4.7 Article

Durability of plasma sprayed Thermal Barrier Coatings with controlled properties part II: Effects of geometrical curvature

期刊

SURFACE & COATINGS TECHNOLOGY
卷 424, 期 -, 页码 -

出版社

ELSEVIER SCIENCE SA
DOI: 10.1016/j.surfcoat.2021.127671

关键词

Thermal Barrier Coatings (TBCs); Yttria Stabilized Zirconia (YSZ); Geometry effects; Furnace Cycle Testing (FCT); Finite Element Modeling (FEM)

资金

  1. Center for Thermal Spray Research's Industrial Consortium for Thermal Spray Technology
  2. US Department of Energy, Office of Fossil Energy, Turbine Program
  3. AFOSR-CONACYT collaborative research project [FA9550-18-1-0118]

向作者/读者索取更多资源

The study found that substrate curvature has a significant impact on the durability of Air Plasma Sprayed Thermal Barrier Coatings. TBCs sprayed on curved substrates exhibited lower durability compared to those sprayed on flat substrates, with durability increasing with higher porosity. The thermal stresses unique to curved geometries resulted in different failure processes compared to those observed with planar disks.
The present investigation elucidates the effects of substrate curvature on the durability of Air Plasma Sprayed (APS) Thermal Barrier Coatings (TBCs). Traditionally, planar disk specimens are utilized in Furnace Cycle Testing (FCT). In most cases, delamination is initiated at the disk's free edge and then propagates along the TBC-bond coat interface. However, in turbine components (e.g., blades/vanes), they lack significant free edges and the coatings are deposited on non-flat surfaces of varying radii of curvature. These geometrical discrepancies imply significant differences in the stress states as compared to planar disk specimens. Therefore, the part geometry inevitably affects the TBC failure mechanisms in the turbine system, and consequently influences TBC durability. Nevertheless, these effects have not been fully explored in the past, despite the anecdotal knowledge which suggests the leading edge of turbine blades to be one of the most common failure/spallation locations. In this study, representative TBC systems were deposited onto superalloy disks with flat substrate and rods with curved substrate. The experimental results from FCT suggest TBC durability on rods is significantly lower than when sprayed on disks. Furthermore, the durability of TBCs on rods appears to increase with higher porosity, which is contradictory to reported trends for TBCs on disks. In addition, the effects of various bond coats are not consistent with those observed in disks. To clarify the underlying effects of curved geometries, detailed stress analyses were performed. They revealed a state of thermal stresses which is unique to curved geometries. It was found that TBC on rods experience tensile radial stresses as well as tensile hoop stresses during the cooling. These stresses result in a complex interplay in failure processes in rods, which explains the different observed trends in the durability from those obtained with disks.

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