Question 7.5: Safety Factor against Fatigue Failure of a Tensile Link A te...

Safety Factor against Fatigue Failure of a Tensile Link

A tensile link of thickness t with two fillets is subjected to a load fluctuating between P_{\min} and P_{\max} (Figure 7.15). Calculate the factor of safety n for unlimited life based on the Goodman criterion.

Given: D = 120 mm, d = 80 mm, r = 16 mm,

t = 15 mm, P_{\min} = 90 kN, P_{\max} = 210 kN.

Design Decisions: The link is made of steel with S_{u} = 700 MPa. The fillets and adjacent surfaces are ground. A reliability of 99.9% is desired.

F7.15
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The minimum cross-sectional area equals A = 80 × 15 = 1200 mm². The maximum mean and range stresses are

\begin{array}{c} \sigma_m=\frac{(210+90)\left(10^3\right)}{2\left(1200 \times 10^{-6}\right)}=125  MPa \\ \sigma_a=\frac{(210-90)\left(10^3\right)}{2\left(1200 \times 10^{-6}\right)}=50  MPa \end{array}

Referring to Figure C.1, for D/d = 1.5 and r/d = 0.2, we obtain K_{t} = 1.72. Inasmuch as the given 16 mm fillet radius is large, we use the value of the notch sensitivity for the steel having S_{u} = 700 MPa, corresponding to r = 4 mm in Figure 7.9a; that is, q = 0.85. Hence, K_f=1+0.85(1.72-1)=1.61 .

For axial loading, there is no size factor, C_{s} = 1.0. Corresponding to a round surface finish, from Equation 7.7 and Table 7.2,

C_f=A S_u^b       (7.7)

\begin{aligned} C_f &=A\left(S_u\right)^b \\ &=1.58(700)^{-0.085}=0.91 \end{aligned}

By Table 7.3, for 99.9% material reliability, C_{r} = 0.75. The temperature is not elevated, C_{t} = 1.0. The modified endurance limit, using Equations 7.3 and 7.6, is

\begin{aligned} S_e &=C_f C_r C_s C_t\left(1 / K_f\right)\left(0.45 S_u\right) \\ &=(0.91)(0.75)(1.0)(1.0)(1 / 1.61)(0.45 \times 700) \\ &=133.5  MPa \end{aligned}

The factor of safety, applying Equation 7.22, is therefore

n=\frac{S_u}{\sigma_m+\frac{S_u}{S_e} \sigma_a}            (7.22)

n=\frac{700}{125+\frac{700}{133.5}(50)}=1.81

Comments: If the load is well controlled and there is no impact, this factor guards the link against the fatigue failure.

Table 7.2
Surface Finish Factors C_{f}
A
Surface Finish MPa ksi b
Ground 1.58 1.34 −0.085
Machined or cold drawn 4.51 2.7 −0.265
Hot rolled 57.7 14.4 −0.718
Forged 272.0 39.9 −0.995
Table 7.3
Reliability Factors
Survival Rate (%) C_{r}
50 1.00
90 0.89
95 0.87
98 0.84
99 0.81
99.9 0.75
99.99 0.70
C.1
F7.9

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