ProgramMaster Logo
Conference Tools for 2017 TMS Annual Meeting & Exhibition
Register as a New User
Submit An Abstract
Propose A Symposium
Presenter/Author Tools
Organizer/Editor Tools
About this Abstract
Meeting 2017 TMS Annual Meeting & Exhibition
Symposium Energy Materials 2017: Materials for Gas Turbines
Presentation Title Multilayered, Multifunctional Thermal Barrier Coatings for Gas Turbine Engines
Author(s) Sanjay Sampath, Vaishak Vishwanathan, Gopal Dwivedi
On-Site Speaker (Planned) Sanjay Sampath
Abstract Scope Thermal barrier coatings (TBCs) are increasingly playing a vital role in enhancing efficiency and performance of gas turbine engines. As engine operating temperatures rise, yttria-stabilized zirconia (YSZ), the currentTBC, has reached its operational limits. Gadolinium Zirconate (GDZ)-based pyrochlores are now emerging contenders, as they offer low conductivity and resist attack by silicate deposits. However, GDZ cannot be directly substituted for YSZ due to its incompatibility with the thermally grown alumina layer, requiring multilayer strategies. In this study several multilayer architectures, based on both YSZ and the YSZ–GDZ system,have been developed and tested for durability under furnace thermal cycling conditions. Coating designs considered optimization of microstructure and properties of individual layers based on their location within the top-coat thickness to address competing interests of thermal conductivity, compliance, and resistance to silicates. The results point to new strategies in the design and manufacturing of optimal multilayer coatings.
Proceedings Inclusion? Planned: Stand-alone book in which only your symposium’s papers would appear (indicate title in comments section below)


Advanced Characterization of the Hot Corrosion Behavior of Gas Turbine Alloys under Burner Rig Test Exposures
Alloy Development for Promoting γ/γ' Microstructural Stability and Creep Properties of Multi-component Co-base Superalloys
C-11: Effect of Thermal Debinding and Sintering Conditions on Mechanical Properties of Silica-based Ceramic Cores
C-12: Microstructures and Deposition Mechanisms of Thermal Barrier Coatings Produced by PS-PVD
C-13: Mullitization of Fused Silica on Silica-based Ceramic Cores by Colloidal Alumina Infiltration
C-14: Solidification Behavior and Microstructure of Inconel 625 Superalloy under Electromagnetic Field
C-15: Study on the Undercoolability and Single Crystal Castability of Nickel-Based Superalloys
C-16: Temperature Dependence of the Fracture Behavior of X-750 Alloy and Effect of Heat Treatment
Deposit-Induced Hot Corrosion and Materials Design Strategies to Reduce Its Impact
Development Activities for the Manufacture of Rotor Forgings for Turbines in High Efficiency Power Plants
Development of a New High Strength and Hot Corrosion Resistant Directionally Solidified Superalloy DZ409
Development of High Strength Hot Corrosion Resistant Single Crystal Superalloys Based on Understanding the Effect of Key Elements on Hot Corrosion Behavior
Effect of Alloying Elements (Cr and Al) in Nickel-based Alloys in Molten Sulfate Environments
Effect of C Addition on Creep and Microstructure Stability of Lamellar TiAl Alloys
Efforts to Introduce TiAl Alloys for Gas Turbine Applications
Electrodeposited MCrAlY Coatings for Gas Turbine Engine Applications
Evolution of the Thermal Conductivity of Sm2Zr2O7 under CMAS Attack
Grain Refinement of Cast FeAl-Alloys for Gas Turbine Blades
Mechanisms of Fracture in Laser Powder Bed Additive Manufactured Superalloys
Microstructures and Mechanical Properties of Ultrafine Grained Ni Based Superalloy Matrix Nanocomposites Fabricated by Powder Metallurgy Route
Modeling the Diffusion of Minor Elements in Different MCrAlY – Superalloy Substrates at High Temperature
Multilayered, Multifunctional Thermal Barrier Coatings for Gas Turbine Engines
On Healing Mechanism of Cast Porosities in Cast Ni-Based Superalloy by Hot Isostatic Pressing
Porous Yttria-stabilized Zirconia Microspheres for Advanced Reflective Thermal Barrier Coatings
Rafting Prediction Criterion and Creep Life for Nickel-based Single Crystal Superalloys under Multiaxial Stress States
Rejuvenation of a Co Based Superalloy to Prevent the Quickest Microstructural Degradation during the Following Operating Cycle
Rejuvenation Process Definition for IN792SX Gas Turbine Blades Aimed to Extend Their Expected Life
Revisiting the Sources of Creep Dislocations in Ni-base, Single Crystal Superalloys
Simulation of Precipitation Behavior of Nickel-based Superalloys
Tensile Behavior of Inconel X-750: Effect of Heat Treatment
The Effect of Superalloy and Coating Composition and Specimen Geometry on TBC Lifetime
The Influence of Dendritic Segregation Degree to the Recrystallization Nucleation in U4720LI
The Materials, Manufacturing and Equipments of the Large Disk Forgings for Industrial Gas Turbines
Thermal Barrier Coatings for More Efficient Gas-Turbine Engines
Wang: High Temperature Oxidation of the New Type γ'-strengthened Cobalt-base Superalloys

Questions about ProgramMaster? Contact