Udimet 630

Technical Reference Library

Udimet 630

Type Ni-Cr-Co Superalloy Nickel ~50% Chromium ~17%

Material Overview

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.

Chemical Composition

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.

Machinability Explained

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.

Recommended Cutting Speeds

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.

Recommended FM Carbide Grades by Operation

Turning

Grade Coating ISO Application Range
FM524 CVD S05 - S10
FM2533 CVD S15

Parting / Grooving

Grade Operation Coating ISO Application Range
FM2543 Parting CVD S20
FM2553 Parting CVD S30
FM2533 Grooving CVD S10

Milling

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

Recommended Insert Cutting-Edge Geometry

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