Development of Advanced Low Conductivity Thermal Barrier Coatings

Abstract

Advanced multi‐component, low‐conductivity oxide thermal barrier coatings have been developed using an approach that emphasizes real‐time monitoring of thermal conductivity under conditions that are engine‐like in terms of temperatures and heat fluxes. This is in contrast to the traditional approach where coatings are initially optimized in terms of furnace and burner rig durability with subsequent measurement in the as‐processed or furnace‐sintered condition. The present work establishes a laser high‐heat‐flux test as the basis for evaluating advanced plasma‐sprayed and electron beam‐physical vapor deposited (EBPVD) thermal barrier coatings under the NASA Ultra‐Efficient Engine Technology (UEET) Program. The candidate coating materials for this program are novel thermal barrier coatings that are found to have significantly reduced thermal conductivities and improved thermal stability due to an oxide defect‐cluster design. Critical issues for designing advanced low‐conductivity coatings with improved coating durability are also discussed.