The significance of thermal contact resistance in two-layer thermal-barrier-coated turbine vanes |
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Authors: | Curt H Liebert Raymond E Gaugler |
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Affiliation: | Lewis Research Center, National Aeronautics and Space Administration, Cleveland, Ohio 44135 U.S.A. |
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Abstract: | A study was conducted to determine whether the thermal contact resistance (TCR) between layers is important in heat transfer through two-layer plasma-sprayed thermal barrier coatings (TBCs) applied to turbine vanes. The results obtained with a TBC system of an NiCrAlY bond and an yttria-stabilized zirconia ceramic showed that the TCR between the layers was negligible. This result also verified other results obtained with a different coating system of an NiCr bond and a calcia-stabilized zirconia ceramic. |
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