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      Adhesion improvements of Thermal Barrier Coatings with HVOF thermally sprayed bond coats

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      Surface and Coatings Technology
      Elsevier BV

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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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            Mechanisms controlling the durability of thermal barrier coatings

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              An analytical model for predicting residual stresses in progressively deposited coatings Part 1: Planar geometry

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                Author and article information

                Journal
                Surface and Coatings Technology
                Surface and Coatings Technology
                Elsevier BV
                02578972
                January 2007
                January 2007
                : 201
                : 8
                : 4694-4701
                Article
                10.1016/j.surfcoat.2006.10.005
                7a0be90c-10cb-4504-8a95-3bffeb9edb72
                © 2007

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

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