Udimet 630 is a precipitation-hardenable nickel-chromium-cobalt superalloy in the Special Metals Udimet family, associated with the DIN-style designation NiCr19NbMo. Like other Udimet grades, it is strengthened by gamma-prime (γ') precipitation from combined aluminum and titanium additions, with niobium (columbium) and molybdenum contributing further precipitation and solid-solution strengthening. Compared with the older, more widely documented Udimet 500 and Udimet 700 grades, Udimet 630 carries a notably higher aluminum fraction relative to titanium, consistent with the later, higher-strength direction the Udimet family took as alloy design matured.
As with other members of this alloy family, Udimet 630 is intended for elevated-temperature service in gas turbine and similar high-temperature rotating or static hardware, where a combination of high strength, creep resistance, and oxidation resistance is required. This is a less commonly documented trade name compared with Udimet 500/700/710; specific mill certificates should always be consulted to confirm exact composition and heat-treatment condition for a given lot.
| Element | Amount |
|---|---|
| Nickel (Ni) | ~50% (Balance) |
| Chromium (Cr) | ~17% |
| Cobalt (Co) | ~18% |
| Aluminum (Al) | ~6.5% |
| Molybdenum (Mo) | ~3% |
| Niobium (Nb/Cb) | ~3% |
| Titanium (Ti) | ~1% |
| Iron (Fe) | ~0.7% |
Composition is nominal and reflects the most consistent published reference figures available for this less-documented trade name; treat as indicative rather than a certified mill specification. Minor/trace elements (C, B, Zr) were not available in a verifiable published source and are omitted rather than estimated. Confirm exact composition against mill certification for your specific lot.
Udimet 630 carries the same core difficulties found across the nickel-based superalloy family. Thermal conductivity is low, so heat generated at the cutting edge concentrates at the tool-chip interface rather than dissipating into the chip, accelerating crater wear. The alloy work-hardens rapidly under cutting forces, so a consistent, adequate chip load must be maintained throughout the cut - any hesitation or rubbing produces a hardened surface skin that is markedly tougher to remove on the next pass.
Udimet 630's relatively high combined aluminum and titanium content drives a substantial gamma-prime volume fraction, which means the alloy retains considerable strength and hardness at the elevated temperatures generated during cutting - tool edges stay under heavy mechanical load even as heat builds, and the alloy's affinity for common tool materials makes it prone to galling and built-up edge. Rigid setups, sharp positive-rake carbide grades engineered for superalloys, moderate-to-low cutting speeds, and generous, consistent coolant delivery are the standard countermeasures for this alloy family.
| Application | Vc (m/min) | Vc (SFM) |
|---|---|---|
| Turning | 60-180 | 200-590 |
| Milling | 45-135 | 150-440 |
| Parting | 40-115 | 130-380 |
| Grooving | 55-160 | 180-520 |
| Drilling | 55-160 | 180-520 |
These are general starting-point ranges for heat-resistant Ni/Co-based alloys. Actual optimal speeds depend on tool grade, coating, rigidity, and coolant strategy.
| Grade | Coating | ISO Application Range |
|---|---|---|
| FM524 | CVD | S05 - S10 |
| FM2533 | CVD | S15 |
| Grade | Operation | Coating | ISO Application Range |
|---|---|---|---|
| FM2543 | Parting | CVD | S20 |
| FM2553 | Parting | CVD | S30 |
| FM2533 | Grooving | CVD | S10 |
| Grade | Coating | ISO Application Range |
|---|---|---|
| FM125 | PVD | S15 - S35 |
Ready to cut Udimet 630? Shop FM Carbide inserts engineered for nickel-chromium-cobalt superalloys.
Shop Turning & Grooving Inserts Shop Milling Inserts| Honing Size | 0.02-0.05 mm / 0.001-0.002" |
| Rake Angle | 13° - 18° |
| Land Angle | Neutral |
| Land Width | 0.10-0.20 mm / 0.004-0.008" |
| Ground Insert | Recommended |