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6AL-4V, TITANIUM GRADE 5: Also known as
Ti6Al4V, Ti-6Al-4V or Ti 6-4, is the most commonly used alloy. Alloy 6AL-4V is
used extensively in Aerospace, Medical, Marine, and Chemical Processing. It is
used for connecting rods in internal combustion engines. It is significantly
stronger than commercially pure titanium while having the same stiffness and
thermal properties. Among its many advantages, it is heat treatable. This
grade is an excellent combination of strength, corrosion resistance, weld and
fabricability. In consequence, its uses are numerous such as for military
aircraft or turbines.
Specifications: UNS R56400, Werkstoff
3.7164, Werkstoff 3.7165, EN 3.7164, EN 3.7165
Titanium 6AL-4V Sheet, Titanium 6AL-4V Plate
6AL-4V:
AMS 4911, AMS 4920, MIL-T-9046 AB-1, MIL-T-9046 Type 1 Comp
C, ASTM-B-265 Gr5, wl 3.7164.1, BSTA11 (square section), EN 3464. UNS R56400, ASNA3304,
AIMS 03-18-001, ASNA3462, CR1.2.0.1, AIMS 03-18-001 (ABS 5125A), ASME SB-265,
ASME SB-348, AMS 4928, AMS 4965, AMS 4967, AMS 4907, AMS 4905
6AL-4V Titanium Sheet Plate Per AMS 4911 Rev H,
Rev. J, Rev. L,
AMS-T-9046 A AB-1 DMS 1592, MIL-T-9046 Type Comp
C, AB-1 Am.2 PWA/LCS, MSRR 8632, AIMS 03-18-003, AIMS 03-18-004, BST2A10,
BSTA59, EN3544, ASNA3200, CR1.2.0.1, ASTM B265 Gr5
Thickness from 0.012", 36" x 96" Standard size
=> We have Domestic 6AL-4V sheets
special. Please call now for special
pricing
0.032 x 36 x 96 Per AMS 4911,
0.040 x 36 x 96 Per AMS 4911,
0.063 x 36 x 96 Per AMS 4911
0.071 x 36 x 96 Per AMS 4911,
0.080 x 36 x 96 Per AMS 4911, 0.090 x 36 x 96 Per AMS 4911
Titanium 6AL-4V Bar, Forging
6AL-4V: AMS 4928, AMS 4967, AMS 6931, AMS 2631, MIL-T-9047,
ASTM-B-348 Gr5, ASTM-F-1472, PWA/LCS, GE S400 & S1000, Capable of AMS 4965
ISO5832 Pt3, EN3311, ASME SB-265, ASME SB-348, AMS 4965
0.063" Dia to 6.00 Dia
6AL-4V Titanium Flat Bar Round Bar Per AMS 4928,
ASTM B-348 Grade 5
Titanium 6AL-4V Tubing
1) Seamless Tubing: O.D. 1/8" to 1-1/2"
2) Welded
Tubing:
O.D. 1/2" to 2"
Other sizes are available on request.
, %
|
MIN |
5.5 |
3.5 |
-- |
-- |
-- |
-- |
-- |
-- |
-- |
-- |
-- |
|
MAX |
6.75 |
4.5 |
0.08 |
0.05 |
0.2 |
0.0125 |
0.3 |
0.005 |
0.1 |
0.4 |
Balance |
Density: 0.160 lb/inch3
Melting Range: 2929 - 3020 Degrees F
Beta Transus: 1825 + or - 25 Degrees F
|
Temperature, Degrees F |
70 |
200 |
400 |
600 |
|
Coefficient of Thermal Expansion, in/in
Degrees Fx 10-6 |
- |
5.3 |
5.4 |
5.5 |
Thermal Conductivity,
Btu • Ft/Ft² • Hr Degrees FSTA |
4.0 |
4.3 |
5.2 |
6.1 |
Modulus of Elasticity,
psi X 106 STA |
16.7 |
16.0 |
15.0 |
14.0 |
Specified,
AMS 4911, annealed sheet & plate
|
|
Anneal 1300 Degrees F, Air Cool |
Anneal 1300 Degrees F, Solution anneal 1750
Degrees F, Age 1000 Degrees F |
|
Ultimate Tensile Strength, ksi |
138-155 |
150-172 |
|
0.2% Yield Strength, ksi |
128-147 |
137-156 |
|
Elongation, % |
15-20 |
15-17 |
|
Reduction of Area, % |
38-51 |
41-46 |
Typical Tensile Strength and Fracture
Toughness, Various Heat Treatments for Flat-rolled Products (MCIC-HB-02 1985
reprint)
|
|
0.2% Yield Strength, ksi |
Fracture Toughness K1C, ksi √in |
Annealed
(Continuously Rolled Sheet) |
132
142 (transversea) |
128
140 (transversea) |
|
Beta Annealed (plate) |
131 |
134 |
|
Beta STA 1250 Degrees Fb |
128 |
150 |
|
Beta STA 1000 Degrees Fb |
143 |
120 |
|
STA 1250 Degrees Fc |
137 |
105 |
|
STA 1000 Degrees Fc |
159 |
80 |
(a) Directional variations,
(b) Beta heat treated followed by solution treating and overaging 1250
Degrees F, or aging 1000 Degrees F
(c) Solution treating and overaging 1250 Degrees F, or aging 1000 Degrees F
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