Abstract

It is anticipated that laser cladding assisted with preheat (LCAP)-deposited Tribaloy (T-800) composite coatings enhances resistance to structural degradation upon exposure to elevated-temperature oxidation service environments. The oxidation kinetics of LCAP T-800 composite coatings deposited on EN8 substrate and its mechanisms have not been explored in severe conditions that are similar to operational parameters. The isothermal oxidation behaviour of the T-800 composite coating deposited on EN8 via LCAP was studied at 800 °C in air for up to 120 h (5 × 24 h cycles) and contrasted to that of uncoated samples. The mass gain per unit area of the coating was eight times less than that of the uncoated EN8 substrate. The parabolic rate constant (Kp) for EN8 was 6.72 × 10−12 g2·cm−4·s−1, whilst that for the T-800 composite coating was 8.1 × 10−13 g2·cm−4·s−1. This was attributed to a stable chromium oxide (Cr2O3) layer that formed on the coating surface, thereby preventing further oxidation, whilst the iron oxide film that formed on the EN8 substrate allowed the permeation of the oxygen ions into the oxide. The iron oxide (Fe2O3) film that developed on EN8 spalled, as evidenced by the cracking of oxide when the oxidation time was greater than 72 h, whilst the Cr2O3 film maintained its integrity up to 120 h. A parabolic law was observed by the T-800 composite coating, whilst a paralinear law was reported for EN8 at 800 °C up to 120 h. This coating can be used in turbine parts where temperatures are <800 °C.

Highlights

  • Oxidation occurs when metals/alloys are exposed to oxygen/air [1]

  • Gravimetric analysis was used for the comparison of oxidation behaviour between the EN8 substrate and T-800/WC coating

  • The results reveal that EN8 stainless steel exhibited higher-temperature oxidation compared to the T-800/WC coating

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Summary

Introduction

Oxidation occurs when metals/alloys are exposed to oxygen/air [1]. It results in the formation of porous and noncoherent oxides, which leads to the failure of the component [2]. The dispersion of oxygen on the equipment surfaces leads to oxidation, which propagates into the core of the material. Equipment operating at high temperatures is prone to this phenomenon, which often leads to premature equipment degradation and consequent failure. A thin oxide layer well bonded to the surface of the coating and slow in growth will offer good protection to the substrate from additional oxidation. Various coatings can be used to subvert the oxidation phenomenon. Vasudev et al [2]

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