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22-Mec-A2 Kinematics and Dynamics of Machines · Undated paper

Question 3 of 7: High-speed radial cam — motion program and pressure angle

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

Notes on this paper

Paper: National Exams — 16-Mec-A2 Kinematics and Dynamics of Machines · 3 hours, open book · Rubric: answer Q1 (compulsory) plus any four of Q2–Q7. Marks: 20 each. All seven questions are solved here.

Reference texts (subject). R. L. Norton, Design of Machinery, 6th ed. (mobility Ch. 2, synthesis Ch. 3, velocity/acceleration Ch. 6–7, cams Ch. 8, epicyclic trains §9.6–9.9, balancing Ch. 13); Uicker, Pennock & Shigley, Theory of Machines and Mechanisms, 5th ed.; C. E. Wilson & J. P. Sadler, Kinematics and Dynamics of Machinery, 3rd ed.; S. S. Rao, Mechanical Vibrations, 6th ed. (Part B multi-DOF torsional Ch. 6, impact Ch. 1).

Note — figures printed without dimensions. Every figure on this paper is printed without dimensions, and several carry inconsistent numbers (e.g. Q4 shows two conflicting tooth-count sets, and a ring $N_3=20$ cannot mesh a sun $N_1=32$; Q5 prints $AG_3=BG_3=82.5$ mm with $AB=179$ mm, a geometrically impossible triangle). The methods below are exact and complete; where a numerical answer depends on figure geometry (Q2, Q5) or on internally inconsistent data (Q4), the adopted reading is stated explicitly and the value is flagged as representative. Scale-free results (mobility, Grashof class, angular-velocity ratios, transmission-angle location, mode shapes, non-dimensional natural frequencies) are exact regardless of the figure dimensions.

Question 3: High-speed radial cam — motion program and pressure angle (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. Radial (in-line, translating) roller-follower cam. Follower displacement $s(\theta)=h\sin\theta$ with $h=10$ mm over the rise–return interval $\theta\in[0^\circ,180^\circ]$; cam speed $N=3600$ rpm (constant), i.e. $\omega=N\cdot 2\pi/60$.

Find. (I) $s,v,a$ program with peak values; (II) a base-circle radius $R_b$ that limits the maximum pressure angle to $20^\circ$.

Approach. Differentiate $s(\theta)$ once with respect to time (using $\dot\theta=\omega$) for velocity and twice for acceleration; then apply the in-line roller-follower pressure-angle relation $\tan\phi=(ds/d\theta)/(R_b+s)$ and size $R_b$ for $\phi_{\mathrm{max}}\le20^\circ$.

  1. Cam angular speed. $\displaystyle \omega=\frac{2\pi N}{60}=\frac{2\pi(3600)}{60}=\boxed{376.99\ \text{rad/s}}.$
  2. Displacement. $s(\theta)=10\sin\theta$ mm; it rises to $s_{\mathrm{max}}=10$ mm at $\theta=90^\circ$ and returns to $0$ at $\theta=180^\circ$.
  3. Velocity. $\displaystyle v=\frac{ds}{dt}=\frac{ds}{d\theta}\,\omega=10\,\omega\cos\theta$. Peak at $\theta=0$ (and $180^\circ$): $$v_{\mathrm{max}}=10\,\omega=10(376.99)=3769.9\ \text{mm/s}=\boxed{3.77\ \text{m/s}}.$$
  4. Acceleration. $\displaystyle a=\frac{d^2s}{dt^2}=-10\,\omega^2\sin\theta$. Peak magnitude at $\theta=90^\circ$: $$a_{\mathrm{max}}=10\,\omega^2=10(376.99)^2=1.421\times10^{6}\ \text{mm/s}^2=\boxed{1421\ \text{m/s}^2\ (\approx145\,g)}.$$ The very large acceleration is the reason the problem stresses “high-speed” — inertia loading dominates the cam design.
  5. Pressure angle. For an in-line roller follower, $\tan\phi=\dfrac{ds/d\theta}{R_b+s}=\dfrac{10\cos\theta}{R_b+10\sin\theta}$ (with $ds/d\theta$ in mm/rad). Since the numerator is largest and the denominator smallest at $\theta=0^\circ$ (and $180^\circ$), the maximum pressure angle is $$\phi_{\mathrm{max}}=\arctan\!\frac{10}{R_b}.$$
  6. Size the base circle for $\phi_{\mathrm{max}}\le20^\circ$. Set $\arctan(10/R_b)=20^\circ$: $$R_b=\frac{10}{\tan 20^\circ}=\boxed{27.5\ \text{mm}}.$$ For comparison a $30^\circ$ limit would allow $R_b=10/\tan30^\circ=17.3$ mm. So if the chosen base circle gives $\phi_{\mathrm{max}}>20^\circ$, the corrective action is to increase the base-circle (prime-circle) radius to $\ge27.5$ mm (equivalently add follower offset, or spread the same lift over a larger cam angle); enlarging $R_b$ reduces $\phi$ everywhere without changing the lift program.
s s=10 sinθ, peak 10 mm @90° v v=10ωcosθ, ±3.77 m/s at ends a a=−10ω²sinθ, |a|max 1421 m/s² @90° θ: 0→180°
Fig. 3. Follower $s$–$v$–$a$ diagrams over the $0^\circ$–$180^\circ$ program: displacement a half-sine hump, velocity a cosine (zero at mid-lift, peak at the ends), acceleration a negative half-sine (peak magnitude at mid-lift).
QuantityValue
Cam speed $\omega$376.99 rad/s
Max lift $s_{\mathrm{max}}$10 mm (at 90°)
Max velocity $v_{\mathrm{max}}$3.77 m/s (at 0°, 180°)
Max acceleration $a_{\mathrm{max}}$1421 m/s² ≈ 145 g (at 90°)
Base circle for $\phi_{\mathrm{max}}=20^\circ$$R_b=27.5$ mm