(A) study on the thermal fatigue life prediction considering thickness and equivalent elastic modulus for air plasma sprayed thermal barrier coating

Yun, Junghan 2020년
논문상세정보
' (A) study on the thermal fatigue life prediction considering thickness and equivalent elastic modulus for air plasma sprayed thermal barrier coating' 의 주제별 논문영향력
논문영향력 선정 방법
논문영향력 요약
주제
  • Air plasma spray
  • equivalentelasticmodulus
  • gas turbine
  • thermal barrier coating
동일주제 총논문수 논문피인용 총횟수 주제별 논문영향력의 평균
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' (A) study on the thermal fatigue life prediction considering thickness and equivalent elastic modulus for air plasma sprayed thermal barrier coating' 의 참고문헌

  • ¡°Analyzing the effectiveness of international environmental policies : TheCase of the Kyoto Protocol ,
    Vol . 82 , pp . 125-151 [2017]
  • ¡°A review of developments in technologies and research that have had a direct measurable impact on sustainabilityConsidering the Paris agreement onClimateChange
    Vol . 68 , pp . 835 ? 839 [2017]
  • nfluence of cracks in APS-TBCs on stress around TGO during thermalcycling : A numerical simulation study
    Vol . 285 , pp . 98-112 [2016]
  • composition and property relationships of plasma-sprayed thermal barrier coatings
    Vol . 50 , pp . 141-149 , [1992]
  • [8] R. S. Lima and B. R. Marple, "Nanostructured YSZ thermal barrier coatings engineered to counteract sintering effects,¡° Materials Science and Engineering A, Vol. 485, pp.182?193, 2008.
  • [7] X. Q. Cao, R. Vassen and D. Stoever, "Ceramic materials for thermal barrier coatings," Journal of the European Ceramic Society, Vol. 24, pp. 1?10, 2004.
  • [57] J. S. Wallace and J. Ilavsky, "Elastic Modulus Measurements in Plasma Sprayed Deposits," Journal of Thermal Spray Technology, Vol. 7, No. 4, pp. 521-526, 1998.
  • [53] Song H. W., Lee J. M., Yun J. H., Park S., Kim Y. S., Kum K. S., Lee Y. Z., and Seok C. S., "Oxide Layer Rumpling Control Technology for?High Efciency of?Eco?Friendly Combined?Cycle Power Generation System," International Journal of Precision Engineering and Manufacturing-Green Technology, Vol. 7, pp. 185?193, 2020.
  • [4] Eungsun Byon, "Thermal barrier coatings for gas turbine engine components," KIC News, Vol. 17, No. 4, 2014.
  • [3] T. B. Gibbons* and I. G. Wright, "A Review Of Materials For Gas Turbines Firing Syngas Fuels," Oak ridge national laboratory, 137, TM-2009.
  • [33] V. K. Tolpygo and D. R. Clarke, "Rumpling induced by thermal cycling of an overlay coating: the effect of coating thickness," Acta Materialia, Vol. 52 pp. 615?621, 2004.
  • [31] E. A. G. Shillington and D. R. Clarke, "Spalling failure of a thermal barrier coating associated with aluminum depletion in the bond-coat," Acta Materialia, Vol. 47, No. 4, pp. 1297¡¾1305, 1999.
  • [2] B. Zohuri and P. McDaniel, "Combined Cycle Driven Efficiency for Next Generation Nuclear Power Plants," Springer International Publishing AG, 2018.
  • [28] Kansai Electric Power, Outline of Thermal Power Generation, https://www.kepco.co.jp/english/corporate/energy/thermal_power/shikumi/index.html
  • [26] Mica Grujicic, S. Ramaswami and Jennifer S. Snipes, "Use of the Materials Genome Initiative (MGI) approach in the design of improved-performance fiber-reinforced SiC/SiC ceramic-matrix composites(CMCs)," AIMS Materials Science, Vol. 3, No. 3, pp. 989-1021, 2016.
  • [23] Williams S. Ebhota and Tien-Chien Jen, ¡°Fossil Fuels Environmental Challenges and the Role of Solar Photovoltaic Technology Advances in Fast Tracking Hybrid Renewable Energy System,¡± International Journal of Precision Engineering and Manufacturing-Green Technology, Vol. 7, pp. 97-117, 2019.
  • [22] Ibrahim S. Seddiek and Mohamed M. Elgohary, ¡°Eco-friendly selection of ship emissions reduction strategies with emphasis on SOx and NOx emissions," Int. J. Nav. Archit. Ocean Eng., Vol. 6, pp. 737~748, 2014.
  • [10] Cho H. H., ¡°Korean Gas Turbine Development and Strategy,¡± Journal of the KSME, Vol. 54, No. 8, pp. 32-36, 2014.
  • Yun J. H. and Koo J. M. , Prediction of Thermo-Mechanical Fatigue Life of IN738LC Using the Finite Element Analysis
    Vol . 15 , No . 8 , pp . 1733-1737 [2014]
  • Y. Wang , Influence of cracks in APS-TBCs on stress around TGO during thermal cycling : A
    Coatings Technology , Vol . 285 , pp .
  • What is the suitable segmentation crack density for atmosphericplasma sprayed thick thermal barrier coatings with the improved thermal shock resistance ? ``
    Vol . 431 , pp . 101-111 [2018]
  • Well-to-wheel greenhouse gas emissions of battery electric vehicles in countries dependent on the import of fuels through maritime transportation : A South Korean case study
    Vol . 230 , pp . 135-147 [2018]
  • Thermal barrier coatings for aircraft engines : history and directions
    Vol . 6 , No . 1 [1997]
  • Thermal barrier coatings
  • Thermal barrier coating technology and application status
    Vol . 19 , No . 3 , pp . 46-56 [2016]
  • Thermal barrier coating materials
    Vol . 8 , Issue 6 , pp . 22-29 [2005]
  • Thermal Stress Analysis of the Next Generation Thermal Barrier Coating by Considering Microstructure and Thermal Grown Oxide
    pp . 1398-1399 [2015]
  • Thermal Fatigue Test Methods for Thermal Barrier Coatings of Gas Turbine Blade
    Vol . 26 , pp . 7-15 [2009]
  • Thermal Fatigue Behavior of Thick and Porous Thermal Barrier Coatings Systems
    Vol . 16 , pp.816-821 [2007]
  • Thermal Barrier Coatings for Gas-Turbine Engine Applications
    Vol . 296 , Issue 5566 , pp . 280-294 [2002]
  • The growth and influence of thermally grown oxide in a thermal barrier coating
    Vol . 201 , pp . 1074 ? 1079 [2006]
  • Study on the Conjugate Heat Transfer Analysis Methodology of Thermal Barrier Coating on the Internal Cooled Nozzle ,
    Vol . 18 , No . 3 , pp.38~45 [2015]
  • Some recent trends in research and technologyof advanced thermal barrierCoat
    Vol . 7 , pp . 73-80 [2003]
  • Smart overlayCoatings ?Concept and practice
    Vol . 149 pp . 236 ? 244 [2001]
  • S. Bogner and A. Buhrig-Polaczek , A high thermal gradient directional solidification method for growingsuperalloy singleCrystals
    Vol . 214 , pp . 3112 ? 312 [2014]
  • Processing effects on porosity-propertyCorrelations in plasma sprayed yttria-stabilized zirconiaCoatings
    Vol . A359 pp . 100-111 [2003]
  • Plasma Spray : Study of theCoating Generation
    Vol . 22 , pp . 295-303 [1996]
  • Performance evaluation of the plasma-sprayed thermal barrier coating
    [2014]
  • Nickel Base Superalloy
    Vol . 17 , No . 4 [2014]
  • Modelling of TBC system failure : Stress distribution as a function of TGO thickness and thermal expansion mismatch
    Vol . 13 , pp . 409 ? 426 [2006]
  • Microstructure evolution of NiCoCrAlY overlay coating for Ni3Al based alloy IC6 turbine vane during long term engine test
    Vol . 13 pp . 309 ? 314 [2005]
  • Lifetime Performance of EB-PVD Thermal Barrier Coatings with Coating Thickness in Cyclic Thermal Exposure
    Vol . 25 , No . 10 [2015]
  • Influences of interface morphology and thermally grown oxide thickness on residual stress distribution in thermal barrier coating system
    Vol . 42 , pp . 8338 ? 8350 [2016]
  • Influence of material and testing parameters on the lifetime of TBC systems with MCrAlY and NiPtAl bondcoats
    pp . 5-7 [2012]
  • Influence of Sample Deformation and Porosity On Mechanical Properties by Instrumented Microindentation Technique
    Vol . 18 , pp . 87-93 [1998]
  • High Temperature Coatings_Thermal Barrier Coatings Systems
    https : //www2.virginia.edu/ms/research/wadley/high-temp.html
  • Guilibaldo Tolentino Eslava and Juan Abugaber Francis , Evaluation of the Gas Turbine Inlet Temperature with Relation to the Excess Air , Energy and Power Engineering
    pp . 517-524 [2011]
  • Failure modes in plasma-sprayed thermal barrier coatings
    Vol . A342 , pp . 120-130 [2003]
  • Failure mechanisms of coin-type plasma-sprayed thermal barrier coatings with thermal fatigue ,
    Vol . 205 , pp . S451 ? S458 [2010]
  • Failure mechanisms associated with the thermally grown oxide in plasma-sprayed thermal barrier coatings
    Vol . 48 , pp . 3963-3976 [2000]
  • Evolution of Youngs modulus of air plasma sprayed yttria-stabilized zirconia in thermally cycled thermal barrier coatings , Scripta Materialia
    Vol . 54 pp [2006]
  • Evaluation on the delamination life of isothermally aged plasma sprayed thermal barrierCoating
    Vol . 33 , No . 2 , pp . 162-168 [2009]
  • Evaluation of the Degradation of Plasma Sprayed Thermal Barrier Coatings Using Nano-Indentation , Journal of Nanoscience and Nanotechnology
    Vol . 9 , pp . 7271 ? 7277 [2009]
  • Evaluation of Degradation of Isothermally Aged Plasma-Sprayed Thermal Barrier Coating ,
    Vol . 34 , pp . 475-480 [2010]
  • Estimation of spallation life of thermal barrier coating of gas turbine blade by thermal fatigue test
    Vol . 205 , pp.S157-S160 [2011]
  • Effects of indenter geometry and material properties on the correction factor of Sneddon¡¯s relationship for nanoindentation of elastic and elastic ? plastic materials
    Vol . 56 pp . 1399 ? 1405 [2008]
  • Effects of Composition , Structure Design , and Coating Thickness of Thermal Barrier Coatings on Thermal Barrier Performance
    Vol . 53 , no . 6 , pp . 689-699 [2016]
  • Design and optimization of coating structure for the thermal barrier coatings fabricated by atmospheric plasma spraying via finite element method
    Vol . 2 , pp . 102 ? 116 [2014]
  • Delamination Evaluation of Thermal Barrier Coating on Turbine Blade owing to Isothermal Degradation Using Ultrasonic C-scan Image ,
    Vol . 36 , No . 5 , pp . 353-362 [2016]
  • Control of polymorphism in Al2O3 scale formed by oxidation of alumina-forming alloys
    Vol . 52 , pp . 429 ? 434 [2010]
  • Composite ceramics thermal barrier coatings of yttria stabilized zirconia for aero-engines
    Vol . 35 , no . 12 , pp . 2814-2823 [2019]
  • A Study on Thermal Fatigue Life Variation according to Thermal Exposure Time
    Vol . 598 , pp . 276-280 [2014]