1. Home Page
  2. Articles
  3. Magnesium Alloy and Temper Designations

Magnesium Alloy and Temper Designations

Abstract

Magnesium and magnesium alloys serve critical roles in diverse structural applications across automotive, industrial, materials-handling, commercial, and aerospace sectors. These lightweight materials offer exceptional strength-to-weight ratios, making them ideal for high-speed machinery components, automotive parts like transmission housings, and aerospace applications requiring superior performance at elevated temperatures. Beyond structural uses, magnesium functions as an essential alloying element and reducing agent in metallurgical processes. This article examines the standardized designation system for magnesium alloys according to ASTM B 275, explaining how alloy compositions and temper conditions are systematically classified through alphanumeric codes that indicate principal alloying elements, their percentages, and heat treatment conditions.


Applications of Magnesium Alloys in Modern Industry

Magnesium and magnesium alloys are utilized in an extensive range of structural applications across automotive, industrial, materials-handling, commercial, and aerospace equipment sectors. The versatility of these lightweight materials makes them indispensable in modern manufacturing.

In automotive applications, magnesium alloys are commonly found in clutch and brake pedal support brackets, steering column lock housings, and manual transmission housings. These components benefit from magnesium's excellent strength-to-weight ratio, which contributes to overall vehicle weight reduction and improved fuel efficiency.

Industrial machinery applications leverage magnesium alloys for components that operate at high speeds, where lightweight construction is essential to minimize inertial forces. This characteristic enables more efficient operation and reduced wear on mechanical systems. Commercial applications demonstrate the material's versatility through its use in hand-held tools, luggage, computer housings, and ladders, where portability and durability are paramount.

Aerospace and Specialized Applications

Magnesium alloys prove particularly valuable for aerospace applications due to their lightweight properties combined with excellent strength and stiffness characteristics at both room and elevated temperatures. These properties make them ideal for aircraft components where weight reduction directly impacts fuel efficiency and performance.

Non-Structural Applications and Metallurgical Uses

Beyond structural applications, magnesium serves crucial roles in various non-structural applications. It functions as an alloying element in aluminum, zinc, lead, and other nonferrous metal alloys, enhancing their mechanical properties and performance characteristics.

In metallurgical processes, magnesium acts as an oxygen scavenger and desulfurizer during the manufacture of nickel and copper alloys. The iron and steel industry utilizes magnesium as a desulfurizer, while it serves as a reducing agent in beryllium and titanium production. Gray iron foundries employ magnesium and magnesium-containing alloys as ladle addition agents, introducing them just before casting to improve the final product's properties. Additionally, magnesium finds applications in pyrotechnics due to its combustion characteristics.

Understanding the ASTM B 275 Designation System

The designation system for magnesium alloys follows a standardized format established by ASTM B 275. This systematic approach ensures consistent identification and specification of alloy compositions and temper conditions across the industry.

Alloy designations consist of no more than two letters representing the alloying elements present in the greatest amounts. These letters are arranged in order of decreasing percentages, or alphabetically when percentages are equal. Following the letters, the respective percentages are rounded to whole numbers, and a serial letter completes the designation. While the full name of the base metal typically precedes the designation, it may be omitted for brevity when the context clearly indicates magnesium as the base material.

Table 1. A standard system of alloy and temper designations, according to ASTM B 275

First part Second part Third part Fourth part
Indicates the two principal alloying elements Indicates the amounts of the two principal alloying elements Distinguishes between different alloys with the same percentages of the two principal alloying elements Indicates condition (temper)
Consists of two code letters representing the two main alloying elements arranged in order of decreasing percentage (or alphabetically if percentages are equal) Consists of two numbers corresponding to rounded-off percentages of the two main alloying elements and arranged in same order as alloy designations in first part Consists of a letter of the alphabet assigned in order as compositions become standard Consists of a letter followed by a number (separated from the third part of the designation by a hyphen)
A-aluminum
B-bismuth
C-copper
D-cadmium
E-rare earth
F-iron
G-magnesium
H-thorium
K-zirconium
L-lithium
M-manganese
N-nickel
P-lead
Q-silver
R-chromium
S-silicon
T-tin
W-yttrium
Y-antimony
Z-zinc
Whole numbers Letters of alphabet except I and O F-as fabricated
O-as annealed
H10 and H11- slightly strain hardened
H23,H24 and H26- strain hardened and partially annealed
T4-solution heat treated
T5-artificially aged only
T6-solution heat treated and artificially aged
T8-solution heat treated, cold worked and artificially aged

Practical Example: Decoding AZ81A-T4

To illustrate the designation system's practical application, consider magnesium alloy AZ81A-T4. This designation can be systematically decoded as follows:

The initial portion "AZ" signifies that aluminum and zinc constitute the two principal alloying elements in this magnesium-based alloy. The numerical designation "81" indicates the rounded percentages of these primary alloying elements: 8% aluminum and 1% zinc respectively.

The letter "A" serves as a serial identifier, indicating this represents the first standardized alloy composition with 8% aluminum and 1% zinc as the principal alloying additions. This systematic lettering prevents confusion between different alloys with similar but distinct compositions.

The final designation "T4" specifies the temper condition, indicating that this particular alloy has undergone solution heat treatment. This heat treatment process significantly influences the material's mechanical properties and performance characteristics.

January, 2001

Instantly Find and Compare Materials from Different Standards!

Total Materia Horizon contains detailed and precise property information for hundreds of thousands of materials according to all standards worldwide, updated monthly.

Instantly Find and Compare Materials from Different Standards!

Get a FREE test account at Total Materia Horizon and join a community of over 500,000 users from more than 120 countries.

Contact Us
Solve Your Materials Challenges
Get Free Access!