Project Abstract

Abstract
The demand for high-temperature oxidation resistant coatings in aerospace applications has been increasing due to the harsh operating conditions faced by aerospace components. This research project focuses on the development of advanced coatings that can withstand high temperatures and aggressive environments encountered in aerospace operations. The objective of this study is to investigate the effectiveness of various coating materials and application techniques in enhancing the oxidation resistance of aerospace components. The research methodology includes a comprehensive literature review to understand the current state-of-the-art in high-temperature coatings, followed by experimental work to evaluate the performance of selected coating materials. The study involves the characterization of coating properties such as thickness, adhesion, and microstructure, as well as testing their oxidation resistance under simulated aerospace conditions. Results from the experimental investigations are discussed in detail in Chapter Four, highlighting the performance of different coatings in terms of oxidation resistance and durability. The findings provide valuable insights into the effectiveness of various coating materials and application methods in protecting aerospace components from high-temperature oxidation. The significance of this study lies in its potential to advance the development of high-temperature oxidation resistant coatings for aerospace applications, contributing to the improvement of component performance and longevity in extreme operating conditions. The research also addresses the limitations and challenges associated with current coating technologies, offering new perspectives for future research in this field. In conclusion, this research project provides a systematic investigation into the development of high-temperature oxidation resistant coatings for aerospace applications. The findings contribute to the knowledge base of materials and metallurgical engineering, with practical implications for enhancing the performance and reliability of aerospace components exposed to high-temperature environments.

Project Overview