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22-Mec-A2 Kinematics and Dynamics of Machines · May 2014

Question 2 of 6: Cycloidal radial cam — motion program, profile & pressure angle

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

Notes on this paper

National Exams, May 2014 — 07-Mec-A2, Kinematics and Dynamics of Machines. 3 hours, OPEN BOOK. Six questions of 20 marks each; candidates answer any FIVE. All SIX are solved in full below (Part A — mechanisms and machine dynamics, Q1–Q4; Part B — mechanical vibration, Q5–Q6).

Reference texts: R. L. Norton, Design of Machinery, 5th ed. (instant centres and mechanical advantage, cam design, gear-train kinematics, linkage balancing); S. S. Rao, Mechanical Vibrations, 6th ed. (impulsive loading, single- and two-degree-of-freedom free and forced response); J. E. Shigley & C. R. Mischke, Mechanical Engineering Design (planetary-train cross-check).

Question 2: Cycloidal radial cam — motion program, profile & 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. Constant cam speed $N=1800\ \text{rpm}$, so $\omega=1800\cdot2\pi/60=188.5\ \text{rad/s}$. Lift $h=25.4\ \text{mm}=0.0254\ \text{m}$. Rise interval $\beta_R=90^\circ=\pi/2$; dwell 90°–180°; fall interval $\beta_F=180^\circ=\pi$. Flat-faced follower.

Find. $s,v,a,j$ for rise and fall; $a_{\mathrm{max}}$ and $j_{\mathrm{max}}$ of the rise; base-circle radius and cam profile; pressure angles at 45° and 270°.

Approach. Write the cycloidal motion law on each segment, differentiate with respect to time via $\theta=\omega t$, evaluate the rise peaks, then size the base circle from the flat-faced curvature condition and generate the profile parametrically.

  1. Cycloidal law — rise ($0\le\theta\le\beta_R$). With $\phi=\theta$, $$s=h\!\left[\frac{\phi}{\beta_R}-\frac{1}{2\pi}\sin\frac{2\pi\phi}{\beta_R}\right],\quad v=\frac{h\omega}{\beta_R}\!\left[1-\cos\frac{2\pi\phi}{\beta_R}\right],$$ $$a=\frac{2\pi h\omega^2}{\beta_R^{2}}\sin\frac{2\pi\phi}{\beta_R},\quad j=\frac{4\pi^{2}h\omega^{3}}{\beta_R^{3}}\cos\frac{2\pi\phi}{\beta_R}.$$
  2. Cycloidal law — fall ($180^\circ\le\theta\le360^\circ$, $\psi=\theta-180^\circ$, interval $\beta_F$). $$s=h\!\left[1-\frac{\psi}{\beta_F}+\frac{1}{2\pi}\sin\frac{2\pi\psi}{\beta_F}\right],\quad v=-\frac{h\omega}{\beta_F}\!\left[1-\cos\frac{2\pi\psi}{\beta_F}\right],$$ $$a=-\frac{2\pi h\omega^{2}}{\beta_F^{2}}\sin\frac{2\pi\psi}{\beta_F},\quad j=-\frac{4\pi^{2}h\omega^{3}}{\beta_F^{3}}\cos\frac{2\pi\psi}{\beta_F}.$$ The dwell (90°–180°) has $s=h$, $v=a=j=0$.
  3. Rise peaks. Cycloidal motion has $a_{\mathrm{max}}$ at $\phi=\beta_R/4$ and $j_{\mathrm{max}}$ at $\phi=0$: $$a_{\mathrm{max}}=\frac{2\pi h\omega^{2}}{\beta_R^{2}}=\frac{2\pi(0.0254)(188.5)^2}{(\pi/2)^2},\qquad j_{\mathrm{max}}=\frac{4\pi^{2}h\omega^{3}}{\beta_R^{3}}.$$ $a_{\mathrm{max}}=2298\ \text{m/s}^2\ (\approx 234g)$, $j_{\mathrm{max}}=1.73\times10^{6}\ \text{m/s}^3$; the peak rise velocity is $v_{\mathrm{max}}=2h\omega/\beta_R=6.10\ \text{m/s}$.
  4. Base-circle design (flat-faced follower). The follower face must never lose contact, so the radius of curvature $\rho=R_0+s+s''$ must stay positive, where $s''=d^2s/d\theta^2$. The most negative value of $s+s''$ over the cycle is $-41.7\ \text{mm}$ (near $\phi=3\beta_R/4$ on the rise), hence $R_0>41.7\ \text{mm}$. Choose $R_0=45\ \text{mm}$.
  5. Cam profile. For a radial flat-faced follower the profile is generated by $$x(\theta)=(R_0+s)\sin\theta+\frac{ds}{d\theta}\cos\theta,\qquad y(\theta)=(R_0+s)\cos\theta-\frac{ds}{d\theta}\sin\theta,$$ traced over $0\le\theta\le360^\circ$ (Figure 2.2). The required follower face width is set by the maximum offset of the contact point, $\max|ds/d\theta|=2h/\beta_R=32.3\ \text{mm}$ on the rise side.
  6. Pressure angles. For a flat-faced follower the transmitted force is always normal to the flat face, i.e. always along the follower axis, so the pressure angle is identically zero: $\alpha(45^\circ)=\alpha(270^\circ)=0^\circ$, and indeed $\alpha=0^\circ$ at every cam angle.
s (mm)RISEDWELLFALLv (m/s)a (m/s²)j (m/s³)0°90°180°270°360°Cycloidal motion program (cam angle 0–360°): displacement, velocity, acceleration, jerk.
Figure 2.1 — cycloidal motion program over a full revolution: displacement, velocity, acceleration and jerk. The rise (0–90°) shows the characteristic sinusoidal acceleration returning to zero at both ends.
Oflat-faced followerbase R₀=45Cam profile for the flat-faced follower (base circle R₀ = 45 mm, cam CCW).
Figure 2.2 — generated cam profile for the flat-faced follower (base circle R₀ = 45 mm, cam turning CCW).
QuantityValue
Cam speed $\omega$188.5 rad/s
Rise max acceleration $a_{\mathrm{max}}$2298 m/s² (≈234g)
Rise max jerk $j_{\mathrm{max}}$1.73×10⁶ m/s³
Rise max velocity $v_{\mathrm{max}}$6.10 m/s
Base-circle radius $R_0$45 mm (min 41.7 mm)
Pressure angle (45°, 270°)0° (flat-faced follower)
Design comment. On the pressure-angle criterion the flat-faced follower is ideal — $\alpha=0^\circ$ everywhere, so there is no transverse thrust and no risk of jamming. The governing limits therefore shift to (i) the minimum radius of curvature (which sets $R_0>41.7$ mm to avoid a cusp/undercut) and (ii) the very high inertia loading: a 90° cycloidal rise at 1800 rpm gives $a_{\mathrm{max}}\approx234g$, so the follower spring pre-load and Hertzian contact stress must be checked, or the rise angle widened, before the design is accepted.