Abstract

In the current work, the microstructure, hydrogen permeability, and properties of chromium nitride (CrNx) thin films deposited on the Inconel 718 superalloy using direct current reactive sputtering are investigated. The influence of the substrate bias voltage on the crystal structure, mechanical, and tribological properties before and after hydrogen exposure was studied. It was found that increasing the substrate bias voltage leads to densification of the coating. X-ray diffraction (XRD) results reveal a change from mixed fcc-CrN + hcp-Cr2N to the approximately stoichiometric hcp-Cr2N phase with increasing substrate bias confirmed by wavelength-dispersive X-ray spectroscopy (WDS). The texture coefficients of (113), (110), and (111) planes vary significantly with increasing substrate bias voltage. The hydrogen permeability was measured by gas-phase hydrogenation. The CrN coating deposited at 60 V with mixed c-CrN and (113) textured hcp-Cr2N phases exhibits the lowest hydrogen absorption at 873 K. It is suggested that the crystal orientation is only one parameter influencing the permeation resistance of the CrNx coating together with the film structure, the presence of mixing phases, and the packing density of the structure. After hydrogenation, the hardness increased for all coatings, which could be related to the formation of a Cr2O3 oxide film on the surface, as well as the defect formation after hydrogen loading. Tribological tests reveal that hydrogenation leads to a decrease of the friction coefficient by up to 40%. The lowest value of 0.25 ± 0.02 was reached for the CrNx coating deposited at 60 V after hydrogenation.

Highlights

  • Nickel-based alloys are widely used in the aerospace industry due to their excellent corrosion resistance and good mechanical properties, even at elevated temperatures

  • X-ray diffraction (XRD) results reveal a with an increasing substrate bias. +

  • The hardness increased for all the coatings and the friction coefficient drops up to

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Summary

Introduction

Nickel-based alloys are widely used in the aerospace industry due to their excellent corrosion resistance and good mechanical properties, even at elevated temperatures. IN718 is one of the most frequently used nickel-based alloys in aero-engine hot section components, aerospace structures, rocket components, and power generation turbines [1]. Despite its advantages, this alloy is susceptible to hydrogen embrittlement caused by the penetration of hydrogen resulting in degradation and catastrophic failure [2,3]. This alloy is susceptible to hydrogen embrittlement caused by the penetration of hydrogen resulting in degradation and catastrophic failure [2,3] It is well-known that grain boundaries play an essential role in Coatings 2018, 8, 66; doi:10.3390/coatings8020066 www.mdpi.com/journal/coatings. Hydrogen embrittlement of IN718 occurs preferably at the grain boundaries even at low hydrogen concentration [13]

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