The pitch angles are
γ = tan^{−1} \left( \frac {3}{9}\right) = 18.4° Γ = tan^{−1} \left( \frac{9}{3}\right)= 71.6°
The pitch-line velocity corresponding to the average pitch radius is
V =\frac{2πr_{P}n}{12} =\frac{2π(1.293)(600)}{12} = 406 ft/min
Therefore the transmitted load is
W_{t} =\frac{33 000H}{V} =\frac{(33 000)(5)}{406} = 406 lbf
which acts in the positive z direction, as shown in Fig. 13–36b. We next have
W_{r} = W_{t} tan \phi cos Γ = 406 tan 20° cos 71.6° = 46.6 lbf
W_{a} = W_{t} tan \phi sin Γ = 406 tan 20° sin 71.6° = 140 lbf
where W_{r} is in the −x direction and W_{a} is in the −y direction, as illustrated in the isometric sketch of Fig. 13–36b.
In preparing to take a sum of the moments about bearing D, define the position vector from D to G as
R_{G} = 3.88i − (2.5 + 1.293)j = 3.88i − 3.793j
We shall also require a vector from D to C:
R_{C} = −(2.5 + 3.625)j = −6.125j
Then, summing moments about D gives
R_{G} ×W+ R_{C} × F_{C} + T = 0 (1)
When we place the details in Eq. (1), we get
(3.88i − 3.793j) × (−46.6i − 140j + 406k)+ (−6.125j) × (F^{x}_{C}i + F^{y}_{C}j + F^{z}_{C}k)+ T j = 0 (2)
After the two cross products are taken, the equation becomes
(−1540i − 1575j − 720k) +(−6.125F^{z}_{C}i + 6.125F^{x}_{C}k)+ T j = 0
from which
T = 1575j lbf · in F^{x}_{C} = 118 lbf F^{z}_{C} = −251 lbf (3)
Now sum the forces to zero. Thus
F_{D} + F_{C} +W = 0 (4)
When the details are inserted, Eq. (4) becomes
(F^{x}_{D}i + F^{z}_{D}k)+(118i + F^{y}_{C}j − 251k)+ (−46.6i − 140j + 406k) = 0 (5)
First we see that F^{y}_{C} = 140 lbf, and so
F_{C} = 118i + 140j − 251k lbf
Then, from Eq. (5),
F_{D} = −71.4i − 155k lbf
These are all shown in Fig. 13–36b in the proper directions.The analysis for the pinion shaft is quite similar.