22-Mec-A2 Kinematics and Dynamics of Machines · December 2018
Question 4 of 7: Two-stage planetary gear train
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Reference texts (subject). R. L. Norton, Design of Machinery, 6th ed. (number synthesis & mobility 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: single-DOF transient Ch. 2–4, multi-DOF Ch. 5–6). Open-book exam; everyone answers Q1, then any three of Part A (Q2–Q5) and one of Part B (Q6–Q7). Every question is solved here.
Find. the general $\omega_o$ expression, its value and direction, and the maximum equally-spaced planet count per stage.
Two-stage epicyclic train (schematic). Stage 1: sun 1 (input) → planet 2 → fixed ring 3, carrier $H$ output. Stage 2: carrier $H$ → planet 5 → fixed ring, sun 4 output. Both rings fixed to the casing; $H$ is the common arm.
Approach. Fix the unknown ring 3 from the coaxial (equal-module) condition; apply the fixed-ring planetary reduction to stage 1 (sun in, carrier out) and the carrier-driven relation to stage 2 (carrier in, sun out); then impose the assembly (equal-spacing) and non-interference limits on the planet count.
Coaxial tooth counts. Equal module gives $N_3=N_1+2N_2=21+2(34)=\boxed{89}$, and the stage-2 fixed ring $N_{r2}=N_4+2N_5=81+2(32)=145$.
Stage 1 (fixed ring, sun in, carrier out).
$$\frac{\omega_H}{\omega_i}=\frac{N_1}{N_1+N_3}=\frac{21}{110}=0.1909\quad(\text{same sense as input}).$$
Stage 2 (fixed ring, carrier in, sun out). From $\dfrac{\omega_4-\omega_H}{0-\omega_H}=-\dfrac{N_{r2}}{N_4}$,
$$\frac{\omega_o}{\omega_H}=1+\frac{N_{r2}}{N_4}=\frac{2(N_4+N_5)}{N_4}=\frac{226}{81}=2.790\ (\text{step-up}).$$
(i) General expression.
$$\boxed{\ \frac{\omega_o}{\omega_i}=\frac{N_1}{N_1+N_3}\cdot\frac{2(N_4+N_5)}{N_4}\ },\qquad N_3=N_1+2N_2.$$
(ii) Output speed.
$$\omega_o=1500\left(\frac{21}{110}\right)\!\left(\frac{226}{81}\right)=\boxed{799\ \text{rpm, CCW}}$$
(same direction as the input; overall $\approx1.88{:}1$ reduction).
(iii) Maximum equally-spaced planets. Two limits apply. Assembly / equal spacing: $(N_{\text{sun}}+N_{\text{ring}})/n_p$ must be an integer. Non-interference: $\sin(\pi/n_p)>(N_{\text{planet}}+2)/(N_{\text{sun}}+N_{\text{planet}})$.
Stage 1: $N_1+N_3=110$ and $(N_2+2)/(N_1+N_2)=36/55=0.655\Rightarrow n_p\le4.4$; the only divisor of $110$ that also clears interference is $n_p=\boxed{2}$.
Stage 2: $N_4+N_{r2}=226=2\times113$ and $(N_5+2)/(N_4+N_5)=34/113=0.301\Rightarrow n_p\le10.3$; the only admissible divisor of $226$ is again $n_p=\boxed{2}$.
So each stage takes at most two equally-spaced planets — the assembly condition, not interference, is the binding constraint for these tooth numbers.
Check: the schematic is read as sun-1 input / fixed ring-3 / carrier-$H$ for stage 1 and carrier-$H$ / fixed ring / sun-4 output for stage 2 (the two rings grounded to the casing). If instead the stage-2 output were taken at the ring, the ratio would change; the interpretation above matches the drawn coaxial output shaft on sun 4.