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Loadings in Thermal Barrier Coatings of Jet Engine Turbine Blades

An Experimental Research and Numerical Modeling

  • Book
  • © 2016

Overview

Authors:
  1. Tomasz Sadowski

    1. Department of Solid Mechanics, Lublin University of Technology, Lublin, Poland

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  2. Przemysław Golewski

    1. Department of Solid Mechanics, Lublin University of Technology, Lublin, Poland

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    You can also search for this author in PubMed   Google Scholar

Part of the book series: SpringerBriefs in Applied Sciences and Technology (BRIEFSAPPLSCIENCES)

Part of the book sub series: SpringerBriefs in Computational Mechanics (BRIEFSCOMPUTAT)

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Table of contents (9 chapters)

  1. Front Matter

    Pages i-viii
    Download chapter PDF

  2. Introduction

    • Tomasz Sadowski, Przemysław Golewski
    Pages 1-3

  3. Protective Thermal Barrier Coatings

    • Tomasz Sadowski, Przemysław Golewski
    Pages 5-11

  4. Thermal Loads

    • Tomasz Sadowski, Przemysław Golewski
    Pages 13-24

  5. Mechanical Loads

    • Tomasz Sadowski, Przemysław Golewski
    Pages 25-35

  6. Environmental Loads

    • Tomasz Sadowski, Przemysław Golewski
    Pages 37-44

  7. State of Arts in Experimental Testing of TBCs Systems—Literature Analysis

    • Tomasz Sadowski, Przemysław Golewski
    Pages 45-65

  8. Proposed Experimental Investigations of TBCs Systems

    • Tomasz Sadowski, Przemysław Golewski
    Pages 67-89

  9. Numerical Analysis of Cracks Propagation Process in Turbine Blades TBCs Systems Under Thermo-Mechanical Loading Based on Experimental Results

    • Tomasz Sadowski, Przemysław Golewski
    Pages 91-103

  10. Summary

    • Tomasz Sadowski, Przemysław Golewski
    Pages 105-107
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Keywords

About this book

This book discusses complex loadings of turbine blades and protective layer Thermal Barrier Coating (TBC), under real working airplane jet conditions. They obey both multi-axial mechanical loading and sudden temperature variation during starting and landing of the airplanes. In particular, two types of blades are analyzed: stationary and rotating, which are widely applied in turbine engines produced by airplane factories.

Authors and Affiliations

  • Department of Solid Mechanics, Lublin University of Technology, Lublin, Poland

    Tomasz Sadowski, Przemysław Golewski

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