Development of a Recyclable High-Entropy Alloy Coating System for Turbine Blades | Blazingprojects Postgraduate Thesis
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Development of a Recyclable High-Entropy Alloy Coating System for Turbine Blades

 

Table Of Contents


Chapter ONE

INTRODUCTION

  • 1.1Introduction
  • 1.2Background of the Study
  • 1.3Statement of the Problem
  • 1.4Aim and Objectives of the Study
  • 1.5Research Questions
  • 1.6Research Hypotheses
  • 1.7Significance of the Study
  • 1.8Scope and Delimitation of the Study
  • 1.9Limitations of the Study
  • 1.10Organisation of the Study
  • 1.11Operational Definition of Terms

Chapter TWO

LITERATURE REVIEW

  • 2.1Conceptual Review: High-Entropy Alloys in Coating Technology
  • 2.2Conceptual Review: Recyclability Principles in Coatings
  • 2.3Conceptual Review: Thermal Barrier Coatings versus Protective Coatings
  • 2.4Conceptual Review: Deposition Techniques for HEA Coatings (PVD, CVD, EBPVD)
  • 2.5Conceptual Review: Oxidation and Corrosion Mechanisms in Turbine Environments
  • 2.6Theoretical Framework: Materials by Design and Integrated Computational Materials Engineering (ICME)
  • 2.7Theoretical Framework: Multiscale Modeling of Phase Stability in HEAs
  • 2.8Theoretical Framework: Fracture Mechanics and Spallation of Coatings under Turbine Loads
  • 2.9Empirical Review: Industrial Performance of HEA Coatings in Turbines
  • 2.10Empirical Review: Life-Cycle Assessment of Recyclable Coatings
  • 2.11Gaps in the Literature on Recyclable HEA Coatings for Turbines
  • 2.12Conceptual Model: Linkages Between Recyclability, Mechanical Integrity, and Thermal Performance

Chapter THREE

RESEARCH METHODOLOGY

  • 3.1Research Design: Design, Implementation, and Evaluation of a Recyclable HEA Coating System
  • 3.2Philosophical Paradigm: Pragmatism for Applied Engineering Research
  • 3.3Population of the Study: Turbine-Grade Nickel-Based Substrates and HEA Powder Precursors
  • 3.4Sample Size and Sampling Technique: Fractional Factorial Design for Coating Trials
  • 3.5Sources and Instruments of Data Collection: Coating Deposition Systems, Microstructure Characterization, and Mechanical Test Fixtures
  • 3.6Validity and Reliability of Instruments: Calibration, Reference Standards, and Inter-Laboratory Comparisons
  • 3.7Process Design and Coating Deposition Parameters
  • 3.8Characterization Methods and Analytical Techniques
  • 3.9Data Analysis Methods: Statistical, Microstructural, and Thermodynamic Analyses
  • 3.10Model Specification: Thermodynamic and Kinetic Models for Phase Stability
  • 3.11Ethical Considerations in Materials Research

Chapter FOUR

DATA PRESENTATION AND ANALYSIS

  • ANALYSIS AND DISCUSSION OF FINDINGS
  • 4.1Data Presentation Strategy for Coating System Evaluation
  • 4.2Descriptive Analysis of Coating Microstructure and Composition
  • 4.3Descriptive Analysis of Mechanical and Thermal Properties
  • 4.4Hypotheses Testing: Effect of Deposition Parameters on Coating Adhesion
  • 4.5Hypotheses Testing: Oxidation Resistance under Turbine-Simulated Conditions
  • 4.6Lifecycle Recyclability Assessment Results
  • 4.7Multivariate Analysis: Interdependencies Between Microstructure, Properties, and Recyclability
  • 4.8Interpretation of Results: Alignment with Conceptual Framework and Theoretical Models
  • 4.9Discussion of Findings in Light of Prior Empirical Studies

Chapter FIVE

SUMMARY, CONCLUSION AND RECOMMENDATIONS

  • CONCLUSION AND RECOMMENDATIONS
  • 5.1Summary of Findings
  • 5.2Conclusion and Implications for Turbine Coat Systems
  • 5.3Contributions to Knowledge and Practice
  • 5.4Recommendations for Industry and Further Research
  • 5.5Suggestions for Future Studies

Thesis Abstract

The escalating demand for turbine efficiency and environmental compliance necessitates the development of protective coatings that combine high-temperature performance with recyclability to reduce lifecycle costs and material waste. This study addresses the challenge of designing a recyclable high-entropy alloy (HEA) coating system capable of withstanding extreme turbine operating conditions while enabling straightforward end-of-life material recovery. The aim is to design, fabricate, characterize, and evaluate a HEA coating system for turbine blades that balances high-temperature oxidation resistance, mechanical robustness, and recyclability. Specific objectives include (i) synthesizing a family of Al-Fe-Co-Cr-Ni-Cu-based HEA coatings with controlled microstructure, (ii) optimizing deposition parameters via pulsed laser deposition and magnetron sputtering to achieve dense, adherent coatings on nickel-based superalloy substrates, (iii) assessing high-temperature oxidation, creep, and wear resistance up to 1050°C, (iv) evaluating recyclability through thermomechanical processing routes and traceable alloy recovery, and (v) developing a predictive framework linking compositional design to performance and recyclability. A mixed-methods approach integrates experimental materials science with materials informatics. The population comprises turbine-grade nickel-base superalloy coupons and turbine blade segments (IN738LC equivalent). Sample sizes include 60 coated coupons for initial screening, 20 accelerated oxidation-creep-wear tests at 900–1050°C, and 10 blade-scale segments for field-simulated testing. Data collection instruments include scanning electron microscopy (SEM) with energy-dispersive X-ray spectroscopy (EDS) for microstructural analysis, X-ray diffraction (XRD) for phase identification, transmission electron microscopy (TEM) for interfacial characterization, nanoindentation for hardness and modulus, gravimetric oxidation/fatigue tests, and laser ablation inductively coupled plasma mass spectrometry (LA-ICP-MS) for traceability of alloying elements. Recyclability assessment employs differential scanning calorimetry (DSC) to monitor phase stability during recycling cycles and compositional analysis post-reprocessing to quantify segregation or loss, supported by thermodynamic modeling with CALPHAD databases. Data analysis proceeds through a hierarchical framework. Descriptive statistics summarize coating thickness, adhesion, and microhardness. Inferential analyses include ANOVA to evaluate the effects of deposition parameters on coating adhesion and oxide scale adherence, regression analyses to correlate HEA composition with creep-rupture life and wear resistance, and multivariate principal component analysis (PCA) to identify dominant factors driving performance. A finite element-based thermo-mechanical model assesses residual stresses and thermal gradients in coated blades under turbine-stage loading. The study adopts a design-for-recyclability lens underpinned by the theory of materials circularity and the durable yet repairable materials paradigm, with the multi-criteria decision analysis (MCDA) used to balance performance and recyclability outcomes. The conceptual framework integrates these theories with empirical results to guide alloy-composition selection and process parameters. Expected findings include (i) a coating microstructure featuring a coherent HEA matrix with nano-precipitates that enhance high-temperature strength and oxidation resistance, (ii) deposition parameter windows yielding coatings with superior adhesion, reduced spallation, and maintained integrity after thermal cycles, (iii) oxidational and creep performance meeting or exceeding benchmark coatings at 1050°C with acceptable wear resistance, and (iv) a replicable recycling pathway enabling recovery of constituent elements with minimal degradation (<5% loss in critical elements after three recycling cycles). The study anticipates establishing quantitative relationships between specific element ratios (e.g., Al, Cr, Ni, Co, and Ti) and performance-recyclability metrics, enabling predictive design of recyclable HEA coatings. The contribution to knowledge includes advancing the design of recyclable HEA coatings tailored for turbine blades, establishing a validated methodology for integrating recyclability metrics into high-temperature coating development, and delivering a transferable modeling framework that links composition, processing, performance, and end-of-life recovery. The main conclusion posits that a carefully engineered Al-Fe-Co-Cr-Ni-Cu HEA coating can simultaneously deliver enhanced high-temperature performance and recyclability, with the recommended strategy emphasizing controlled nano-precipitation, optimized deposition to ensure strong interfacial bonding, and a standardized recycling protocol that preserves critical alloying elements with minimal degradation. Policy and practice recommendations include adopting the proposed design-framework in industrial coating development and integrating recyclability assessments early in material selection to reduce lifecycle environmental impact.

Thesis Overview

This research explores designing, producing, and evaluating a recyclable high-entropy alloy (HEA) coating system for turbine blades. HEAs are coatings made from multiple principal elements mixed in near-equal parts, which can yield superior high-temperature strength and corrosion resistance. The goal is to develop a coating that performs well in turbine environments but is easier to recycle or reclaim at end-of-life, reducing long-term environmental impact and material waste. Why it matters: Turbine blades operate under extreme heat, oxidation, and mechanical stress. Conventional coatings can degrade quickly, leading to higher maintenance costs and energy inefficiency. At the same time, coating materials often become waste that is difficult to recycle. A recyclable HEA coating promises both better service life and lower end-of-life environmental burden, addressing both performance and sustainability challenges. Research gaps: While HEA coatings show promise for high-temperature protection, few studies systematically compare their recyclability and lifecycle impacts. There is limited guidance on selecting element combinations and deposition processes that balance performance with recyclability, as well as methods to quantify recyclability and reprocessability. What the researcher will do, step by step: - Literature review to identify candidate HEA compositions and deposition techniques that are compatible with turbine substrates and recyclability goals. - Experimental design to fabricate several HEA coatings (for example, five to seven compositions) via physical vapor deposition and/or arc spraying on nickel-based turbine alloy substrates. - Characterization of coatings using scanning electron microscopy (SEM), energy-dispersive X-ray spectroscopy (EDS), X-ray diffraction (XRD), hardness testing, and high-temperature oxidation tests. - Laboratory recycling simulations to evaluate reprocessing feasibility, including dismantling, elemental recovery, and re-coating potential. - Data collection will include coating thickness, phase composition, microstructure features, oxidation resistance metrics, adhesion tests, and recyclability indicators. - Data analysis will employ descriptive statistics, analysis of variance (ANOVA) to compare performance across coatings, regression analysis to relate composition to properties, and a simple lifecycle assessment (LCA) framework to estimate recyclability benefits. - Synthesis of results to identify a balanced composition that meets performance targets while enabling recyclable end-of-life pathways. - Discussion of practical implications for manufacturing, maintenance, and sustainability. Expected contributions and outcomes: provide a new design blueprint for recyclable HEA coatings, establish quantitative recyclability criteria, and deliver practical guidance on deposition protocols and recycling workflows. The study aims to advance both materials engineering for high-temperature protection and sustainable lifecycle management of turbine components.

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