Description:
Titanium gradu VI Alloy offert bonum weldability, stabilitas et vires ad elevatum temperaturis. Hoc est maxime communiter propter airframe et Jet Engine applications requiring bonum weldability, stabilitas et vires ad elevatum temperaturis.
| Applicatio | Aerospace |
| Signa | ASME SB - CCCLXXXI, AMS (IV) CMLXVI, MILL - T - (IX) XLVI, MIL - T - (IX) XLVII, AMS (IV) CMLVI, AMS (IV) CMLXXVI, (IV) CMXVI, AMS (IV) CMXXVI |
| Available | Bar, sheet, laminam, tubo, pipe, cudens, fastener, conveniens filum |
Chemical compositionem (nominis)%:
|
Fe |
Sn |
Al |
H |
N |
O |
C |
|
≤0.50 |
2.0 - 3.0 |
4.0 - 6.0 |
0.175 - 0,2 |
≤0.05 |
≤0.2 |
0.08 |
Ti = Bal.