LEADER 05067nam 22007935 450 001 9910254232503321 005 20260810145919.0 010 $a981-10-0919-8 024 7 $a10.1007/978-981-10-0919-8 035 $a(CKB)3710000000649514 035 $a(EBL)4505540 035 $a(SSID)ssj0001665859 035 $a(PQKBManifestationID)16455433 035 $a(PQKBTitleCode)TC0001665859 035 $a(PQKBWorkID)15000886 035 $a(PQKB)11494016 035 $a(DE-He213)978-981-10-0919-8 035 $a(MiAaPQ)EBC4505540 035 $z(PPN)258861711 035 $a(PPN)193445174 035 $a(EXLCZ)993710000000649514 100 $a20160415d2016 u| 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 10$aLoadings in Thermal Barrier Coatings of Jet Engine Turbine Blades $eAn Experimental Research and Numerical Modeling /$fby Tomasz Sadowski, Przemys?aw Golewski 205 $a1st ed. 2016. 210 1$aSingapore :$cSpringer Nature Singapore :$cImprint: Springer,$d2016. 215 $a1 online resource (110 p.) 225 1 $aSpringerBriefs in Computational Mechanics,$x2191-5350 300 $aDescription based upon print version of record. 311 08$a981-10-0918-X 320 $aIncludes bibliographical references at the end of each chapters. 327 $aPreface; Acknowledgement; Contents; 1 Introduction; 2 Protective Thermal Barrier Coatings; 2.1 Structure of TBCs; 2.2 Development and Application of New Coating Materials; 2.3 Conclusions; References; 3 Thermal Loads; 3.1 Numerical Methods-Application of Finite Elements Method (FEM) [1, 2]; 3.2 Deformation and Stress in Structural Elements, Caused by Thermal Loads [1, 2]; 3.3 Numerical Analysis of Temperature Fields in Critical Elements of Turbo-Engines by CFD (Computational Fluid Dynamics) with Application of FLUENT Program; 3.4 Conclusions; References; 4 Mechanical Loads 327 $a4.1 Preparation of Model for Simulation4.2 Analysis of Results; 4.3 Blade Vibrations Resonance; 4.4 Conclusions; Reference; 5 Environmental Loads; 5.1 Corrosion; 5.2 Erosion; 5.3 Thermally Growth Oxide (TGO) Layer Growth; 5.4 Author's Own Tests of Moving Blade Surface, Including Chemical Analysis; 5.5 Conclusions; References; 6 State of Arts in Experimental Testing of TBCs Systems-Literature Analysis; 6.1 Review and Analysis of Currently Utilised Tests; 6.2 Conclusions; References; 7 Proposed Experimental Investigations of TBCs Systems; 7.1 Sample Ageing 327 $a7.2 Uniaxial Stretching of Dumbbell Samples with TBC Layers-Author's Own Tests7.2.1 First Batch of Samples Not Subjected to Ageing; 7.2.2 Second Batch of Samples Subjected to Ageing; 7.3 3-Point Bending of Beam Samples with TBC Layers-Author's Own Tests; 7.4 Conclusions; 8 Numerical Analysis of Cracks Propagation Process in Turbine Blades TBCs Systems Under Thermo-Mechanical Loading Based on Experimental Results; 8.1 Formulation of FEM Approach and Brittle Damage of the TBCs System; 8.1.1 Brittle Damage Model; 8.1.2 Cohesive Degradation Model; 8.1.3 Simulation Results 327 $a8.2 Application of Submodeling Technique and X-FEM Methods for Detailed Analysis of Cracking Process in Turbine Blades TBCs8.2.1 Submodeling; 8.2.2 X-FEM Method Basics; 8.2.3 Preparation of Model for Simulation; 8.3 Analysis of Results; 8.4 Conclusions; References; 9 Summary 330 $aThis book discusses complex loadings of turbine blades and protective layer Thermal Barrier Coating (TBC), under real working airplane jet conditions. They obey both multi-axial mechanical loading and sudden temperature variation during starting and landing of the airplanes. In particular, two types of blades are analyzed: stationary and rotating, which are widely applied in turbine engines produced by airplane factories. 410 0$aSpringerBriefs in Computational Mechanics,$x2191-5350 606 $aMechanics, Applied 606 $aSolids 606 $aMaterials$xAnalysis 606 $aMathematical models 606 $aMachinery 606 $aSolid Mechanics 606 $aCharacterization and Analytical Technique 606 $aMathematical Modeling and Industrial Mathematics 606 $aMachinery and Machine Elements 615 0$aMechanics, Applied. 615 0$aSolids. 615 0$aMaterials$xAnalysis. 615 0$aMathematical models. 615 0$aMachinery. 615 14$aSolid Mechanics. 615 24$aCharacterization and Analytical Technique. 615 24$aMathematical Modeling and Industrial Mathematics. 615 24$aMachinery and Machine Elements. 676 $a629.134353 700 $aSadowski$b Tomasz$4aut$4http://id.loc.gov/vocabulary/relators/aut$0720981 702 $aGolewski$b Przemys?aw$4aut$4http://id.loc.gov/vocabulary/relators/aut 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910254232503321 996 $aLoadings in Thermal Barrier Coatings of Jet Engine Turbine Blades$92514731 997 $aUNINA