PROPRIETARY Chrome Core 8 Alloy Structural and constructional steels

Material group: Ferrous Alloys / Structural and constructional steels
Country / Standard: PROPRIETARY

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Latest Update: 2016-02
Total number of updates: 1
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PROPRIETARY Chrome Core 8 Alloy Chemical Composition

CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
C
VALUE
≤ 0.0300
UNIT
%
CAS NUMBER
7440-44-0
CRITERIA
Cr
VALUE
7.5000 – 8.5000
UNIT
%
CAS NUMBER
7440-47-3
CRITERIA
Fe
VALUE
Balance
UNIT
%
CAS NUMBER
7439-89-6
CRITERIA
Mn
VALUE
val1
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UNIT
%
CAS NUMBER
7439-96-5
CRITERIA
Mo
VALUE
val1
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UNIT
%
CAS NUMBER
7439-98-7
CRITERIA
P
VALUE
val1
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UNIT
%
CAS NUMBER
7723-14-0
CRITERIA
S
VALUE
val1
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UNIT
%
CAS NUMBER
7704-34-9
CRITERIA
Si
VALUE
val1
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UNIT
%
CAS NUMBER
7440-21-3

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PROPRIETARY Chrome Core 8 Alloy Physical Properties


Temperature

PROPERTY / VALUE
Modulus of Elasticity
190 — 210 GPa
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Electrical Resistivity
0.49 Ω∙mm²/m
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Density
7.67 — 7.86 kg/dm³
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Electrical Conductivity
val1
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S/m
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Heat Capacity
val1
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J/(kg∙°C)
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Poisson Coefficient
val1
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This material has 32 properties — only a subset is shown here.

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PROPRIETARY Chrome Core 8 Alloy Heat Treatments


  • Due to the relatively low chromium content, Chrome Core 8 alloy will form austenite if heated to too high a temperature, and some hardening will occur if the austentized part is rapidly cooled. Consequently the best heat treatment for improved soft magnetic properties is to subcritically anneal. The recommended heat treatment practice for Chrome Core 8 alloy is to anneal at a temperature of 780°C +/-14°C (1436°F +/-25°F) for 2 to 4 hours. The cooling rate after the anneal is not critical although rapid cooling and quenching may induce stresses which impair the magnetic characteristics. Any inert annealing atmosphere such as vacuum, inert gases or dry forming gas is satisfactory. Attempts to decarburize the alloy using a wet hydrogen atmosphere are not recommended. Similar heat treating practices can be used to soften the alloy for further forming.

PROPRIETARY Chrome Core 8 Alloy Mechanical Properties


Temperature

PROPERTY / VALUE
Tensile Strength
421 MPa
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Elongation, A
40 %
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Reduction of Area
val1
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%
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Rockwell Hardness (HR)
val1
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Yield Strength, Rp0.2
228 MPa
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  • 1Cross References

  • 8Composition
  • 5Mechanical Properties
  • 15Physical Properties
  • 1Heat Treatment
  • -Metallography
  • -Machinability

  • 1Stress-Strain
  • -Formability
  • -Fatigue
  • -Fracture
  • -Creep

  • -Joints
  • -Coatings
  • -Dimensions
  • -Tribology

  • -Corrosion
  • -Ageing
  • -Weatherability
  • -Irradiation

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