Abstract

There is a strong driving force to improve the production efficiency of thermal barrier coatings (TBCs) manufactured via air plasma spray (APS). To address this need, the high-enthalpy APS torch Axial III Plus was employed to successfully manufacture TBCs by spraying a commercial YSZ feedstock at powder feed rate of 100 g/min using an optimized set of N2/H2 spray parameters; which yielded an impressive YSZ deposition efficiency (DE) value of 70%. This exact same set of optimized spray parameters was used to manufacture the same identical YSZ TBC (over ~160 µm-thick bond-coated substrates) but at two distinct YSZ thickness levels: (i) ~420 µm-thick and (ii) ~930 µm-thick. In spite of the high YSZ feed rate and DE levels, the YSZ TBC revealed a ~14% porous (conventional looking) microstructure, without segmented cracking or horizontal delamination at both thickness levels. The bond strength values measured via the ASTM C633 standard for the ~420 µm-thick and ~930 µm-thick YSZ TBCs were ~13.0 and ~11.6 MPa (respectively); which are among at the upper end values reported in the literature. After the first objective was attained, the second key objective of this work was to evaluate the thermal insulating effectiveness of these two as-sprayed YSZ TBCs. To achieve this objective, a thermal gradient laser-rig was employed to generate a temperature reduction (ΔT) along the TBC-coated coupons under different laser power levels. These distinct laser power levels generated YSZ TBC surface temperatures varying for 1100 to 1500 °C, for the ~420 µm-thick YSZ TBC, and from 1100 to 1680 °C YSZ TBC ~930 µm-thick YSZ TBC. The respective ΔT values for both TBCs are reported. The results of this engineering paper are promising regarding the possibility of improving considerably the manufacturing efficiency of industrial quality conventional-looking porous YSZ TBCs, by using a high-enthalpy N2-based APS torch. This is the first paper published in the open literature showing R&D results of coatings manufactured via the Axial III Plus APS torch.

Highlights

  • Thermal Barrier Coatings (TBCs) Manufactured Via Air Plasma Spray (APS)TBCs manufactured via APS provide thermal insulation from the hot combustion gas stream to the static metallic parts located in the hot sections of gas turbine engines

  • The amount oxygen in the as-sprayed bond coat (BC) is *1.4 wt.%. This amount is within the range of those exhibited by NiCoCrAlY?HfSi BCs when deposited via APS at the National Research Council of Canada (NRC) (i.e., *0.7-1.5wt.%) and when measured by the same technique

  • This type of multi-layer TBC assembly could potentially operate at temperatures well-over the established 1300 °C limit for YSZ and still keep the current Ni-based superalloy components at temperatures no higher than 1000 °C. This type of multi-layer TBC assembly and Ni-based superalloy architecture may possibly be an alternative to environmental barrier coatings (EBCs) and ceramic matrix composites (CMCs). This engineering paper demonstrated that a high-enthalpy N2-based APS torch (Axial III Plus) can be successfully employed to manufacture a conventional *14% porous YSZ TBC at high powder feed rate (100 g/min) and deposition efficiency (DE) value (70%)

Read more

Summary

Introduction

Thermal Barrier Coatings (TBCs) Manufactured Via Air Plasma Spray (APS). TBCs manufactured via APS provide thermal insulation from the hot combustion gas stream to the static metallic parts located in the hot sections of gas turbine engines (e.g., combustion chambers, nozzles and afterburners). A thermally sprayed TBC system typically exhibits a bi-layered structure, which includes a ceramic top coat and a metallic MCrAlY (M = Ni, Co, NiCo or CoNi) bond coat (BC). The ceramic top coat (e.g., ZrO2-7-8wt.%Y2O3, a.k.a., YSZ) provides thermal insulation and reduces the heat flow to the turbine metallic part; which is made of a Ni-based high temperature superalloy (e.g., Hastelloy X). The metallic MCrAlY BC is an oxidation/corrosion-resistant metallic layer. It protects the underlying component and improves the adhesion of the ceramic top coat on the part.

Objectives
Methods
Results
Conclusion
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