Factor of Safety for a Stepped Shaft under Torsional Shock Loading
A stepped shaft of diameters D and d with a shoulder fillet radius r has been machined from AISI 1095 annealed steel and fixed at end A (Figure 9.6). Determine the factor of safety n, using the maximum shear stress theory incorporated with the Goodman fatigue relation.
Given: The free end C of the shaft is made to rotate back and forth between 1.0° and 1.5° under torsional minor shock loading. The shaft is at room temperature.
Data:
L=300 mm , \quad d=30 mm , \quad D=60 mm , \quad r=2 mm ,
K_{s t}=1.5 \quad(\text { by Table 9.1), } \quad G=79 GPa (from Table B.1)
S_u=658 MPa \text { and } H_B=192 \text { (by Table B.4) }
Design Assumption: A reliability of 95% is used.
TABLE 9.1 Shock Factors in Bending and Torsion |
|
Nature of Loading | K_{s b}, K_{s t} |
Gradually applied or steady | 1.0 |
Minor shocks | 1.5 |
Heavy shocks | 2.0 |
TABLE B.4 Mechanical Properties of Selected Heat-Treated Steels |
|||||||
AISI Number | Treatment | Temperature (°C) | Ultimate Strength S_u (MPa) | Yield Strength S_y (MPa) | Elongation in 50 mm (%) | Reduction in Area (%) | Brinell Hardness (HB) |
1030 | WQ&T | 205 | 848 | 648 | 17 | 47 | 495 |
WQ&T | 425 | 731 | 579 | 23 | 60 | 302 | |
WQ&T | 650 | 586 | 441 | 32 | 70 | 207 | |
Normalized | 925 | 521 | 345 | 32 | 61 | 149 | |
Annealed | 870 | 430 | 317 | 35 | 64 | 137 | |
1040 | OQ&T | 205 | 779 | 593 | 19 | 48 | 262 |
OQ&T | 425 | 758 | 552 | 21 | 54 | 241 | |
OQ&T | 650 | 634 | 434 | 29 | 65 | 192 | |
Normalized | 900 | 590 | 374 | 28 | 55 | 170 | |
Annealed | 790 | 519 | 353 | 30 | 57 | 149 | |
1050 | WQ&T | 205 | 1120 | 807 | 9 | 27 | 514 |
WQ&T | 425 | 1090 | 793 | 13 | 36 | 444 | |
WQ&T | 650 | 717 | 538 | 28 | 65 | 235 | |
Normalized | 900 | 748 | 427 | 20 | 39 | 217 | |
Annealed | 790 | 636 | 365 | 24 | 40 | 187 | |
1060 | OQ&T | 425 | 1080 | 765 | 14 | 41 | 311 |
OQ&T | 540 | 965 | 669 | 17 | 45 | 277 | |
OQ&T | 650 | 800 | 524 | 23 | 54 | 229 | |
Normalized | 900 | 776 | 421 | 18 | 37 | 229 | |
Annealed | 790 | 626 | 372 | 11 | 38 | 179 | |
1095 | OQ&T | 315 | 1260 | 813 | 10 | 30 | 375 |
OQ&T | 425 | 1210 | 772 | 12 | 32 | 363 | |
OQ&T | 650 | 896 | 552 | 21 | 47 | 269 | |
Normalized | 900 | 1010 | 500 | 9 | 13 | 293 | |
Annealed | 790 | 658 | 380 | 13 | 21 | 192 | |
4130 | WQ&T | 205 | 1630 | 1460 | 10 | 41 | 467 |
WQ&T | 425 | 1280 | 1190 | 13 | 49 | 380 | |
WQ&T | 650 | 814 | 703 | 22 | 64 | 245 | |
Normalized | 870 | 670 | 436 | 25 | 59 | 197 | |
Annealed | 865 | 560 | 361 | 28 | 56 | 156 | |
4140 | OQ&T | 205 | 1770 | 1640 | 8 | 38 | 510 |
OQ&T | 425 | 1250 | 1140 | 13 | 49 | 370 | |
OQ&T | 650 | 758 | 655 | 22 | 63 | 230 | |
Normalized | 870 | 870 | 1020 | 18 | 47 | 302 | |
Annealed | 815 | 655 | 417 | 26 | 57 | 197 | |
Source: ASM Metals Reference Book, 3rd ed. Materials Park, OH, American Society for Metals, 1993. | |||||||
Notes: To convert from MPa to ksi, divide given values by 6.895. Values tabulated for 25 mm round sections and of gage length 50 mm. The properties for quenched and tempered steel are from a single heat: OQ&T, oil-quenched and tempered; WQ&T, water-quenched and tempered. |
From the geometry of the shaft, D=2d and L_{AB} =L_{BC} =L . The polar moment of inertia of the shaft segments are
J_{B C}=\frac{\pi d^4}{32} \quad J_{A B}=\frac{\pi D^4}{32}=16 J_{B C}
in which
J_{B C}=\frac{\pi}{32}(0.030)^4=79.52\left(10^{-9}\right) m ^4
The total angle of twist is
\phi=\frac{T L}{G}\left(\frac{1}{16 J_{B C}}+\frac{1}{J_{B C}}\right)
or
T=\frac{16 G J_{B C} \phi}{17 L}
Substituting the numerical data, this becomes T=19,708.5 \phi . Accordingly, for \phi_{\max }=0.0262 rad and \phi_{\min }=0.0175 rad , it follows that T_{\max }=516.4 N \cdot m \text { and } T_{\min }=344.9 N \cdot m . Hence,
T_m=430.7 N \cdot m \quad T_a=85.8 N \cdot m
The modified endurance limit, using Equation (7.6), is
S_e=C_f C_r C_s C_t\left(1 / K_f\right) S_e^{\prime} (7.6)
S_e=C_f C_r C_s C_t\left(\frac{1}{K_f}\right) S_e^{\prime}
where
C _f=A_u^b=4.51\left(658^{-0265}\right)=0.808 (by Equation (7.7) and Table 7.2)
C_f=A S_u^b (7.7)
C_r=0.87 (from Table 7.3)
C_{ s }=0.85 (by Equation (7.9))
C_s= \begin{cases}0.85 & (13 mm <D \leq 50 mm ) \quad\left(\frac{1}{2}<D \leq 2 \text { in. }\right) \\ 0.70 & (D>50 mm ) \quad(D>2 in .)\end{cases} (7.9)
C_t=1 (for normal temperature)
S_e^{\prime}=0.29 S_u=190.8 MPa (applying Equation (7.4))
\text { Iron} \left(S_{e s}^{\prime}\right)=0.32 S_u (7.4)
and
K_t=1.6 (from Figure C.8, for D/d =2 and r/d =0.067)
q = 0.92 (from Figure 7.9, for r =2 mm and H_B =192 annealed steel)
K_f=1+0.92(1.6-1)=1.55 (using Equation (7.13b))
K_f=1+q\left(K_t-1\right) (7.13b)
Therefore,
S_e=(0.808)(8.87)(0.85)(1)(1 / 1.55)(190.8)=73.55 MPa
We now use Equation (9.13) with M_m =M_a =0 to estimate the factor of safety:
\frac{S_u}{n}=\frac{32}{\pi D^3}\left[K_{s b}\left(M_m+\frac{S_u}{S_e} M_a\right)^2+K_{s t}\left(T_m+\frac{S_u}{S_e} T_a\right)^2\right]^{1 / 2} (9.13)
\frac{S_u}{n}=\frac{32}{\pi d_{B C}^3}\left[K_{s t}\left(T_m+\frac{S_u}{S_e} T_a\right)^2\right]^{1 / 2} (9.17)
Introducing the numerical values,
\frac{658\left(10^6\right)}{n}=\frac{32}{\pi(0.03)^3}\left[1.5\left(430.2+\frac{658}{73.55} 86.2\right)^2\right]^{1 / 2}
This results in n=1.19.
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 | 27 | -0.265 |
Hot rolled | 57.7 | 144 | -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 |