Liu et al., 2013 - Google Patents
Effect of substrate curvature on residual stresses and failure modes of an air plasma sprayed thermal barrier coating systemLiu et al., 2013
View PDF- Document ID
- 5940764106737569726
- Author
- Liu D
- Seraffon M
- Flewitt P
- Simms N
- Nicholls J
- Rickerby D
- Publication year
- Publication venue
- Journal of the European Ceramic Society
External Links
Snippet
A set of aerofoil shaped air plasma sprayed thermal barrier coated (APS-TBC) specimens were adopted in this paper to investigate the stress distributions in the ceramic top coat (TC) and the thermally grown oxide (TGO), the mechanism of local crack generation and …
- 239000000758 substrate 0 title abstract description 24
Classifications
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/32—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
- C23C28/321—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer
- C23C28/3215—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer at least one MCrAlX layer
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or anti-vibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/288—Protective coatings for blades
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Liu et al. | Effect of substrate curvature on residual stresses and failure modes of an air plasma sprayed thermal barrier coating system | |
Naumenko et al. | Overview on recent developments of bondcoats for plasma-sprayed thermal barrier coatings | |
Nowak et al. | Effect of processing parameters on MCrAlY bondcoat roughness and lifetime of APS–TBC systems | |
Wang et al. | Commercial thermal barrier coatings with a double-layer bond coat on turbine vanes and the process repeatability | |
Weng et al. | Comparison of microstructural evolution and oxidation behaviour of NiCoCrAlY and CoNiCrAlY as bond coats used for thermal barrier coatings | |
Jonnalagadda et al. | Thermal barrier coatings: Life model development and validation | |
Dong et al. | Propagation feature of cracks in plasma-sprayed YSZ coatings under gradient thermal cycling | |
Texier et al. | Tensile properties of a non-line-of-sight processed β-γ-γ′ MCrAlY coating at high temperature | |
Vaidyanathan et al. | Surface geometry and strain energy effects in the failure of a (Ni, Pt) Al/EB-PVD thermal barrier coating | |
Essa et al. | Failure mechanisms of APS-YSZ-CoNiCrAlY thermal barrier coating under isothermal oxidation and solid particle erosion | |
Weng et al. | Cracking evolution of atmospheric plasma-sprayed YSZ thermal barrier coatings subjected to isothermal heat treatment | |
Zhang et al. | Dependence of scale thickness on the breaking behavior of the initial oxide on plasma spray bond coat surface during vacuum pre-treatment | |
Peichl et al. | Behaviour of an EB-PVD thermal barrier coating system under thermal–mechanical fatigue loading | |
Fang et al. | Performance of TBCs system due to the different thicknesses of top ceramic layer | |
Wen et al. | Effect of temperature on rumpling and thermally grown oxide stress in an EB-PVD thermal barrier coating | |
Cui et al. | Evolution of the residual stress in porous ceramic abradable coatings under thermal exposure | |
Slámečka et al. | Thermal cycling damage in pre-oxidized plasma-sprayed MCrAlY+ YSZ thermal barrier coatings: Phenomenon of multiple parallel delamination of the TGO layer | |
Karaoglanli et al. | Comparison of oxidation and thermal shock performance of thermal barrier coatings | |
Ashofteh et al. | Effect of layer thickness on thermal shock behavior in double-layer micro-and nano-structured ceramic top coat APS TBCs | |
Zhao et al. | Thermal barrier coatings on nickel superalloy substrates | |
Lyu et al. | Fracture behavior and thermal durability of lanthanum zirconate-based thermal barrier coatings with buffer layer in thermally graded mechanical fatigue environments | |
Li et al. | Effects of substrate material and TBC structure on the cyclic oxidation resistance of TBC systems | |
Liu et al. | Residual stresses in environmental and thermal barrier coatings on curved superalloy substrates: Experimental measurements and modelling | |
Seraffon et al. | Performance of thermal barrier coatings in industrial gas turbine conditions | |
Ke et al. | Progressive damage during thermal shock cycling of D-gun sprayed thermal barrier coatings with hollow spherical ZrO2–8Y2O3 |