Abstract

The aluminum alloy 2618A is applied for engine components such as radial compressor wheels which operate for long time at elevated temperatures. This results in coarsening of the hardening precipitates and degradation in mechanical properties during the long-term operation, which is not taken into account in the current lifetime prediction models due to the lack of quantitative microstructural and mechanical data. To address this issue, a quantitative investigation on the evolution of precipitates during long-term aging at 190 °C for up to 25,000 h was conducted. Detailed transmission electron microscopy (TEM) was combined with Brinell hardness measurements and thorough differential scanning calorimetry (DSC) experiments. The results show that GPB zones and S-phase Al2CuMg grow up to < 1,000 h during which the GPB zones dissolve and S-phase precipitates form. For longer aging times, only S-phase precipitates coarsen, which can be well described using the Lifshitz–Slyozov–Wagner theory of ripening. A thorough understanding of the underlying microstructural processes is a prerequisite to enable the integration of aging behavior into the established lifetime models for components manufactured from alloy 2618A.

Highlights

  • The Al-Cu-Mg alloy EN AW 2618A (EN AW AlCu2Mg1.5Ni) is used for applications subjected to long-term service at elevated temperatures in the aerospace and transportation industry due to its favorable material properties [1]

  • The aluminum alloy 2618A is applied for engine components such as radial compressor wheels which operate for long time at elevated temperatures

  • The aim of the present study is to develop a quantitative investigation of isothermal aging by complementing transmission electron microscopy (TEM) with thorough differential scanning calorimetry (DSC) measurements and hardness tests to allow a more in-depth understanding of the S-phase aging process

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Summary

Introduction

The Al-Cu-Mg alloy EN AW 2618A (EN AW AlCu2Mg1.5Ni) is used for applications subjected to long-term service at elevated temperatures in the aerospace and transportation industry due to its favorable material properties (e.g., slow long-term degradation) [1] It contains Fe and Ni in the form of intermetallic compounds of lm size, which retain microstructural stability and provide dispersion hardening at elevated temperatures [2,3,4,5]. The size and distribution of the nm-sized secondary S-phase and its precursors are the main factors influencing the material strength These precipitates are formed within the supersaturated solid solution (SSSS) during aging [6,7,8,9,10]. The first decomposition sequence proposed was [13, 14]: SSSS

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