The reactions in the xz plane from Fig. 11–18b are
R_{zA} = \frac{3980\left(50\right)}{150}= 1327 N
R_{zB} = \frac{3980\left(100\right)}{150}= 2653 N
The reactions in the xyplane from Fig. 11–18c are
R_{yA} = \frac{1770\left(50\right)}{150}+\frac{169 000)}{150}= 1716.7 = 1717 N
R_{yB} = \frac{1770\left(100\right)}{150}-\frac{169 000)}{150}= 53.3 N
The radial loads F_{rA} \ and \ F_{rB} are the vector additions of R_{yA} \ and \ R_{zA} \ , \ and \ R_{yB} \ and \ R_{zB} , respectively:
F_{rA} = \left(R^2_{zA}+ R^2_{yA} \right)^{{1}/{2}} = \left(1327^2 + 1717^2 \right)^{{1}/{2}} = 2170 N
F_{rB} = \left(R^2_{zB}+ R^2_{yB} \right)^{{1}/{2}} = \left(2653^2 + 53.3^2 \right)^{{1}/{2}} = 2654 N
Trial \ 1 :With direct mounting of the bearings and application of the external thrust to the shaft, the squeezed bearing is bearing A as labeled in Fig. 11–18a. Using K of 1.5 as the initial guess for each bearing, the induced loads from the bearings are
F_{iA} = \frac{0.47 F_{rA}}{K_A}= \frac{0.47 \left(2170\right)}{1.5}= 680 N
F_{iB} = \frac{0.47 F_{rB}}{K_B}= \frac{0.47 \left(2654\right)}{1.5}= 832 N
Since F_{iA} is clearly less than F_{iB} + F_{ae} , bearing A carries the net thrust load, and Eq. (11–16)
if \ F_{iA}\leq \left(F_{iB+F_ae}\right) \begin{cases}F_{eA}+0.4 F_{rA}+K_A\left(F _{iB}+F_{ae}\right)\\ F_{eB}=F_{rB} \end{cases}
is applicable. Therefore, the dynamic equivalent loads are
F_{eA} = 0.4 F_{rA} + K_A \left(F_{iB} + F_{ae}\right) = 0.4\left(2170\right) + 1.5\left(832 + 1690\right) = 4651 N
F_{eB} = F_{rB} = 2654 N
The multiple of rating life is
x_D = \frac {L_D}{L_R}=\frac{\mathscr{L}_{D} n_{D} 60}{L_R}= \frac {\left(5000\right)\left(800\right)\left(60\right)}{90 \left(106\right)}= 2.67
Estimate R_D as \sqrt{0.99} = 0.995 for each bearing. For A, from Eq. (11–7) the catalog entry
C_{10} should equal or exceed
C_{10} = \left(1\right)\left(4651\right)\left[ \frac{2.67}{\left(4.48\right)\left(1-0.995\right)^{{2}/{3}} } \right]^{{3}/{10}}= 11 486 N
From Fig. 11–15, tentatively select type TS 15100 cone and 15245 cup, which will work: K_A = 1.67 \ , \ C_{10} = 12 100 N.
For bearing B , from Eq. (11–7),
C_{10} \doteq a_f F_D \left[\frac{x_D}{x_0+\left(\theta-x_0\right)\left(1-R_D\right)^{{1}/{b}} } \right]^{{1}/{a}} \ R \ge 0.90
the catalog entry C_{10} should equal or exceed
C_{10} = \left(1\right)2654 \left[\frac{2.67}{\left(4.48\right)\left(1 − 0.995\right)^{{2}/{3}}}\right]^{{3}/{10}}= 6554 N
Tentatively select the bearing identical to bearing A, which will work:
K_B = 1.67 \ , \ C_{10} = 12 100 N.
Trial \ 2: Repeat the process with K_A = K_B = 1.67 from tentative bearing selection.
F_{iA}= \frac{0.47 F_{rA}}{K_A}=\frac{0.47 \left(2170\right)}{1.67}= 611 N
F_{iB}= \frac{0.47 F_{rB}}{K_B}=\frac{0.47 \left(2654\right)}{1.67}= 747 N
Since F_{iA} is still less than F_{iB} + F_{ae} , Eq. (11–16)
is still applicable.
F_{eA} = 0.4F_{rA} + K_A \left(F{iB} + F_{ae}\right) = 0.4 \left(2170\right) + 1.67\left(747 + 1690\right) = 4938 N
F_{eB} =F_{rB} = 2654 N
For A, from Eq. (11–7) the corrected catalog entry C_{10} should equal or exceed
C_{10}= \left(1\right) \left(4938\right)\left[\frac{2.67}{\left(4.48\right)\left(1-0.995\right)^{{2}/{3}} } \right]^{{3}/{10}} =12195 N
Although this catalog entry exceeds slightly the tentative selection for A, we will keep it since the reliability of bearing B exceeds 0.995. In the next section we will quantitatively show that the combined reliability of A and B will exceed the reliability goal of 0.99. For bearing B \ , \ F_{eB} = F_{rB} = 2654 N. From Eq. (11–7),
C_{10}= \left(1\right) \left(2654\right)\left[\frac{2.67}{\left(4.48\right)\left(1-0.995\right)^{{2}/{3}} } \right]^{{3}/{10}} = 6554 N
Select cone and cup 15100 and 15245, respectively, for both bearing
A and B. Note from Fig. 11–14 the effective load center is located at a = −5.8 mm, that is, 5.8 mm into the cup from the back. Thus the shoulder-to-shoulder dimension should be 150 − 2\left(5.8\right) = 138.4 mm. Note that in each iteration of Eq. (11–7) to find the catalog load rating, the bracketed portion of the equation is identical and need not be re-entered on a calculator each time.