Abstract

Suspension plasma spraying (SPS) has been shown as a promising process to produce porous columnar strain tolerant coatings for thermal barrier coatings (TBCs) in gas turbine engines. However, the highly porous structure is vulnerable to crack propagation, especially near the topcoat-bondcoat interface where high stresses are generated due to thermal cycling. A topcoat layer with high toughness near the topcoat-bondcoat interface could be beneficial to enhance thermal cyclic lifetime of SPS TBCs. In this work, a bilayer coating system consisting of first a dense layer near the topcoat-bondcoat interface followed by a porous columnar layer was fabricated by SPS using Yttria-stabilised zirconia suspension. The objective of this work was to investigate if the bilayer topcoat architecture could enhance the thermal cyclic lifetime of SPS TBCs through experiments and to understand the effect of the column gaps/vertical cracks and the dense layer on the generated stresses in the TBC during thermal cyclic loading through finite element modeling. The experimental results show that the bilayer TBC had significantly higher lifetime than the single-layer TBC. The modeling results show that the dense layer and vertical cracks are beneficial as they reduce the thermally induced stresses which thus increase the lifetime.

Highlights

  • Thermal barrier coatings (TBCs) are widely used in the gas turbine industry to protect the metallic components from the high temperature environment

  • A thin crack can be observed along the topcoat-bondcoat interface which is deemed to occur during metallographic preparation of the sample

  • A bilayer topcoat with a dense layer close to the topcoat-bondcoat interface followed by a porous columnar layer was fabricated by Suspension plasma spraying (SPS) and its lifetime under thermal shock testing was compared to the singlelayer porous columnar SPS topcoat in thermal barrier coatings (TBCs)

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Summary

Introduction

Thermal barrier coatings (TBCs) are widely used in the gas turbine industry to protect the metallic components from the high temperature environment. They allow the turbine to operate in higher temperature so that turbine will run with increased efficiency (Ref 1). These coatings are applied by either thermal spraying or electron beamphysical vapor deposition (EB-PVD). The columnar microstructure fabricated by SPS typically contains much higher porosity than EB-PVD coatings and SPS TBCs exhibit lower thermal conductivity (Ref 4, 5) than conventional TBCs produced by atmospheric plasma sprayed (APS) and EB-PVD (Ref [6, 7]). The lifetime of SPS TBCs under thermal shock loading is still an issue as the highly porous microstructure produced by SPS is prone to detrimental cracking

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