22-Mec-A2 Kinematics and Dynamics of Machines · December 2019
Question 5 of 8: Radial cam‑follower motion design (rise–dwell–fall)
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams, December 2019 — 16‑Mec‑A2 Kinematics and Dynamics of Machines, 3 hours, open book. Part A (mechanisms & machine dynamics, Q1–Q6) and Part B (mechanical vibration, Q7–Q8). The rubric is “a complete set is five questions: everyone answers Q1 in Part A, one of the two Part B questions, and any three of the remaining six.” Every one of the eight questions is solved here.
Reference texts (subject). R. L. Norton, Design of Machinery, 6th ed. (mobility/number synthesis Ch. 2, position & velocity Ch. 4–6, cam design Ch. 8, epicyclic trains §9.6–9.9, balancing Ch. 13); J. J. Uicker, G. R. Pennock & J. E. 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).
Check — incomplete data (please read). Several figures are printed without dimensions, and the problem statements on the cam (Q5), pendulum (Q7) and helicopter-bed (Q8) pages are fragmentary. Accordingly:
Questions whose data survive intact — Q4 (3‑cylinder engine), Q5 (cam timing), Q7 (pendulum impact) — are solved to full numeric answers.
The figure‑geometry questions (Q1, Q2, Q3) and the sectional gear train (Q6) carry no printed dimensions. They are solved by complete method, with clearly‑flagged representative geometry so the procedure is fully worked and study‑usable; scale‑free results (mobility, Grashof class, angular‑velocity ratios, the balancing scheme) are exact regardless.
Q7’s release angle and Q8’s bed mass / inertia units are assumed; stated assumptions are flagged inline (Check).
(a) Displacement programs, cam speed and SVAJ maxima.
Find. Cam speed; the motion programs that minimise (rise) peak acceleration and (fall) peak velocity while obeying the fundamental law; the $s$‑$v$‑$a$‑$j$ maxima; base‑circle / pressure‑angle discussion.
Cam speed and segment angles. One motion cycle = one revolution in $T=0.030$ s, so
$$\omega=\frac{2\pi}{T}=\frac{2\pi}{0.030}=\boxed{209.4\ \text{rad/s}}=2000\ \text{rpm}.$$
The segment angles are $\beta=\omega\,\Delta t$: rise $\beta_r=209.4(0.015)=\pi=\boxed{180^\circ}$, dwell $60^\circ$, fall $\beta_f=209.4(0.010)=\boxed{120^\circ}$ (sum $360^\circ$ ✓).
Fundamental law ⇒ full‑rise/full‑fall smooth programs. The fundamental law of cam design requires $s$, $v$ and $a$ continuous (finite $j$) across the whole cycle, so at each rise–dwell and dwell–fall boundary $v=0$ and $a=0$. Double‑dwell programs (3‑4‑5 polynomial, cycloidal, modified trapezoid, modified sine) all satisfy this. The objective then selects which:
Rise — minimise peak acceleration ⇒ MODIFIED TRAPEZOIDAL. Of the smooth double‑dwell curves it has the lowest acceleration factor $C_a=4.888$ (vs. 5.77 for 3‑4‑5, 6.28 for cycloidal). (Parabolic is lower at 4.0 but has infinite jerk — it violates the fundamental law — so it is disqualified.)
Fall — minimise peak velocity ⇒ MODIFIED SINE. It has the lowest velocity factor $C_v=1.760$ (vs. 1.875 for 3‑4‑5, 2.00 for cycloidal/modified‑trapezoid).
Maxima from the standard factors $v_{\mathrm{max}}=C_v h\omega/\beta$, $a_{\mathrm{max}}=C_a h\omega^2/\beta^2$, $j_{\mathrm{max}}=C_j h\omega^3/\beta^3$.
Rise (modified trapezoid, $\beta_r=\pi$): $C_a=4.888,\ C_v=2.000,\ C_j=61.4$
$$v_{\mathrm{max}}=\boxed{5.33\ \text{m/s}},\quad a_{\mathrm{max}}=\boxed{869\ \text{m/s}^2},\quad j_{\mathrm{max}}\approx\boxed{7.28\times10^{5}\ \text{m/s}^3}.$$
Fall (modified sine, $\beta_f=2\pi/3$): $C_a=5.528,\ C_v=1.760,\ C_j=69.5$
$$v_{\mathrm{max}}=\boxed{7.04\ \text{m/s}},\quad a_{\mathrm{max}}=\boxed{2211\ \text{m/s}^2},\quad j_{\mathrm{max}}\approx\boxed{2.78\times10^{6}\ \text{m/s}^3}.$$
The fall values are larger because $\beta_f<\beta_r$ (the same lift is done in a smaller angle, and $a\propto1/\beta^2$, $j\propto1/\beta^3$).
Sketch. Displacement diagram over one revolution below; $v$, $a$, $j$ follow the standard modified‑trapezoid (rise) and modified‑sine (fall) shapes, each returning to zero at the segment ends so the curves connect smoothly through the dwell.
Follower displacement vs. cam angle: modified‑trapezoid rise ($0$–$180^\circ$), dwell ($180$–$240^\circ$), modified‑sine fall ($240$–$360^\circ$). Peak $v$/$a$/$j$ per segment are boxed above.
(b) Base circle, pressure angle, improvements. For a roller follower the pressure angle is $\phi=\arctan\!\big[(ds/d\psi)/(R_b+s)\big]$; it peaks where the follower velocity is greatest (mid‑rise / mid‑fall) and must be kept below $\approx30^\circ$ to avoid side thrust and jamming. Because the fall is fast ($\beta_f=120^\circ$) its peak $\phi$ is the binding one. If the computed $\phi_{\mathrm{max}}>30^\circ$, the only effective remedy that does not change the motion program is to enlarge the base circle $R_b$ (which reduces $\phi$ everywhere); a larger roller and adequate return‑spring preload (to keep the follower on the cam against the high $a_{\mathrm{max}}=2211$ m/s$^2$ inertia during the fall) complete the check. For a flat‑faced follower the pressure angle is identically $0^\circ$ and the base circle is instead limited by convexity, $R_b+s+s''>0$ everywhere.
Quantity
Rise (mod‑trapezoid)
Fall (mod‑sine)
Segment angle $\beta$
$180^\circ$
$120^\circ$
$v_{\mathrm{max}}$
5.33 m/s
7.04 m/s
$a_{\mathrm{max}}$
869 m/s$^2$
2211 m/s$^2$
$j_{\mathrm{max}}$
$7.28\times10^{5}$ m/s$^3$
$2.78\times10^{6}$ m/s$^3$
Cam speed $\omega=209.4$ rad/s (2000 rpm). Programs chosen to satisfy the fundamental law and the stated objectives (min accel on rise, min velocity on fall).