SAE AF 1753 Nickel Alloys

Material group: Nonferrous Alloys / Nickel Alloys
Country / Standard: United States / SAE

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This material has 39 properties — only a subset is shown here.

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SAE AF 1753 Chemical Composition

CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
Al
VALUE
1.90
UNIT
%
CAS NUMBER
7429-90-5
CRITERIA
B
VALUE
0.008
UNIT
%
CAS NUMBER
7440-42-8
CRITERIA
C
VALUE
0.24
UNIT
%
CAS NUMBER
7440-44-0
CRITERIA
Co
VALUE
val1
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UNIT
%
CAS NUMBER
7440-48-4
CRITERIA
Cr
VALUE
val1
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UNIT
%
CAS NUMBER
7440-47-3
CRITERIA
Fe
VALUE
val1
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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
Ni
VALUE
val1
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UNIT
%
CAS NUMBER
7440-02-0
CRITERIA
Si
VALUE
val1
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UNIT
%
CAS NUMBER
7440-21-3
CRITERIA
Ti
VALUE
val1
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UNIT
%
CAS NUMBER
7440-32-6
CRITERIA
W
VALUE
val1
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UNIT
%
CAS NUMBER
7440-33-7
CRITERIA
Zr
VALUE
val1
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UNIT
%
CAS NUMBER
7440-67-7

SAE J 467b: 1968 / Special Purpose Alloys (ʺSuperalloysʺ)

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SAE AF 1753 Physical Properties

Temperature

PROPERTY / VALUE
Modulus of Elasticity
185 — 213.7 GPa
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Density
val1
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kg/dm³
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Electrical Conductivity
val1
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S/m
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Poisson Coefficient
val1
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Electrical Resistivity
1.32 Ω∙mm²/m
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This material has 39 properties — only a subset is shown here.

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SAE AF 1753 Heat Treatments

  • Material condition: 1177°C; 760°C.

SAE AF 1753 Mechanical Properties

Temperature

PROPERTY / VALUE
Tensile Strength
1338 MPa
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Elongation, A
20 %
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Yield Strength, Rp0.2
val1
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MPa
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Reduction of Area
val1
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%
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  • -Cross References
  • 13Composition
  • 8Mechanical Properties
  • 15Physical Properties
  • 1Heat Treatment
  • -Metallography
  • -Machinability
  • 1Stress-Strain
  • -Formability
  • -Fatigue
  • -Fracture
  • 1Creep
  • -Joints
  • -Coatings
  • -Dimensions
  • -Tribology
  • -Corrosion
  • -Ageing
  • -Weatherability
  • -Irradiation
  • -Total Suppliers