Question 11.41: For the shaft application defined in Prob. 3–74, p. 138, per...

For the shaft application defined in Prob. 3–74, p. 138, perform a preliminary specification for tapered roller bearings at C and D. A bearing life of 10^{8} revolutions is desired with a 90 percent combined reliability for the  bearing set. Should the bearings be oriented with direct mounting or indirect mounting for the axial thrust to be carried by the bearing at C? Assuming bearings are available with K = 1.5, find the required radial rating for each bearing. For this preliminary design, assume an application factor of one.

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The thrust load on shaft CD is from the axial component of the force transmitted through the bevel gear, and is directed toward bearing C. By observation of Fig. 11-14, direct mounted bearings would allow bearing C to carry the thrust load.

From the solution to Prob. 3-74, the axial thrust load is F_{a e}=362.8  lbf, and the bearing radial forces are F_{C x}=287.2  lbf , F_{C z}=500.9  lbf , F_{D x}=194.4  lbf \text {, and } F_{D z}=307.1  lbf \text {. }

Thus, the radial forces are

\begin{aligned}&F_{r C}=\sqrt{287.2^{2}+500.9^{2}}=577  lbf \\&F_{r D}=\sqrt{194.4^{2}+307.1^{2}}=363  lbf\end{aligned}

The induced loads are

Eq. (11-15):       F_{i C}=\frac{0.47 F_{r C}}{K_{C}}=\frac{0.47(577)}{1.5}=181  lbf

Eq. (11-15):       F_{i D}=\frac{0.47 F_{r D}}{K_{D}}=\frac{0.47(363)}{1.5}=114  lbf

Check the condition on whether to apply Eq. (11-16) or Eq. (11-17), where bearings C and D are substituted, respectively, for labels A and B in the equations.

F_{i C} \leq ? \geq F_{i D}+F_{a e}

181  lbf <114+362.8=476.8  lbf , so Eq.(11-16) applies

Eq. (11-16a):

\begin{aligned}F_{e C} &=0.4 F_{r C}+K_{C}\left(F_{i D}+F_{a e}\right) \\&=0.4(577)+1.5(114+362.8)=946 lbf >F_{r C,} \text { so use } F_{e C}\end{aligned}

Assume for tapered roller bearings that the specifications for Manufacturer 1 on p. 608 are applicable.

\begin{aligned}&x_{D}=\frac{L_{D}}{L_{R}}=\frac{10^{8}}{90\left(10^{6}\right)}=1.11 \\&R=\sqrt{0.90}=0.949\end{aligned}

Eq. (11-7):               F_{R C}=1(946)\left(\frac{1.11}{4.48(1-0.949)^{1 / 1.5}}\right)^{3 / 10}=1130  lbf

Eq. (11-16b):           F_{e D}=F_{r D}=363  lbf

Eq. (11-7):               F_{R D}=1(363)\left(\frac{1.11}{4.48(1-0.949)^{1 / 1.5}}\right)^{3 / 10}=433  lbf

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Eq. (11-15):  F_{i}=\frac{0.47 F_{r}}{K}

Eq. (11-16):  \text { If } \quad F_{i A} \leq\left(F_{i B}+F_{a e}\right) \quad\left\{\begin{array}{l}F_{e A}=0.4 F_{r A}+K_{A}\left(F_{i B}+F_{a e}\right) \\F_{e B}=F_{r B}\end{array}\right.

Eq. (11-17):   \text { If } \quad F_{i A}>\left(F_{i B}+F_{a e}\right) \quad\left\{\begin{array}{l}F_{e B}=0.4 F_{r B}+K_{B}\left(F_{i A}-F_{a e}\right) \\F_{e A}=F_{r A}\end{array}\right.

 

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