Shaft Design Calculator

ASME Shaft Design Minimum diameter under combined bending & torsion
Transmitted (mean) torque
Maximum resultant bending moment
τ = min(0.30·Sy, 0.18·Sut)
Keyseat reduces the allowable by 25%

Formula & Engineering Reference

d = [ (16 / πτ) · √( (CmM)² + (CtT)² ) ]1/3

Based on the maximum-shear-stress theory of failure for a solid circular shaft under combined bending and torsion.

SymbolVariableUnit (SI)
dMinimum solid shaft diameterm
τAllowable shear stress (effective)Pa
MBending momentN·m
TTorqueN·m
CmCombined shock/fatigue factor — bending
CtCombined shock/fatigue factor — torsion

Allowable shear stress: τ = min(0.30·Sy, 0.18·Sut), reduced 25% with a keyway.

Equivalent twisting moment: Te = √( (CmM)² + (CtT)² ), so d = (16 Te / πτ)1/3.

Rotating shaft: T = 500 N·m, M = 300 N·m, τ = 40 MPa, steady load (Cm = 1.5, Ct = 1.0), no keyway.

Te = √((1.5×300)² + (1.0×500)²) = √(450² + 500²) = 672.7 N·m.

d = [16 × 672,700 / (π × 40)]1/3 = (85,640)1/3 = 44.1 mm. Round up to a standard 45 mm shaft, giving a factor of safety of (45/44.1)³ ≈ 1.06 over the rounded size.

Solid circular shaft. The equation is for a solid round shaft. For a hollow shaft, divide the right-hand side by (1 − k⁴), where k = di/do.

The allowable already carries a margin. Setting τ = min(0.30·Sy, 0.18·Sut) builds in a safety factor against yield and ultimate. The extra FoS shown here is only the bonus from rounding up to a standard size.

Cm and Ct reflect how the load is applied. Steady belt or gear drives sit near 1.5/1.0; reciprocating machinery, sudden engagements, and heavy shock push them higher. Choosing the factors honestly matters more than decimal precision in the inputs.

Sizing, not final fatigue design. This gives an excellent first diameter. Critical rotating shafts should then get a full fatigue check (Soderberg/Goodman) with stress-concentration factors at every shoulder, fillet, and keyway, plus surface and size factors.

Check deflection and critical speed too. A shaft strong enough in stress can still fail on excessive deflection (misaligning bearings and gears) or by running near a critical speed. Verify lateral and torsional stiffness separately for long or high-speed shafts.

d = [(16/πτ)·√((Cm·M)² + (Ct·T)²)]^(1/3), from the maximum-shear-stress theory for a solid shaft under combined bending and torsion. Cm and Ct are shock/fatigue factors on the bending moment and torque.

The smaller of 0.30·Sy or 0.18·Sut for the shaft material, reduced 25% if there is a keyway. The result already includes a margin against yielding.

Combined shock and fatigue factors on bending and torsion. Steady ≈ 1.5/1.0, minor shock ≈ 2.0/1.5, heavy shock ≈ 2.5/2.0. They turn nominal static loads into realistic design loads.

Stock shafts, bearings, seals, and couplings come in standard sizes. Rounding up gives an available shaft slightly stronger than the minimum — a small bonus factor of safety. Rounding down would leave it understrength.

Approximately, through the factors and the conservative allowable — ideal for sizing. A rigorous Soderberg/Goodman fatigue check with stress-concentration, surface, and size factors should follow for critical shafts.

This sizes a solid shaft. For a hollow shaft, divide the right side of the equation by (1 − k⁴), k = di/do. Hollow shafts save weight for a small diameter increase.

Shaft Design Engineering Guide

3 topics  •  Combined loading & ASME sizing

A power-transmission shaft rarely sees just one kind of load. It carries torque from whatever it drives, and at the same time it bends under the weight of gears, pulleys, and the belt or mesh forces pulling on them. The shaft has to survive both at once, and as it rotates the bending stress reverses every revolution — which is why fatigue, not a single overload, is what usually kills a shaft. Sizing one is about finding the diameter that handles the combined load with a sensible margin.

The ASME shaft method is the classic, fast way to do that. It rolls the bending moment and torque into a single equivalent load, multiplies them by shock and fatigue factors that reflect how the load is applied, and compares against an allowable shear stress that already carries a safety margin. The result is a minimum diameter you round up to a standard size. This guide explains the combined-loading physics, the factors, and where the method stops and detailed fatigue analysis begins.

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