4.2.1 AZ31B
4.2.1.0
Comments and Properties — AZ31B is a wrought magnesium-base alloy containing aluminum and zinc. It is available in the form of sheet, plate, extruded sections, forgings, and tubes. AZ31B has good room-temperature strength and ductility and is used primarily for applications where the temperature does not exceed 300°F. Increased strength is obtained in the sheet and plate form by strain hardening with a subsequent partial anneal (H24 and H26 temper). No treatments are available for increasing the strength of this alloy after fabrication.
Forming of AZ31B must be done at elevated temperatures if small radii or deep draws are required. If the temperatures used are too high or the times too great, H24 and H26 temper material will be softened. This alloy is readily welded but must be stress relieved after welding to prevent stress corrosion cracking.
Material specifications covering AZ31B wrought products are given in Table 4.2.1.0(a). Room-temperature mechanical and physical properties are shown in Tables 4.2.1.0(b) through (d). The effect of temperature on physical properties is shown in Figure 4.2.1.0.
Table 4.2.1.0(a). Material Specifications
for AZ31B Magnesium Alloy
| Specification | Form |
|---|---|
| AMS 4375 | Sheet and plate |
| AMS 4376 | Plate |
| AMS 4377 | Sheet and plate |
| ASTM B 107 | Extrusion |
| ASTM B 91 | Forging |
The temper index for AZ31B is as follows:
| Section | Temper |
|---|---|
| 4.2.1.1 | O |
| 4.2.1.2 | H24 |
| 4.2.1.3 | H26 |
| 4.2.1.4 | F |
4.2.1.1
AZ31B-O Temper — Effect of temperature on the tensile modulus of sheet and plate is presented in Figure 4.2.1.1.4. Typical room-temperature stress-strain and tangent-modulus curves are presented in Figure 4.2.1.1.6.
4.2.1.2
AZ31B-H24 Temper — Effect of temperature on the mechanical properties of sheet and plate is shown in Figures 4.2.1.2.1 through 4.2.1.2.4, and 4.2.1.2.6. Typical room-temperature tension and compression stress-strain and tangent-modulus curves for sheet are shown in Figure 4.2.1.2.6.
4.2.1.3 AZ31B-H26 Temper
4.2.1.4
AZ31B-F Temper — Figures 4.2.1.4.8 (a) and (b) contain fatigue data for forged disk at room temperature.
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4.2.2 AZ61A
4.2.2.0
Comments and Properties — AZ61A is a wrought magnesium-base alloy containing aluminum and zinc. It is available in the form of extruded sections, tubes, and forgings in the as-fabricated (F) temper. AZ61A is much like AZ31B in general characteristics. The increased aluminum content increases the strength and decreases the ductility slightly.
Severe forming must be done at elevated temperatures. This alloy is readily welded but must be stress relieved after welding to prevent stress corrosion cracking.
Material specifications covering AZ61A are given in Table 4.2.2.0(a). Room-temperature mechanical and physical properties are shown in Table 4.2.2.0(b).
| Specification | Form |
|---|---|
| AMS 4350 | Extrusion |
| ASTM B 91 | Forging |
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4.2.3 ZK60A
4.2.3.0
Comments and Properties — ZK60A is a wrought magnesium-base alloy containing zinc and zirconium. It is available as extruded sections, tubes, and forgings. Increased strength is obtained by artificial aging (T5) from the as-fabricated (F) temper. ZK60A has the best combination of high room-temperature strength and ductility of the wrought magnesium-base alloys. It is used primarily at temperatures below 300°F.
ZK60A has good ductility as compared with other high-strength magnesium alloys and can be formed or bent cold into shapes not possible with those alloys having less ductility. It is not considered a weldable alloy.
Material specifications for ZK60A are given in Table 4.2.3.0(a). Room-temperature mechanical and physical properties are shown in Tables 4.2.3.0(b) and (c). Elevated temperature curves for physical properties are shown in Figures 4.2.3.0.
| Specification | Form |
|---|---|
| ASTM B 107 | Extrusion |
| AMS 4352 | Extrusion |
| AMS 4362 | Die and hand forgings |
The temper index for ZK60A is as follows:
| Section | Temper |
|---|---|
| 4.2.3.1 | F |
| 4.2.3.2 | T5 |
4.2.3.1 ZK60A-F Temper
4.2.3.2
ZK60A-T5 Temper — Typical room-temperature tension and compression stress-strain curves for extrusions are shown in Figures 4.2.3.2.6(a) and (b). Fatigue curves are presented in Figure 4.2.3.2.8(a) through (c).