Question 14.2: Creating the Modified-Goodman Diagram for a Helical Spring P...

Creating the Modified-Goodman Diagram for a Helical Spring

Problem     Construct the Goodman line for the spring wire of Example 14-1.

Given    The required cycle life is N = 1E6 cycles. Wire is 0.042-in (1.1-mm) dia.

Assumptions    The torsional strengths and torsional shear stresses will be used on the Goodman diagram.

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See Figure 14-16.

1    The material’s ultimate tensile strength from Figure 14-3 or equation 14.3 (p. 792), converted to ultimate torsional strength with equation 14.4 (p. 793) using data from Table 14-4 (p. 792) allows one point on the Goodman line to be determined.

S_{u t} \cong A d^b     (14.3)

S_{u s} \cong 0.67 S_{u t}       (14.4)

S_{u t} \cong 184649(0.042)^{-0.1625}=309071  psi       (a)

\begin{aligned} S_{u s} & \cong 0.67 S_{u t} \\ &=0.67(309071)=207078  psi \end{aligned}         (b)

This value is plotted as point A on the diagram in Figure 14-16.

2    The S-N diagrams each provide one data point (S_{fw} or S_{ew}, depending on whether for finite or infinite life) on the modified-Goodman line for a material/size combination in pure torsional loading. The fatigue strength S_{fw} for that wire material and condition is taken from the S-N line of Figure 14-15 or calculated from the data in Table 14-9 (p. 813) as

@  N = 1E6  :  S_{f w} \cong 0.33(309071)=101993 psi      (c)

The x and y intercepts are 0.5S_{fw} = 50 996 psi. This is plotted as point B on the diagram in Figure 14-16. Note that for infinite life the value of S_{ew} from equation 14.13 would be plotted at B instead of this value of S_{fw} for a finite life.

\begin{array}{l} S_{e w^{\prime}} \cong 45.0  kpsi (310  MPa ) \quad \text {for unpeened springs} \\ S_{e w} \cong 67.5  kpsi (465  MPa ) \quad \text {for peened springs} \end{array}       (14.13)

3    Note in Figure 14-16 that the wire fatigue strength S_{fw} is plotted at point B (\tau _{a} = \tau _{m} = 0.5 S_{fw}) corresponding to the test conditions of equal mean and alternating stress components (stress ratio R = \tau _{min}/\tau _{max} = 0). Point B is then connected with the ultimate shear strength S_{us} on the mean-stress axis at point A to draw the Goodman line, which is extended to point C.

4    We can now find the value of the fully reversed fatigue strength (R = –1), which is point C on the diagram. This value can be found from the equation for the Goodman line, defined in terms of its two known points, A and B:

\begin{aligned} m &=-\frac{0.5 S_{f w}}{S_{u s}-0.5 S_{f w}} \\ S_{f s} &=-m S_{u s} \\ S_{f s} &=0.5 \frac{S_{f w} S_{u s}}{S_{u s}-0.5 S_{f w}} \\ &=0.5 \frac{101993(207078)}{207078-0.5(101993)}=67658  psi \end{aligned}         (d)

5    This use of the Goodman line is conservative for stress ratios R ≥ 0, and its use is justified in this case because springs should always be loaded in the same direction. Helical compression springs tend to have stress ratios between 0 and 0.8, which puts their stress coordinates to the right of the 45° line in the figure, where the Goodman line is more conservative than the Gerber line.

6    Any other combination of mean and alternating stress with a stress ratio R ≥ 0 for this material and number of cycles can now be plotted on this diagram to obtain a safety factor.

Table 14-4 Coefficients and Exponents for Equation 14.3
Source: Reference 1
ASTM# Material Range Exponent
b
Coefficient A Correlation Factor
mm in MPa psi
A227 Cold drawn 0.5–16 0.020–0.625 –0.182 2 1 753.3 141 040 0.998
A228 Music wire 0.3–6 0.010–0.250 –0.1625 2 153.5 184 649 0.9997
A229 Oil tempered 0.5–16 0.020–0.625 –0.183 3 1 831.2 146 780 0.999
A232 Chrome-v 0.5–12 0.020–0.500 –0.145 3 1 909.9 173 128 0.998
A401 Chrome-s. 0.8–11 0.031–0.437 –0.093 4 2 059.2 220 779 0.991
Table 14-9 Maximum Torsional Fatigue Strength S_{fw}‘ for Round-Wire Helical
Compression Springs in Cyclic Applications (Stress Ratio, R = 0)
No Surging, Room Temperature, and Noncorrosive Environment. Source: Ref. 1
Percent of Ultimate Tensile Strength
Fatigue Life
(cycles)
ASTM 228, Austenitic Stainless
Steel and Nonferrous
ASTM A230 and A232
Unpeened Peened Unpeened Peened
10^5 36% 42% 42% 49%
10^6 33 39 40 47
10^7 30 36 38 46
14-3
14-15
14-16

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