Abstract

This paper reports studying the effect of such highly active, surface-active modifying elements as Y, Hf, and La on the structure and properties of the Ni–Cr–Al system's consumable cathodes, which are used to apply heat-resistant coatings onto the gas-turbine engines' blades. Y, Hf, and La are introduced to form the nanoscale separation of phases that stabilize the alloy structure. In order to obtain cathodes of the required quality, a method of vacuum-arc autocrucible melting has been chosen. The selected technique makes it possible to use raw materials of different dispersity for the manufacture of ingots (in the form of powders or pig metal). The charge was prepared by shredding the materials mechanically, using various methods (cutting and crushing). It has been shown that the introduction of elements such as Y and La into the cathodes has a similar effect on structural formation processes. It has been established that when Hf is introduced, the structure of the resulting consumable cathodes is characterized by a greater degree of homogeneity. There is also a positive effect of Hf on the uniformity of the distribution of doping elements (Al, Cr) in the volume of the material compared to alloy samples modified by Y and La. It has been shown that the introduction of Hf has made it possible to achieve the higher quality indicators in comparison with Y and La. An analysis of coating structure has revealed that samples with Hf have a greater degree of homogeneity and fewer defects, which is especially important when applying coatings of greater thickness (over 40 µm). It has been established that the introduction of Hf makes it possible to apply coatings up to 90 µm thick by obtaining a less defective structure. It has been found that the Hf modification increases the adhesion between the substrate and coating, as well as makes it possible to achieve maximum even distribution of doping elements throughout the entire thickness of the coating applied

Highlights

  • The operational reliability of the gas turbine engine (GTE) blades depends primarily on the resistance of the surface to the high-temperature effects of the oxidative environment [1, 2] as the destruction of a turbine’s blades mostly originates from the surface

  • The authors carried out preliminary studies into obtaining cathodes and applying protective coatings made from them on the blades of GTE with heat-resistant alloys based on Co [7] and Ni [8]

  • The aim of this study is to improve the quality of consumable cathodes used in the application of heat-resistant ion-plasma coatings, by selecting the optimal modification composition and devising the technology of their introduction

Read more

Summary

Introduction

The operational reliability of the gas turbine engine (GTE) blades depends primarily on the resistance of the surface to the high-temperature effects of the oxidative environment [1, 2] as the destruction of a turbine’s blades mostly originates from the surface. One of the main ways to improve the resistance of blades to various types of hot corrosion is to Materials science apply protective coatings by an ion-plasma method. The quality indicators of heat-resistant coatings include: ‒ the uniformity of the chemical composition; ‒ the homogeneity of the structure and phase composition; ‒ adhesive properties; ‒ the uniformity of application (a layer thickness); ‒ manufacturability (a layer thickness, a drip phase) [4]. These parameters, in turn, depend on the characteristics of cathodes used as a consumable material in the application of coatings by an ion-plasma method. The issue of applying the heat-resistant coatings in modern aviation engine construction is a relevant field of technology and materials science

Literature review and problem statement
The aim and objectives of the study
Research materials and methods
Findings
Conclusions
Full Text
Published version (Free)

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call