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contributor authorH. M. Tawancy
contributor authorLuai M. Al-Hadhrami
date accessioned2017-05-09T00:50:40Z
date available2017-05-09T00:50:40Z
date copyrightJanuary, 2012
date issued2012
identifier issn1528-8919
identifier otherJETPEZ-27180#012101_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/148941
description abstractIt is known that the relative performance of thermal barrier coatings is largely dependent upon the oxidation properties of the bond coat utilized in the system. Also, the oxidation properties of diffusion-type bond coats (aluminides and their modifications) are functions of the superalloy substrate used in blade applications. Therefore, the performance of a given coating system utilizing a diffusion-type bond coat can significantly vary from one superalloy to another. Toward the objective of developing coating systems with more universal applicability, it is essential to understand the mechanisms by which the superalloy substrate can influence the coating performance. In this study, we examined the relative performance of yttria-stabilized zirconia/platinum aluminide coating system on alloys CMSX-4 and MAR M 002DS representing single-crystal and directionally-solidified alloy systems respectively using thermal exposure tests at 1150 °C with a 24-h cycling period to room temperature. Changes in coating microstructure were characterized by various electron-optical techniques. Experiment showed that the coating system on alloy MAR M 002DS had outperformed that on alloy CMSX-4, which could be related to the high thermal stability of the bond coat on alloy MAR M 002DS. From a detailed microstructural characterization, this difference in behavior could be explained at least partially in terms of variation in chemical composition of the two alloys, which was also reflected on the exact failure mechanism of the coating system.
publisherThe American Society of Mechanical Engineers (ASME)
titleComparative Performance of a Thermal Barrier Coating System Utilizing Platinum Aluminide Bond Coat on Alloys CMSX-4® and MAR M® 002DS
typeJournal Paper
journal volume134
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4004131
journal fristpage12101
identifier eissn0742-4795
keywordsCoating processes
keywordsCoatings
keywordsAlloys
keywordsoxidation
keywordsPlatinum
keywordsThermal barrier coatings
keywordsThermal stability
keywordsTemperature
keywordsSuperalloys
keywordsMechanisms AND Failure mechanisms
treeJournal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 001
contenttypeFulltext


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