PROPRIETARY Rene 41 Nickel Alloys

Material group: Nonferrous Alloys / Nickel Alloys
Country / Standard: PROPRIETARY

Data updates

Latest Update: 2024-05
Total number of updates: 10
Update History

This material has 273 properties — only a subset is shown here.

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PROPRIETARY Rene 41 Chemical Composition

CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
Al
VALUE
1.4 – 1.8
UNIT
%
CAS NUMBER
7429-90-5
CRITERIA
B
VALUE
0.003 – 0.01
UNIT
%
CAS NUMBER
7440-42-8
CRITERIA
C
VALUE
≤ 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
Cu
VALUE
val1
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UNIT
%
CAS NUMBER
7440-50-8
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
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

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PROPRIETARY Rene 41 Physical Properties

Temperature

PROPERTY / VALUE
Modulus of Elasticity
185 — 218 GPa
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Electrical Resistivity
1.31 Ω∙mm²/m
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Thermal Conductivity
9 W/(m∙°C)
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Density
val1
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kg/dm³
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Dynamic Modulus of Elasticity
val1
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GPa
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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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Service Temperature
val1
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°C
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Shear Modulus
val1
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GPa
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Poisson Coefficient
val1
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This material has 273 properties — only a subset is shown here.

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PROPRIETARY Rene 41 Heat Treatments

  • Annealed at 1065°C (1950°F)
    Spring temper + aged (after spring coiling): Solution annealed at 1065°C (1950°F) for 4 h; Aged at 760°C (1400°F) for 16 h
  • Heat Treatment of Finished Parts; Annealed, Age hardened at 760°C (1400°F) for 16 h, air cooling.
    Spring Temper: Solution annealed at 1065°C (1950°F) for 4 h, air cooling, Age hardened at 760°C (1400°F) for 16 h, air cooling.
    Spring Temper, Age hardened at 760°C (1400°F) for 16 h, air cooling.

PROPRIETARY Rene 41 Mechanical Properties

Temperature

PROPERTY / VALUE
Tensile Strength
800 — 2000 MPa
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Elongation, A
14 — 21 %
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Yield Strength, Rp0.2
val1
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MPa
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Rockwell Hardness (HR)
val1
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PROPRIETARY Rene 41 International Equivalent Materials

Showing 13 of 17 results.

MATERIAL
STANDARD
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
MATERIAL
5829
STANDARD
SAE
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
MATERIAL
Rene 41
STANDARD
SAE
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
MATERIAL
N07041
STANDARD
UNS
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
MATERIAL
Nimonic alloy 90
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Implicit
MATERIAL
HAYNES R-41
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Implicit
MATERIAL
UDIMET alloy R41
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Implicit
MATERIAL
N07090
STANDARD
UNS
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Implicit
MATERIAL
Pyromet Alloy 41
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Implicit
MATERIAL
VBC Alloy 0004
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Implicit
MATERIAL
VBC Alloy 0241
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Implicit
MATERIAL
S A 50 Ni
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Implicit
MATERIAL
CarTech 41 Alloy
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Implicit
MATERIAL
Rene 41
STANDARD
SAE
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Implicit

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  • 17Cross References
  • 36Composition
  • 113Mechanical Properties
  • 76Physical Properties
  • 3Heat Treatment
  • -Metallography
  • 1Machinability
  • 3Stress-Strain
  • -Formability
  • 2Fatigue
  • -Fracture
  • 1Creep
  • -Joints
  • -Coatings
  • -Dimensions
  • -Tribology
  • -Corrosion
  • -Ageing
  • -Weatherability
  • -Irradiation
  • 21Total Suppliers