SAE Ti-13V-11Cr-3Al Titanium Alloys

Material group: Nonferrous Alloys / Titanium Alloys

Country / Standard: United States / SAE

Data updates

Latest Update: 2023-05

Total number of updates: 12

Update History

2021-05 2021-01 2020-08 2020-07 2020-06 2019-06 2019-04 2017-09 2017-03 2015-11 2013-12

This material has 4877 properties — only a subset is shown here.

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SAE Ti-13V-11Cr-3Al Chemical Composition

CRITERIA

VALUE

UNIT

CAS NUMBER

CRITERIA

VALUE

2.50 – 3.50

UNIT

CAS NUMBER

7429-90-5

CRITERIA

VALUE

≤ 0.05

UNIT

CAS NUMBER

7440-44-0

CRITERIA

VALUE

10.00 – 12.00

UNIT

CAS NUMBER

7440-47-3

CRITERIA

VALUE

val1

UNIT

CAS NUMBER

7439-89-6

CRITERIA

VALUE

val1

UNIT

CAS NUMBER

1333-74-0

CRITERIA

VALUE

val1

UNIT

CAS NUMBER

7727-37-9; 17778-88-0

CRITERIA

VALUE

val1

UNIT

CAS NUMBER

7782-44-7; 17778-80-2

CRITERIA

Other each

VALUE

val1

UNIT

CAS NUMBER

CRITERIA

Other total

VALUE

val1

UNIT

CAS NUMBER

CRITERIA

VALUE

val1

UNIT

CAS NUMBER

7440-32-6

CRITERIA

VALUE

val1

UNIT

CAS NUMBER

7440-62-2

CRITERIA

VALUE

val1

UNIT

CAS NUMBER

7440-65-5

SAE AMS T 9046B: 2002 / Titanium and Titanium Alloy, Sheet, Strip, and Plate

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SAE Ti-13V-11Cr-3Al Physical Properties

Temperature

≤ 0°C 0 - 30°C 30 - 100°C 100 - 300°C ≥ 300°C

PROPERTY / VALUE

Modulus of Elasticity

80 — 130 GPa

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Thermal Conductivity

val1 W/(m∙°C)

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Electrical Resistivity

val1 Ω∙mm²/m

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Density

val1 kg/dm³

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Heat Capacity

val1 J/(kg∙°C)

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Electrical Conductivity

val1 S/m

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Coefficient of Thermal Expansion (CTE)

val1 10^-6/°C

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This material has 4877 properties — only a subset is shown here.

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SAE Ti-13V-11Cr-3Al Heat Treatments

Bars and forgings shall be solution heat treated and aged by heating to a temperature within the range 788 to 816°C (1450 to 1500°F), holding at the selected temperature within ±14°C (±25°F) for time commensurate with section thickness and the heating equipment and procedure used, and water quenched (except that sections under 12.7 mm may be air cooled) and then aged by heating to 482°C ± 8°C (900°F ± 15°F), holding at heat for 2 to 60 hours, and cooled in air to room temperature.
Bars and forgings shall be solution heat treated by heating to a temperature within the range 788 to 816°C (1450 to 1500°F), holding at the selected temperature within ±14°C (±25°F) for time commensurate with section thickness and the heating equipment and procedure used, and water quenched (except that sections under 12.7 mm may be air cooled).
Precipitation heat treated by heating to 482°C ± 14°C (900°F ± 25°F), holding at heat for 2 to 60 hours, and cooled in air to room temperature.

SAE Ti-13V-11Cr-3Al Mechanical Properties

Temperature

≤ 0°C 0 - 30°C 30 - 100°C

PROPERTY / VALUE

Tensile Strength

≥ 861 MPa

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Elongation, A

val1 %

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Yield Strength, Rp0.2

val1 MPa

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Impact Energy

val1 J

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Reduction of Area

val1 %

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Vickers Hardness (HV)

val1

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SAE Ti-13V-11Cr-3Al International Equivalent Materials

Showing 6 of 25 results.

MATERIAL

STANDARD

COUNTRY / PRODUCER

EQUIVALENCE CATEGORY

MATERIAL

B-1

STANDARD

SAE

COUNTRY / PRODUCER

United States

EQUIVALENCE CATEGORY

Identical

MATERIAL

Ti-13V-11Cr-3Al

STANDARD

MIL

COUNTRY / PRODUCER

United States

EQUIVALENCE CATEGORY

Official

MATERIAL

B-1

STANDARD

MIL

COUNTRY / PRODUCER

United States

EQUIVALENCE CATEGORY

Composition 100%

MATERIAL

Ti-13.5V-11Cr-3Al

STANDARD

SAE

COUNTRY / PRODUCER

United States

EQUIVALENCE CATEGORY

Implicit

MATERIAL

Ti-3Al-13V-11Cr

STANDARD

SAE

COUNTRY / PRODUCER

United States

EQUIVALENCE CATEGORY

Implicit

MATERIAL

R58010

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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See all 25 equivalent grades with detailed mapping by standard, producer and equivalence category.

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25Cross References

48Composition
289Mechanical Properties
60Physical Properties
4Heat Treatment
-Metallography
1Machinability

62Stress-Strain
23Formability
42Fatigue
1Fracture
-Creep

-Joints
-Coatings
31Dimensions
-Tribology

4283Corrosion
2Ageing
-Weatherability
-Irradiation

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