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首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >High Temperature Radiation Heat Transfer Performance of Thermal Barrier Coatings With Multiple Layered Structures
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High Temperature Radiation Heat Transfer Performance of Thermal Barrier Coatings With Multiple Layered Structures

机译:多层结构热障涂层的高温辐射传热性能

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摘要

Meeting the demands for ever increasing operating temperatures in gas turbines requires concurrent development in cooling technologies, new generations of superalloys, and thermal barrier coatings (TBCs) with increased insulation capability. In the case of the latter, considerable research continues to focus on new coating material compositions, the alloying/doping of existing yttria stabilized zirconia ceramics, and the development of improved coating microstructures. The advent of the electron beam physical vapor deposition coating process has made it possible to consider the creation of multiple layered coating structures to meet specific performance requirements. In this paper, the advantages of layered structures are first reviewed in terms of their functions in impeding thermal conduction (via phonons) and thermal radiation (via photons). Subsequently, the design and performance of new multiple layered coating structures based on multiple layered stacks will be detailed. Designed with the primary objective to reduce thermal radiation transport through TBC systems, the multiple layered structures consist of several highly reflective multiple layered stacks, with each stack used to reflect a targeted radiation wavelength range. Two ceramic materials with alternating high and low refractive indices are used in the stacks to provide multiple-beam interference. A broadband reflection of the required wavelength range is obtained using a sufficient number of stacks. In order to achieve an 80% reflectance to thermal radiation in the wavelength range 0.3-5.3 μm, 12 stacks, each containing 12 layers, are needed, resulting in a total thickness of 44.9 μm. Using a one dimensional heat transfer model, the steady state heat transfer through the multiple layered TBC system is computed. Various coating configurations combining multiple layered stacks along with a single layer are evaluated in terms of the temperature profile in the TBC system. When compared with a base line single layered coating structure of the same thickness, it is estimated that the temperature on the metal surface can be reduced by as much as 90℃ due to the use of multiple layered coating configurations. This reduction in metal surface temperature, however, diminishes with increasing the scattering coefficient of the coating and the total coating thickness. It is also apparent that using a multiple layered structure throughout the coating thickness may not offer the best thermal insulation; rather, placing multiple layered stacks on top of a single layer can provide a more efficient approach to reducing the heat transport of the TBC system.
机译:为了满足不断增长的燃气轮机运行温度的要求,需要同时开发冷却技术,新一代的高温合金以及具有增强绝热能力的隔热涂层(TBC)。在后者的情况下,大量的研究继续集中在新的涂层材料成分,现有的氧化钇稳定的氧化锆陶瓷的合金化/掺杂以及改进的涂层微观结构的开发上。电子束物理气相沉积涂覆工艺的出现使得考虑多层涂覆结构的产生以满足特定的性能要求成为可能。在本文中,首先从层状结构在阻止热传导(通过声子)和热辐射(通过光子)的功能方面进行了综述。随后,将详细描述基于多层堆叠的新型多层涂层结构的设计和性能。旨在减少通过TBC系统的热辐射传输的主要目的,多层结构由几个高反射率的多层堆栈组成,每个堆栈用于反射目标辐射波长范围。堆叠中使用交替具有高低折射率的两种陶瓷材料来提供多光束干涉。使用足够数量的堆叠可以获得所需波长范围的宽带反射。为了在0.3-5.3μm的波长范围内达到80%的热辐射反射率,需要12个堆叠(每个堆叠包含12层),总厚度为44.9μm。使用一维热传递模型,计算通过多层TBC系统的稳态热传递。根据TBC系统中的温度曲线,评估了将多层堆叠与单层结合在一起的各种涂层配置。与相同厚度的基线单层涂层结构相比,据估计,由于使用了多层涂层结构,金属表面的温度可降低多达90℃。然而,金属表面温度的这种降低随着涂层的散射系数和总涂层厚度的增加而减小。同样明显的是,在整个涂层厚度上使用多层结构可能无法提供最佳的隔热性能。相反,将多层堆叠放置在单层顶部可以提供更有效的方法来减少TBC系统的热传递。

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