22-Mec-A2 Kinematics and Dynamics of Machines · May 2017
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Reference texts (subject). R. L. Norton, Design of Machinery, 6th ed. (mobility Ch. 2, cams Ch. 8, epicyclic/compound 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, Ch. 3 base excitation, Ch. 6 multi-DOF torsional).
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. $\omega_i=1500$ rpm (CCW viewed from the output end); target $\omega_o=39$ rpm, i.e. a reduction of $1500/39=38.46\!:\!1$; one common module $m$ and one pressure angle (take $20^\circ$ full depth).
Find. the general expression $\omega_o(\omega_i,N_k)$, and tooth numbers $N_1,N_2,N_{2'},N_3,N_4$ satisfying constraints (i)–(iv).
The exam calls the unit a “2-stage PGT” and the drawing bears that out. Three features settle it, all measurable on the printed figure:
So: sun 1 in, ring 3 fixed, compound planet 2–2′ on free carrier H, ring 4 out — a two-stage (three-central-member, 3K) epicyclic. Stage 1 is the meshes $1\!-\!2\!-\!3$; stage 2 is the mesh $2'\!-\!4$.
Use the Willis (relative-to-carrier) equation: viewed from the arm, an epicyclic becomes an ordinary train.
Stage 1 — from sun 1 to ring 3 through planet 2 (one external mesh, then one internal mesh):
$$\frac{\omega_3-\omega_H}{\omega_1-\omega_H}=\left(-\frac{N_1}{N_2}\right)\left(+\frac{N_2}{N_3}\right)=-\frac{N_1}{N_3}.$$
Ring 3 is held, $\omega_3=0$, which gives the carrier speed
$$\omega_H=\omega_1\,\frac{N_1}{N_1+N_3},\qquad \omega_1-\omega_H=\omega_1\,\frac{N_3}{N_1+N_3}.$$
Planet speed, from the same first-stage mesh, $\dfrac{\omega_2-\omega_H}{\omega_1-\omega_H}=-\dfrac{N_1}{N_2}$.
Stage 2 — the compound planet turns as one body ($\omega_{2'}=\omega_2$) and drives ring 4 through an internal mesh:
$$\frac{\omega_4-\omega_H}{\omega_{2'}-\omega_H}=+\frac{N_{2'}}{N_4}.$$
Substituting the previous two lines into this one and collecting $\omega_1$:
$$\boxed{\;\frac{\omega_o}{\omega_i}=\frac{\omega_4}{\omega_1}=\frac{N_1}{N_1+N_3}\left(1-\frac{N_3\,N_{2'}}{N_2\,N_4}\right)\;}$$
The bracket is the signature of the two-stage design: the output is the small difference between the carrier motion and what the second ring takes back from it, which is how such a compact train reaches a 38:1 reduction with only three meshes.
With one module $m$, pitch radii are $r=\tfrac{m}{2}N$. The first stage is coaxial only if the sun, planet and ring radii close on the same centre:
$$r_3=r_1+2r_2\;\Longrightarrow\; \boxed{N_3=N_1+2N_2}\qquad\text{(the first-stage geometric constraint).}$$
The second stage must put planet 2′ on the same planet shaft, i.e. at the same carrier radius $r_1+r_2$, so
$$r_4=r_1+r_2+r_{2'}\;\Longrightarrow\; N_4=N_1+N_2+N_{2'}.$$
Searching integer sets that satisfy both coaxial conditions and hit $39$ rpm gives a clean solution:
$$N_1=26,\quad N_2=25,\quad N_{2'}=29,\quad N_3=76,\quad N_4=80.$$
Intermediate speeds, useful for bearing and shaft sizing:
$$\omega_H=1500\frac{26}{102}=382.4\ \text{rpm (same sense as the input)},\qquad \omega_2=\omega_{2'}=\omega_H-\frac{26}{25}(\omega_1-\omega_H)=-780.0\ \text{rpm}.$$
$$\boxed{\;N_1{=}26,\ N_2{=}25,\ N_{2'}{=}29,\ N_3{=}76,\ N_4{=}80\ \Rightarrow\ \omega_o=-39.0\ \text{rpm (reversed)},\ \text{error }0.0\%\;}$$
As a design note the train also assembles with equally spaced planets: $(N_1+N_3)/n_p=102/n_p$ is an integer for $n_p=3$, and the adjacency check $\sin(\pi/3)=0.866>(N_{2'}+2)/(N_1+N_2)=31/51=0.608$ is satisfied, so three compound planets can be fitted — sharing the load three ways at the 38:1 reduction the rolling mill needs.
| Quantity | Value |
|---|---|
| Device read from the schematic | 2-stage epicyclic: sun 1 in, fixed ring 3, compound planet 2–2′ on free carrier H, ring 4 out |
| General expression | $\dfrac{\omega_o}{\omega_i}=\dfrac{N_1}{N_1+N_3}\left(1-\dfrac{N_3N_{2'}}{N_2N_4}\right)$ |
| First-stage geometric constraint | $N_3=N_1+2N_2$ (and $N_4=N_1+N_2+N_{2'}$) |
| Tooth numbers | $N_1{=}26,\ N_2{=}25,\ N_{2'}{=}29,\ N_3{=}76,\ N_4{=}80$ |
| Carrier / planet speeds | $\omega_H=382.4$ rpm, $\omega_2=\omega_{2'}=-780.0$ rpm |
| Output speed | $-39.0$ rpm (reversed; $0.0\%$ error) |
| Mating ratios (all hunting) | $25/26$, $76/25$, $80/29$; $\gcd=1$ each |