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25-Nav-B1 Applied Thermodynamics and Heat Transfer (25-Mec-A1) · May 2016

Question 5 of 6: Rotating Shaft — Fatigue Diameter and Deflections

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

National Exams — May 2016 · 98-Mar-B1 Advanced Machine Design. Open-book, 3 hours, 100 marks. Part I (Problems 1–2) is compulsory; candidates answer any three of the four Part II problems (3–6). For study value, complete worked solutions to all six problems are provided below.

Reference texts. R.G. Budynas & J.K. Nisbett, Shigley’s Mechanical Engineering Design, 10th ed. (power screws §8-2, clutches §16-5, shaft fatigue §7-4/§6, notch factors §6-10); R.C. Juvinall & K.M. Marshek, Fundamentals of Machine Component Design (screws, clutches); R.C. Hibbeler, Mechanics of Materials (beam reactions, bending stress, deflection).

Check — paper content and assumptions. This paper, although listed under Applied Thermodynamics and Heat Transfer, is headed “98-Mar-B1” with printed title “Advanced Machine Design”; it is a general mechanical machine-design paper — green-design/yield-theory short answers, Acme power-screw torque, beam reactions/SFD/BMD/bending stress, disk-clutch sizing, shaft fatigue with deflections, and notched-bar fatigue — with zero thermodynamics or heat-transfer content, and it is solved as the exam actually printed. Engineering assumptions stated per the exam rubric: (1) “ton” is read as the US short ton (2000 lb), consistent with the inch/ft·min/hp unit set of Problem 2. (2) In Problem 3 the concentrated couple Mz is taken counter-clockwise (out of the page, per the dot symbol in the figure); a clockwise reading would give RA = 0, RB = 9.5 kN. (3) In Problem 5 the fluctuating torque is assumed transmitted over the 18 in from the drive end to the load; no stress concentration is used as the problem directs.

Question 5: Rotating Shaft — Fatigue Diameter and Deflections (20 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Given. Self-aligning bearings (simple supports) at $x=0$ and $x=14$ in; a constant $1000$ lb transverse load at $x=18$ in (4 in overhang); torque fluctuating $0\!\to\!2000$ lb·in; $S_{ut}=108$ ksi, $S_y=62$ ksi; design factor $n=2$; $K_f=K_{fs}=1$.

1000 lb14 in18 in20 inbearings = simple supports
Problem 5: shaft on two self-aligning bearings with the 1000 lb load overhung 4 in beyond the right bearing.

Find. The shaft diameter for $n=2$ in combined fatigue (DE-Goodman), and the corresponding maximum torsional twist and bending deflection.

Approach. Because the shaft rotates under a fixed transverse load, the bending is fully reversed; the torque gives its own mean and alternating parts. Locate the critical section (the right bearing, where $M$ peaks), build the Marin endurance limit, and iterate the DE-Goodman diameter (size factor depends on $d$). Then compute twist $\theta=TL/GJ$ and the overhang deflection.

  1. Critical bending moment. Reactions for the overhung load give $R_B=1000(18)/14=1286$ lb up, $R_A=-286$ lb; the bending moment peaks at the right bearing: $$M_{max}=P\times\text{overhang}=1000(4)=4000\ \text{lb}\!\cdot\!\text{in}.$$ Rotation makes this fully reversed: $M_a=4000$, $M_m=0$. The torque splits as $T_m=T_a=1000$ lb·in.
  2. Endurance limit (Marin). $S_e'=0.5S_{ut}=54$ ksi. Surface (machined) $k_a=2.70\,S_{ut}^{-0.265}=0.781$; load, temperature and reliability factors $=1$; the size factor $k_b=0.879\,d^{-0.107}$ depends on $d$, so the diameter is found iteratively. Converged $k_b\approx0.851$, giving $$S_e=k_a k_b S_e'=0.781(0.851)(54)=35.9\ \text{ksi}.$$
  3. DE-Goodman diameter. With $K_f=K_{fs}=1$ and $M_m=0$, $$d=\left\{\frac{16n}{\pi}\!\left[\frac{\sqrt{4M_a^2+3T_a^2}}{S_e}+\frac{\sqrt{3T_m^2}}{S_{ut}}\right]\right\}^{1/3}.$$ Substituting ($M_a=4000$, $T_a=T_m=1000$ lb·in; $S_e=35{,}900$, $S_{ut}=108{,}000$ psi), $$d=\left\{\frac{16(2)}{\pi}\!\left[\frac{8185}{35{,}900}+\frac{1732}{108{,}000}\right]\right\}^{1/3}=\boxed{1.36\ \text{in}}\ \Rightarrow\ \text{specify }d=1\tfrac38\ \text{in }(1.375).$$
  4. Torsional deflection. For $d=1.375$ in, $J=\pi d^4/32=0.351\ \text{in}^4$, $G=11.5\times10^6$ psi. Taking the peak torque over the 18 in drive length, $$\theta=\frac{T L}{GJ}=\frac{2000(18)}{11.5\times10^6(0.351)}=0.0089\ \text{rad}=\boxed{0.51^\circ}.$$
  5. Bending deflection. With $I=\pi d^4/64=0.175\ \text{in}^4$, $E=30\times10^6$ psi, the deflection of the overhung end (overhang $a=4$ in, span $L=14$ in) is $$\delta=\frac{P a^2(L+a)}{3EI}=\frac{1000(4^2)(18)}{3(30\times10^6)(0.175)}=\boxed{0.018\ \text{in}}.$$
Final results — Problem 5
QuantityValue
Required diameter (DE-Goodman, $n=2$)1.36 in → specify 1⅜ in
Maximum torsional twist0.0089 rad (0.51°)
Maximum bending deflection0.018 in