Skip to main content
Log in

Vibration-Based Bending Fatigue of a Hybrid Insert-Plate System

  • Published:
Experimental Mechanics Aims and scope Submit manuscript

Abstract

A hybrid bending specimen system was developed to reduce material waste when using the vibration-based fatigue method to gather high cycle fatigue (HCF) data. In the vibration-based fatigue method, a base-excited plate specimen is driven into a high frequency resonant mode until failure. Compared to the axial testing methods, vibration-based failure better represents the conditions and surface-initiated cracks experienced by structural components subject to high frequency vibrations, like blades and vanes in gas turbine engines. In addition, the method produces data over 40 times faster than conventional axial testing methods. Only a small portion of the vibration-based bending specimen is needed to determine crack initiation failure. In order to reduce material waste, a hybrid bending system was designed to test a small specimen held in a reusable carrier plate, thereby reducing material costs to gather HCF data. The final optimized design, the Bruns-Zearley plate specimen, produced fatigue data using 95 % less material. The results are comparable tofatigue data acquired from standard vibration-based plate specimen methods within a 95 % confidence interval.

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.

Fig. 1
Fig. 2
Fig. 3
Fig. 4
Fig. 5
Fig. 6
Fig. 7
Fig. 8
Fig. 9
Fig. 10
Fig. 11
Fig. 12
Fig. 13
Fig. 14
Fig. 15
Fig. 16
Fig. 17
Fig. 18
Fig. 19
Fig. 20

Similar content being viewed by others

References

  1. Engine Structural Integrity Program (ENSIP) MIL-HDBK-1783B (USAF), 15 Feb 2002

  2. Nicholas T (2006) High Cycle Fatigue - A Mechanics of Materials Perspective, Oxford, UK, Elsevier

  3. Goodman J (1899) Mechanics Applied to Engineering, Longmans, Green, and Co., London

  4. Wohler A (1867) Wohlers experiments on the strength of metals. Eng Paris Exposition 4:160–161

    Google Scholar 

  5. Scott-Emuakpor O, Shen MHH, George T, Cross C (2008) An energy-based uniaxial fatigue life prediction method for commonly used gas turbine engine materials. J Eng Gas Turbines Power 130(6). paper No. 062504

  6. American Society for Testing and Materials E466-07: Standard Practice for Conducting Force Controlled Constant Amplitude Axial Fatigue Tests of Metallic Materials. ASTM Book of Standards, 2009, Vol. 03.01, ASTM International, West Conshohocken, PA

  7. George T, Seidt J, Shen M HH, Cross C, Nicholas T (2004) Development of a novel vibration-based fatigue testing methodology. Int J Fatigue 26:477–486

    Article  Google Scholar 

  8. George T, Shen MHH, Scott-Emuakpor O, Nicholas T, Cross C, Calcaterra J (2005) Goodman Diagram via Vibration-Based Fatigue Testing. J Eng Mater Technol 127(1):58–64

    Article  Google Scholar 

  9. Leissa A (1993) Vibration of Plates. Acoustical Society of America through the American Institute of Physics

  10. Beer FP, Johnston ER (1992) Mechanics of Materials: Second Edition. McGraw-Hill, Inc

  11. Scott-Emuakpor O, Schwartz J, Holycross C, George T, Cross C, Shen MHH (2013) In-situ Study on Coaxing during Vibration-Based Bending Fatigue of Inconel 625 and 718. ASME/IGTI Turbo Expo, paper No. GT2013-94233

  12. Scott-Emuakpor O, George T, Cross C (2010) Multi-Axial Fatigue-Life Prediction via a Strain-Energy Method. AIAA J 48(1):63–72

    Article  Google Scholar 

  13. Nicholas T, Maxwell D (2003) Mean Stress Effects on the High Cycle Fatigue Limit Stress in Ti-6Al-4V. Fatigue and Fracture Mechanics: 33rd Volume, ASTM STP 1417, W.G. Reuter and R.S. Piascik, Eds., American Society for Testing and Materials, West Conshohocken, PA pp. 476-492

  14. Bellows R, Muju S, Nicholas T (1999) Validation of the Step Test Method for Generating Haigh Diagrams for Ti-6Al-4V. Int J Fatigue 21(7):687–697

    Article  Google Scholar 

  15. Scott-Emuakpor O, George T, Cross C, Wertz J, Shen MHH (2012) A New Distortion Energy-Based Equivalent Stress for Multiaxial Fatigue Life Prediction. International Journal of Non-Linear Mechanics 47(3):29–37

    Article  Google Scholar 

  16. Kutner M, Nachtsheim C, Neter J (2004) Applied Linear Regression Models. McGraw-Hill Irwin

  17. American Society for Testing and Materials E739 - 10: Standard Practice for Statistical Analysis of Linear or Linearized Stress-Life (S-N) and Strain-Life (𝜖-N) Fatigue Data, ASTM Book of Standards, 2010; Vol. 03.01, ASTM International, West Conshohocken, PA

  18. Metallic Materials and Elements for Aerospace Vehicle Structures, MIL-HDBK-5J (USAF). (2003)

  19. Nashif A, Jones D, Henderson J (1985) Vibration Damping. Wiley-Interscience Publication

  20. Introduction to Aluminum and Aluminum Alloys, Metals Handbook Desk Edition (1998) ASM International, pp 417–423

Download references

Acknowledgments

The authors would like to thank the Air Force Research Laboratories (AFRL), specifically the Turbine Engine Fatigue Facility (TEFF) for their financial support, facility and equipment access, and encouragement of this research.

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Onome Scott-Emuakpor.

Additional information

Jeffery Bruns, Alyssa Zearley contributed equally to the work

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Bruns, J., Zearley, A., George, T. et al. Vibration-Based Bending Fatigue of a Hybrid Insert-Plate System. Exp Mech 55, 1067–1080 (2015). https://doi.org/10.1007/s11340-015-0004-6

Download citation

  • Received:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s11340-015-0004-6

Keywords

Navigation