SAE Rene 41 Nickel Alloys

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

Data updates

Latest Update: 2023-06
Total number of updates: 18
Update History

This material has 503 properties — only a subset is shown here.

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SAE Rene 41 Chemical Composition

CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
Al
VALUE
1.40 – 1.80
UNIT
%
CAS NUMBER
7429-90-5
CRITERIA
B
VALUE
0.003 – 0.010
UNIT
%
CAS NUMBER
7440-42-8
CRITERIA
C
VALUE
0.06 – 0.12
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
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
CRITERIA
Ti
VALUE
val1
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UNIT
%
CAS NUMBER
7440-32-6

SAE AMS 5399D: 2006 / Nickel Alloy, Corrosion and Heat-Resistant, Investment Castings 52Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum-Melted, Vacuum-Cast, Solution Heat Treated

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SAE Rene 41 Physical Properties


Temperature

PROPERTY / VALUE
Compression Modulus
218 GPa
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Modulus of Elasticity
185 — 219.9 GPa
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Density
val1
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kg/dm³
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Thermal Conductivity
val1
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W/(m∙°C)
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Electrical Resistivity
val1
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Ω∙mm²/m
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Electrical Conductivity
val1
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S/m
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Melting Temperature
val1
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°C
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Poisson Coefficient
val1
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Shear Modulus
val1
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GPa
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Coefficient of Thermal Expansion (CTE)
val1
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10-6/°C
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This material has 503 properties — only a subset is shown here.

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SAE Rene 41 Heat Treatments


  • Solution heat treated by heating in a suitable atmosphere to 1975°F ± 25°F (1079 °C ± 14°C), held at heat for not less than 60 minutes per inch (25 mm) of nominal thickness, and cooled at a rate equivalent to a rapid air cool or faster
    Precipitation heat treated by heating to 1400°F ± 15°F (760°C ± 8°C), held at heat for not less than 16 hours, and cooled at a rate equivalent to cooling in air
  • Solution heat treatment: Heated in a suitable protective atmosphere to 1066 ± 14°C (1950 ± 25°F), held at heat for not less than three hours, and rapid quench
    Re-Solution heat treatment: Heated in a suitable protective atmosphere to 1066 ± 14°C (1950 ± 25°F), held at heat for not less than 30 minutes, and rapid cooled
    Precipitation heat treatment: Heated to 760 ± 14°C (1400 ± 25°F), held at heat for not less than 16 hours, and cooled in air

SAE Rene 41 Mechanical Properties


Temperature

PROPERTY / VALUE
Tensile Strength
1103 — 1420 MPa
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Brinell Hardness (HB)
≥ 311
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Elongation, A
val1
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%
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Compression Yield Strength
val1
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MPa
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Grain Size
val1
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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
val1
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MPa
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SAE Rene 41 International Equivalent Materials


Showing 9 of 14 results.

MATERIAL
STANDARD
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
MATERIAL
STANDARD
UNS
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
MATERIAL
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Official
MATERIAL
STANDARD
SAE
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Implicit
MATERIAL
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Implicit
MATERIAL
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Implicit
MATERIAL
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Implicit
MATERIAL
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Implicit
MATERIAL
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Implicit
MATERIAL
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Implicit

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  • 14Cross References

  • 67Composition
  • 155Mechanical Properties
  • 99Physical Properties
  • 5Heat Treatment
  • -Metallography
  • 1Machinability

  • 112Stress-Strain
  • 1Formability
  • 2Fatigue
  • -Fracture
  • 3Creep

  • -Joints
  • -Coatings
  • 26Dimensions
  • -Tribology

  • -Corrosion
  • 2Ageing
  • -Weatherability
  • 2Irradiation

  • 14Total Suppliers