Abstract

Dealloying is involved in materials science responsible for fabrication of nanoscale structures beneficially but for corrosion degradations detrimentally. Detailed understanding related to the latter is critical for designing corrosion-resistance alloys and dedicated inhibition systems. Thus, direct nanoscopic observations of nano-structural and compositional evolutions during the process are essential. Here using liquid phase-transmission electron microscopy (LP-TEM), for the first time, we show dynamic evolution of intricate site-specific local corrosion linked to intermetallic particles (IMPs) in aerospace aluminium alloys. To thoroughly probe degradation events, oxidation direction is controlled by purposefully masking thin specimens, allowing for observing top-view surface initiation to cross-sectional depth propagation of local degradations. Real-time capturing validated and supported by post-mortem examinations shows a dealloying-driven process that initiates at IMPs and penetrates into the depth of the alloy, establishing macroscopic corrosion pits. Besides, controversial mechanisms of noble-metal redistribution are finally elucidated.

Highlights

  • High-strength-to-weight ratio in aluminium alloys (AAs) is key to many transport industries like aerospace as it reduces dead-weight and energy consumption and beneficially increases loading capacity [1]

  • High angle annular dark field-scanning TEM (HAADF-STEM), taken at 0 min in the absence of the electrolyte, shows a large bright particle of Al2CuMg embedded in the alloy matrix

  • The digitally-magnified view of the rectangular region shown in Fig. 2b reveals that the initially-corroded zone (Region I) is finely porous in morphology whereas Region II has coarser porosities (15 nm < pore size < 20 nm)

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Summary

Introduction

High-strength-to-weight ratio in aluminium alloys (AAs) is key to many transport industries like aerospace as it reduces dead-weight and energy consumption and beneficially increases loading capacity [1]. The main contributors to mechanical properties are nano-to microscale intermetallic compounds that are introduced to the aluminium-based systems by specific alloying followed by precipitation hardening processes [2,3,4,5,6] (Fig. 1 and Movie S1), but they are typically undesirably detrimental to the corrosion resistance [7]. Contemporary aerospace AAs benefit from a comprehensive metallurgical knowledge of tuning the microstructure towards desirable mechanical properties [8]. Complicated site-specific local degradation events that predominantly take place at surface intermetallic particles (IMPs) dispersed in the AAs matrix eventually lead to progressive pitting and intergranular corrosion [9].

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