首页> 外文期刊>Oxidation of Metals >On the Degradation Modes and Oxidation Behavior of Platinum Aluminide Bond Coats in Thermal Barrier Coating Used as Surface Protection System for a Turbine Blade Superalloy
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On the Degradation Modes and Oxidation Behavior of Platinum Aluminide Bond Coats in Thermal Barrier Coating Used as Surface Protection System for a Turbine Blade Superalloy

机译:涡轮叶片高温合金表面防护体系中热障涂层中铝化铂键合涂层的降解方式和氧化行为

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Adhesion of thermally grown oxide (TGO) to the bond coat is known to limit the useful life of thermal barrier coatings used in gas turbine blade applications. This is determined by the structure and composition of the bond coat as well as its thermal stability and in turn, its ability to develop and maintain a protective oxide. In this study, the degradation modes of platinum aluminides of the β-(Ni,Pt)Al- and PtAl_2 + β-(Ni,Pt)Al-types used as bond coats in thermal barrier coatings deposited on Ni-base superalloy and utilizing zirconia-7 wl% yttria and as top coat have been examined. Thermal exposure tests have been carried out at 1150℃ with cycling to room temperature every 24 h. Various electron-optical techniques have been used to characterize the microstructures of the bond coats and TGO. Particular emphasis has been placed upon the susceptibility of the bond coat to degradation by interdiffusion, oxidation, rumpling and formation of internal cavities. It is shown that the oxidation behavior and thermal stability characteristics are functions of the exact distribution of Pt in the bond coats. The β-(Ni,Pt)Al-type bond coat is found to have higher thermal stability and oxidize at a slower rate in comparison with the PtAl_2 + β-(Ni,Pt)Al_2-type. However, both bond coats are observed to exhibit a similar behavior in that the Al-rich and Pt-modified P-phase is progressively transformed into the Al-depleted γ'- and γ-phases with continued thermal exposure but at a slower rate in the β-(Ni,Pt)Al bond coat. Under the test conditions used in the study, there has been no evidence for rumpling, however, internal cavities are observed near the surface of each bond coat during the later stages of thermal exposure showing that rumpling is not necessarily a prerequisite. Failure of the respective thermal barrier coating systems is found to occur by loss of adhesion between the TGO and bond coat whose composition has approached that of the superalloy substrate by interdiffusion.
机译:已知将热生长氧化物(TGO)粘附到粘结涂层上会限制燃气轮机叶片应用中使用的隔热涂层的使用寿命。这取决于粘结涂层的结构和组成及其热稳定性,进而取决于其形成和维持保护性氧化物的能力。在这项研究中,β-(Ni,Pt)Al-和PtAl_2 +β-(Ni,Pt)Al型铂铝化物的降解方式用作沉积在镍基高温合金上的热障涂层的粘结层并利用已经研究了氧化锆-7 wl%的氧化钇和作为面漆。热暴露测试已在1150℃下进行,每24小时循环到室温。各种电子光学技术已被用来表征涂层和TGO的微观结构。已经特别强调了粘合层由于相互扩散,氧化,起皱和形成内腔而易于降解的敏感性。结果表明,氧化行为和热稳定性是Pt在粘结层中精确分布的函数。与PtAl_2 +β-(Ni,Pt)Al_2-型相比,发现β-(Ni,Pt)Al-型粘结涂层具有更高的热稳定性并以较慢的速率氧化。然而,观察到两种粘结涂层都表现出相似的行为,因为在持续的热暴露下,富铝和Pt改性的P相逐渐转变为贫铝的γ'和γ相,但在C中的速率较慢。 β-(Ni,Pt)Al键合涂层。在研究中使用的测试条件下,没有任何起皱的证据,但是,在热暴露的后期阶段,在每个粘合涂层的表面附近观察到内腔,这表明起皱不一定是先决条件。发现各个热障涂层系统的失效是由于TGO和粘结涂层之间的粘合损失而发生的,该涂层的组成已经通过相互扩散达到了超合金基体的组成。

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