二氧化硅气凝胶作为燃烧室内衬隔热材料的实验评价

IF 1.1 Q4 ENGINEERING, MECHANICAL Journal of the Global Power and Propulsion Society Pub Date : 2020-09-09 DOI:10.33737/gpps20-tc-46
Yeongmin Pyo, T. Robertson, Sean Yun, Zekai Hong
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引用次数: 2

摘要

对使用二氧化硅气凝胶作为燃烧室内衬隔热材料的可行性进行了实验研究。气凝胶是一种优良的材料,由于其低导热性,可使到达燃烧衬套金属结构的热通量最小化。在本研究中,使用锥形天然气燃烧旋流火焰燃烧器来再现燃烧环境。二氧化硅气凝胶毯被连接到一个穿孔燃烧室内衬的内侧。使用校准的红外相机测量燃烧衬套外侧的温度分布。为了在气凝胶表面上形成保护性冷却膜,从穿孔金属衬里的背面提供冷却空气,并允许冷却空气穿透二氧化硅气凝胶毯以排放到燃烧器。当燃烧器以0.83的固定当量比运行时,改变冷却空气流速,以评估不同冷却流速下气凝胶毯上蒸发冷却的有效性。测得的温度分布演变证实了蒸腾冷却条件下每个试验条件下的热平衡。金属内衬的温度分布表明,在冷却膜的保护下,气凝胶毯具有良好的隔热性能,燃烧产物温度与背面金属内衬温度之间的温差高达1580K。此外,在燃烧试验前后对二氧化硅气凝胶样品进行了检查,以使用高分辨率扫描电子显微镜(SEM)了解其在典型燃气轮机燃烧器环境中的材料降解情况。测试结果表明,燃烧测试中的二氧化硅气凝胶毯样品具有多种降解机制。例如,可以通过取代二氧化硅气凝胶中的玻璃纤维来改进二氧化硅气凝胶毡,以获得更具弹性的隔热材料。
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Experimental Evaluation of Using Silica Aerogels as the Thermal Insulator for Combustor Liners
An experimental study was conducted for evaluating the feasibility of using silica aerogel as thermal insulator for combustor liners. Aerogels are a superior material for minimizing heat flux to the metal structure of the combustion liner due to their low thermal conductivity. In this study, a conical natural gas fired swirling-flame combustor was utilized for reproducing the combustion environment. The silica aerogel blanket was attached to the inner side of a perforated combustor liner. Temperature distribution on the outer side of the combustion liner was measured using a calibrated IR camera. To create a protective cooling film over the aerogel surface, cooling air was supplied from the back side of the perforated metal liner and was allowed to penetrate the silica aerogel blanket to be discharged to the combustor. As the combustor was operated at a fixed equivalence ratio of 0.83, cooling air flow rates were varied to evaluate the effectiveness of transpiration cooling on the aerogel blanket as various cooling flow rates. The measured evolution of temperature distribution confirmed thermal equilibriums for every test condition with transpiration cooling. The measured temperature distribution of metal liner demonstrated superior thermal insulation of aerogel blanket under the protection of cooling film with a temperature difference as high as 1580 K between combustion products temperature and the metal liner temperature on the back side. In addition, silica aerogel samples were examined before and after the combustion tests to understand their material degradation exposing to a typical gas turbine combustor environment using high-resolution scanning electron microscope (SEM). Test results suggest multiple degradation mechanisms to the silica aerogel blanket samples from the combustion tests. Improvements can be made to the silica aerogel blankets for a more resilient thermal insulator, for example, by replacing glass fibers in silica aerogels.
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来源期刊
Journal of the Global Power and Propulsion Society
Journal of the Global Power and Propulsion Society Engineering-Industrial and Manufacturing Engineering
CiteScore
2.10
自引率
0.00%
发文量
21
审稿时长
8 weeks
期刊最新文献
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