In projecting applications of magnesium alloys at elevated temperatures, the tensile and other mechanical properties
at the particular service temperatures must be considered. On account of their relatively low melting points, below
about 650°C (1200°F), the commercial alloys are necessarily confined to use at only moderately elevated temperatures.
As in the case of aluminum alloys, the safe operating temperatures for magnesium alloys are far below those of steels.
Depending upon the composition, magnesium alloys begin to melt at a temperature in the range of about
685°F (360°C) to 1200°F (650°C). The common alloys begin to soften and weaken appreciably on exposure to temperatures
as low as 200°F (95°C). However, some special compositions have been recently developed which maintain yield and
tensile strength quite well at temperatures up to 400°F (205°C) or higher.
The strength, hardness, and modulus of elasticity of magnesium-base materials decrease with increasing temperature.
Also, the elongation increases with rising temperature up to just below the melting point where it drops to nearly zero.
As indicated, some magnesium alloys have been developed for use at moderately elevated temperatures. In several of
these the principal alloying ingredient is mischmetal; other additions may include manganese or zirconium. These
compositions make possible the utilization of magnesium alloys under load at substantially higher temperatures than formerly.
Creep and stress-rupture data are important in considering magnesium alloys for various high-temperature applications.
Not many test data are available which show the effect of elevated temperatures on the fatigue strength of magnesium alloys.
Under conditions where creep may arise (static loading at elevated temperature), it is useful in design to compare with
the yield strength and tensile strength, for the temperatures of interest, the stress for a certain deformation or the
stress-to-rupture under creep-loading conditions. Creep data may be used in a comparative and qualitative way.
The usual commercial magnesium alloys of the aluminum-zinc (manganese) type are relatively stable up to about
300°F (150°C) and may be used for some applications below that temperature. Solution heat-treated castings and
hard-rolled sheet in the usual alloys are unstable above 300°F (150°C) and are not suitable for use at elevated
As indicated, the ordinary magnesium-base materials used for castings or for wrought products have comparatively poor
strength and poor resistance to creep at elevated temperatures. Investigations have shown that the addition of rare-earth
metals, in the form of mischmetal, to magnesium will yield alloys that retain much of their strength at elevated
temperatures and exhibit relatively high resistance to creep over a wide range of temperature.
Tests have shown that various zinc-bearing magnesium alloys containing also, for example, small amounts of zirconium or
manganese exhibit good resistance to creep at elevated temperatures. This refers to compositions for sand casting.
Among these alloys ZK61 and ZM60 may be mentioned. They have higher creep resistance than AZ92 and AZ63 alloys but
lower than the RE-bearing alloys. Also, these zinc-bearing alloys have good tensile properties at both room and elevated
Other recent investigations have shown that additions of thorium to magnesium yield alloys with the highest creep resistance
up to 600°F (315°C) of any magnesium alloy standard to date. Also, additions of zirconium to thorium-bearing alloys refine
the grain without impairing the creep properties at elevated temperatures. An investigation was recently carried out to
develop a magnesium alloy, for wrought products, having optimum mechanical properties at elevated temperatures.
The selection of an alloy for applications requiring high creep resistance must take into consideration the temperature
to be encountered as well as the level of stress. In the use of cast magnesium alloys it has been suggested that service
conditions be divided into three ranges of temperature. These are as follows: (1) Up to 250°F (120°C); (2) from
250° to 400°F (120°C to 205°C), approximately; and (3) above 400° or perhaps 450°F (205°C or 230°C).
This division would allow the use of certain alloys in the lower range, although their creep resistance is relatively poor
at higher temperatures. At the same time, advantage would be taken of their relatively good mechanical properties at room
temperature and their satisfactory castability. Alloys ZK61 and ZM60 fall into this category. For the highest temperature
range, alloys with the best creep resistance may be requisite irrespective of their mechanical properties at the ordinary
temperature or their foundry behavior. The ranges of temperature given also apply in the case of wrought compositions.
The structural or metallographic condition having the maximum resistance to creep at elevated temperatures is produced by
means of suitable heat treatment. This varies with the alloy composition and the form of the material (whether cast or
wrought). The most suitable conditions for resisting creep are T2, T6, and T7. These are effected, respectively, by
stabilization of as fabricated (F) products, solution heat treatment and aging, and solution heat treatment followed by
Properties After Heating
Some data are available which show the effect of heating magnesium alloys to elevated temperatures on their mechanical
properties at room temperatures.
Short-time heating at temperatures up to 650°F (340°C), as may be required in forming sheet or for straightening certain
products, or as may occur during the service life of a part or structure, effects changes in the room-temperature properties
of various magnesium alloys.
In general, magnesium-alloy castings used in the as-cast (F) or solution heat-treated (T4) condition gain in yield strength
and lose in elongation on heating for a sufficient period of time in the range up to 650°F (340°C). Castings in the solution
heat-treated and aged (T6) condition lose in yield strength on such heating.
In nearly all cases, the short-time heating of annealed or hot finished magnesium-base products at temperatures up to
650°F (340°C) is without effect on the mechanical properties. The heating of alloy sheet in the hard-rolled temper (H) to
500°-600°F (260°-315°C) practically results in complete annealing and yields the properties of the soft temper (O).
Mechanical Properties at Low Temperatures
In general, the yield strength, tensile strength, and hardness of magnesium-base alloys increase more or less substantially
with decrease in temperature below zero while the elongation and impact resistance decrease. Also, the endurance limit is
raised appreciably as the temperature is lowered. These changes apply to both cast and wrought alloys. The individual effects
vary depending upon the alloy composition, temper, condition (whether cast or wrought), and the subzero temperature.
As concerns the cast alloys, it appears that the T4 temper is better than the F or T6 temper in behavior at the low
temperature -108°F (-80°C). Thus, it exhibits the greatest increase in strength and hardness and the least loss of elongation
and impact resistance on cooling to the temperature stated. In addition, the alloys in the T4 temper more nearly assume their
original properties on again attaining room temperature.
The wrought alloys in the F temper undergo greater overall changes in tensile properties than do the cast compositions on
cooling to -108°F (-80°C). Rather remarkable increases in yield strength and tensile strength are exhibited by the wrought
materials on cooling to -320°F (-195°C).
The modulus of elasticity of magnesium alloys generally increases at low temperatures. The increase from room temperature
to -320°F (-195°C) was 14.7 per cent. Some data are available which show the effect of low temperatures on the fatigue
strength of magnesium alloys. In general, the fatigue strength increases with decreasing temperature. The amount of increase
is quite variable depending upon the composition of the alloy, condition (whether cast or wrought), and number of fatigue
cycles, temperature, and other factors.
The notch-impact resistance of magnesium-base alloys, both cast and wrought, shows a downward trend as the temperature is
lowered. The total change is markedly variable depending on sundry factors.