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22-Mec-A2 Kinematics and Dynamics of Machines · December 2019

Question 4 of 8: Shaking force and balancing of a 3‑cylinder single‑plane engine

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).

Question 4 — Shaking force and balancing of a 3‑cylinder single‑plane engine (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.

Crank radius $r$0.06 mConnecting rod $l$0.6 m ⇒ $n=l/r=10$
Crank speed $\omega$100 rad/s (ccw)Reciprocating mass/cyl $m$2.5 kg
Cylinder axes$0^\circ,120^\circ,240^\circ$Rotating massesalready balanced

Find. Unbalanced shaking force at the three crank–centreline positions; a balancing scheme; residual force; effectiveness.

Cyl 1Cyl 2Cyl 3crank rF₁=2250 Ncrank shown coincident with Cyl 1 (θ=0)
Three cylinders $120^\circ$ apart on a single crankpin. When the crank aligns with a cylinder axis, that cylinder is at TDC and its inertia force is maximal along its own centreline.

Approach. Each cylinder’s reciprocating inertia force acts along its own centreline with magnitude $m\omega^2 r(\cos\phi + \tfrac1n\cos 2\phi)$, $\phi$ measured from that cylinder’s TDC. Sum the three force vectors; the primary ($\cos\phi$) terms and secondary ($\cos2\phi$) terms each collapse to a constant‑magnitude rotating resultant.

  1. Force scale. $m\omega^2 r = (2.5)(100)^2(0.06)=\boxed{1500\ \text{N}}$. Each cylinder’s axial inertia force is $F_i = 1500\left(\cos\phi_i + \tfrac{1}{10}\cos2\phi_i\right)$ N, along axis $\hat u_i$ at $\alpha_i\in\{0^\circ,120^\circ,240^\circ\}$, with $\phi_i=\theta-\alpha_i$.
  2. Primary resultant. Summing $\sum_i 1500\cos(\theta-\alpha_i)\,\hat u_i$ over three axes $120^\circ$ apart gives a vector of constant magnitude that rotates with the crank: $$F_{p}=\tfrac{N}{2}\,m\omega^2 r=\tfrac{3}{2}(1500)=\boxed{2250\ \text{N}},$$ independent of $\theta$ — a “direct” rotating primary force (verified at $\theta=0^\circ,30^\circ,60^\circ,90^\circ$: all 2250 N).
  3. Secondary resultant. The $\tfrac1n\cos2\phi$ terms sum, for three equally‑spaced axes, to another constant‑magnitude vector rotating at $2\omega$ (in the opposite sense): $$F_{s}=\tfrac{N}{2}\,\frac{m\omega^2 r}{n}=\tfrac{3}{2}\frac{1500}{10}=\boxed{225\ \text{N}}.$$
  4. (i) Unbalanced shaking force at a centreline. When the crank coincides with a cylinder axis ($\theta=0^\circ$, $120^\circ$ or $240^\circ$), the primary and secondary resultants both point along that same axis and add directly: $$F_{\text{shake}}=F_p+F_s=2250+225=\boxed{2475\ \text{N}}$$ — the same magnitude at all three centreline positions (by symmetry).
  5. (ii) Balancing scheme. Because the primary is a pure rotating vector (unlike an in‑line engine, where the primary oscillates along one line), it is cancelled completely by a single rotating counterweight on the crankshaft, placed opposite the crank with $$m_c r_c = \tfrac{3}{2} m r = 1.5(2.5)(0.06)=\boxed{0.225\ \text{kg}\cdot\text{m}}$$ (e.g. 3.75 kg at 60 mm, or a lighter mass at a larger radius). After this counterweight the primary is zero at every crank angle, leaving only the secondary: $$F_{\text{shake,balanced}}=F_s=\boxed{225\ \text{N}}\ \text{(constant, rotating at }2\omega).$$ To remove the secondary as well would require two counter‑rotating balance shafts spinning at $2\omega$.
  6. (iii) Effectiveness. The single counterweight removes $2250/2475 = \boxed{90.9\%}$ of the peak shaking force. The $9.1\%$ residual is the second‑order (secondary) force, small because $1/n=0.1$; it is smooth and rotating, so for most service it is acceptable, and if vibration limits demand it, a pair of $2\omega$ balance shafts eliminates it entirely.
QuantityValue
Force scale $m\omega^2 r$1500 N
Primary resultant (rotating with crank)2250 N
Secondary resultant (rotating at $2\omega$)225 N
(i) Unbalanced shaking force at each centreline2475 N
(ii) Counterweight $m_c r_c$0.225 kg·m (opposite crank)
(ii) Balanced residual (secondary only)225 N
(iii) Peak force removed90.9 %