Results 101 to 110 of about 3,429 (183)
Effect of Heat Treatment on Pore Architecture and Associated Property Charges in Plasma Sprayed TBCs
Plasma sprayed TBCs exhibit many interlamellar pores, voids and microcracks. These microstructural features are primarily responsible for the low global stiffnesses and the low thermal conductivities commonly exhibited by such coatings.
Cipitria, A. +5 more
core
Thermal-barrier-coated turbine blade study [PDF]
The effects of coating TBC on a CF6-50 stage 2 high-pressure turbine blade were analyzed with respect to changes in the mean bulk temperature, cooling air requirements, and high-cycle fatigue. Localized spallation was found to have a possible deleterious
Hillig, W. B., Siemers, P. A.
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Experimental Studies on Slurry Based Thermal Barrier Coatings [PDF]
Thermal barrier coatings were introduced to reduce operating temperatures and thermal stresses in structures and machine components across a wide range of industries and applications.
Harding, Steven +2 more
core
Thermal Barrier Coatings (TBCs) are multi-layer protective coatings used in the hot section components such as combustor and turbine of advanced gas turbine engines to protect them from degrading affects of hot gases.
Serdar Dalkılıç, A. Akide Tanatmış
doaj
Thermal barrier coatings (TBCs), commonly used in industrial gas turbines and aero-engines, have become a vital technology for prolonging their lifespan.
Lubin Wang +4 more
doaj +1 more source
Modelling of gas permeation through ceramic coatings produced by thermal spraying
An analytical model has been developed for simulation of gas permeation through thermal spray coatings, and for prediction of the permeability. The model is based on a geometrical representation of the coating microstructure.
Clyne, T.W., Golosnoy, I.O., Paul, S.
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The demand for efficient engineering components operating in harsh environments has necessitated the exploration of advanced protective measures.
Amjad Iqbal +4 more
doaj +1 more source
Delamination-Indicating Thermal Barrier Coatings [PDF]
The risk of premature failure of thermal barrier coatings (TBCs), typically composed of yttria-stabilized zirconia (YSZ), compromises the reliability of TBCs used to provide thermal protection for turbine engine components.
Eldridge, Jeffrey I.
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This work concentrates on the phase, composition, thermo-physical properties, microstructure, service lifetime, and failure behaviour of GdEuZrO/YSZ thermal barrier coatings fabricated via electron beam-physical vapor deposition.
Zaoyu Shen +5 more
doaj +1 more source
Thermal barrier coating evaluation needs [PDF]
A 0.025 cm (0.010 in) thick thermal barrier coating (TBC) applied to turbine airfoils in a research gas turbine engine provided component temperature reductions of up to 190 C.
Brindley, William J., Miller, Robert A.
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