SAE Ti-6Al-2Sn-2Zr-2Mo-2Cr-0.15Si Titanium Alloys

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

Data updates

Latest Update: 2015-05
Total number of updates: 3
Update History
2014-08 2014-04

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SAE Ti-6Al-2Sn-2Zr-2Mo-2Cr-0.15Si Chemical Composition

CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
Al
VALUE
5.25 – 6.25
UNIT
%
CAS NUMBER
7429-90-5
CRITERIA
C
VALUE
≤ 0.08
UNIT
%
CAS NUMBER
7440-44-0
CRITERIA
Cr
VALUE
1.75 – 2.25
UNIT
%
CAS NUMBER
7440-47-3
CRITERIA
Fe
VALUE
val1
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UNIT
%
CAS NUMBER
7439-89-6
CRITERIA
H
VALUE
val1
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UNIT
%
CAS NUMBER
1333-74-0
CRITERIA
Mo
VALUE
val1
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UNIT
%
CAS NUMBER
7439-98-7
CRITERIA
N
VALUE
val1
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UNIT
%
CAS NUMBER
7727-37-9; 17778-88-0
CRITERIA
O
VALUE
val1
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UNIT
%
CAS NUMBER
7782-44-7; 17778-80-2
CRITERIA
Other each
VALUE
val1
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UNIT
%
CAS NUMBER
CRITERIA
Other total
VALUE
val1
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UNIT
%
CAS NUMBER
CRITERIA
Si
VALUE
val1
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UNIT
%
CAS NUMBER
7440-21-3
CRITERIA
Sn
VALUE
val1
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UNIT
%
CAS NUMBER
7440-31-5
CRITERIA
Ti
VALUE
val1
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UNIT
%
CAS NUMBER
7440-32-6
CRITERIA
Zr
VALUE
val1
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UNIT
%
CAS NUMBER
7440-67-7

SAE AMS 4898F: 2022 / Titanium Alloy, Sheet 6Al - 2Sn - 2Zr - 2Mo - 2Cr - 0.15Si Annealed

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SAE Ti-6Al-2Sn-2Zr-2Mo-2Cr-0.15Si Physical Properties

Temperature

PROPERTY / VALUE
Modulus of Elasticity
80 — 130 GPa
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Density
4.3 — 5.1 kg/dm³
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SAE Ti-6Al-2Sn-2Zr-2Mo-2Cr-0.15Si Heat Treatments

  • Annealing: heat to a temperature within the range 704 to 899°C (1300 to 1650°F), hold at the selected temperature within ± 14°C ( 25°F ) for a time commensurate with product thickness and the heating equipment and procedure used, and cool to room temperature at a rate equivalent to an air cool or faster.
    Solution heat treated by heating to a temperature within the range 871 to 927°C (1600 to 1700°F), holding at the selected temperature within ± 14°C (± 25°F ) for 15 to 60 minutes, cooling to room temperature at a rate equivalent to an air cool or faster, followed by aging within the range of 482 to 538°C (900 to 1000°F), holding at the selected temperature within ± 8°C (± 15°F) for 8 to 12 hours, and cooling to room temperature.

SAE Ti-6Al-2Sn-2Zr-2Mo-2Cr-0.15Si Mechanical Properties

Temperature

PROPERTY / VALUE
Tensile Strength
≥ 1069 MPa
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Elongation, A
≥ 5 %
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Grain Size
val1
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Yield Strength, Rp0.2
≥ 1034 MPa
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SAE Ti-6Al-2Sn-2Zr-2Mo-2Cr-0.15Si International Equivalent Materials

Showing 15 of 20 results.

MATERIAL
STANDARD
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
MATERIAL
B 861 Grade 18
STANDARD
ASTM
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
MATERIAL
B 265 Grade 18
STANDARD
ASTM
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
MATERIAL
B 338 Grade 18
STANDARD
ASTM
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
MATERIAL
SB-265 Grade 18
STANDARD
ASME
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
MATERIAL
B 348 Grade 18
STANDARD
ASTM
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
MATERIAL
B 862 Grade 18
STANDARD
ASTM
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
MATERIAL
B 863 Grade 18
STANDARD
ASTM
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
MATERIAL
SB-338 Grade 18
STANDARD
ASME
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
MATERIAL
SB-348 Grade 18
STANDARD
ASME
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
MATERIAL
SB-861 Grade 18
STANDARD
ASME
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
MATERIAL
SB-862 Grade 18
STANDARD
ASME
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
MATERIAL
B 265 Grade Ti-3Al-2.5V-0.05Pd
STANDARD
ASTM
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
MATERIAL
B 861 Grade R56322
STANDARD
ASTM
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
MATERIAL
B 862 Grade R56322
STANDARD
ASTM
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
MATERIAL
R56222
STANDARD
UNS
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official

Equivalence categories reflect chemical-composition and mechanical-property comparison — always verify suitability against the governing specification for your application.

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  • 20Cross References
  • 14Composition
  • 20Mechanical Properties
  • 5Physical Properties
  • 1Heat Treatment
  • -Metallography
  • -Machinability
  • 37Stress-Strain
  • 1Formability
  • 12Fatigue
  • 2Fracture
  • 1Creep
  • -Joints
  • -Coatings
  • 59Dimensions
  • -Tribology
  • 4283Corrosion
  • -Ageing
  • -Weatherability
  • -Irradiation
  • 5Total Suppliers