A precipitation hardenable Nickel-Iron-Chromium alloy having outstanding controllable thermoelastic coefficient characteristics and excellent strength and oxidation resistance in high temperature atmospheres.  The alloy can be processed to have a constant modulus of elasticity at temperatures ranging from -45oC to +65oC (-50 to +150oF).
 

Applications include:

Springs in precise applications, such as watches and
weighing machinesSpacer

Approximate Chemical Composition
Ni 41-43.5%
Cr 4.9-5.75%
Ti 2.2-2.75%
Fe 48%
DENSITY 8.05 g/cm3 0.291 lb/in3
MELTING POINT 1480oC 2700oF
COEFFICIENT OF EXPANSION 7.6 µm/m °C
( 20 - 100°C)
4.2 x 10-6 in/in °F
( 70 - 212°F)
MODULUS OF RIGIDITY 62-69 kN/m2 8993-10008 ksi
MODULUS OF ELASTICITY 165-200 kN/m2 23932-29008 ksi
 
CONDITION OF SUPPLY HEAT TREATMENT (AFTER FORMING)
Spring Temper
For good all round properties:
Age harden at 650°C (1200°F) for 2 hours and air cool.
For maximum stability: Stress equalise at 400°C (750°F) for 2 hours and air cool and
age harden at 650°C (1200°F) for 2 hours and air cool.
For min. hysterisis & low thermo elastic coefficient: Stress equalise at 400°C (750°F) for 2 hours and air cool.
(Very high precision applications will require each batch to be pilot tested to determine
the specific heat treatment necessary to produce the required thermo elastic coefficient).
CONDITION  

APPROX TENSILE STRENGTH

 

APPROX SERVICE TEMPERATURE

Annealed 450-650 N/mm2 65-94 ksi -45 to +65°C -50 to 150°F
      (for constant modulus applications)
Spring Tempered 900-1100 N/mm2 131-159 ksi -45 to +65°C -50 to 150°F
      (for constant modulus applications)
Spring Temper + Aged 1300-1500 N/mm2 189-218 ksi -45 to +65°C -50 to 150°F
      (for constant modulus applications)
 
STANDARDS
AMS 5255
 


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