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Showing 1 to 4 of 4 for “"high-temperature coatings"”.

  1. Cyclic deformation of monocrystalline nickel aluminide and high temperature coatings

    Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1990.

    mit Repository record for Cyclic deformation of monocrystalline nickel aluminide and high temperature coatings (opens in a new tab)

  2. Modelling Thermal Conductivity of Porous Thermal Barrier Coatings for High-Temperature Aero Engines

    Thermal Barrier Coatings (TBC) are used to shield hot sections of gas turbine engines, helping to prevent the melting of metallic surfaces. TBC is a sophisticated layered system that can be divided into top coat, bond coat, and the super-alloy substrate. The highly heterogeneous microstructure of …

    ottawa-retro Repository record for Modelling Thermal Conductivity of Porous Thermal Barrier Coatings for High-Temperature Aero Engines (opens in a new tab)

  3. Understanding surface and sub-surface phenomena in nickel-based superalloy castings

    Nickel-based superalloys are high-temperature materials, created to operate in the aggressive conditions found within gas turbine engines. Single crystal turbine blades are investment cast, followed by a complex series of operations including heat treatment, machining, blasting, etching and …

    cambridge Repository record for Understanding surface and sub-surface phenomena in nickel-based superalloy castings (opens in a new tab)

  4. In-Situ Investigations of Calcium-Magnesium-Aluminosilicates (CMAS) Infiltration Effects on Thermal Barrier Coatings Under Extreme Environments Replicating Jet Engines

    … engines during operation. When operating within high abundance regions, these particulates negatively interact and degrade the high temperature thermal barrier coatings (TBC) protecting underlying superalloy turbine blades vital to engine operation. These CMAS particulates melt within the engine …

    embry-riddle Repository record for In-Situ Investigations of Calcium-Magnesium-Aluminosilicates (CMAS) Infiltration Effects on Thermal Barrier Coatings Under Extreme Environments Replicating Jet Engines (opens in a new tab)