PSI - Issue 19
Okan Yılmaz et al. / Procedia Structural Integrity 19 (2019) 302 – 311 Yılmaz et al. / Structural Integrity Procedia 00 (2019) 000–000
309
8
S500MC – Δσ nom =225 MPa
S700MC - Δσ nom =300 MPa
Plasma Drilled Waterjet Laser
Plasma Drilled Waterjet Laser
806%
119%
142%
92%
158%
Punched (Flat) Punched (90°) Punched (0°)
14%
Punched (Flat) Punched (90°) Punched (0°)
31%
0% 2%
16%
(a)
(b)
0%
0%
500%
1000%
0%
500%
1000%
S960MC - Δσ nom =300 MPa
Plasma Drilled Waterjet Laser
567%
249%
161%
Punched (Flat) Punched (90°) Punched (0°)
69%
0% 0%
(c)
0%
500%
1000%
Fig. 6. Fatigue life improvement for samples produced by various hole-making procedures (a) S500MC, 6 mm-thick samples, ∆ σ nom = 225 MPa; (b) S700MC, 5 mm-thick samples, ∆ σ nom = 300 MPa; (c) S960MC, 5 mm-thick samples, ∆ σ nom = 300 MPa. Arrows denote the run-out condition, which corresponds to 5e6 cycles.
fretting fatigue – net section mode. For S960MC samples, the detrimental e ff ect of the increased preload was more notable. On average, all samples with the highest bolt pre-tension endured less fatigue cycles than S960MC samples with the lowest pre-tension. For the detailed analysis, the reader is referred to [13]. The out-of-plane bending loading results obtained for the same pre-tension levels are plotted in Fig. 7. Under this loading mode, we did not observe any consistent e ff ect with respect to the applied bending force or the material as all fatigue life values fall under [ N f / 2 , 2 N f ] scatter band for the mid pre-tension level. Table 2 summarizes the fatigue tests for di ff erent flange configurations. Test side is denoted as the face where tensile stresses occur while pre-tension is applied from the opposite side. We observed lower fatigue lives when the pre-tension is applied over the bolt rather than the nut. Alternative bolt head orientation did not have an e ff ect on fatigue life, however it must be noted that it is di ffi cult to ensure a perfect alignment of both flanges when applying pre-tension from one side. Having a shot-peened layer covered by a cataphoretic primer coating improved the fatigue life is both conditions, 20% in average.
Table 2. Four-point bending fatigue test results for the flanged bolt, alternative bolt head orientation, and shot-peened layer with coating. The material is 5-mm-thick S700MC grade steel and applied maximum bending force is F fpb , max = 10 kN. Fatigue life values (cycles)
M16 grade 10.9 (130%)
Alt. bolt head orientation
Shot-peened
Test side: bolt, torqued over the nut Test side: nut, torqued over the bolt
50621 35156
52128 35825
60055 46096
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