysis, the information on the distribution of principal stress was obtained. The values of the principal stresses were used for numerical e-N fatigue analysis using the aforementioned models of fatigue, hardening, and mean stress correction. Obtained results were compared to previously published experimental research, where a notch was created at the leading edge in 8 blades. The blades damaged under laboratory conditions were subjected to experimental fatigue tests during which the effect of resonance amplitude on the number of damage cycles was determined. As a result of the comparison work carried out, the impact of the vibration amplitude on the durability of the element with plastic deformation was determined.
Twórcy
  • Rzeszow University of Technology, Al. Powstancow Warszawy 8, 35-959 Rzeszow
Bibliografia
  • 1. Bednarz A. Evaluation of Material Data to the Numerical Strain-Life Analysis of the Compressor Blade Subjected to Resonance Vibrations. Advances in Science and Technology Research Journal, 14(1), 2020.
  • 2. Bednarz A., Bąk Ł. and Boltynjuk E., Wpływ naprężeń wstępnych w okolicy wierzchołka karbu na trwałość zmęczeniową łopatki sprężarki. TTS 12, 2016, 52–55
  • 3. Browell R. and Hancq A. Calculating and Displaying Fatigue Results. ANSYS Inc., 2006.
  • 4. Byczkowska P., Sawicki J., Januszewicz B. and Stegliński M. Analysis of the Impact of Double Shot Peening on the Value of Roughness Parameter and Distribution of Stresses in the RSA 501 Alloy (Al Mg5 Mn1 Sc0.8 Zr0.4). Advances in Science and Technology Research Journal, 11(3), 2017, 1–9
  • 5. Chengzong L., Zhiyong Z., Xin C. and Yuanxiao S. Low-Cycle Fatigue Analysis and Experiment of Steel Specimens with Stress Concentration. Journal of Applicatied Mechanics, 17(3), 2000, 107–110.
  • 6. Dowling N.E. Mean Stress Effects in Stress-Life and Strain-Life Fatigue. Blackburg: Virginia Polytechnic Institute and State University, F2004/51, 2004.
  • 7. Kubit A., Trzepiecinski T., Święch Ł., Faes K. and Slota, J. Experimental and Numerical Investigations of Thin-Walled Stringer-Stiffened Panels Welded with RFSSW Technology under Uniaxial Compression. Materials, 12, 2019, 1785.
  • 8. Hunecke K. Jet Engine: Fundamentals of theory, design and operation. Airlife Publishing, England, 2014.
  • 9. Meggiolaro M.A. and Castro J.T.P. Statistical evaluation of strain-life fatigue crack initiation predictions. International Journal of Fatigue, 26, 2004, 463–476.
  • 10. Mihaliková M., Lišková A., Vojtko M. and Kvačkaj T. Research of fatigue and mechanical properties AlMg1SiCu aluminum alloys. Advances in Science and Technology Research Journal, 9(28), 2015, 56–60.
  • 11. Nakhodchi S. and Salimpour M.E. Fatigue life prediction in damaged and un-damaged compressor blades. Engineering Solid Mechanics, 2, 2013, 43–50.
  • 12. Neimitz A., Galkiewicz J., Lipiec S. and Dzioba I. Estimation of the Onset of Crack Growth in Ductile Materials. Materials 10, 2018.
  • 13. Stephens R.I., Fatemi A., Stephens R.R. and Fuchs H.O. Metal Fatigue in Engineering. John Wiley& Sons, Ottawa, Canada, 2000.
  • 14. Święch Ł. Experimental and Numerical Studies of Low-Profile, Triangular Grid-Stiffened Plates Subjected to Shear Load in the Post-Critical States of Deformation. Materials, 12, 2019, 3699
  • 15. Witek L., Bednarz A. and Stachowicz F. Fatigue analysis of compressor blade with preliminary defect. Engineering Failure Analysis 58, 2015, 229–237.
Uwagi
Opracowanie rekordu ze środków MNiSW, umowa Nr 461252 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2020).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-6f103e64-2d1a-4c8d-b899-b13ef03d4d90
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