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Question 9.2: Shaft Design for Combined Bending and Torsion The gear A is ......

Shaft Design for Combined Bending and Torsion

The gear A is attached to the AISI 1010 CD steel shaft AB of yield strength S_y that carries a vertical load of 360 lb (Figure 9.3(a)). The shaft is fitted with gear D that forms a set with gear E .

Find: (a) The value of the torque T_E applied on the gear E to support the loading and reactions at the bearings, and (b) the required shaft diameter D , applying the maximum shear stress failure criterion.

Given: S_y =300/6.895=43.5 ksi (from Table B.3).

Assumptions: The bearings at B and C are taken as simple supports. A safety factor of n =1.6 is to be used with respect to yielding.

TABLE B.3
Mechanical Properties of Some Hot-Rolled (HR) and Cold-Drawn (CD) Steels
UNS Number AISI/ SAE Number Processing Ultimate

\text {Strength}^a

S_u (MPa)

Yield

\text {Strength}^a

S_y (MPa)

Elongation in 50 mm (%) Reduction in Area (%) Brinell Hardness (H_B)
G10060 1006 HR 300 170 30 55 86
CD 330 280 20 45 95
G10100 1010 HR 320 180 28 50 95
CD 370 300 20 40 105
G10150 1015 HR 340 190 28 50 101
CD 390 320 18 40 111
G10200 1020 HR 380 210 25 50 111
CD 470 390 15 40 131
G10300 1030 HR 470 260 20 42 137
CD 520 440 12 35 149
G10350 1035 HR 500 270 18 40 143
CD 550 460 12 35 163
G10400 1040 HR 520 290 18 40 149
CD 590 490 12 35 170
G10450 1045 HR 570 310 16 40 163
CD 630 530 12 35 179
G10500 1050 HR 620 340 15 35 179
CD 690 580 10 30 197
G10600 1060 HR 680 370 12 30 201
G10800 1080 HR 770 420 10 25 229
G10950 1095 HR 830 460 10 25 248
Source: ASM Handbook, vol. 1, ASM International, Materials Park, OH, 2020.
Note: To convert from MPa to ksi, divide given values by 6.895.
{ } ^ {a} Values listed are estimated ASTM minimum values in the size range 18–32 mm.
F9.3
Step-by-Step
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a. Conditions of equilibrium are applied to Figure 9.3(b) to find tangential force F_D acting on gear D . Then support reactions are determined using equilibrium conditions and marked on the figure. Referring to Figure 9.3(a), we thus have T_E=F_D(2)=480(2)=960  lb \cdot in .

b. Observe from Figure 9.3(c) through Figure 9.3(e) that, since M_C>M_D , the critical section where largest value of the stress is expected to occur is at C. Through the use of Equation (9.7), we have

\frac{S_y}{n}-\frac{32}{\pi D^3}\left[M^2+T^2\right]^{1 / 2}        (9.7)

D=\left[\frac{32 n}{\pi S_y} \sqrt{M_C^2+T_C^2}\right]^{1 / 3}        (a)

Substituting the numerical values results in

D=\left[\frac{32(1.6)}{\pi(43.5)} \sqrt{(1.8)^2+(1.44)^2}\right]^{1 / 3}=0.952 \text { in. }

Comment: It is interesting to note that, similar to the distortion energy criterion, Equation (9.8) gives D=0.936 in. Thus, a standard diameter of 1.0 in. shaft can be safely used.

\frac{S_y}{n}=\frac{32}{\pi D^3}\left[M^2+\frac{3}{4} T^2\right]^{1 / 2}       (9.8)

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