Loose Leaf for Shigley's Mechanical Engineering Design Format: LooseLeaf
Loose Leaf for Shigley's Mechanical Engineering Design Format: LooseLeaf
10th Edition
ISBN: 9780073399652
Author: BUDYNAS
Publisher: Mcgraw Hill Publishers
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Chapter 13, Problem 44P

The figure shows a 10 diametral pitch 18-tooth 20° straight bevel pinion driving a 30-tooth gear. The transmitted load is 25 lbf. Find the bearing reactions at C and D on the output shaft if D is to take both radial and thrust loads.

Problem 13–44

Dimensions in inches.

Chapter 13, Problem 44P, The figure shows a 10 diametral pitch 18-tooth 20 straight bevel pinion driving a 30-tooth gear. The

Expert Solution & Answer
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To determine

The bearing reaction at A.

The bearing reaction at B.

Answer to Problem 44P

The bearing reaction at A is FA=(94.4lbf)i^(64.2lbf)j^(1209.9lbf)k^.

The bearing reaction at B is FB=(222.8lbf)i^+(815.6lbf)k^.

Explanation of Solution

The figure below shows the forces acting at the bevel gear and pinion assembly.

Loose Leaf for Shigley's Mechanical Engineering Design Format: LooseLeaf, Chapter 13, Problem 44P

Figure-(1)

Write the expression for the diameter of gear 2.

    d2=N2pd                                                                 (I)

Here, the diametrical pitch is pd and the number of teeth on gear 2 is N2.

Write the expression for the diameter of gear 3.

    d3=N3pd                                                                 (II)

Here, the number of teeth on gear 3 is N3.

Write the expression for the pitch angle for gear 2.

    γ=tan1((d22)d32)                                                          (III)

Write the expression for the pitch angle for gear 3.

    Γ=90°γ                                                                  (IV)

Write the expression fort the pitch radius at the mid-point of the bevel gear.

    rav=d32ls2sinγ2                                                   (V)

Here, the lateral side of the gear 2 is ls2.

Write the expression for DE.

    DE=DK+ls2sinγ2                                               (VI)

Here, the distance between the points D and K is DK.

Write the expression for the radial load.

    Wr=WttanϕcosΓ                                                       (VII)

Here, the pressure angle is ϕ.

Write the expression for the axial load.

    Wa=WttanϕsinΓ                                                        (VIII)

Write the expression of the load in vector form.

    W=Wri^Waj^+Wtk^                                                       (IX)

Write the expression for the position vector of DG.

    RDG=rav(i^)+(DE)j^

Write the expression for the position vector of DC.

    RDC=DCj^

Write the expression for the force on the bearing C.

    FC=FCxi^+FCzk^                                                               (X)

Here, the force on bearing C in x direction is FCx and the force on bearing C in y direction is FCy.

Write the expression for the moment about D in vector form.

    RDG×W+RDC×FC+Tj^=0                                               (XI)

Here, the torque is T.

Write the expression for the force equilibrium for the set of bearings.

    FC+FD+W=0                                                                  (XII)

Substitute FCxi^+FCzk^ for FC, DCj^ for RDC, rav(i^)+(DE)j^ for RDG, Wri^Waj^+Wtk^ for W in Equation (XII).

    {(rav(i^)+(DE)j^)×(Wri^Waj^+Wtk^)+(DCj^)×(FCxi^+FCzk^)+Tj^}=0{[ravWa]k^+[ravWt(j^)]+DE(Wr(k^))+DEWt(i^)+[(DC)FCx(k^)+(DC)FCzi^]+Tj^}=0     (XIII)

Conclusion:

Substitute 18 for N2 and 10in1 for pd in Equation (I).

    d2=1810in1=1.8in

Substitute 30 for N3 and 10in1 for pd in Equation (II).

    d3=3010in1=3in

Substitute 3in for d3 and 1.8in for d2 in Equation (III).

    γ=tan1((1.8in2)3in2)=tan1(0.9in1.5in)=tan1(0.6)=30.96°

Substitute 30.96° for γ in Equation (IV).

    Γ=90°30.96°=59.04°

Substitute 3in for d3, 0.5in for ls2 and 59.04° for Γ in Equation (V).

    rav=3in2(0.5in)sin59.04°2=1.5in0.214in=1.286in

Substitute 916in for DK, 0.5in for ls2 and 59.04° for Γ in Equation (VI).

    DE=916in+(0.5in)sin(59.04°)2=916in+0.214in=0.6911in

Substitute 25lbf for Wt, 20° for ϕ and 59.04° for Γ in Equation (VII).

    Wr=25lbftan20°cos59.04°=9.099cos59.04°lbf=4.681lbf

Substitute 25lbf for Wt, 20° for ϕ and 59.04° for Γ in Equation (VIII).

    Wa=(25lbf)tan20°sin59.04°=9.099sin59.04°lbf=7.803lbf

Substitute 25lbf for Wt, 7.803lbf for Wa and 4.681lbf for Wr in Equation (IX).

    W=(4.681lbf)i^(7.803lbf)j^+(25lbf)k^

Substitute 25lbf for Wt, 7.803lbf for Wa, 1.286in for rav, 0.6911in for DE, 4.681lbf for Wr  and 58in for DC in Equation (XIII).

    {[(1.286in)(7.803lbf)]k^+[(1.286in)(25lbf)(j^)]+[(58in)FCx(k^)+(58in)FCzi^]+Tj^+0.6911in((4.681lbf)(k^))+0.6911in(25lbf)(i^)}=0{[10.034lbfin]k^+[32.15lbfin(j^)]+(3.235lbfin)k^+(17.2775lbfin)i^+[(0.625in)FCx(k^)+(0.625in)FCzi^]+Tj^}=0{(17.2775lbfin0.625inFCz)i^+(T32.15lbfin)j^+(3.235lbfin10.034lbfin+(0.625in)FCx)k^}=0       (XIV)

Compare the i^ coordinates of Equation (XIV).

    17.2775lbfin0.625inFCz=0FCz=27.65lbf

Compare the j^ coordinates of Equation (XIV).

    T32.15lbfin=0T=32.15lbfin

Compare the k^ coordinates of Equation (XIV).

    3.235lbfin10.034lbfin+(0.625in)FCx=0FCx=10.88lbf

Substitute 222.8lbf for FBx and 815.6lbf for FBz in Equation (X).

    FB=(222.8lbf)i^+(815.6lbf)k^=(222.8lbf)i^+(815.6lbf)k^

Thus, the bearing reaction at B is FB=(222.8lbf)i^+(815.6lbf)k^.

Substitute (222.8lbf)i^+(815.6lbf)k^ for FB and (128.4lbf)i^(64.2lbf)j^+(394.3lbf)k^ for W in Equation (XII).

    {FA+[(222.8lbf)i^+(815.6lbf)k^]+[(128.4lbf)i^(64.2lbf)j^+(394.3lbf)k^]}=0FA=(222.8lbf128.4lbf)i^+(64.2lbf)j^(815.6lbf+394.3lbf)k^FA=(94.4lbf)i^(64.2lbf)j^(1209.9lbf)k^

Thus, the bearing reaction at A is FA=(94.4lbf)i^(64.2lbf)j^(1209.9lbf)k^.

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Chapter 13 Solutions

Loose Leaf for Shigley's Mechanical Engineering Design Format: LooseLeaf

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