PROPRIETARY Pyromet Alloy 41 Nickel Alloys

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

Data updates

Latest Update: 2021-11
Total number of updates: 3
Update History
2016-02 2014-02

This material has 91 properties — only a subset is shown here.

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PROPRIETARY Pyromet Alloy 41 Chemical Composition

CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
Al
VALUE
1.40 – 1.60
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
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 Pyromet Alloy 41 Physical Properties


Temperature

PROPERTY / VALUE
Modulus of Elasticity
185 — 218 GPa
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Density
val1
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kg/dm³
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Poisson Coefficient
val1
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This material has 91 properties — only a subset is shown here.

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PROPRIETARY Pyromet Alloy 41 Heat Treatments


  • Solution treated at 1066°C, 4 hours, air cooled and aged at 760°C, 16 hours, air cooled. Solution temperatures: gamma prime solvus temp 1071/1082°C, M6C carbide 1149°C and higher, M23C6 carbide 982°C and higher. If fine grain size and best tensile ductility are desired, the solution treatment should be executed in the range of 1038/1052°C, hold 4 hours at temperature, then air cool. If the M6C carbide, normally present in this alloy, is solutioned by treating above 1149°C, it will precipitate during cooling or aging as M23C6, a continuous grain boundary film which results in low ductility. Resolutioning - at least 982°C and preferably 1038°C - is required to restore ductility by reforming M6C. Precipitation hardening treatment: heat to 760°C, hold at heat for 16 hours, then air cool. Hardness will be in the Rockwell C 40/45 range. Lowest hardness is obtained by quenching from temperatures above the gamma prime solvus temperature 1066°C is usually satisfactory. In some cases it may be desirable to anneal at lower temperatures, but preferably not lower than 982°C.

PROPRIETARY Pyromet Alloy 41 Mechanical Properties


Temperature

PROPERTY / VALUE
Tensile Strength
1420 MPa
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Elongation, A
14 %
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Yield Strength, Rp0.2
val1
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MPa
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PROPRIETARY Pyromet Alloy 41 International Equivalent Materials


Showing 9 of 11 results.

MATERIAL
STANDARD
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
MATERIAL
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Composition 100%
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
SE
COUNTRY / PRODUCER
Germany
EQUIVALENCE CATEGORY
Implicit
MATERIAL
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Implicit
MATERIAL
STANDARD
SE
COUNTRY / PRODUCER
Germany
EQUIVALENCE CATEGORY
Implicit

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  • 11Cross References

  • 11Composition
  • 24Mechanical Properties
  • 26Physical Properties
  • 1Heat Treatment
  • -Metallography
  • -Machinability

  • 4Stress-Strain
  • -Formability
  • -Fatigue
  • -Fracture
  • 1Creep

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

  • 1Corrosion
  • -Ageing
  • -Weatherability
  • -Irradiation

  • 12Total Suppliers