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7178

AMS QQ-A-200/13 / AlZn7MgCu / 7178 / T6

Kimyasal Kompozisyon % Değer
Silicon (Si)0,00 - 0,40
Chromium (Cr)0,18 - 0,28
Manganese (Mn)0,00 - 0,30
Magnesium (Mg)2,40 - 3,10
Copper (Cu)1,60 - 2,40
Titanium (Ti)0,00 - 0,20
Iron (Fe)0,00 - 0,50
Zinc (Zn)6,30 - 7,30
Aluminium (Al)Balance
Fiziksel Özellikler Değer
Yoğunluk2,83 g/cm³
Erime Sıcaklığı477 °C
Isıl Genleşme K.23.5 x 10^-6 /K
Elastisite Modülü%10
Isıl Kapasite140 W/m.K
Mekanik Özellikler Değer
Akma Dayanımı550 MPa
Çekme Dayanımı610 MPa
Kesme Dayanımı340 MPa
Uzama%10
Elastisite72 GPa
7178 aluminum is a strong, high strength material having moderate temperature applications. This alloy was intended primarily for advanced subsonic aircraft applications.

 

ALLOY DESIGNATIONS
AMS QQ-A-250/21, 7178 has similarities to the following standard designations and specifications ;

 

Alloy 7178, UNS A97178, ASTM B209

AlZn7MgCu

 

TEMPER TYPES

7178 is supplied in a wide range of tempers:
 
  • O - Soft
  • T6 - Solution heat-treated and then artificially aged.
  • T6510 - Solution heat-treated, stress-relieved by controlled stretching (permanent set 1% to 3% for extruded rod, bar, shapes and tube, 0.5% to 3% for drawn tube) and then artificially aged. The products receive no further straightening after stretching.
  • T6511 - Same as T6510 except that minor straightening is allowed after stretching to comply with standard tolerances
  • T76 - Solution heat-treated and then artificially overaged in order to achieve a good exfoliation corrosion resistance.
  • T7651 - Solution heat-treated, stress-relieved by controlled stretching (permanent set 1% to 3% for extruded rod, bar, shapes and tube, 0.5% to 3% for drawn tube) and then artificially overaged in order to achieve a good exfoli-ation corrosion resistance. The products receive no further straightening after stretching.
  • T76510 - Solution heat-treated, stress-relieved by controlled stretching and then artificially overaged in order to achieve a good exfoli-ation corrosion resistance. The products receive no further straightening after stretching.
  • T76511 - Solution heat-treated, stress-relieved by controlled stretching and then artificially overaged in order to achieve a good exfoli-ation corrosion resistance. The products receive no further straightening after stretching except that minor straightening is allowed after stretching to comply with standard tolerances.
 
 
SUPPLIED FORMS
7178 is supplied in plate, sheet and extrusions.
  • Plate
  • Sheet
  • Tube / Extrusions
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