Haynes 214* Specification
*Trade name of Haynes International

  • W.NR 2.4646
  • UNS N07214
  • AWS 061

Applicable Standards:

  • -

Haynes 214 is a Nickel-Chromium-Aluminium-Iron alloy which is principally intended for use at temperatures of 955oC (1750oF) and above. It exhibits resistance to oxidation that far exceeds virtually all conventional heat resistant wrought alloys at these temperatures.

Good Mechanical Properties at Elevated Temperatures Yes
Corrosion Resistant at Ambient Temperatures Yes
Corrosion Resistant & Good Mechanical Properties at Elevated Temperatures No
Oxidation Resistant Yes
Precipitation Hardenable No

Applications include:

  • Mesh belts
  • Trays and fixtures for the firing of pottery and china
  • The heat treatment of electronic devices and technical grade ceramics
Approximate Chemical Composition
Ni 75%
Cr 16%
Al 4.5%
Fe 3%
Mn 0.5% max
Properties
DENSITY 8.05 g/cm3 0.291 lb/in3
MELTING POINT 1400oC 2550oF
COEFFICIENT OF EXPANSION 13.3 µm/m °C
(20 - 100°C)
7.4 x 10-6 in/in °F
(70 - 212°F)
MODULUS OF RIGIDITY 84 kN/mm2 12183 ksi
MODULUS OF ELASTICITY 217 kN/mm2 31474 ksi
CONDITION OF SUPPLY HEAT TREATMENT (AFTER FORMING)
Annealed/Spring Temper Stress relieve at 400 - 450oC (750 - 840oF) for 2 hours and air cool.
CONDITION APPROX TENSILE STRENGTH APPROX SERVICE TEMPERATURE
Annealed 900 - 1050 N/mm2 131 - 152 ksi -200 to +1100oC -330 to +2010oF
      (for lightly stressed applications)
Spring Temper 1300 - 1700 N/mm2 189 - 247 ksi -200 to +1100oC -330 to +2010oF
      (for lightly stressed applications)
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