Fretting Fatigue Strength and Life Estimation Considering the Fretting Wear Process

Abstract:

In this paper we present the estimation methods of fretting wear process and fretting fatigue life using this wear process. Firstly the fretting-wear process was estimated using contact pressure and relative slippage. And then the stress intensity factor for cracking due to fretting fatigue was calculated by using contact pressure and frictional stress distributions, which were analyzed by the finite element method. The S-N curves of fretting fatigue were predicted by using the relationship between the calculated stress intensity factor range ( #K) with the threshold stress intensity factor range ( #Kth) and the crack propagation rate (da/dN) obtained using CT specimens of the material. Finaly fretting fatigue tests were conducted on Ni-Mo-V steel specimens. The S-N curves of our experimental results were in good agreement with the analytical results obtained by considering fretting wear process. Using these estimation methods we can explain many fretting troubles in industrial fields.

• Periodical: Key Engineering Materials (Volumes 353-358)
• Pages: 882-885
• DOI: https://doi.org/10.4028/www.scientific.net/KEM.353-358.882
• Online since: September 2007
• Authors: Toshio Hattori, Naoya Nishimura, Minoru Yamashita
• Keywords: Contact Edge, Contact Pressure, Crack Propagation, Fracture Mechanic, Fretting Fatigue, Fretting Wear, Relative Slippage

References

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[5] T. Hattori and M. Nakamura: (1994) Fretting Fatigue, ESIS Publication 18, pp.453-460.

[6] T. Hattori, M. Nakamura and T. Watanabe: Tribology International, Vol. 36 (2003), pp.87-97.

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[3] 5 0 0. 5 1 1. 5 2 Crack length a (mm) Stress intensitty factor K (MPa √√√√m) Treshold stress intensity factor range Stress intensity factor range.

DOI: 10.1046/j.1460-2695.2002.00514.x

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[3] 5 0. 0 0. 5 1. 0 1. 5 2. 0 Crack length a (mm) Stress intensity factor range K (MPa √√√√ m) Threshold stress intensity factor range Stress intensity factor range 10６６６６ 10１０１０１０１０ 10９９９９ 10８８８８ 105 10７７７７ Experiment Calculated 0 100 150 200 Stress amplitude σσσσa MPa Number of cycle to failure Nf.

DOI: 10.1016/j.tafmec.2019.102377