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      Thermal barrier coatings technology: critical review, progress update, remaining challenges and prospects

      International Materials Reviews
      Maney Publishing

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          Thermal barrier coatings for gas-turbine engine applications.

          Hundreds of different types of coatings are used to protect a variety of structural engineering materials from corrosion, wear, and erosion, and to provide lubrication and thermal insulation. Of all these, thermal barrier coatings (TBCs) have the most complex structure and must operate in the most demanding high-temperature environment of aircraft and industrial gas-turbine engines. TBCs, which comprise metal and ceramic multilayers, insulate turbine and combustor engine components from the hot gas stream, and improve the durability and energy efficiency of these engines. Improvements in TBCs will require a better understanding of the complex changes in their structure and properties that occur under operating conditions that lead to their failure. The structure, properties, and failure mechanisms of TBCs are herein reviewed, together with a discussion of current limitations and future opportunities.
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            Materials selection guidelines for low thermal conductivity thermal barrier coatings

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              Mechanisms controlling the durability of thermal barrier coatings

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                Author and article information

                Journal
                International Materials Reviews
                International Materials Reviews
                Maney Publishing
                0950-6608
                1743-2804
                November 18 2013
                August 2013
                November 18 2013
                August 2013
                : 58
                : 6
                : 315-348
                Article
                10.1179/1743280413Y.0000000019
                5f45e50c-e2e6-429b-8fb0-027b1c1a553b
                © 2013
                History

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