Durum aircraft aluminium laminam altum tensile vires Alloy Type MMCXXIV Grade
Durum aircraft aluminium laminam altum tensile vires Alloy Type MMCXXIV Grade
MMCXXIV Alloy est typical durum Aluminium Aluminium in Aluminium-aeris, Magnesium series. In characteres huius materiales sunt cum princeps viribus et cum quadam calor resistentia, potest esse ut opus pars infra CL ℃. Vires altior quam (VII) LXXV si opus temperatus super CXXV ℃. Formability est melius sub calidum, annealing et extinguantur conditionibus. Et effectus caloris confirmatur significantly. In Alloy MMCXXIV late in aircraft structurae, rivets, salsissimus vir vivens hubs, propeller components et alia structural components.
Chemical compositionem WT (%) | |||||||||
Silicon | Ferrum | Aes | Magnesium | Manganese | Chromium | Zinc | Titanium | Alii | Aluminium |
0,2 | 0,3 | 3,8 ~ 4,9 | 1.2 ~ 1.8 | 0,3 ~ 0.9 | 0.1 | 0,25 | 0.15 | 0.15 | Statera |
Typical mechanica proprietatibus | |||
Crassities (M) | Tensile vires (MPa) | CEDITAS (MPa) | Elongatio (%) |
0,3 ~ CCCL | CCCXLV ~ CDXXV | CCXLV ~ CCLXXV | ≥7 |
Applications
Vivamus structururibus
![Aviation1-01](http://www.aviationaluminum.com/uploads/094854b11.jpg)
Praecisione partes
![CNC cum Aluminium](http://www.aviationaluminum.com/uploads/d5945e7a.jpg)
Cornu tensio membra
![Cornu, tensio, membris](http://www.aviationaluminum.com/uploads/0558cdc1.jpg)
PARTIS
![CNC cum Aluminium](http://www.aviationaluminum.com/uploads/0d3346c9.jpg)
Nostro
![1050Aluminum04](http://www.aviationaluminum.com/uploads/0e25dce32.jpg)
![1050Aluminum05](http://www.aviationaluminum.com/uploads/821ac2ed1.jpg)
![1050Aluminum-III](http://www.aviationaluminum.com/uploads/5189bf3d2.jpg)
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.