Nickel Alloy Inconel 718 Shaft
Product Details
| Grade: | UNS N07718/W.Nr. 2.4668/Inconel 718/GH4169 | Standard: | ASTM B637 / ASME SB637 AMS 5662 / AMS 5663 NACE MR0175 (≤40 HRC |
|---|---|---|---|
| Dia: | 5 – 500 (hot-rolled/forged/cold-drawn) Customizable Up To 800 | Length: | 1000 – 6000 (Standard) Customizable Up To 12,000 |
| Surface: | Hot-rolled / Forged / Cold-drawn Turned / Ground / Polished Peeled / Pickled / Bright |
Product Description
Engineered from precipitation-hardenable nickel-chromium alloy, this shaft provides ultra-high strength, exceptional corrosion resistance, and superior fatigue performance. It is designed to maintain structural integrity in extreme temperature environments ranging from –250 °C to 700 °C.
- Extreme Temperature Stability: Reliable performance from –250 °C to 700 °C
- Superior Durability: High fatigue resistance for critical rotating components
- Industry Versatility: Ideal for aerospace engine shafts, oil & gas downhole tools, power generation turbines, and high-performance racing systems
| Element | Content (%) | Element | Content (%) |
|---|---|---|---|
| Nickel (Ni) | 50.0 – 55.0 | Iron (Fe) | Balance (≈18%) |
| Chromium (Cr) | 17.0 – 21.0 | Manganese (Mn) | ≤ 0.35 |
| Molybdenum (Mo) | 2.80 – 3.30 | Silicon (Si) | ≤ 0.35 |
| Niobium (Nb) + Tantalum | 4.75 – 5.50 | Carbon (C) | ≤ 0.08 |
| Titanium (Ti) | 0.65 – 1.15 | Sulfur (S) | ≤ 0.015 |
| Aluminum (Al) | 0.20 – 0.80 | Phosphorus (P) | ≤ 0.015 |
| Cobalt (Co) | ≤ 1.00 | Copper (Cu) | ≤ 0.30 |
| Boron (B) | ≤ 0.006 |
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