
DIN 1.4980 (chemically designated as X6NiCrTiMoVB25-15-2 under EN 10269 and EN 10302) is a premium iron-base, precipitation-hardening austenitic superalloy. It is the European direct equivalent to UNS S66286 (Alloy A-286) and ASTM A638 Grade 660.
By undergoing a solution treatment followed by precipitation aging, it forms a strengthening gamma prime ($\gamma^\prime$) intermetallic phase. This microstructure provides high tensile strength, long-term creep resistance, and excellent oxidation resistance at continuous operating temperatures up to 700°C (1292°F).
The mechanical behavior, grain orientation, and typical application boundaries of DIN 1.4980 shift significantly based on its geometric profile and manufacturing method:
| Profile Type | Dimensional Standards | Material Finish Options | Primary Mechanical Advantage |
| Round Bars |
EN 10060 (Hot Rolled) EN 10278 (Bright Drawn) |
Centerless ground, peeled, or cold drawn | Symmetrical axial grain flow; ideal for high-speed automated CNC machining. |
| Flat Bars | EN 10058 (Hot Rolled) | HRAP (Hot Rolled, Annealed, Pickled) or sandblasted | Planar grain orientation; optimized for structural bending loads. |
| Square Bars |
EN 10059 (Hot Rolled) EN 10278 (Bright Drawn) |
Canned, bright drawn, or smooth machined | Identical biaxial ($X-Y$) stress distribution across sharp 90° geometries. |
| Forged Bars | EN 10250-4 (Open Die) | Rough turned, peeled, or black as-forged skin | Highly refined 3D grain flow; eliminates internal micro-voids and casting segregation. |
Engineering Profile: Features uniform radial grain deformation. Bright drawn variants offer exceptionally tight dimensional tolerances (such as h9 or h11).
Common Applications: High-temperature fasteners, engine cylinder studs, aerospace bolts, and gas turbine downstream components. Often specified alongside DIN 2510 standards for resilient bolted connections.
Engineering Profile: Produced via rolling or shearing from plate stock. It exhibits mechanical anisotropy, meaning its transverse ductility is slightly lower than its longitudinal strength.
Common Applications: High-temperature structural brackets, aerospace exhaust frames, furnace guide rails, and linear reinforcement plates.
Engineering Profile: Features sharp 90-degree corners with balanced cross-sectional area distribution. It retains dimensional stability well during precipitation aging treatments.
Common Applications: Heavy-duty machine keys, high-temperature torque-transmission bars, slide blocks for industrial vacuum furnaces, and specialized aerospace framing components.
Engineering Profile: Created via heavy open-die hydraulic pressing. This process yields the highest structural integrity and fatigue resistance of all forms, though it requires a higher machining allowance to remove the superficial oxide layer.
Common Applications: Large-diameter turbine rotors, high-pressure pump shafts, critical valve stems, and thick-walled flanges operating under severe cyclic thermal stress.
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