Related Specifications
Surface Treatments
Certifications
- ISO 9001 - 2015 Certified
- PED 2014/68/EC
- NACE MR0175/ISO 15156-2
- NORSOK M-650
- DFAR
- MERKBLATT AD 2000 W2/W7/W10
Cr-Mo-V (Grade B16) vs Cr-Mo (Grade B7) High-Temperature Bolting - Full Side-by-Side Comparison
ASTM A193 Grade B16 and Grade B7 are the two most commonly specified alloy-steel bolting grades under ASTM A193. Both grades hit the same 125 ksi (860 MPa) minimum tensile strength and 105 ksi (725 MPa) minimum yield strength in the standard 2-1/2 in and under diameter class - so the strength is the same on paper. The structural differences appear when you read past the room-temperature mechanical row into chemistry, tempering, creep, stress rupture, and companion nut selection.
| Element | A193 B7 (% by mass) | A193 B16 (% by mass) | Why it differs |
|---|---|---|---|
| C | 0.37 - 0.49 | 0.36 - 0.47 | Near-identical Cr-Mo alloy base |
| Mn | 0.65 - 1.10 | 0.45 - 0.70 | B16 leaner Mn for tempering control |
| P (max) | 0.035 | 0.035 | Same impurity limit |
| S (max) | 0.040 | 0.040 | Same |
| Si | 0.15 - 0.35 | 0.15 - 0.35 | Same |
| Cr | 0.75 - 1.20 | 0.80 - 1.15 | Near-identical |
| Mo | 0.15 - 0.25 | 0.50 - 0.65 | B16 has 2-3x Mo for creep resistance |
| V | not specified | 0.25 - 0.35 | B16 vanadium addition - forms fine V4C3 carbides resisting tempered-martensite embrittlement at high temperature |
UNS designations: A193 B7 = UNS G41400 (AISI 4140), A193 B16 = UNS K14072 (vanadium-modified Cr-Mo-V).
| Property | A193 B7 | A193 B16 |
|---|---|---|
| Tensile strength, min (in. ≤2-1/2) | 125 ksi (860 MPa) | 125 ksi (860 MPa) |
| Yield strength, min | 105 ksi (725 MPa) | 105 ksi (725 MPa) |
| Elongation in 4D, min | 16 % | 18 % |
| Reduction of area, min | 50 % | 50 % |
| Hardness, max | 35 HRC | 35 HRC |
| Min. tempering temperature | 1100 °F (593 °C) | 1200 °F (650 °C) |
B16 ductility (elongation 18 % vs 16 %) is marginally higher than B7 at room temperature, reflecting the more thermodynamically stable tempered structure produced at the elevated 1200 °F temper.
| Service window | A193 B7 | A193 B16 |
|---|---|---|
| Continuous service (ASME B31.1 / B31.3 / B16.5) | up to 750 °F (399 °C) | up to 840 °F (450 °C) |
| Stress-rupture qualified (S12 supplement) | not available in standard | up to 1100 °F (595 °C) with B16R suffix (25 h rupture life at 20 ksi) |
| Tempered-martensite embrittlement risk | high above 750 °F (no V to pin grain boundaries) | low - V4C3 carbides resist grain-boundary coarsening |
| Practical peak / occasional | 750 - 800 °F | 1000 - 1100 °F |
| Below -20 °F | not recommended (use A320 L7) | not recommended (use A320 L7) |
| Bolt grade | Default nut grade | Notes |
|---|---|---|
| A193 B7 | A194 Grade 2H | Q&T carbon-steel nut, general-service pairing per ASME B16.5 |
| A193 B16 | A194 Grade 7 (Cr-Mo-V nut to match bolt CTE and creep behaviour); Grade 4 legacy | Pairing per ASME B16.5 + indanasteel canonical citation |
Do NOT pair B16 studs with Grade 2H nuts for sustained service above 750 °F: the Grade 2H carbon-steel nut creeps while the B16 stud retains tension, producing thread-jacking and loss of clamp force. Do NOT pair B7 studs with Grade 7 nuts either - the Grade 7 nut is over-specified and adds cost without benefit at B7 service temperatures.
B16 typically commands a 25 to 50 % premium over B7 at the bolt level, driven by:
Companion nut cost: A194 Grade 7 is roughly 20 to 30 % more expensive than Grade 2H. Total assembly premium for B16 + Grade 7 vs B7 + Grade 2H is in the 25 to 40 % range.
| Property | A193 B7 | A193 B16 | A193 B8 / B8M |
|---|---|---|---|
| Material family | Cr-Mo alloy steel | Cr-Mo-V alloy steel | Austenitic stainless (304 / 316) |
| Tensile strength, min | 125 ksi | 125 ksi | 30 - 100 ksi (depends on Class 1 / 2) |
| Continuous service temp | up to 750 °F | up to 840 °F (1100 °F with S12) | up to 1500 °F (B8) |
| Corrosion resistance | low (coated only) | low (coated only) | high |
| Companion nut | A194 Gr. 2H | A194 Gr. 7 | A194 Gr. 8 / 8M |
| Cost (relative to B7) | 1.0x | 1.25 - 1.5x | 2 - 3x |
| NACE MR0175 (sour service) | NO (use B7M) | NO (project waiver) | YES (B8M qualifies) |
| Cryogenic service | NO (use A320 L7) | NO (use A320 L7) | YES (B8 retains toughness to -325 °F) |
No. Above 750 °F continuous service, B7 will undergo tempered-martensite embrittlement over service life and lose preload through stress relaxation. B16 retains strength and preload through V4C3 carbide pinning. Substituting B7 for B16 in a high-temperature design is a code violation under ASME B31.1 / B31.3.
Not for service above 750 °F. The Grade 2H carbon-steel nut creeps while the B16 stud holds tension, producing thread-jacking and loss of clamp force. Use A194 Grade 7.
No - the opposite. B16 elongation is higher (18 % vs 16 %) and the V4C3 carbides actually improve toughness at elevated temperature by resisting grain coarsening. B16 is more ductile than B7 across the service envelope.
Vanadium ferro-alloy is more expensive than the molybdenum ferro-alloy used in B7; higher temper temperature requires longer furnace time + tighter temperature control; S12 stress-rupture qualification adds per-lot testing cost; production volume is lower. Total premium is 25 to 50 % on the bolt + 20 to 30 % on the companion nut.