The nominal velocity ratio is
VR = 575/275 = 2.09
Specify an overload factor of K_o = 1.50 from Table 9–1 for a uniform power source and moderate shock for the meat grinder. Then compute design power,
P_{des} = K_{o}P = (1.50)(15 kW) = 22.5 kW
From Figure 9–11, m = 5 is a reasonable trial module. Then
N_P = 18 (design decision)
D_P = N_Pm = (18)(5) = 90 mm
N_G = N_P(VR) = (18)(2.09) = 37.6 (Use 38)
D_G = N_Gm = (38)(5) = 190 mm
Final output speed = n_G = n_P(N_P/N_G)
n_G = 575 rpm × (18/38) = 272 rpm (OK)
Center distance = C = (N_P + N_G)m/2[Table 8–1]
C = (18 + 38)(5)/2 = 140 mm (OK)
In SI units, the pitch line speed in meters per second (m/s) is
v_t = πD_Pn_P/(60 000) = [(π)(90)(575)]/(60 000) = 2.71 m/s
In SI units, the transmitted load, W_t, is in newtons (N). If the power, P, is in kW, and v_t is in m/s,
W_t = 1000(P)/v_t = (1000)(15)/(2.71) = 5536 N
Face width, F: Let’s specify the nominal F = 12m = 12(5) = 60 mm
Factors in stress analysis:
K_o = 1.50 (found earlier)
K_s = 1.00 (Table 9–2; m = 5) K_B = 1.00 (Use solid gear blanks)
K_R = 1.00 (Table 9–11; 0.99 reliability) S_F = 1.00 (No unusual conditions)
K_v = 1.31 (Figure 9–16; A_v = 11)
K_m = 1.21 (Figures 9–12 and 9–13; F = 60 mm; F/D_P = 60/90 = 0.67)
J_P = 0.315; J_G = 0.380 (Figure 9–10; N_P = 18, N_G = 38)
C_p = 191 (Table 9–7) I = 0.092 (Figure 9–17)
Pinion contact stress:
(Equation 9–23)
S_{c}=C_{P} \sqrt{\frac{W_{t} K_{o} K_{s} K_{m} K_{v}}{F D_{P} l}}=191 \sqrt{\frac{(5536)(1.50)(1.0)(1.21)(1.31)}{(60)(90)(0.092)}}=983 \mathrm{MPa}
Adjustments for number of cycles, from Figures 9-21 and 9-22:
Y_{N p}=0.94 \quad Z_{N P}=0.91 \quad Y_{N G}=0.96 \quad Z_{N G}=0.92
Required s_{a C P}=s_{C}(S F)\left(K_{R}\right) / Z_{N P}=983 \mathrm{MPa}(1.0)(1.0) / 0.91=1080 \mathrm{MPa}
Using S_{a c P}=1080 \mathrm{MPa}, Figure 9-19 shows the required hardness =\mathrm{HB} 396 for through-hardened Grade 1 steel. This is acceptable but near the upper end of recommended range.
Material specification:
From Figure A4–5 (other possibilities exist),
SAE 4340 OQT 800; HB 415; s_y = 1324 MPa; s_u = 1448 MPa; 12% elongation.
Check other stresses:
The contact stress for the gear and the bending stress for the pinion and the gear are expected to require less material hardness and strength.
Required s_{acG} = s_c(SF)(K_R)/Z_{NG} = 983 MPa(1.0)(1.0)/0.92 = 1068 MPa
This is slightly lower than for the pinion (OK)
\begin{aligned}S_{t P} &=\frac{W_{t} K_{0} K_{S} K_{B} K_{m} K_{v}}{F m J_{P}}=\frac{(5536)(1.50)(1)(1)(1.21)(1.31)}{(60)(5)(0.315)}=139 \mathrm{MPa} \\\text { Required } S_{a t P} &=S_{t P}(S F)\left(K_{R}\right) / Y_{N P}=139 \mathrm{MPa}(1.0)(1.0) / 0.94=148 \mathrm{MPa}\end{aligned}
Referring to Figure 9-18, it is obvious that bending stress requires far lower hardness for the gear teeth, less than HB 180. The stress in the gear is always less than that in the pinion so it will obviously be safe as well.
Summary of the Design:
P=15.0 \mathrm{~kW} from an electric motor to a large meat grinder
Pinion speed: n_{P}=575 \mathrm{rpm}
Gear speed: n_{G}=272 \mathrm{rpm}
Number of teeth: N_{P}=18 ; N_{G}=38 Center distance: C=140.00 \mathrm{~mm}
Module: m=5 \mathrm{~mm}
Diameters: D_{P}=90 \mathrm{~mm} ; D_{G}=190 \mathrm{~mm}
Material: Steel-SAE 4340 OQT 800
Comment:
A redesign may be considered with several possible approaches:
1. Increase the face width, F, to lower the stresses and permit the choice of a material with more moderate required hardness and better ductility. The recommended upper limit of face width is 16m = 16(5) = 80 mm.
2. Increase the size of pinion and its number of teeth (same module) to lower stresses.
Possible trial: Module: m = 5 mm Number of teeth: N_P = 22; N_G = 46
Center distance: C = 170.00 mm Diameters: D_P = 110[latex] mm; [latex]D_G = 230 mm
3. Consider case-hardened steel for the initial design, rather than through-hardened steel. A smaller design is possible.
TABLE 9–1 Suggested Overload Factors, K_o |
Driven Machine |
Power source |
Uniform |
Light shock |
Moderate shock |
Heavy shock |
Uniform |
1.00 |
1.25 |
1.50 |
1.75 |
Light shock |
1.20 |
1.40 |
1.75 |
2.25 |
Moderate shock |
1.30 |
1.70 |
2.00 |
2.75 |
TABLE 9–11 Reliability Factor, K_R |
Reliability |
K_R |
0.90, one failure in 10 |
0.85 |
0.99, one failure in 100 |
1.00 |
0.999, one failure in 1000 |
1.25 |
0.9999, one failure in 10 000 |
1.5 |
TABLE 9–2 Suggested Size Factors, K_s |
Diametral pitch, P_d |
Metric module, m |
Size factor, K_s |
≥ 5 |
≤ 5 |
1.00 |
4 |
6 |
1.05 |
3 |
8 |
1.15 |
2 |
12 |
1.25 |
1.25 |
20 |
1.40 |
TABLE 9–7 Elastic Coefficient, C_p |
Gear material and modulus of elasticity, E_G, lb/in^2 (MPa) |
Pinion
material |
Modulus of
elasticity,
E_P,lb/in^2
(MPa) |
Steel
30×10^6(2×10^5) |
Malleable
iron
25×10^6(1.7×10^5) |
Nodular
iron
24×10^6(1.7×10^5) |
Cast iron
22×10^6(1.5×10^5) |
Aluminum
bronze
17.5×10^6(1.2×10^5) |
Tin bronze
16×10^6(1.1×10^5) |
Steel |
30×10^6 |
2300 |
2180 |
2160 |
2100 |
1950 |
1900 |
|
(2×10^5) |
191 |
181 |
179 |
174 |
162 |
158 |
Mall. Iron |
25×10^6 |
2180 |
2090 |
2070 |
2020 |
1900 |
1850 |
|
(1.7×10^5) |
181 |
174 |
172 |
168 |
158 |
154 |
Nod. Iron |
24×10^6 |
2160 |
2070 |
2050 |
2000 |
1880 |
1830 |
|
(1.7×10^5) |
179 |
172 |
170 |
166 |
156 |
152 |
Cast iron |
22×10^6 |
2100 |
2020 |
2000 |
1960 |
1850 |
1800 |
|
(1.5×10^5) |
174 |
168 |
166 |
163 |
154 |
149 |
Al. bronze |
1.75×10^6 |
1950 |
1900 |
1880 |
1850 |
1750 |
1700 |
|
(1.2×10^5) |
162 |
158 |
156 |
154 |
145 |
141 |
Tin bronze |
16×10^6 |
1900 |
1850 |
1830 |
1800 |
1700 |
1650 |
|
(1.1×10^5) |
158 |
154 |
152 |
149 |
141 |
137 |
TABLE 8–1 Gear and Tooth Features, Diameters, Center Distance for a Gear Pair |
|
|
|
|
Formulas |
|
|
|
|
|
U.S. Full-depth involute system |
Metric
module
system
(mm) |
Number of teeth and Pitches |
Symbol |
Definition |
Typical unit |
General formula |
Coarse pitch P_d < 20 (in) |
Fine pitch P_d ≥ 20 (in) |
Number of teeth |
N |
Integer count of teeth on a gear |
|
|
|
|
|
Circular pitch |
P |
Arc distance between corresponding points on adjacent teeth |
in or mm |
p = πD/N |
p = π/P_d |
p = πm |
Diametral pitch |
P_d |
Number of teeth per inch of pitch diameter |
in^{-1} |
P_d = N/D |
|
Module |
m |
Pitch diameter divided by number of teeth |
mm |
m = D/N |
|
|
m = 25.4/P_d |
Diameters |
Pitch diameter |
D |
Kinematic characteristic diameter for a gear; Diameter of the pitch circle |
in or mm |
|
D = N/P_d |
D = mN |
Outside diameter |
D_o |
Diameter to the outside surface of the gear teeth |
in or mm |
|
D_o = (N + 2)/P_d |
D_o = m(N + 2) |
Root diameter |
D_R |
Diameter to the root circle of the gear at the base of the teeth |
in or mm |
D_R = D - 2b |
|
Gear Tooth Features |
Addendum |
a |
Radial distance from pitch circle to outside of tooth |
in or mm |
|
a = 1.00/P_d |
a = 1.00m |
Dedendum |
b |
Radial distance from pitch circle to bottom of tooth space |
in or mm |
|
b = 1.25/P_d |
b = 1.20/P_d + 0.002 |
b = 1.25m^1 |
Clearance |
c |
Radial distance from top of fully engaged tooth of mating gear to bottom of tooth space |
in or mm |
|
c = 0.25/P_d |
c = 0.20/P_d + 0.002 |
c = 0.25m^1 |
Whole depth |
h_t |
Radial distance from top of a tooth to bottom of tooth space |
in or mm |
h_t = a + b |
h_t = 2.00/P_d |
h_t = 2.20/P_d + 0.002 |
h_t = 2.25m^1 |
Working depth |
h_k |
Radial distance a gear tooth projects into tooth space of mating gear |
in or mm |
h_k = a + a = 2a |
h_k = 2.25/P_d |
h_k = 2.25/P_d |
h_k = 2.00m^1 |
Tooth thickness |
Tensile strength |
Theoretical arc distance equal to 1/2 of circular pitch |
in or mm |
t = p/2 |
t = π/[2(P_d)] |
t = πm/2 |
Face width |
F |
Width of tooth parallel to axis of gear |
in or mm |
Design decision |
Approximately 12/P_d |
|
Pressure angle |
\phi |
Angle between the tangent to the pitch circle and the perpendicular to the gear tooth surface |
degrees |
Design decision |
Most common value = 20°
Others: 14 1/2°, 25° |
|
Center Distance |
C |
Distance from between centerlines of mating gears |
in or mm |
C = (D_P + D_G)/2 |
C = (N_P + N_G)/2P_d |
C = m(N_P + N_G)/2 |