Precipitation hardening alloys based on the Al-Cu-Li system are experiencing currently a strong research effort in the framework of the development of new alloys, [1,2] particularly for aerospace components. These alloys, where the main solute elements Cu and Li are often supplemented with additions of Mg and Ag, show a complex precipitation sequence. [3][4][5][6][7] The main strengthening precipitate in this system is the T 1 phase of nominal composition Al 2 CuLi that forms very thin platelets of high aspect ratio on the {111} planes of the Al matrix. [3,8,9] Decreus et al. [10] have studied in detail the influence of alloy chemistry on the precipitation sequence of two recently developed alloys. The AA2198 alloy, which has a relatively low Li content, experiences a precipitation sequence involving Cu-rich solute clusters after natural ageing, which dissolve during the heating ramp to the ageing temperature of 155°C, and are later replaced by T 1 precipitates together with smaller proportions of Cu-rich GP zones and u 0 phases. Numerous studies on earlier generations of alloys have shown that nucleation of the T 1 phase depends strongly on the presence of minor solute species [7,[11][12][13] and on the presence of dislocations. [3,6,7,14,15] Seemingly it was shown to be relatively independent on natural ageing [7] contrarily to most other precipitates in Al alloys (such as in 6000 or 7000 series), however the data concerning this point is scarce. The aim of the present paper is to clarify, on the AA2198 alloy, the effect of the processing conditions preceding artificial ageing at 155°C on the precipitation processes and related strengthening. The parameters that have been varied are: natural ageing, plastic deformation, and the order between these two. The precipitate microstructure has been evaluated using small-angle X-ray scattering (SAXS) and transmission electron microscopy (TEM) and the strengthening has been evaluated by microhardness measurements.
Materials and MethodsAlloy AA2198 has the composition range (all in wt%) [2.9-3.5] Cu -[0.8-1.1] Li -[0.25-0.8] Mg -[0.1-0.5] Ag -[0.04-0.18] Zr. It was provided by Constellium -Voreppe Research Centre, France, as rolled sheet of 6 mm thickness with a fully fibrous grain structure. The sheet showed a marked Brass (h112i {110}) texture.The precipitation treatment consisted in several steps whose order was varied, as summarized in Table 1. Initially the samples were all solution treated and quenched in cold water (15°C). For the solution treated material (sample O) the artificial ageing treatment started within 10 min after this quench. In other samples the deformation step was carried out right after the quench, with a delay of 5 min. In this case the artificial ageing was either carried out right after the deformation step (sample D) or after a room temperature natural ageing of 7 days at room temperature of 20°C (sample DN). Another case was when the natural ageing of 7 days was carried out before the deformation step (sample ND). In these three last samples,...