ENGINEERING TOOL

M18 Bolt Torque Chart

Target preload and tightening torque ranges (min–typ–max) for M18 bolts across six property classes and five friction states. K-factor method, basis fully disclosed.

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Torque by Property Class and Friction State

Quick answer: class 8.8 · electro zinc ≈ 263 N·m (232–310); other classes and friction states below.

ClassRp0.2 (MPa)Target preload (kN)Dry / Black
K 0.18–0.22 · N·m
Electro Zinc
K 0.15–0.2 · N·m
Hot-Dip Galv.
K 0.18–0.25 · N·m
Oiled
K 0.12–0.15 · N·m
Wax / PTFE / Anti-seize
K 0.08–0.12 · N·m
4.834045.7165
148–181
140
123–165
181
148–206
107
99–123
82
66–99
8.864086310
279–341
263
232–310
341
279–387
201
186–232
155
124–186
10.9940126.3455
409–500
387
341–455
500
409–569
296
273–341
227
182–273
12.91100147.8532
479–585
452
399–532
585
479–665
346
319–399
266
213–319
A2-7045060.5218
196–240
185
163–218
240
196–272
142
131–163
109
87–131
A4-8060080.6290
261–319
247
218–290
319
261–363
189
174–218
145
116–174

Cell shows the typical value; the small line below is the range (min–max).

Fine-Thread Torque Matrix

Fine-thread series (M18 × 1.5 mm) target preload and tightening torque ranges, same basis as the coarse chart; the fine-thread stress area As follows ISO 898-1:2013 Table 6 (this page takes M18 As = 216 mm²).

ClassRp0.2 (MPa)Target preload (kN)Dry / Black
K 0.18–0.22 · N·m
Electro Zinc
K 0.15–0.2 · N·m
Hot-Dip Galv.
K 0.18–0.25 · N·m
Oiled
K 0.12–0.15 · N·m
Wax / PTFE / Anti-seize
K 0.08–0.12 · N·m
4.834051.4185
167–204
157
139–185
204
167–231
120
111–139
93
74–111
8.864096.8348
314–383
296
261–348
383
314–435
226
209–261
174
139–209
10.9940142.1512
460–563
435
384–512
563
460–640
333
307–384
256
205–307
12.91100166.3599
539–659
509
449–599
659
539–748
389
359–449
299
240–359
A2-7045068245
220–269
208
184–245
269
220–306
159
147–184
122
98–147
A4-8060090.7327
294–359
278
245–327
359
294–408
212
196–245
163
131–196

Cell shows the typical value; the small line below is the range (min–max).

Basis of Calculation & Sources

Torque follows the K-factor (nut factor) method T = K·D·F: D is the nominal diameter and F the target preload = 70% of Rp0.2 × thread stress area (M18 As = 192 mm²). Yield strengths are published values from ISO 898-1 (carbon/alloy steel) and ISO 3506-1 (stainless A2/A4). K follows published empirical ranges per friction condition (Machinery's Handbook; the wax/PTFE/anti-seize band K≈0.10 follows Machine Design test data). The grease/MoS₂ band (K≈0.11) nearly overlaps anti-seize and is available in the calculator instead of a separate column.

Stainless note: A2/A4 austenitic thread pairs gall easily under frictional heating. Always apply anti-seize and follow the Wax/PTFE/Anti-seize column (K≈0.10).

Boundary: this chart is a simplified K-factor estimate, not a full VDI 2230 analysis (which accounts for joint resilience, embedment and assembly method). Friction is the dominant variable — no single torque value exists without its friction state. Always follow the design specification or manufacturer torque table.

FAQ

What is the tightening torque for an M18 class 8.8 bolt?

It depends on the friction state (typical values at 70% of Rp0.2 target preload): oiled ≈ 201 N·m, electro zinc ≈ 263 N·m, hot-dip galvanized ≈ 341 N·m, dry/black ≈ 310 N·m, anti-seize ≈ 155 N·m. See the matrix above for ranges — no single torque value exists without its friction state.

What is the target preload for an M18 bolt?

At 70% of Rp0.2: class 4.8 ≈ 45.7 kN, 8.8 ≈ 86 kN, 10.9 ≈ 126.3 kN; stainless A2-70 ≈ 60.5 kN and A4-80 ≈ 80.6 kN.

Can I use carbon-steel torque values for stainless M18 (A2-70/A4-80)?

No. The classes have different yield strengths (A2-70 = 450 MPa, A4-80 = 600 MPa), so target preloads differ; and stainless thread pairs gall easily — always apply anti-seize and follow the Wax/PTFE/Anti-seize column (K≈0.10).

What basis are these torque values calculated on?

The K-factor method T = K·D·F with target preload = 70% of Rp0.2 × stress area (yield strengths per ISO 898-1 / ISO 3506-1 published values) and K per published empirical friction ranges. Estimated values, not assembly instructions; run a full VDI 2230 analysis for critical joints.

Related References

Disclaimer: This chart is an engineering estimation for selection and budgeting only. It does not constitute assembly instructions or acceptance criteria.

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