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Callister - An introduction - 8th edition

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440 • Chapter 11 / Applications and Processing of Metal Alloys<br />

Solvent (Al) atom<br />

Solute (Cu)<br />

atom<br />

" Phase particle Phase particle<br />

Figure 11.26 A transmission electron<br />

micrograph showing the microstructure<br />

of a 7150-T651 aluminum alloy (6.2 Zn,<br />

2.3 Cu, 2.3 Mg, 0.12 Zr, the balance Al)<br />

that has been precipitation hardened.<br />

The light matrix phase in the<br />

micrograph is an aluminum solid<br />

solution. The majority of the small<br />

plate-shaped dark precipitate particles<br />

are a transition h phase, the remainder<br />

being the equilibrium h (MgZn 2 )<br />

phase. Note that grain boundaries are<br />

“decorated” by some of these particles.<br />

90,000. (Courtesy of G. H. Narayanan<br />

and A. G. Miller, Boeing Commercial<br />

Airplane Company.)<br />

(a) (b) (c)<br />

Figure 11.25 Schematic depiction of several stages in the formation of the equilibrium<br />

precipitate () phase. (a) A supersaturated solid solution. (b) A transition, , precipitate<br />

phase. (c) The equilibrium phase, within the -matrix phase.<br />

transition phases (denoted as and ), before the formation of the equilibrium <br />

phase (Figure 11.25c). Transition phase particles for a precipitation-hardened 7150<br />

aluminum alloy are shown in the electron micrograph of Figure 11.26.<br />

The strengthening and hardening effects shown in Figure 11.23 result from the<br />

innumerable particles of these transition and metastable phases. As noted in the<br />

figure, maximum strength coincides with the formation of the phase, which may<br />

100 nm<br />

be preserved upon cooling the alloy to room temperature. Overaging results from<br />

continued particle growth and the development of and phases.<br />

The strengthening process is accelerated as the temperature is increased. This<br />

is demonstrated in Figure 11.27a, a plot of tensile strength versus the logarithm of<br />

time for a 2014 aluminum alloy at several different precipitation temperatures. Ideally,<br />

temperature and time for the precipitation heat treatment should be designed<br />

to produce a hardness or strength in the vicinity of the maximum. Associated with<br />

an increase in strength is a reduction in ductility, which is demonstrated in Figure<br />

11.27b for the same 2014 aluminum alloy at the several temperatures.<br />

Not all alloys that satisfy the aforementioned conditions relative to composition<br />

and phase diagram configuration are amenable to precipitation hardening. In

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