Skip to main content
Log in

Synchronous impact phenomenon of a high-dimension complex nonlinear dual-rotor system subjected to multi-frequency excitations

  • Article
  • Published:
Science China Technological Sciences Aims and scope Submit manuscript

Abstract

The “synchronous impact” is a phenomenon that increases the dynamic load of the inter-shaft bearing, when the frequency of the aerodynamic excitation is close to the contact frequency of the inter-shaft bearing. This work addresses the “synchronous impact” phenomenon of an aero-engine. The 104 degree-of-freedom dynamical model of an aero-engine is established by the finite element method, in which the complex nonlinearity of the Hertzian contact force of the inter-shaft bearing with clearance is included, and the multi-frequency excitations such as the unbalanced excitations of the high- and low-pressure rotors and the aerodynamic excitation are considered. A harmonic balance method combined with the alternating frequency time-domain method (HB-AFT) is introduced to obtain periodic responses of the high-dimension complex nonlinear dual-rotor system. The results show that there emerges a peak value of the amplitude-frequency response for the contact frequency harmonic component of the outer ring of the inter-shaft bearing, when the aerodynamic excitation frequency is close to the contact frequency. In addition, the dynamic load of the inter-shaft bearing increases significantly. Moreover, the parametric analysis shows that the “synchronous impact” phenomenon is sensitive to the change of the speed ratio of the high- and low-pressure rotors. The dynamic load of inter-shaft bearing can be significantly reduced by changing the speed ratio by 1%. The results obtained in this paper not only provide more insight into the mechanism of the “synchronous impact” phenomenon but also demonstrate the HB-AFT method as a potential semi-analytical tool to explore the high-dimension complex nonlinear system.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

References

  1. Chen Y, Zhang H. Review and prospect on the research of dynamics of complete aero-engine systems (in Chinese). Acta Aeronaut et Astronaut Sin, 2011, 32: 1371–1391

    Google Scholar 

  2. Kim Y B, Noah S T. Bifurcation analysis for a modified Jeffcott rotor with bearing clearances. Nonlinear Dyn, 1990, 1: 221–241

    Article  Google Scholar 

  3. Tiwari M, Gupta K, Prakash O. Dynamic response of an unbalanced rotor supported on ball bearings. J Sound Vib, 2000, 238: 757–779

    Article  Google Scholar 

  4. Harsha S P. Nonlinear dynamic analysis of an unbalanced rotor supported by roller bearing. Chaos Solitons Fractals, 2005, 26: 47–66

    Article  MATH  Google Scholar 

  5. Harsha S P. Nonlinear dynamic analysis of a high-speed rotor supported by rolling element bearings. J Sound Vib, 2006, 290: 65–100

    Article  Google Scholar 

  6. Hou L, Chen Y, Cao Q, et al. Turning maneuver caused response in an aircraft rotor-ball bearing system. Nonlinear Dyn, 2014, 79: 229–240

    Article  Google Scholar 

  7. Hou L, Chen Y, Cao Q. Nonlinear vibration phenomenon of an aircraft rub-impact rotor system due to hovering flight. Commun Nonlinear Sci Numer Simul, 2014, 19: 286–297

    Article  MathSciNet  MATH  Google Scholar 

  8. Shi M, Wang D, Zhang J. Nonlinear dynamic analysis of a vertical rotor-bearing system. J Mech Sci Technol, 2013, 27: 9–19

    Article  Google Scholar 

  9. Huang D, Liu Y, Liu H, et al. Resonances of elastic rotor induced by roller bearing with consideration of cage vibration. Proc Inst Mech Eng Part K, 2018, 232: 446–456

    Google Scholar 

  10. Wang N, Jiang D. Vibration response characteristics of a dual-rotor with unbalance-misalignment coupling faults: Theoretical analysis and experimental study. Mech Machine Theor, 2018, 125: 207–219

    Article  Google Scholar 

  11. Wang N, Liu C, Jiang D, et al. Casing vibration response prediction of dual-rotor-blade-casing system with blade-casing rubbing. Mech Syst Signal Process, 2019, 118: 61–77

    Article  Google Scholar 

  12. Yang Y, Ouyang H, Yang Y, et al. Vibration analysis of a dual-rotor-bearing-double casing system with pedestal looseness and multi-stage turbine blade-casing rub. Mech Syst Signal Process, 2020, 143: 106845

    Article  Google Scholar 

  13. Liao M, Ma Z, Liu Y, et al. Fault characteristics and diagnosis method of intershaft bearing in aero-engine (in Chinese). J Aerosp Power, 2013, 28: 2752–2758

    Google Scholar 

  14. Cao H, Niu L, Xi S, et al. Mechanical model development of rolling bearing-rotor systems: A review. Mech Syst Signal Process, 2018, 102: 37–58

    Article  Google Scholar 

  15. Tandon N, Choudhury A. An analytical model for the prediction of the vibration response of rolling element bearings due to a localized defect. J Sound Vib, 1997, 205: 275–292

    Article  Google Scholar 

  16. Rafsanjani A, Abbasion S, Farshidianfar A, et al. Nonlinear dynamic modeling of surface defects in rolling element bearing systems. J Sound Vib, 2009, 319: 1150–1174

    Article  Google Scholar 

  17. Gnagy J, Houpert L, Chevalier F. Rolling bearing stress based life—Part II: Experimental calibration and validation. J Tribol, 2012, 134: 021104

    Article  Google Scholar 

  18. Oswald F B, Zaretsky E V, Poplawski J V. Effect of internal clearance on load distribution and life of radially loaded ball and roller bearings. Tribol Trans, 2012, 55: 245–265

    Article  Google Scholar 

  19. Flouros M, Hirschmann M, Cottier F, et al. Active outer ring cooling of high-loaded and high-speed ball bearings. J Eng Gas Turbines Power, 2013, 135: 081902

    Article  Google Scholar 

  20. Gao P, Hou L, Yang R, et al. Local defect modelling and nonlinear dynamic analysis for the inter-shaft bearing in a dual-rotor system. Appl Math Model, 2019, 68: 29–47

    Article  MathSciNet  MATH  Google Scholar 

  21. Ma H, Li H, Zhao X, et al. Effects of eccentric phase difference between two discs on oil-film instability in a rotor-bearing system. Mech Syst Signal Process, 2013, 41: 526–545

    Article  Google Scholar 

  22. Chandra N H, Sekhar A S. Fault detection in rotor bearing systems using time frequency techniques. Mech Syst Signal Process, 2016, 72–73: 105–133

    Article  Google Scholar 

  23. Liu J. A dynamic modelling method of a rotor-roller bearing-housing system with a localized fault including the additional excitation zone. J Sound Vib, 2020, 469: 115144

    Article  Google Scholar 

  24. Liu J, Shao Y. Dynamic modeling for rigid rotor bearing systems with a localized defect considering additional deformations at the sharp edges. J Sound Vib, 2017, 398: 84–102

    Article  Google Scholar 

  25. Yang R, Jin Y, Hou L, et al. Advantages of pulse force model over geometrical boundary model in a rigid rotor-ball bearing system. Int J Non-Linear Mech, 2018, 102: 159–169

    Article  Google Scholar 

  26. Wang Y, Liao M F, Zhang J. Dynamic load reduction design for inter-shaft bearing of aircraft engine (in Chinese). J Aerosp Power, 2017, 32: 492–499

    Google Scholar 

  27. Yang R, Jin Y L, Hou L, et al. Super-harmonic resonance characteristic of a rigid-rotor ball bearing system caused by a single local defect in outer raceway. Sci China Tech Sci, 2018, 61: 1184–1196

    Article  Google Scholar 

  28. Yang R, Jin Y, Hou L, et al. Study for ball bearing outer race characteristic defect frequency based on nonlinear dynamics analysis. Nonlinear Dyn, 2017, 90: 781–796

    Article  Google Scholar 

  29. Naeem M. Impacts of low-pressure (LP) compressors’ fouling of a turbofan upon operational-effectiveness of a military aircraft. Appl Energy, 2008, 85: 243–270

    Article  Google Scholar 

  30. Chen G. Vibration modelling and verifications for whole aero-engine. J Sound Vib, 2015, 349: 163–176

    Article  Google Scholar 

  31. Lin R Z, Hou L, Sun C Z, et al. Nonlinear vibration analysis of the overall aeroengine system (in Chinese). J Vib Eng, 2022, 35: 557–568

    Google Scholar 

  32. Ju R, Fan W, Zhu W D. Comparison between the incremental harmonic balance method and alternating frequency/time-domain method. J Vib Acoustics, 2021, 143: 004500

    Article  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Lei Hou.

Additional information

This work was supported by the National Natural Science Foundation of China (Grant No. 11972129), the National Major Science and Technology Projects of China (Grant No. 2017-IV-0008-0045), Department of Science & Technology of Liaoning Province (Grant No. 2019BS182), and the Educational Department of Liaoning Province (Grant No. LJGD2019009).

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Lin, R., Hou, L., Dun, S. et al. Synchronous impact phenomenon of a high-dimension complex nonlinear dual-rotor system subjected to multi-frequency excitations. Sci. China Technol. Sci. 66, 1757–1768 (2023). https://doi.org/10.1007/s11431-022-2215-0

Download citation

  • Received:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s11431-022-2215-0

Navigation