Thesis Abstract

Abstract
This thesis presents the research conducted on the development of high-temperature resistant coatings for aerospace applications. The aerospace industry demands materials that can withstand extreme temperatures, corrosion, and wear, making the development of advanced coatings a critical area of research. The primary objective of this study was to investigate novel coating materials and techniques that can enhance the performance and durability of components used in aerospace applications operating under high-temperature conditions. Chapter One provides an introduction to the research topic, detailing the background of the study, problem statement, objectives, limitations, scope, significance, structure of the thesis, and definitions of key terms. The importance of developing high-temperature resistant coatings for aerospace applications is highlighted, setting the stage for the subsequent chapters. Chapter Two presents a comprehensive literature review covering ten key areas related to high-temperature coatings, including existing coating materials, deposition techniques, challenges in aerospace applications, and recent advancements in the field. The review of existing literature provides a foundation for the research methodology outlined in Chapter Three. Chapter Three details the research methodology employed in this study, including the selection of materials, experimental procedures, testing protocols, and data analysis methods. The chapter also discusses the equipment and facilities utilized to develop and characterize the high-temperature resistant coatings. The methodology is designed to investigate the performance and properties of the coatings under simulated aerospace operating conditions. Chapter Four presents a detailed discussion of the findings obtained from the experimental work conducted in this study. The chapter discusses the performance of the developed coatings in terms of temperature resistance, corrosion protection, wear resistance, adhesion strength, and other relevant properties. The results are analyzed and compared with existing coatings to evaluate the effectiveness of the developed materials. Finally, Chapter Five provides a conclusion and summary of the research work, highlighting the key findings, contributions, limitations, and recommendations for future research. The study demonstrates the feasibility of developing high-temperature resistant coatings for aerospace applications and suggests avenues for further improvement and optimization. In conclusion, this thesis contributes to the advancement of materials science and engineering by proposing novel solutions for enhancing the performance and durability of aerospace components operating under high-temperature conditions. The research findings have implications for the aerospace industry, offering potential benefits in terms of efficiency, safety, and cost-effectiveness.

Thesis Overview

The project titled "Development of High-Temperature Resistant Coatings for Aerospace Applications" aims to address the critical need for advanced materials in the aerospace industry that can withstand extreme temperatures and harsh environmental conditions. High-temperature resistant coatings play a crucial role in enhancing the performance and durability of aerospace components, such as turbine blades, engine components, and thermal protection systems. The research will focus on the development of novel coatings that exhibit superior thermal stability, oxidation resistance, and mechanical properties at elevated temperatures. By employing advanced materials science and engineering principles, the project seeks to design coatings that can withstand temperatures exceeding 1000°C while maintaining their structural integrity and functional properties. The study will begin with a comprehensive review of the existing literature on high-temperature coatings, including an analysis of their composition, manufacturing processes, and performance characteristics. This literature review will provide a solid foundation for understanding the current state-of-the-art in high-temperature coating technology and identify key research gaps and opportunities for innovation. The research methodology will involve experimental work to synthesize and characterize high-temperature resistant coatings using state-of-the-art techniques such as physical vapor deposition, chemical vapor deposition, and sol-gel processing. The coatings will be subjected to a series of rigorous tests to evaluate their thermal stability, oxidation resistance, adhesion strength, and other relevant properties. The findings of the study will be discussed in detail, highlighting the performance of the developed coatings in simulated aerospace environments and their potential applications in real-world aerospace components. The discussion will also address the challenges encountered during the research process and propose strategies for overcoming them in future studies. In conclusion, the project aims to contribute to the advancement of high-temperature coating technology for aerospace applications by developing innovative coatings with enhanced thermal and mechanical properties. The research outcomes are expected to have significant implications for the aerospace industry, leading to the development of more efficient, reliable, and durable aerospace components that can operate under extreme conditions.