MMXIV gradu aircraft aluminium laminam princeps vires customized crassitudine
MMXIV gradu aircraft aluminium laminam princeps vires customized crassitudine
MMXIV Aluminium laminam habet princeps vires et bonum cutting perficientur, sed pauper corrosio resistentia. Late usus est in aircraft structurae (cutis, ossa, costa trabem, bulkhead, etc.) rivets, missile components, salsissimus vir vivens rotam hubs, propeller components et alia structural components.
T3 ingenium, T4 et T6.
| Chemical compositionem WT (%) | |||||||||
| Silicon | Ferrum | Aes | Magnesium | Manganese | Chromium | Zinc | Titanium | Alii | Aluminium |
| 0,5 ~ 1.2 | 0,7 | 3,9 ~ V | 0,2 ~ 0,8 | 0,4 ~ 1.2 | 0.1 | 0,25 | 0.15 | 0.15 | Statera |
| Typical mechanica proprietatibus | |||
| Crassities (M) | Tensile vires (MPa) | CEDITAS (MPa) | Elongatio (%) |
| 0,5 ~ CC | ≥360 | ≥240 | VI ~ XV |
Applications
Aircraft structurae
CARRUS rota hubs
Nostro
Inventarium et partus
Habemus satis uber in stirpe, possumus offerre satis materiam ad customers. Et plumbum tempus potest esse in VII dies pro stirpe.
Qualis
Omnis uber sunt ex maximus fabrica, possumus offerre MTC tibi. Et non potest etiam offerre tertius-pars test fama.
Consuetudo
Nos have cutting apparatus, consuetudo mole sunt available.
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