|
:: Titanium Aerospace grade
sheets/plates
A40, Ti CP Grade 2, AMS 4902 / MIL-T 9046 (UNS R50400)
A70, Ti CP Grade 4, AMS 4901 / MIL-T 9046 (UNS
R50700)
Ti6Al4V (6AL-4V), AMS 4911 / MIL-T 9046 (UNS
R56400)
>
A40, Ti CP Grade 2, AMS 4902 / MIL-T 9046 (UNS R50400)
Typical applications include : Industrial,
aerospace components; heat exchangers, wire, CPI
equipment, medical and dental devices, tubing, pickling baskets.
Standard stock sizes
|
Sheet/Plate Thickness in mm (metric) |
|
0.30 |
0.40 |
0.50 |
0.65 |
0.80 |
1.0 |
1.6 |
|
|
|
Nominal Chemical composition in %
| C |
Fe |
H |
N |
O |
Ti |
| 0.10 max |
0.30 max |
0.015 max |
0.03 max |
0.25 max |
rem |
Typical
Mechanical Properties
| Density lb/in3 (g/cm3) |
0.163 (4.51) |
| Metallurgical Condition |
1,300 °F anneal |
| Tensile Strength, ksi (MPa) |
50 (345) |
| 0.2% Yield Strength, ksi (MPa) |
40 (276) |
| Elongation, % |
20 |
| Reduction in Area, % |
30 |
| Typical Hardness |
80 HRB |
> A70, Ti CP Grade 4, AMS 4901 / MIL-T 9046 (UNS
R50700) Typical applications include :
Industrial, aerospace components; heat exchangers,
cryogenic vessels, wire, CPI equipment, medical and
dental devices, tubing.
Standard stock sizes
|
Sheet/Plate Thickness in mm (metric) |
|
0.30 |
0.40 |
0.50 |
0.65 |
0.80 |
1.0 |
1.6 |
2.0 |
|
|
Nominal Chemical composition in %
| C |
Fe |
H |
N |
O |
Ti |
| 0.10 max |
0.50 max |
0.015 max |
0.05 max |
0.40 max |
rem |
Typical
Mechanical Properties
| Density lb/in3 (g/cm3) |
0.163 (4.51) |
| Metallurgical Condition |
1,300 °F anneal |
| Tensile Strength, ksi (MPa) |
80 (552) |
| 0.2% Yield Strength, ksi (MPa) |
70 (483) |
| Elongation, % |
15 |
| Reduction in Area, % |
25 |
| Typical Hardness |
100 HRB |
> Ti6Al4V
(6AL-4V), AMS 4911 / MIL-T 9046 (UNS
R56400) Typical
applications include :
Blades, wheels, discs,
rings, fasteners, cases, hubs, vessels, forgings, wire, CPI equipment,
medical and dental devices
Standard stock sizes
|
Sheet/Plate Thickness in mm (metric) |
|
0.30 |
0.40 |
0.50 |
0.65 |
0.80 |
1.0 |
1.6 |
1.8 |
2.0 |
2.3 |
|
2.5 |
3.175 |
4.75 |
6.35 |
9.5 |
12.7 |
19.0 |
25.4 |
31.75 |
38.1 |
Nominal Chemical composition in %
| C |
Fe |
H |
N |
O |
Al |
V |
Ti |
| 0.10 max |
0.20 |
0.015 max |
0.03 |
0.20 max |
6.0 |
4.0 |
rem |
Typical
Mechanical Properties
| Density lb/in3 (g/cm3) |
0.160 (4.43) |
| Metallurgical Condition |
1,300 °F anneal |
| Tensile Strength, ksi (MPa) |
135 (931) |
| 0.2% Yield Strength, ksi (MPa) |
125 (862) |
| Elongation, % |
15 |
| Reduction in Area, % |
30 |
| Typical Hardness |
36 HRC |
*Alloys A40 & A70 are trade marks of
Allegheny Technologies USA. |
