PROPRIETARY Ti64 Titanium Alloys

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

Data updates

Latest Update: 2025-05
Total number of updates: 11
Update History

This material has 414 properties — only a subset is shown here.

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PROPRIETARY Ti64 Chemical Composition

CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
Al
VALUE
5.50 – 6.75
UNIT
%
CAS NUMBER
7429-90-5
CRITERIA
C
VALUE
≤ 0.08
UNIT
%
CAS NUMBER
7440-44-0
CRITERIA
Fe
VALUE
≤ 0.30
UNIT
%
CAS NUMBER
7439-89-6
CRITERIA
H
VALUE
val1
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UNIT
%
CAS NUMBER
1333-74-0
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
Ti
VALUE
val1
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UNIT
%
CAS NUMBER
7440-32-6
CRITERIA
V
VALUE
val1
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UNIT
%
CAS NUMBER
7440-62-2
CRITERIA
Y
VALUE
val1
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UNIT
%
CAS NUMBER
7440-65-5

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PROPRIETARY Ti64 Physical Properties

Temperature

PROPERTY / VALUE
Modulus of Elasticity
103 — 117 GPa
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Density
≥ 4.4 kg/dm³
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This material has 414 properties — only a subset is shown here.

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PROPRIETARY Ti64 Heat Treatments

  • Heat Treatment Description: 120 min (± 30 min) at 800 °C (± 10 °C) measured from the part in vacuum (1.3 x 10-3 -1.3 x 10-5 mbar) followed by cooling under vacuum.
  • Stress relieved at 649°C (1200ºF +/- 25º) for 3 hours +/- 15 minutes in vacuum. Vacuum solution treated at 940°C (1725ºF +/- 25º) for 45 minutes the 6 bar argon quench. Hot Isostatic Pressing (HIP) optional.

PROPRIETARY Ti64 Mechanical Properties

Temperature

PROPERTY / VALUE
Tensile Strength
845 — 1320 MPa
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Elongation, A
5 — 17 %
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Reduction of Area
val1
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%
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Rockwell Hardness (HR)
val1
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Vickers Hardness (HV)
val1
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Yield Strength, Rp0.2
730 — 1180 MPa
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PROPRIETARY Ti64 International Equivalent Materials

Showing 15 of 185 results.

MATERIAL
STANDARD
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
MATERIAL
R56400
STANDARD
UNS
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
MATERIAL
TA 11
STANDARD
B.S.
COUNTRY / PRODUCER
United Kingdom
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
TA 56
STANDARD
B.S.
COUNTRY / PRODUCER
United Kingdom
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
F2924 Ti-6Al-4V Class A
STANDARD
ASTM
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
F2924 Ti-6Al-4V Class B
STANDARD
ASTM
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
Ti-6Al-4V
STANDARD
MIL
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
LaserForm Ti Gr5 (A)
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
Ti-6Al-4V
STANDARD
SAE
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
AB-1
STANDARD
SAE
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
F2924 Ti-6Al-4V Class C
STANDARD
ASTM
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
F2924 Ti-6Al-4V Class D
STANDARD
ASTM
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
F2924 Ti-6Al-4V Class E
STANDARD
ASTM
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
F2924 Ti-6Al-4V Class F
STANDARD
ASTM
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
Ti6Al4V Grade 5
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
Ti-6Al-4V
STANDARD
SAE
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Composition 100%

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

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  • 185Cross References
  • 50Composition
  • 65Mechanical Properties
  • 10Physical Properties
  • 3Heat Treatment
  • -Metallography
  • -Machinability
  • 1Stress-Strain
  • -Formability
  • -Fatigue
  • -Fracture
  • -Creep
  • -Joints
  • -Coatings
  • -Dimensions
  • -Tribology
  • -Corrosion
  • -Ageing
  • -Weatherability
  • -Irradiation
  • 100Total Suppliers