The welding of aluminium and its alloys

Precipitation (age) hardening

Microstructures with two or more phases present possess a number of ways in which the phases can form. The geometry of the phases depends on their relative amounts, whether the minor phase is dispersed within the grains or is present on the grain boundaries and the size and shape of the phases. The phases form by a process known as precipitation, which is both time and temperature controlled and which requires a reduction in solid solubility as the temperature falls, i. e. more of the solute can dissolve in the solvent at a high temperature than at a low temperature. A simple analogy here is salt in water - more salt can be dissolved in hot water than in cold. As the tem­perature is allowed to fall, the solution becomes saturated and crystals of salt begin to precipitate.

A similar effect in metals enables the microstructure of a precipitation hardenable alloy to be precisely controlled to give the desired mechanical properties. To precipitation or age harden an alloy the metal is first of all heated to a sufficiently high temperature that the second phase goes into solution. The metal is then ‘rapidly’ cooled, perhaps by quenching into water or cooling in still air - the required cooling rate depends upon the alloy system. Most aluminium alloys are quenched in water to give a very fast cooling rate. This cooling rate must be sufficiently fast that the second phase does not have time to precipitate. The second phase is retained in solution at room temperature as a super-saturated solid solution which is metastable,

Precipitation (age) hardening

SHAPE * MERGEFORMAT

Precipitation (age) hardening

Annealed structure - coarse

precipitates on the grain boundaries

Solution treated - precipitates retained in solution

Correctly aged - fine dispersion of precipitates within the grains

Overaged - coarse precipitates within the grains

2.6 Illustration of the solution treatment and age-(precipitation) hardening heat treatment cycle.

that is, the second phase will precipitate, given the correct stimulus. This stimulus is ageing, heating the alloy to a low temperature. This allows dif­fusion of atoms to occur and an extremely fine precipitate begins to form, so fine that it is not resolvable by normal metallographic techniques. This precipitate is said to be coherent, the lattice is still continuous but distorted and this confers on the alloy extremely high tensile strength. In this world, there is no such thing as a free lunch, so there is a marked drop in ductil­ity to accompany this increase in strength.

If heating is continued or the ageing takes place at too high a tempera­ture the alloy begins to overage, the precipitate coarsens, perhaps to a point where it becomes metallographically visible. Tensile strength drops but duc­tility increases. If the overageing process is allowed to continue then the alloy will reach a point where its mechanical properties match those of the annealed structure.

Too slow a cooling rate will fail to retain the precipitate in solution. It will form on the grain boundaries as coarse particles that will have a very limited effect on mechanical properties. The structure is that of an annealed metal with identical mechanical properties. The heat treatment cycle and its effects on structure are illustrated in Fig. 2.6.

Table 2.1 Summary of mechanical properties for some aluminium alloys

Alloy

Condition

Proof (N mm2)

UTS (N mm2)

Elongation

(%)

1060

O

28

68

43

1060

H18

121

130

6

5083

O

155

260

14

5083

H34

255

325

5

6063

O

48

89

32

6063

TB(T4)

100

155

15

6063

TF(T6)

180

200

8

2024

O

75

186

20

2024

TB(T4)

323

468

20

UTS: ultimate tensile strength

Summary

This chapter is only the briefest of introductions to the science of metals, how crystal structures affect the properties and how the fundamental mech­anisms of alloying, hardening and heat treatment, etc., are common to all metals. Table 2.1 gives the effects of solid solution strengthening, cold working and age hardening. It illustrates how by adding an alloying element such as magnesium, the strength can be improved by solid solution alloy­ing from a proof strength of 28N/mm2 in an almost pure alloy, 1060, to 115 N/mm2 in an alloy with 4.5% magnesium, the 5083 alloy. Similarly, the effects of work hardening and age hardening can be seen in the increases in strength in the alloys listed when their condition is altered from the annealed (O) condition. Note, however, the effect that this increase in strength has on the ductility of the alloys.

The welding of aluminium and its alloys

Alloy designations: wrought products

Table A.4 BS EN BS EN Old BS/DTD Temperature (°C) numerical chemical number designation designation Liquidus Solidus IVIdUng range Al 99.99 1 660 660 0 AW-1080A Al 99.8 1A AW-1070A …

Principal alloy designations: cast products

Table A.3 BS EN numerical designation BS EN chemical designation Old BS number ANSI designation Temperature (°C) Liquidus Solidus Melting range Al 99.5 LM0 640 658 18 AC-46100 Al Si10Cu2Fe …

Physical, mechanical and chemical properties at 20°C

Table A.2 Property Aluminium Iron Nickel Copper Titanium Crystal structure FCC BCC FCC FCC HCP Density (gm/cm3) 2.7 7.85 8.9 8.93 4.5 Melting point (°C) 660 1536 1455 1083 1670 …

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