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Mechanisms of High Temperature Degradation of Thermal Barrier Coatings.

机译:高温降解热障涂层的机理。

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摘要

Thermal barrier coatings (TBCs) are crucial for increasing the turbine inlet temperature (and hence efficiency) of gas turbine engines. The thesis describes PhD research aimed at improving understanding of the thermal cycling failure mechanisms of electron beam physical vapour deposited (EB-PVD) yttria stabilised zirconia (YSZ) TBCs on single crystal superalloys.ududThe research consisted of three different stages. The first stage involved designing a coupled one-dimensional thermodynamic-kinetic oxidation and diffusion model capable of predicting the concentration profiles of alloying elements in a single-phase γ nickel-rich Ni-Al-Cr ternary alloy by the finite difference method. The aim of this investigation was to improve the understanding of interactions between alloying species and developing oxide. The model demonstrated that in the early stages of oxidation, Al consumption by oxide scale growth is faster than Al replenishment by diffusion towards the scale, resulting in an initial Al depletion in the alloy near the scale.ududThe second stage involved a systematic study of the life-time of TBC systems on different single crystal superalloys. The study aimed at demonstrating that the compatibility of modern nickel-based single crystal superalloys with TBC systems is influenced strongly by the content of alloying element additions in the superalloy substrate. The results can be explained by postulating that the fracture toughness parameters controlling decohesion are influenced strongly by small changes in composition arising from interdiffusion with the bond coat, which itself inherits elemental changes from the substrate.ududThe final stage of study involved a detailed study of different bond coats (two β-structured Pt-Al types and a γ/γ’ Pt-diffusion type) in TBC systems based on an EB-PVD YSZ top coat and a substrate material of CMSX-4 superalloy. Generation of stress in the thermally grown oxide (TGO) on thermal cycling, and its relief by plastic deformation and fracture, were investigated experimentally in detail.
机译:隔热涂层(TBC)对于提高燃气涡轮发动机的涡轮进口温度(从而提高效率)至关重要。本文描述了博士学位研究,旨在增进对单晶高温合金上电子束物理气相沉积(EB-PVD)氧化钇稳定的氧化锆(YSZ)TBC的热循环破坏机理的了解。 ud ud该研究包括三个不同的阶段。第一阶段涉及设计耦合的一维热力学-动力学氧化和扩散模型,该模型能够通过有限差分法预测单相富γ镍的Ni-Al-Cr三元合金中合金元素的浓度分布。这项研究的目的是增进对合金物质与发展中的氧化物之间相互作用的理解。该模型表明,在氧化的早期阶段,氧化物鳞片生长所消耗的Al快于通过向鳞片扩散而进行的Al补充,从而导致在鳞片附近合金中的初始Al耗尽。不同单晶高温合金的TBC系统寿命研究。该研究旨在证明现代镍基单晶高温合金与TBC系统的相容性受高温合金基底中合金元素添加量的强烈影响。该结果可以通过以下假设来解释:控制脱粘的断裂韧性参数受与粘结涂层相互扩散引起的成分的微小变化的强烈影响,而粘结涂层本身会继承基材的元素变化。 ud ud研究的最后阶段涉及详细EB-PVD YSZ面漆和CMSX-4高温合金基体材料在TBC系统中研究不同的粘结层(两种β结构的Pt-Al型和γ/γ'Pt扩散型)。通过实验详细研究了热循环中热生长氧化物(TGO)中应力的产生,以及由于塑性变形和断裂而引起的应力释放。

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    Wu Rudder T.C.;

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  • 年度 2009
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  • 正文语种 eng
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