Alloy 2017

Chemical Composition Limits Others
Weight % Si Fe Cu Mn Mg Cr Zn Ti Each Total
Minimum 0.20 - 3.5 0.40 0.40 - - - - -
Maximum 0.8 0.7 4.5 1.0 0.8 0.10 0.25 0.15 0.05 0.15

Typical Physical Properties
Characteristic English Metric
Nominal Density (68 °F/20 °C) 0.101 lbs./in.3 2.80 Mg/m3
Melting Range 955 °F - 1185 °F 513 °C - 640 °C
Specific Heat (212 °F/100 °C) - -
Coefficient of Thermal Expansion
Linear
68 °F-212 °F
20 °C-100 °C
12.7 micro in./in.-°F 22.9 micro m/m -°K
Volumetric
68 °F/20 °C
3.67 x 10-5in.3/in.3 -°F 66 x 10-6m3/m3 -°K
Thermal Conductivity (68°F/20°C) O Temper 112 BTU/ft. - hr. - °F 193 W/m - °K
T4, T451 77.5 BTU/ft. - hr. - °F 134 W/m - °K
Electrical Conductivity (68°F/20°C) Equal Volume O Temper 50% IACS
T4, T451 34% IACS
Equal Weight O Temper 159% IACS
T4, T451 108% IACS

Typical Mechanical Properties
  Tensile (.500" Dia. Specimen) Hardness Shear Fatigue1 Modulus
Temper Yield Ultimate Elongation/4D
Brinell
500kg
10 mm
Ultimate Shearing Strength Endurance Limit R.R. Moore Type Modulus of Elasticity
KSI MPa KSI MPa %   KSI MPa KSI MPa KSI x 103 Gpa
O 10 69 26 179 22 45 18 124 13 90 10.5 72.4
T4, T451 40 276 62 427 22 105 38 262 18 124 10.5 72.4
1 5 x 10E8 cycles of reversed stress
Comparative Characteristics
Temper Corrosion Resistance
Cold
Workability3
Machin-
ability3
Anodize
Response3
Braze-
ability4
Weldability4
General1 Stress2 Gas Arc Spot
T4,T451 D C C B C D D B B
1 Ratings A through E are relative ratings in decreasing order of merit, based on exposures to sodium chloride solution by intermittent spraying or immersion. Alloys with A and B ratings can be used in industrial and seacoast atmospheres without protection. Alloys with C, D and E ratings generally should be protected at least on faying surfaces.
2 Stress-corrosion cracking ratings are based on service experience and laboratory tests of specimens exposed to the 3.5% sodium chloride alternate immersion test.
A= No known instance of failure in service or in laboratory tests.
B= No known instance of failure in service; limited failures in laboratory tests of short transverse specimens.
C= Service failures with sustained tension stress acting in short transverse direction relative to grain structure; limited failures in laboratory tests of long transverse specimens.
D= Limited service failures with sustained longitudinal or long transverse

3 Ratings A through D for Workability (cold), A through E for Machinability and A through C for Anodize Response, are relative ratings in decreasing order of merit.
4 Ratings A through D for Weldability and Brazeability are relative ratings defined as follows:
A= Generally weldable by all commercial procedures and methods.
B= Weldable with special techniques or for specific applications that justify preliminary trails or testing to develop welding procedure and weld performance.
C= Limited weldability because of crack sensitivity or loss in resistance to corrosion and mechanical properties.
D= No commonly used welding methods have been developed.
Applicable Specifications  
Cold Finished Extruded
ASTM B211  
QQ-A-225/3  
AMS 4118  

Alloy Description
Like 2011, this is also a general-purpose alloy for automatic screw machine work. It is stronger than 2011, but harder to machine and does not have the fine chip associated with 2011. It is recommended for heavy-duty parts because of its high strength. Workability is fair, with ductility and formability considered better that 2014. Arc and resistance weldability are satisfactory. Corrosion resistance is fair. It is used for rivets, fasteners and aircraft components.

 
 
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