AFNOR NF Ti-6Al-4V Titanium

Material group: Nonferrous Alloys / Titanium / Titanium Alloys
Country/Standard: France / AFNOR NF

Data updates

Latest Update: 2024-03
Total number of updates: 6
Update History
2022-09 2022-04 2022-03 2020-10 2018-12

This material has 4826 properties — only a subset is shown here.

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AFNOR NF Ti-6Al-4V Chemical Composition

CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
Al
VALUE
5.5 – 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+2N
VALUE
val1
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UNIT
%
CAS NUMBER
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

EN 3311: 2023 / Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bar for machining - D ≤ 300 mm - 900 MPa ≤ Rm ≤ 1160 MPa

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AFNOR NF Ti-6Al-4V 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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This material has 4826 properties — only a subset is shown here.

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AFNOR NF Ti-6Al-4V Heat Treatments

  • Annealed (A): heated within range 690 - 840°C for minimum 30 min., air cooling or inert atmosphere.
  • Annealed: 690°C <= Θ <= 840°C / t >= 30 min / AC or inert amosphere.

AFNOR NF Ti-6Al-4V Mechanical Properties


Temperature

PROPERTY / VALUE
Yield Strength, Rp0.2
780 MPa
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Tensile Strength
860 — 1180 MPa
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Elongation, A
6 %
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Reduction of Area
val1
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%
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  • 132 Cross References

  • 114 Composition
  • 114 Mechanical Properties
  • 2 Physical Properties
  • 8 Heat Treatment
  • 11 Metallography
  • - Machinability

  • 30 Stress-Strain
  • 31 Formability
  • - Fatigue
  • - Fracture
  • - Creep

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

  • 4283 Corrosion
  • - Ageing
  • - Weatherability
  • - Irradiation

  • 95 Total Suppliers