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      Emerging materials and processes for thermal barrier systems

      Current Opinion in Solid State and Materials Science
      Elsevier BV

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          Lower limit to the thermal conductivity of disordered crystals

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            The Scattering of Low-Frequency Lattice Waves by Static Imperfections

            P. Klemens (1955)
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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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                Author and article information

                Journal
                Current Opinion in Solid State and Materials Science
                Current Opinion in Solid State and Materials Science
                Elsevier BV
                13590286
                January 2004
                January 2004
                : 8
                : 1
                : 77-91
                Article
                10.1016/j.cossms.2004.03.009
                6cde0bd8-72fa-4c8e-afdb-34e37a3ea389
                © 2004

                http://www.elsevier.com/tdm/userlicense/1.0/

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