Spur Gear Pair (Lewis Bending)

stresstorque-power

Verified build 10 relations · 2 identities proven · 3 modeling steps · 3 parity samples

A spur gear pair is the workhorse of parallel-shaft power transmission: two toothed wheels whose pitch circles roll without slipping, trading speed for torque by the ratio of their tooth counts. The planetary gearset folds three of these meshes into one hub; a single external pair is the atom they are built from. Fix the module mm (the tooth size, in mm of pitch diameter per tooth) and the geometry is set: pitch diameter d=mNd = mN, centre distance c=m(Np+Ng)/2c = m(N_p + N_g)/2, and gear ratio

i=NgNp=ωpωgi = \frac{N_g}{N_p} = \frac{\omega_p}{\omega_g}

Power arrives as torque on the pinion and leaves as a single tangential tooth force at the pitch point. Balance moments about the pinion axis — torque against force times pitch radius — and

Wt=2TmNpW_t = \frac{2T}{m\,N_p}

That same WtW_t pushes back on the gear (action–reaction), so both members carry the identical load. This is the power screw trick in rotary form: a torque becomes a force at a radius, exactly as a screw’s torque becomes an axial thrust.

The Lewis equation, and why the pinion is the weak one

Wilfred Lewis (1892) modelled a gear tooth as a cantilever loaded at its tip, and inscribed the largest parabola of uniform strength inside the tooth outline. The root bending stress that falls out is

σb=KvWtbmY\sigma_b = \frac{K_v\,W_t}{b\,m\,Y}

where bb is the face width and YY is the dimensionless Lewis form factor — everything about the tooth’s shape, distilled to one number. YY grows with the number of teeth: a 12-tooth pinion is stubby and sharply curved (Y=0.245Y = 0.245), a 100-tooth gear is nearly a rack and far beefier (Y=0.447Y = 0.447). Because σb1/Y\sigma_b \propto 1/Y, at identical load, module, and material the pinion always carries the higher stress — it has the fewer teeth, so the smaller YY. That is the single most useful fact in gear design: check the pinion; it governs. Dial NpN_p and NgN_g in the widget and watch SFp\mathrm{SF}_p sit stubbornly below SFg\mathrm{SF}_g even when both gears are the same steel.

YY is not a formula. It comes from a graphical layout of the tooth (or its digital equivalent) and is published as a table — Shigley’s Table 14-2, for 20° full-depth teeth with the load near the tip. This page carries that table as cited data with provenance: the widget interpolates linearly between the published tooth counts and refuses (per gear, leaving the rest standing) outside the tabulated range of 12–400 teeth, because there is no published value to stand on. The /verification/ page states exactly what is machine-proven here (the interpolation, the refusal, the algebra) and what rests on citation (the tabulated numbers themselves).

The velocity factor

Real teeth engage a hair out of step, so the load a running mesh feels exceeds the static one. Barth’s empirical velocity factor scales the stress up with pitch-line velocity V=ωpmNp/2V = \omega_p\,m\,N_p/2:

Kv=6.1+V6.1K_v = \frac{6.1 + V}{6.1}

(metric, for cut or milled teeth; the 6.16.1 carries units of m/s). It is a fit, not a theorem — push VV high enough and a banner warns that the fit has left its cited range, the same honesty the belt drive applies to its capstan speed ceiling. Torque, speed, and the tooth bending stress it drives all live on one page here, the way the torsion shaft ties twist to shear.

Try it

Material

T3, bare flat sheet 0.010-0.128 in. thick, AMS 4037 / AMS-QQ-A-250/4 (MIL-HDBK-5J Table 3.2.3.0(b1), p. 3-71)

Bound properties of 2024-T3 aluminum sheet (bare)
sigma_y47 ksidesign min.mil-hdbk-5j
Inputs
N·m
Gear ratio
Centre distance
Pitch-line velocity
m/s
Velocity (Barth) factor
Transmitted (tangential) load
Transmitted power
Pinion Lewis form factor
Gear Lewis form factor
Pinion tooth bending stress
Gear tooth bending stress
Pinion bending safety factor
Gear bending safety factor

3 materials in the database are not listed here: no published value in our cited sources for every property this THING needs.

Materials modeled here: 2024-T3 aluminum sheet (bare) 304 stainless steel 6061-T6 aluminum 7075-T6 aluminum AISI 1045 medium-carbon steel AISI 4340 low-alloy steel (Ni-Cr-Mo) ASTM A36 structural steel (hot-rolled) C26000 Cartridge Brass (70/30) Nylon 6/6 (PA66), unfilled Ti-6Al-4V

Governing relations

i=NgNpi = \frac{N_g}{N_p}

Assumes: external mesh; N_p is the pinion (the smaller, harder-working member); speed ratio is the inverse of the torque ratio for an ideal (lossless) mesh · Valid while: The smaller member of this mesh has fewer teeth than the interference-free minimum for this ratio and pressure angle (Shigley eq 13-11): its flank will be undercut, weakening the tooth and voiding the Lewis form-factor geometry. Add teeth to the small member, raise the pressure angle, or use profile shift.

Source: Budynas, R. G., & Nisbett, J. K., Shigley's Mechanical Engineering Design, 10th ed., McGraw-Hill, 2015 — §13-5/13-7 (involute geometry; interference, eq 13-11), §14-1 (the Lewis bending equation), Table 14-2 (Lewis form factor Y, 20° full-depth, tip load), eq 14-6b (Barth velocity factor, metric).

c=m(Np+Ng)2c = \frac{m\,(N_p + N_g)}{2}

Assumes: standard (non-profile-shifted) teeth on parallel axes; pitch diameter d = m N

Source: Budynas, R. G., & Nisbett, J. K., Shigley's Mechanical Engineering Design, 10th ed., McGraw-Hill, 2015 — §13-5/13-7 (involute geometry; interference, eq 13-11), §14-1 (the Lewis bending equation), Table 14-2 (Lewis form factor Y, 20° full-depth, tip load), eq 14-6b (Barth velocity factor, metric).

V=ωpmNp2V = \frac{\omega_p\, m\, N_p}{2}

Assumes: V is the tangential speed at the pitch circle, radius d_p/2 = m N_p / 2

Source: Budynas, R. G., & Nisbett, J. K., Shigley's Mechanical Engineering Design, 10th ed., McGraw-Hill, 2015 — §13-5/13-7 (involute geometry; interference, eq 13-11), §14-1 (the Lewis bending equation), Table 14-2 (Lewis form factor Y, 20° full-depth, tip load), eq 14-6b (Barth velocity factor, metric).

Kv=6.1+V6.1K_v = \frac{6.1 + V}{6.1}

Assumes: Barth velocity factor for cut or milled profile teeth (Shigley eq 14-6b, metric); the 6.1 carries units of m/s (v_b) — an empirical dynamic-load amplifier, not a first-principles result · Valid while: Barth's linear velocity factor is an empirical fit for cut/milled teeth at moderate pitch-line velocity; here the dynamic amplification K_v exceeds 3 (V above ≈ 12 m/s), where the fit loses its cited meaning and AGMA dynamic-factor methods are preferred.

Source: Budynas, R. G., & Nisbett, J. K., Shigley's Mechanical Engineering Design, 10th ed., McGraw-Hill, 2015 — §13-5/13-7 (involute geometry; interference, eq 13-11), §14-1 (the Lewis bending equation), Table 14-2 (Lewis form factor Y, 20° full-depth, tip load), eq 14-6b (Barth velocity factor, metric).

Wt=2TmNpW_t = \frac{2T}{m\,N_p}

Assumes: tangential tooth load from torque about the pinion axis, W_t = T / (d_p/2); the same W_t acts on both gears at the pitch point (action–reaction)

Source: Budynas, R. G., & Nisbett, J. K., Shigley's Mechanical Engineering Design, 10th ed., McGraw-Hill, 2015 — §13-5/13-7 (involute geometry; interference, eq 13-11), §14-1 (the Lewis bending equation), Table 14-2 (Lewis form factor Y, 20° full-depth, tip load), eq 14-6b (Barth velocity factor, metric).

P=TωpP = T\,\omega_p

Assumes: mechanical power through the mesh; ideal (lossless) transmission

Source: Budynas, R. G., & Nisbett, J. K., Shigley's Mechanical Engineering Design, 10th ed., McGraw-Hill, 2015 — §13-5/13-7 (involute geometry; interference, eq 13-11), §14-1 (the Lewis bending equation), Table 14-2 (Lewis form factor Y, 20° full-depth, tip load), eq 14-6b (Barth velocity factor, metric).

σb,p=KvWtbmYp\sigma_{b,p} = \frac{K_v\, W_t}{b\, m\, Y_p}

Assumes: Lewis equation (metric form σ = K_v W_t / (b m Y)); tooth as a cantilever, load at the tip; static bending only — no surface/contact (pitting) check; that is the AGMA S_c story

Source: Budynas, R. G., & Nisbett, J. K., Shigley's Mechanical Engineering Design, 10th ed., McGraw-Hill, 2015 — §13-5/13-7 (involute geometry; interference, eq 13-11), §14-1 (the Lewis bending equation), Table 14-2 (Lewis form factor Y, 20° full-depth, tip load), eq 14-6b (Barth velocity factor, metric).

σb,g=KvWtbmYg\sigma_{b,g} = \frac{K_v\, W_t}{b\, m\, Y_g}

Assumes: same transmitted load and velocity factor as the pinion; only the form factor Y differs

Source: Budynas, R. G., & Nisbett, J. K., Shigley's Mechanical Engineering Design, 10th ed., McGraw-Hill, 2015 — §13-5/13-7 (involute geometry; interference, eq 13-11), §14-1 (the Lewis bending equation), Table 14-2 (Lewis form factor Y, 20° full-depth, tip load), eq 14-6b (Barth velocity factor, metric).

SFp=σallσb,p\mathrm{SF}_p = \frac{\sigma_{all}}{\sigma_{b,p}}

Assumes: factor of safety on bending strength; σ_all taken as the material yield here (educational)

Source: Budynas, R. G., & Nisbett, J. K., Shigley's Mechanical Engineering Design, 10th ed., McGraw-Hill, 2015 — §13-5/13-7 (involute geometry; interference, eq 13-11), §14-1 (the Lewis bending equation), Table 14-2 (Lewis form factor Y, 20° full-depth, tip load), eq 14-6b (Barth velocity factor, metric).

SFg=σallσb,g\mathrm{SF}_g = \frac{\sigma_{all}}{\sigma_{b,g}}

Assumes: same allowable stress; the gear's larger Y gives it the larger margin at equal geometry

Source: Budynas, R. G., & Nisbett, J. K., Shigley's Mechanical Engineering Design, 10th ed., McGraw-Hill, 2015 — §13-5/13-7 (involute geometry; interference, eq 13-11), §14-1 (the Lewis bending equation), Table 14-2 (Lewis form factor Y, 20° full-depth, tip load), eq 14-6b (Barth velocity factor, metric).

Derivation

Steps marked modeling step are where physics enters by citation — every other line is machine-proven to follow from them, and the cited models are independently re-derived in the test pipeline where possible. See what is and isn't machine-verified.

V=Npmmodωp2V = \frac{N_{p} m_{mod} \omega_{p}}{2}

1. The gears touch at the pitch point, a distance d_p/2 = m·N_p/2 from the pinion axis. That point moves at the pitch-line velocity V = ω_p·(m·N_p/2) — the common rubbing speed the two pitch circles share. — kinematics: pitch-line velocity

Wt=2TNpmmodW_{t} = \frac{2 T}{N_{p} m_{mod}}

2. Resolve the pinion torque into a single tangential tooth force at that same radius: W_t = T / (d_p/2) = 2T/(m·N_p). By action–reaction the identical force pushes back on the gear, so both members carry the same W_t. — statics: tangential force at the pitch circle

Kv=V+vbvbK_{v} = \frac{V + v_{b}}{v_{b}}

3. Real teeth strike each other slightly out of step, so the dynamic load exceeds the static one. Barth's factor K_v = (6.1 + V)/6.1 (metric, cut/milled teeth) is the empirical multiplier that captures this — physics entering by citation, not derivation. — modeling: Barth velocity factor (empirical, Shigley 14-6b) modeling step

σbp=KvWtYpbmmod\sigma_{b p} = \frac{K_{v} W_{t}}{Y_{p} b m_{mod}}

4. Lewis modelled the tooth as a cantilever loaded at its tip; the root bending stress is σ = K_v·W_t/(b·m·Y), where the dimensionless form factor Y encodes the tooth's shape. Y is read from Table 14-2 by tooth count — cited tabulated data, not a formula (see /verification/). — modeling: Lewis bending stress; Y_p from Table 14-2 modeling step

SFpσbp=σySF_{p} \sigma_{b p} = \sigma_{y}

5. The margin is the allowable stress over the working stress. Because Y grows with tooth count, the pinion (fewer teeth → smaller Y_p) always carries the higher stress at equal load and module: the pinion governs the design, even in identical material. — definition: bending factor of safety — the pinion governs modeling step

How it fails

The widget answers one question — will a tooth break in bending? — with the oldest model that does so honestly. Real gears fail in several ways the Lewis equation cannot see, and the biggest one is not bending at all.

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Chains with

Outputs whose SI dimension and quantity kind match another THING's input — the only wires the planner's connectionLegal accepts (invariant 2, computed at build time, not hand-listed). Wire these on the chaining demo.

+ 26 more THINGs its outputs can legally feed (showing the first 8 in course order).

Sources