How to Calculate Gear Contact and Tooth-Root Bending Stress (ISO 6336)
ISO 6336
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Gears fail in two ways: pitting on the tooth flank caused by cyclic Hertzian contact stress, and fatigue cracks at the tooth root caused by bending stress. Both are driven by the transmitted load, the tooth geometry and the material, but they respond differently to changes in module, face width and profile shift — which is why a single-number torque capacity rating is not enough for design. You need two separate stress checks, each against a material fatigue limit, to know whether a gear pair will survive its service life.
ISO 6336 is the international standard that defines both checks. Part 2 governs surface durability (pitting) via the Hertz contact stress σH and its safety factor SH; Part 3 governs tooth-root bending strength via σF and its safety factor SF. Part 1 defines the shared load factors — KA (application), KV (dynamic), KHβ/KFβ (face load) and KHα/KFα (transverse load) — that scale the nominal tooth load to the actual worst-case contact. The MechanixCalc cylindrical gears calculator applies a simplified version of this chain — ISO 6336-2/-3 (2006) stress and life factors, with Part 1 load factors as noted below — and reports SF and SH. Two of the Part 1 factors are not ISO 6336 expressions: KHβ follows the AGMA/Shigley commercial-enclosed-unit form (you can supply your own ISO 6336-1 Method B/C value to override it), and KHα / KFα follow the §8.3.4 Method B expression with both upper limits (or your own Method A value). The SF ≥ 1.4 and SH ≥ 1.2 minima quoted here are DIN 3990-11 values in common use, not limits ISO 6336 itself specifies.
Tooth-root bending stress (based on ISO 6336-3)
The tooth-root bending stress σF is computed at the 30°-tangent section of the root fillet — the point of highest bending stress for a rack-generated tooth. The nominal specific load Ft/(b·mn) is the tangential force per unit face width per unit module; multiplying by the tooth form factor YF (which captures the lever arm from the load-application point to the root section — in ISO 6336-3 Method B the outer point of single-pair tooth contact, where one tooth alone carries the full load) and the stress-correction factor YS (which captures the stress concentration from the fillet curvature) converts this to a nominal root bending stress. The helix angle factor Yβ and rim factor YB then adjust for oblique contact and thin-rim geometries. Finally the combined load factor KF = KA·KV·KFβ·KFα scales the nominal stress to the actual operating stress.
On the permissible side, ISO 6336-3 §6.1 rates the material's tooth-root fatigue limit σFlim at a reference stress-correction factor YST = 2.0 (corresponding to the standard test gear). The allowable root stress is therefore σFG = σFlim·YST·YNT, where YNT is the life factor (1.0 for N > 3×10⁶ cycles). The safety factor SF = σFG/σF must reach at least 1.4. A common non-conservative mistake is to omit YST from the permissible side while also omitting YSa from the stress side — the two errors partly cancel, but they leave the SF calculation inconsistent with the standard.
σF = (Ft / (b · mn)) · YF · YS · Yβ · YB · KFwhere Ft = tangential force at the reference cylinder (N); b = face width (mm); mn = normal module (mm); YF = tooth form factor (lever-arm geometry, load at the outer point of single-pair contact); YS = stress-correction factor (fillet stress concentration); Yβ = helix angle factor; YB = rim factor (1.0 for solid gears); KF = KA · KV · KFβ · KFα (combined bending load factor)
SF = (σFlim · YST · YNT) / σF [SF_min = 1.4]where σFlim = tooth-root fatigue limit of the material (MPa; typical values calculated from hardness (for quality-controlled material, about the ISO 6336-5 MQ line) — verify against ISO 6336-5 / your supplier); YST = 2.0 (reference stress-correction factor per ISO 6336-3 §6.1); YNT = bending life factor (1.0 for continuous duty / N ≥ 3×10⁶ cycles; > 1 for a finite required life); SF_min = 1.4 (typical target, DIN 3990-11 guide value)
Hertz contact stress — surface durability (based on ISO 6336-2)
The Hertz contact (pitting) stress is calculated at the pitch point using the two-cylinder contact model, then transformed to the inner single-pair contact point via the single-tooth-contact factors ZB (pinion, point B) and ZD (gear, point D). For spur gears with εα ≤ 2 — where only one tooth pair carries the full load at the inner contact point — ZB or ZD can raise the governing flank stress by 3–13% compared with the pitch-point value. For helical gears with full axial overlap (εβ ≥ 1), ZB = ZD = 1 because the inclined contact line means no single-pair loading event occurs.
The zone factor ZH converts the pitch-point curvature into the equivalent radius ratio needed by the Hertz formula; its value is determined by the operating (working) transverse pressure angle αtw and the base helix angle βb. For a standard spur gear (αn = 20°, no profile shift, β = 0°), ZH ≈ 2.495. The elasticity factor ZE = 189.8 MPa^0.5 applies to a steel–steel pair (E = 206 GPa, ν = 0.3). The contact-ratio factor Zε shares the load across simultaneously meshing teeth; for spur meshes it equals √((4−εα)/3), which is about 0.89 for a typical contact ratio of 1.64. The helix factor Zβ = 1/√(cos β), on the reference helix angle β accounts for the oblique contact line in helical gears (1.0 for spur).
σH = ZH · ZE · Zε · Zβ · √( Ft · K / (b · d1) · (u + 1) / u )where ZH = zone factor (geometry of the pitch-point contact); ZE = elasticity factor (MPa^0.5); Zε = contact-ratio factor; Zβ = helix factor; Ft = tangential force (N); K = KA · KV · KHβ · KHα (combined contact load factor); b = face width (mm); d1 = pinion reference diameter (mm); u = gear ratio z2/z1
SH = (σHlim · ZNT) / σH [SH_min = 1.2]where σHlim = allowable contact stress / material contact fatigue limit (MPa; typical values calculated from hardness (for quality-controlled material, about the ISO 6336-5 MQ line) — verify against ISO 6336-5 / your supplier); ZNT = pitting life factor (1.0 for continuous duty; > 1 for a finite required life N_L, ISO 6336-2 — for through/case-hardened steels the conservative no-pitting line is used); SH_min = 1.2 (typical target, DIN 3990-11 guide value)
Load factors KA, KV, KHβ and KHα
The load factors are the bridge between the nominal transmitted load and the actual worst-case tooth load that the stress formulas must be evaluated at. KA (application factor) accounts for external shock and inertia from the driven machine; typical values range from 1.0 (uniform electric-motor drive, smooth load) to 1.75 (heavy shock). KV (dynamic factor) accounts for the internal dynamic overload caused by mesh-frequency excitation; it depends on the pitch-line velocity, the pinion tooth count and the ISO accuracy grade — lower quality gears at high speed carry a significantly larger KV. KHβ (face-load distribution factor) accounts for misalignment of the contact line across the face width, caused by shaft deflection, bearing clearance and tooth crowning; it is sensitive to the ratio b/d1 and to whether the pinion is symmetrically mounted. KHα (transverse load-sharing factor) accounts for unequal load sharing between simultaneously meshing tooth pairs; by Method B it grows as the base-pitch deviation rises relative to the specific load, up to the limits set by the total contact ratio (for spur gears up to ≈ 1.27 on contact and ≈ 1.41 on bending at εα 1.64); a finer accuracy grade or a heavier specific load brings it towards 1.0. For the bending stress path, KFβ and KFα replace KHβ and KHα using slightly different weighting: ISO 6336-1 defines KFβ = KHβ^NF with the exponent NF = (b/h)²/(1 + b/h + (b/h)²), which is always < 1, so KFβ ≤ KHβ. The simplification KFβ = KHβ is widely quoted and is conservative (it over-states the root face load), but the MechanixCalc calculator applies the faithful ISO 6336-1 exponent rather than the simplification.
KHβ is usually the factor that decides a lightly loaded pair: with unmodified flanks the helix tolerance puts the load on part of the face. Crowned or end-relieved flanks, a mesh adjusted to a checked contact pattern at assembly and a finer accuracy grade lower it; a stiffer shaft lowers it for an overhung pinion. Narrowing the face raises KHβ's share less than it raises the unit load, so it usually lowers SH. Improving the accuracy grade is also the most effective lever for reducing KV at high speed.
Profile shift and its effect on both stresses
Profile shift (addendum modification) with coefficient x moves the generating rack radially outward (positive x) or inward (negative x) when the gear is cut. A positive shift on the pinion increases the tooth thickness at the root — reducing the form factor YF and improving bending strength — and moves the pitch point away from the undercut zone. The penalty is a change in the operating centre distance (when x1 + x2 ≠ 0) and a slight change in the operating pressure angle αtw, both computed by solving the involute equation inv(αtw) = inv(αt) + 2·tan(αn)·(x1+x2)/(z1+z2).
For the contact stress, a positive total shift (x1 + x2 > 0) increases αtw, which raises ZH slightly — a mild debit on pitting. The dominant benefit of profile shift is therefore on the bending side, particularly for pinions with low tooth counts (z1 < 17) where undercut otherwise weakens the root. The calculator applies profile shift across the full geometry chain — pitch diameters, tip/root radii, contact ratio and all stress factors — so both SF and SH reflect the actual shifted geometry.
Worked example
Find the tooth-root bending stress σF and contact stress σH for a spur gear pair: normal module mn = 4 mm, pinion teeth z1 = 20, gear teeth z2 = 40, face width b = 40 mm, no profile shift, material 42CrMo4 (QT), power P = 10 kW, pinion speed n1 = 1 500 rpm, ISO quality grade 8.
Given
- Normal module mn4 mm
- Pinion teeth z120
- Gear teeth z240
- Face width b40 mm
- Helix angle β0° (spur gear)
- Profile shift x1, x20, 0
- Material42CrMo4 QT (σFlim = 300 MPa, σHlim = 785 MPa — typical values calculated from hardness HB 300 (for quality-controlled material, about the ISO 6336-5 MQ line); verify against ISO 6336-5 / your supplier)
- Power P10 kW
- Pinion speed n11 500 rpm
- ISO accuracy gradeQ8
Result
- Pinion pitch diameter d180 mm
- Centre distance a120 mm
- Tangential force Ft1 592 N
- Combined load factor K (contact / bending)≈ 4.78 / ≈ 4.10
- Tooth-root bending stress σF1≈ 134.8 MPa
- Bending safety factor SF1≈ 3.78 (min 1.4)
- Hertz contact stress σH≈ 843 MPa
- Contact safety factor SH≈ 0.69 (min 1.2) — FAIL
- Gear geometry: spur gear (β = 0°), so transverse module mt = mn = 4 mm. Pinion pitch diameter d1 = 4 × 20 = 80 mm; gear pitch diameter d2 = 4 × 40 = 160 mm; gear ratio u = 40/20 = 2; standard centre distance a = (80 + 160)/2 = 120 mm.
- Pinion torque: T1 = P × 9 550 / n1 = 10 × 9 550 / 1 500 ≈ 63.7 N·m.
- Tangential force: Ft = 2 000 · T1 / d1 = 2 000 × 63.7 / 80 ≈ 1 592 N.
- Pitch-line velocity: v = π · d1 · n1 / (60 × 1 000) = π × 80 × 1 500 / 60 000 ≈ 6.28 m/s.
- Load factors: KA = 1.25 (moderate shock); KV ≈ 1.51 (Method C, v = 6.28 m/s, z1 = 20; the tool reads the entered grade 8 1.5 grades coarser for K_V, so its K1 is not below either standard's for that grade — the conservative side). Face-load factor by ISO 6336-1 Method C for unmodified flanks as mounted: the grade-8 helix tolerance f_Hβ ≈ 19.0 µm (+ 0.4 µm pinion body deflection) gives F_βx ≈ 19.5 µm, less the running-in allowance y_β ≈ 7.9 µm → F_βy ≈ 11.6 µm; at the light unit load F_m/b = Ft·KA·KV/b ≈ 74.9 N/mm the load sits on part of the face, KHβ = √(2·F_βy·c_γβ/(F_m/b)) ≈ 2.04 (the AGMA enclosed-unit estimate, 1.18, would be about half as severe). Transverse factors by ISO 6336-1 Method B (F_tH/b ≈ 154 N/mm, grade-8 pitch deviation ≈ 19 µm): KHα = KFα ≈ 1.25 (below the upper limit 3/(4 − εα) ≈ 1.27). Combined CONTACT factor K = 1.25 × 1.51 × 2.04 × 1.25 ≈ 4.78. The BENDING factor is NOT the same number: ISO 6336-1 defines KFβ = KHβ^NF with NF = (b/h)²/(1 + b/h + (b/h)²) < 1, which gives KFβ ≈ 1.75 here, so KF = 1.25 × 1.51 × 1.75 × 1.25 ≈ 4.10.
- Bending stress factors (ISO 6336-3 Method B, z = 20, x = 0, load at the outer point of single-pair contact, tool fillet 0.20·mn): tooth form factor YF1 ≈ 1.72; stress-correction factor YS1 ≈ 1.93; helix factor Yβ = 1.0 (spur); rim factor YB = 1.0 (solid gear). Product YF1 · YS1 · Yβ · YB = 1.72 × 1.93 × 1.0 × 1.0 ≈ 3.31.
- Tooth-root bending stress: σF1 = (Ft / (b · mn)) · YF1 · YS1 · KF = (1 592 / (40 × 4)) × 3.31 × 4.10 ≈ 9.95 × 3.31 × 4.10 ≈ 134.8 MPa.
- Bending safety factor: SF1 = (σFlim · YST · YNT) / σF1 = (300 × 2.0 × 0.85) / 134.8 ≈ 3.78 — well above SF_min = 1.4 (YNT = 0.85: continuous duty, rated at 10¹⁰ cycles on the ISO 6336 critical-service long-life line).
- Contact stress factors (ISO 6336-2, spur αtw = 20°): zone factor ZH ≈ 2.495; elasticity factor ZE = 189.8 MPa^0.5; transverse contact ratio εα ≈ 1.64 → contact-ratio factor Zε = √((4 − 1.64)/3) ≈ 0.888; helix factor Zβ = 1.0 (spur).
- Hertz contact stress (pitch point): σH = ZH · ZE · Zε · Zβ · √(Ft · K / (b · d1) · (u + 1)/u) = 2.495 × 189.8 × 0.888 × 1.0 × √(1 592 × 4.78 / (40 × 80) × 3/2) ≈ 420.4 × √(3.567) ≈ 420.4 × 1.889 ≈ 794.1 MPa. The engine also applies the ISO 6336-2 single-pair contact factor ZB ≈ 1.06 for this spur geometry, giving σH ≈ 843 MPa.
- Contact safety factor: SH = σHlim · ZNT · ZL · ZV · ZR / σH = 785 × 0.85 × 1.0 × 0.974 × 0.897 / 843 ≈ 0.69 — below 1.0, so this pair FAILS on pitting (ZV and ZR are the ISO 6336-2 velocity and roughness factors for v = 6.28 m/s and hobbed / shaved flanks Rz 6 µm, the usual finish of a through-hardened gear; ground flanks at Rz 3 µm give SH ≈ 0.77; ZNT = 0.85 on the critical-service long-life line (1.0 only with optimum material, lubrication and manufacturing); ZL = 1 for ISO VG 220). The face-load factor decides it: crowned flanks or a mesh adjusted to a checked contact pattern lower KHβ, and a case-hardened pair carries far more. With the AGMA KHβ 1.18 and the flat 1.0 life line the same pair read about 1.06 — what an unmodified, lightly loaded grade-8 mesh hides is how little of the face carries the load.
Illustrative example — the steps are rounded for readability, so they land within about 0.5 % of the engine. Run through the MechanixCalc gear calculator, these inputs give σF1 = 134.82 MPa, SF1 = 3.783, σH = 843.11 MPa and SH = 0.691. Real designs require the actual KA for the machine type, the material certificate σFlim/σHlim, and a complete load spectrum before safety factors can be accepted.
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Frequently asked questions
Which standard governs gear tooth-root bending and contact stress?
ISO 6336 is the international standard. Part 2 covers surface durability (pitting) via the Hertz contact stress σH and safety factor SH; Part 3 covers tooth-root bending strength via σF and safety factor SF. Part 1 defines the shared load factors (KA, KV, KHβ, KHα). The North American equivalent is AGMA 2001 / 2101, which gives comparable results but uses different notation and factor definitions. The MechanixCalc gear calculator applies ISO 6336-2/-3 (2006) stress and life factors in simplified form, with KHβ per AGMA 2001-D04 / Shigley.
What is the minimum safety factor for gears under ISO 6336?
ISO 6336 leaves minimum safety factors to agreement; typical targets (DIN 3990-11 guide values) are SF_min = 1.4 for tooth-root bending and SH_min = 1.2 for Hertz contact (pitting). Note that the contact safety factor is not a simple factor on stress: because σH appears as a stress while pitting life scales with σH², an SH of 1.2 corresponds to a life ratio of 1.2² = 1.44. For critical applications (continuous duty, consequences of failure) many designers use higher targets such as SF ≥ 1.6 and SH ≥ 1.4, confirmed by a licensed gear engineer.
Why does the gear form factor YF matter for bending strength?
YF captures the bending lever arm from the point where the load is applied to the critical root section, relative to the root thickness. A gear with fewer teeth has a root that narrows toward the base (the involute flanks curve in), so the root section is thinner relative to the lever arm and YF is larger — small pinions are weaker in bending per unit load than gears with many teeth, all else equal. Positive profile shift thickens the root and lowers YF, improving bending margin. YF must always be used together with the stress-correction factor YS (fillet stress concentration) to give the correct root stress; omitting YS while also omitting YST from the permissible side produces a partly-cancelling but non-conservative SF estimate.
How does face width affect contact stress versus bending stress?
Increasing face width b reduces both σF and σH — both formulas have b in the denominator. For σF, the specific load Ft/(b·mn) drops directly with b. For σH, the term √(Ft·K/(b·d1)) drops as 1/√b. However, a wider face also increases the face-load distribution factor KHβ (because misalignment effects grow with b), which partly offsets the gain. Beyond a ratio of roughly b/d1 ≈ 1.0–1.2, the KHβ penalty can eliminate the benefit of additional width, so there is a practical optimum face width for a given shaft and support stiffness.
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