A 360° journal bearing of length 45 mm and L/D = 1 has been scored due to dirty oil. The surface roughness of the bearing increases due to dirty oil and causes to increase the viscosity of the oil by 10% due to the working environment. Decide whether the bearing is to be replaced based on the criterion that 5% increase in power loss justifies the replacement. Consider the radial load 900 N, speed= 3000 rpm, radial clearance= 0.02 mm. SAE 10 oil is to be used and the inlet temperature is limited to 60°C.
Given L = 45 mm, D = 45 mm, W = 900 N, N* = 3000/60 = 50 rps, C_r=0.02 \mathrm{~mm}
Let the temperature rise be ΔT = 20° C
Average temperature is
T_{\text {average }}=T_{\mathrm{in}}+\frac{\Delta T}{2}=60+10=70^{\circ} \mathrm{C}
For SAE 10 oil, from graph at temperature 70°C, μ = 9.2 mPa·s = 0.0092 Ns/m²
p=\frac{W}{L D}=\frac{900}{45 \times 45}=0.44 \mathrm{~MPa}
Sommerfeld number is
S=\left(\frac{\mu N^*}{p}\right)\left(\frac{r}{C_r}\right)^2=\left(\frac{0.0092 \times 50}{0.44 \times 10^6}\right)\left(\frac{22.5}{0.02}\right)^2=1.33
Corresponding to S = 1.3, the temperature rise variable is determined as follows.
From Table 21.7 corresponding to S = 1.33
CFV = 26.4 and FV = 3.37
\frac{\rho C_p \Delta T}{p}=\frac{f\left(\frac{r}{C_r}\right)}{\left(\frac{Q}{r C_r N^* L}\right)}(4 \pi)=\frac{\mathrm{CFV}}{\mathrm{FV}} \times 4 \pi=\frac{26.4}{3.37} \times 4 \pi=98.44
\Delta T=\frac{98.44 \times p}{\rho C_p}=\frac{98.82 \times 0.44 \times 10^6}{860 \times 1760}=28.62^{\circ} \mathrm{C}
In the second iteration, the average temperature is
T_{\text {average }}=T_{\text {in }}+\frac{\Delta T}{2}=60+\frac{28.62}{2}=74.31^{\circ} \mathrm{C}=75^{\circ} \mathrm{C}
Viscosity corresponding to temperature 75°C is μ = 1.5 mPa·s = 0.0075 Ns/m²
Sommerfeld number is
S=\left(\frac{\mu N^*}{p}\right)\left(\frac{r}{C_r}\right)^2=\left(\frac{0.0075 \times 50}{0.44 \times 10^6}\right)\left(\frac{22.5}{0.02}\right)^2=1.078
Corresponding to S = 1.078 from graph,
FV = 3.4
CFV = 20
\frac{\rho C_p \Delta T}{p}=\frac{\mathrm{CFV}}{\mathrm{FV}} \times 4 \pi=\frac{20}{3.4} \times 4 \pi=73.92
\Delta T=\frac{73.92 \times p}{\rho C_p}=\frac{73.92 \times 0.44 \times 10^6}{860 \times 1760}=21.5^{\circ} \mathrm{C}
In the second iteration, the average temperature is
T_{\text {average }}=T_{\mathrm{in}}+\frac{\Delta T}{2}=60+\frac{21.5}{2}=70.75^{\circ} \mathrm{C}=71^{\circ} \mathrm{C}
which is very close to the first iteration value.
Viscosity corresponding to temperature 71°C is μ= 9.0 mPa·s = 0.009 Ns/m²
Sommerfeld number is 1.3
Hence μ = 9.0 mPa·s = 0.009 Ns/m²
f=2 \pi^2\left(\frac{\mu N^*}{p}\right)\left(\frac{r}{C_r}\right)+0.002=2 \pi^2\left(\frac{0.009 \times 50}{0.44 \times 10^6}\right)\left(\frac{22.5}{0.02}\right)+0.002=0.0247
Power loss
H=f W V=0.0247 \times 900 \times \frac{\pi \times 45 \times 3000}{60,000}=157.135 \mathrm{~W}
If viscosity of the oil increases by 10%,
\mu^{\prime}=1.1 \mu=1.1 \times 9=9.9 \mathrm{~mPa} \cdot \mathrm{s}=0.0099 \mathrm{~Ns} / \mathrm{m}^2
f^{\prime}=2 \pi^2\left(\frac{\mu^{\prime} N^*}{p}\right)\left(\frac{r}{C_r}\right)+0.002=2 \pi^2\left(\frac{0.0099 \times 50}{0.44 \times 10^6}\right)\left(\frac{22.5}{0.02}\right)+0.002=0.02698
The power loss due to increase in viscosity will be
H^{\prime}=f^{\prime} W V=0.02698 \times 900 \times \frac{\pi \times 45 \times 3000}{60,000}=171.64 \mathrm{~W}
\text { Percentage change in power loss }=\frac{171.64-157.135}{171.64} \times 100=8.45 \%
which is greater than the specified percentage, i.e. 5%. So the bearing must be changed.
Attitude \varepsilon | \frac{h_0}{C_r} | S | \phi | \frac{r}{C_r} f | \frac{Q}{r C_r N^* L} | \frac{Q_s}{Q} | \frac{p}{p_{\max }} |
0 | 1 | 00 | 85 | \infty | \pi | 0 | – |
0.1 | 0.9 | 1.33 | 79.5 | 26.4 | 3.57 | 0.15 | 0.54 |
0.2 | 0.8 | 0.631 | 74.02 | 12.8 | 3.59 | 0.28 | 0.529 |
0.4 | 0.6 | 0.264 | 63.10 | 5.79 | 3.99 | 0.497 | 0.484 |
TABLE 21.7 Dimensionless Performance Parameters for 360° Journal Bearing | ||||||||
\frac{L}{D} | S | \frac{h_0}{C_r} | \left(\frac{r}{C_r}\right) f | \frac{Q_s}{Q} | \frac{Q}{r C_r N^* L} | \phi | \frac{p_{\max }}{p} | \varepsilon |
0.25 | \infty | 1 | \infty | 0 | \pi | 89.5 | – | 0.00 |
16.2 | 0.9 | 322 | 0.18 | 3.45 | 82.31 | 0.515 | 0.10 | |
7.57 | 0.8 | 153 | 0.33 | 3.78 | 75.18 | 0.489 | 0.20 | |
2.83 | 0.6 | 61.1 | 0.567 | 4.37 | 60.86 | 0.415 | 0.40 | |
1.07 | 0.4 | 26.7 | 0.746 | 4.99 | 46.72 | 0.334 | 0.60 | |
0.261 | 0.2 | 8.8 | 0.884 | 5.6 | 31.04 | 0.240 | 0.80 | |
0.0736 | 0.1 | 3.5 | 0.945 | 5.91 | 21.85 | 0.180 | 0.90 | |
0.0101 | 0.03 | 0.922 | 0.984 | 6.12 | 12.22 | 1.108 | 0.97 | |
0 | 0 | 0 | 1 | – | 0 | 0.000 | 1.00 | |
0.5 | \infty | 1.00 | \infty | 0 | \pi | 88.50 | – | 0.00 |
4.3100 | 0.90 | 85.60 | 0.173 | 3.43 | 81.62 | 0.532 | 0.10 | |
2.0300 | 0.80 | 40.90 | 0.318 | 3.72 | 74.94 | 0.506 | 0.20 | |
0.7790 | 0.60 | 17.00 | 0.552 | 4.29 | 61.45 | 0.441 | 0.40 | |
0.3190 | 0.40 | 8.10 | 0.730 | 4.85 | 48.14 | 0.365 | 0.60 | |
0.0923 | 0.20 | 3.26 | 0.874 | 5.41 | 33.31 | 0.206 | 0.80 | |
0.0313 | 0.10 | 1.60 | 0.939 | 5.69 | 23.66 | 0.126 | 0.90 | |
0.0061 | 0.03 | 0.61 | 0.980 | 5.88 | 13.75 | 0.000 | 0.97 | |
0 | 0 | 0 | 1.0 | 0 | 0 | 0 | 1.00 | |
1.0 | \infty | 1.00 | \infty | 0 | \pi | 85.00 | – | 0.00 |
1.33 | 0.90 | 26.400 | 0.150 | 3.37 | 79.50 | 0.54 | 0.10 | |
0.631 | 0.80 | 12.800 | 0.280 | 3.59 | 74.02 | 0.529 | 0.20 | |
0.264 | 0.60 | 5.790 | 0.497 | 3.99 | 63.10 | 0.484 | 0.40 | |
0.121 | 0.40 | 3.220 | 0.680 | 4.33 | 50.58 | 0.415 | 0.60 | |
0.0446 | 0.20 | 1.700 | 0.842 | 4.62 | 36.24 | 0.313 | 0.80 | |
0.0188 | 0.10 | 1.050 | 0.919 | 4.74 | 26.45 | 0.247 | 0.90 | |
0.00474 | 0.03 | 0.514 | 0.973 | 4.82 | 15.47 | 0.152 | 0.97 | |
0 | 0.00 | 0.000 | 1.000 | 0 | 0.00 | 0 | 1.00 | |
\infty | \infty | 1.00 | \infty | 0 | \pi | 70.92 | – | 0.00 |
0.24 | 0.90 | 4.8 | 0 | 3.03 | 69.1 | 0.826 | 0.10 | |
0.123 | 0.80 | 2.57 | 0 | 2.83 | 67.26 | 0.814 | 0.20 | |
0.0626 | 0.60 | 1.52 | 0 | 2.26 | 61.94 | 0.764 | 0.40 | |
0.0389 | 0.40 | 1.2 | 0 | 1.56 | 54.31 | 0.667 | 0.60 | |
0.021 | 0.20 | 0.961 | 0 | 0.76 | 42.22 | 0.495 | 0.80 | |
0.0115 | 0.10 | 0.756 | 0 | 0.411 | 31.62 | 0.358 | 0.90 | |
– | 0.03 | – | 0 | – | – | – | 0.97 | |
0 | 0 | 0 | 0 | 0 | 0 | 0 | 1.00 |