Review Article
A Study on Surface Modification of Al7075-T6 Alloy against Fretting Fatigue Phenomenon
Table 1
The reduction coefficient of fretting fatigue life for some engineering alloys [
26].
| Fatigue specimen | Contact pad | Contact pressure (MPa) | Fatigue mean stress (MPa) | Fatigue strength unfretted (MPa) | Fatigue strength fretted (MPa) | Strength reduction factor | Relative slip range (m) |
| Steels | 3.5NiCrMoV | 1CrMo | 30 | 0 | ±300 | ±140 | 2.1 | 15 | 3.5NiCrMoV | 1CrMo | 30 | 300 | ±215 | ±60 | 3.6 | 6.2 | 3.5NiCrMoV | 1CrMo | 300 | 0 | ±300 | ±130 | 2.3 | 12 | 3.5NiCrMoV | 1CrMo | 300 | 300 | ±215 | ±60 | 3.6 | 4 | 3.5NiCrMoV | 2014 A | 30 | 0 | ±300 | ±140 | 2.1 | 1.5 | 3.5NiCrMoV | 2014 A | 30 | 300 | ±215 | ±75 | 2.9 | 6.8 | 18M114Cr | 3.5NiCrMoV | 20.7 | 0 | ±250 | ±100 | 2.5 | 10 | 18M114Cr | 3.5NiCrMoV | 20.7 | 300 | ±125 | ±50 | 2.5 | 4.5 | 18M114Cr | 3.5NiCrMoV | 20.7 | 0 | ±250 | ±165 | 1.5 | 17.4 | 18M114Cr | 3.5NiCIMoV | 20.7 | 300 | ±185 | ±70 | 2.6 | 6.7 |
| Aluminum | 2014A Al | 3.5NiCrMoV | 30.8 | 75 | ±140 | ±15 | 9.3 | 2 | 2014A Al | 3.5NiCrMoV | 30.8 | 125 | ±135 | ±12.5 | 10.8 | 1.5 | 2014A Al | 3.5NiCrMoV | 30.8 | 125 | ±135 | ±50 | 2.7 | 9.6 | Peened | | | | | | | |
| Aluminum | 2014A | BS S98 | 103.5 | 0 | ±148 | ±72 | 2.05 | 2 | 2014A | BS S98 | 103.5 | 0 | ±148 | ±47 | 3.14 | 4.2 | 2014A | BS S98 | 103.5 | 0 | ±148 | ±36 | 4.11 | 8.35 | 2014A | BS S98 | 103.5 | 0 | ±148 | ±36 | 4.11 | 17.4 |
| Titanium | Ti6Al4V | Ti6Al4V | 20 | 61.25 | ±260 | ±125 | 2.1 | 30 |
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