
Inconel 718 (UNS N07718) and Inconel 625 (UNS N06625) are the two most widely used nickel-based superalloys. They share a nickel-chromium base, but 718 is precipitation-hardened with niobium and titanium to yield strengths above 1000 MPa, while 625 is solid-solution strengthened with molybdenum and niobium for corrosion resistance and weldability.
1. Chemical Composition (%)
| Element | Grade A | Grade B |
|---|---|---|
| Ni | 50.0–55.0 | ≥58.0 |
| Cr | 17.0–21.0 | 20.0–23.0 |
| Mo | 2.80–3.30 | 8.0–10.0 |
| Nb+Ta | 4.75–5.50 | 3.15–4.15 |
| Fe | Balance | ≤5.0 |
| Ti | 0.65–1.15 | ≤0.40 |
| Al | 0.20–0.80 | ≤0.40 |
2. Mechanical Properties (Typical)
| Property | Grade A | Grade B |
|---|---|---|
| Tensile (MPa) | ≥1240 | ≥827 |
| Yield (MPa) | ≥1034 | ≥414 |
| Elongation (%) | ≥12 | ≥30 |
| Hardness | ≥331 HBW | ≤95 HRB |
| Max Service Temp | ~700°C (strength) | ~980°C (oxidation) |
3. Key Technical Differences
- 718 has nearly double the yield strength of 625, ideal for turbine blades and high-stress parts.
- 625 has higher Mo and Cr, giving superior pitting and seawater resistance.
- Both are weldable; 718 is specifically designed to resist post-weld cracking.
- 625 is easier to form and process in annealed state.
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Frequently asked questions
Which is stronger at high temperature?
718 maintains high strength up to 700°C.
Which is better for subsea?
625, due to high Mo and chloride resistance.
Can 718 be welded?
Yes, with excellent weldability and post-weld crack resistance.
Is 625 magnetic?
No, non-magnetic in all conditions.
What are 718 main applications?
Aerospace engine parts, liquid-fueled rockets, fasteners.
Does Hangbo provide third-party testing?
Yes, full MTRs and SGS/TUV inspection supported.