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7178

ASTM B221 / AlZn7MgCu / 7178 / T6511

化学性质 % 值
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
物理特性
Density2,83 g/cm³
Melting Point479 °C
Thermal Expansion23.5 x 10^-6 /K
Modulus of Elasticity71 GPa
Thermal Conductivity130 W/m.K
Electrical Resistivity31% IACS
机械性能
Proof Strength560 MPa
Yield Strength630 MPa
Shear Strength370 MPa
Elongation A50 mm5%
Hardness160 HB
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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