Question 14.3: Design of a Helical Compression Spring for Static Loading Pr...

Design of a Helical Compression Spring for Static Loading

Problem    Design a compression spring for a static load over a known deflection.

Given    The spring must give a minimum force of 100 lb and a maximum force of 150 lb over an adjustment range of 0.75-in deflection.

Assumptions    Use the least expensive, unpeened, cold-drawn spring wire (ASTM A227) since the loads are static.

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See Table 14-10

1    Assume a trial wire diameter of 0.162 in from the available sizes in Table 14-2 (p. 791).

2    Assume a spring index of 8, which is in the middle of the recommended range, and calculate the mean coil diameter D from equation 14.5 (p. 797).

C=\frac{D}{d}      (14.5)

D=C d=8(0.162)=1.30 \text { in }      (a)

3    Find the direct shear factor K_{s} and use it to calculate the shear stress in the coil at the larger force.

K_s=1+\frac{0.5}{C}=1+\frac{0.5}{8}=1.06     (b)

\tau=K_s \frac{8 F D}{\pi d^3}=1.06 \frac{8(150)(1.30)}{\pi(0.162)^3}=123714  psi       (c)

4    Find the ultimate tensile strength of this wire material from equation 14.3 and Table 14-4 (p. 792) and use it to find the torsional yield strength from Table 14- 8 (p. 803), assuming that the set has been removed and using the low end of the recommended range.

S_{u t} \cong A d^b     (14.3)

S_{u t}=A d^b=141040(0.162)^{-0.1822}=196503  psi     (d)

S_{y s}=0.60 S_{u t}=0.60(196503)=117902  psi       (e)

5    Find the safety factor against yielding at this working deflection from equation 14.15 (p. 809).

N_s=\frac{S_{y s}}{\tau}     (14.15)

N_s=\frac{S_{y s}}{\tau}=\frac{117902  psi }{123714  psi }=0.95      (f)

This is obviously not acceptable, so the design must be iterated with some parameters changed.

6    Try increasing the wire diameter slightly, perhaps to 0.192 in, keeping the same spring index. Recalculate the coil diameter, stress, strength, and safety factor.

D=C d=8(0.192)=1.54 \text { in }     (g)

\tau=K_s \frac{8 F D}{\pi d^3}=1.06 \frac{8(150)(1.54)}{\pi(0.192)^3}=88074  psi        (h)

S_{u t}=A d^b=141040(0.192)^{-0.1822}=190513  psi         (i)

S_{y s}=0.60 S_{u t}=0.60(190513)=114308  psi      (j)

N_s=\frac{S_{y s}}{\tau}=\frac{114308  psi }{88074  psi }=1.30        (k)

This appears to be acceptable, so we can go on to design the other spring parameters.

7    The spring rate is defined in this problem because of the two specified forces at a particular relative deflection.

k=\frac{\Delta F}{y}=\frac{150-100}{0.75}=66.7  lb / in     (l)

8    To achieve this spring rate, the number of active coils must satisfy equation 14.7 (p. 797):

k=\frac{F}{y}=\frac{d^4 G}{8 D^3 N_a}       (14.7)

k=\frac{d^4 G}{8 D^3 N_a} \quad \text { or } \quad N_a=\frac{d^4 G}{8 D^3 k}=\frac{(0.192)^4 11.5 E 6}{8(1.54)^3 66.67}=8.09 \equiv 8        (m)

Note that we round it to the nearest 1/4 coil, as the manufacturing tolerance cannot achieve better than that accuracy. This makes the spring rate k = 67.4 lb/in.

9    Assume squared and ground ends, making the total number of coils from Figure 14-9 (p. 796):

N_t=N_a+2=8+2=10     (n)

10    The shut height can now be determined.

L_s=d N_t=0.192(10)=1.92  \text { in }          (o)

11    The initial deflection to reach the smaller of the two specified loads is

y_{\text {initial }}=\frac{F_{\text {initial }}}{k}=\frac{100}{67.4}=1.48  \text { in }        (p)

12    Assume a clash allowance of 15% of the working deflection:

y_{\text {clash }}=0.15 y=0.15(0.75)=0.113  \text { in }     (q)

13    The free length (see Figure 14-8, p. 796) can now be found from

L_f=L_s+y_{\text {clash }}+y_{\text {working }}+y_{\text {initial }}=1.92+0.113+0.75+1.48=4.26  \text { in }       (r)

14    The deflection to the shut height is

y_{\text {shut }}=L_f-L_s=4.26-1.92=2.34  \text { in }     (s)

15    The force at this shut-height deflection is

F_{\text {shut }}=k y_{\text {shut }}=67.4(2.34)=158  lb       (t)

16    The shut-height stress and safety factor are

\tau_{\text {shut }}=K_s \frac{8 F D}{\pi d^3}=1.06 \frac{8(158)(1.54)}{\pi(0.192)^3}=92794  psi     (u)

N_{s_{\text {shut }}}=\frac{S_{s y}}{\tau_{\text {shut }}}=\frac{114308  psi }{92794  psi }=1.2      (v)

which is acceptable.

17    To check for buckling, two ratios need to be calculated, L_{f} / D and y_{max} / L_{f}

\begin{array}{c} \frac{L_f}{D}=\frac{4.26}{1.54}=2.77 \\ \frac{y_{\max }}{L_f}=\frac{y_{\text {initial }}+y_{\text {working }}}{L_f}=\frac{1.48+0.75}{4.26}=0.52 \end{array}         (w)

Take these two values to Figure 14-14 (p. 801) and find that their coordinates are safely within the zones that are stable against buckling for either end-condition case.

18    The inside and outside coil diameters are

\begin{aligned} D_o &=D+d=1.54+0.192=1.73  \text { in } \\ D_i &=D-d=1.54-0.192=1.34  \text { in } \end{aligned}        (x)

19    The smallest hole and largest pin that should be used with this spring are

\begin{array}{c} \text { hole }_{\min }=D_o+0.05 D=1.73+0.05(1.54)=1.81 \cong 1 \frac{13}{16}  \text { in } \\ \operatorname{pin}_{\max }=D_i-0.05 D=1.34-0.05(1.54)=1.26 \cong 1 \frac{1}{4}  \text { in } \end{array}          (y)

20    The total weight of the spring is

W_t=\frac{\pi^2 d^2 D N_t \rho}{4}=\frac{\pi^2(0.192)^2(1.54)(10)(0.28)}{4}=0.40  lb      (z)

21    We now have a complete design specification for this A227 wire spring:

d = 0.192 in    OD = 1.73 in    N_{t} 10, sq & g      L_{f} = 4.26 in       (aa)

Other calculated spring parameters for this example are shown in Table 14-10.

22    Models for this example are on the CD-ROM as EX14-03. There are also alternate approaches to the solution of this example shown in separate Mathcad and TKSolver files on the CD-ROM with a letter added to their name.

 

Table 14-10     Example 14-3 – Helical Compression Spring Design for Static Loading
Input Variable Output Unit Comments
8.000 C trial spring index
0.192 dia trial wire diameter
0.750 y in deflection of spring
1 clash % % of deflect for clash allowance
‘hdrawn matl ‘music, ‘oiltemp, ‘hdrawn, ‘chromev, etc.
‘sqgrnd end one of ‘plain, ‘pgrnd, ‘square, ‘sqgrnd
‘unpeen surface one of ‘unpeen or ‘peen
‘set setflag one of ‘set or ‘unset
150 Fmax lb maximum applied force
100 Fmin lb minimum applied force
Fshut 158 lb force at shut height
k 67.4 lb/in spring rate with N_{a} rounded
Na 8 no. of active coils—to nearest 1/4 coil
Ntot 10 no. of total coils
D 1.54 in mean coil diameter
Dout 1.73 in outside coil diameter
Din 1.34 in inside coil diameter
Ks 1.06 static factor—direct shear – Eq. 13.8
Kw 1.18 Wahl Factor—Eq. 13.9
tauinit 58 716 psi shear stress at installed length
taustat 88 074 psi shear stress at Fmax for static loading
taushut 92 478 psi stress at shut height
Sut 190 513 psi tensile strength—Eq. 13.3 & Table 13-4
Sus 127 644 psi ultimate shear strength—Eq. 13.4
Sys 114 308 psi shear yield based on Table 13-6
 Ns_static 1.3 safety factor—static loading at Fmax
 Ns_shut 1.23 safety factor—shut height (yielding)
Lf 4.26 in free length
Linstal 2.78 in installed length
Lcomp 2.03 in compressed length
Lshut 1.92 in shut height
yinit 1.48 in initial deflection at assembly
ymax 2.23 in max working deflection
yclash 0.113 in coil clash allowance
yshut 2.34 in deflection to shut height

 

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 14-8 Maximum Torsional Yield Strength S_{ys} for Helical Compression Springs in Static Applications
Bending or Buckling Stresses Not Included. Source: Adapted from Ref. 1
Material Maximum Percent of Ultimate Tensile Strength
Before Set Removed (Use Eq. 13.10b) After Set Removed (Use Eq. 13.9b)
Cold-drawn carbon steel (e.g., A227, A228) 45% 60–70%
Hardened and tempered carbon and low-alloy steel (e.g., A229, A230, A232, A401) 50 65–75
Austenitic stainless steel (e.g., A313) 35 55–65
Nonferrous alloys (e.g., B134, B159, B197) 35 55–65

 

T14-2
F14-14
F14-9
F14-8

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