SAE Allvac 718Plus Nickel Alloys

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

Data updates

Latest Update: 2023-07
Total number of updates: 5
Update History
2020-03 2018-02 2017-02 2013-12

This material has 140 properties — only a subset is shown here.

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SAE Allvac 718Plus Chemical Composition

CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
Al
VALUE
1.20 – 1.70
UNIT
%
CAS NUMBER
7429-90-5
CRITERIA
B
VALUE
0.003 – 0.008
UNIT
%
CAS NUMBER
7440-42-8
CRITERIA
Bi
VALUE
<= 0.00003%
UNIT
%
CAS NUMBER
7440-69-9
CRITERIA
C
VALUE
val1
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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
Nb
VALUE
val1
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UNIT
%
CAS NUMBER
7440-03-1
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
Pb
VALUE
val1
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UNIT
%
CAS NUMBER
7439-92-1
CRITERIA
S
VALUE
val1
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UNIT
%
CAS NUMBER
7704-34-9
CRITERIA
Se
VALUE
val1
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UNIT
%
CAS NUMBER
7782-49-2
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

SAE AMS 5441C: 2023 / Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings Ni - 18Cr - 2.8Mo - 5.5Cb(Nb) - 0.70Ti - 1.50Al - 10Fe - 9Co - 1W Consumable Electrode Remelted or Vacuum Induction Melted 1775°F (968°C) Solution Heat Treated, Precipitation-Hardenable

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SAE Allvac 718Plus Physical Properties


Temperature

PROPERTY / VALUE
Modulus of Elasticity
185 — 205 GPa
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Density
7.9 — 8.8 kg/dm³
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Poisson Coefficient
0.32 — 0.34
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This material has 140 properties — only a subset is shown here.

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SAE Allvac 718Plus Heat Treatments


  • Bars, forgings and flash welded rings shall be solution heat treated by heating to a temperature within the range 954 to 982°C (1750 to 1800°F), holding at the selected temperature within ±14°C (±25°F) for 1 hour or a time commensurate with cross-sectional thickness, and cooling at a rate equivalent to an air cool or faster.
    Response to Heat Treatment: Product, 127 mm and under in nominal diameter or least distance between parallel sides, after being precipitation heat treated by heating to 788°C ± 8 (1450°F ± 15°F ), hold at temperature for not less than 8 hours, cool at a rate not less than 56°C (100 °F) degrees per hour to 704°C ± 8 (1300°F ± 15°F), hold at 704°C ± 8 (1300 °F ± 15 °F) for not less than 8 hours, and cool at a rate equivalent to air cool or faster.
  • Solution Heat Treatment: heat to a temperature within the range 954 to 982°C (1750 to 1800 °F), hold at the selected temperature within ± 14°C (±25 °F) for 1 hour or a time commensurate with cross-sectional thickness, and cool at a rate equivalent to an air cool or faster.
    Precipitation Heat Treatment: heat to a temperature of 788°C ± 8 (1450 °F ± 15 °F), hold at temperature for not less than 8 hours, cool at a rate not less than 56°C (100 °F) degrees per hour to 704°C ± 8 (1300 °F ± 15 °F) , hold at 704°C ± 8 (1300 °F ± 15 °F) for not less than 8 hours, and cool at a rate equivalent to air cool or faster.

SAE Allvac 718Plus Mechanical Properties


Temperature

PROPERTY / VALUE
Tensile Strength
≥ 1206 MPa
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Brinell Hardness (HB)
≥ 285
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Elongation, A
val1
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%
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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 Allvac 718Plus International Equivalent Materials


Showing 3 of 4 results.

MATERIAL
STANDARD
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
MATERIAL
STANDARD
UNS
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Implicit

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  • 4Cross References

  • 55Composition
  • 36Mechanical Properties
  • 3Physical Properties
  • 4Heat Treatment
  • -Metallography
  • -Machinability

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

  • -Joints
  • -Coatings
  • 35Dimensions
  • -Tribology

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

  • 1Total Suppliers