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Effects of impingement plate on thermal performance of premixed impinging flame jets.

机译:冲击板对预混冲击火焰射流热性能的影响。

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摘要

Experiments have been carried out to investigate the effects of an impingement plate on the heat transfer characteristics of the impinging flame jet system. For the present study, the impingement plates were fabricated with three materials, viz. brass (k = 61W/mK), bronze ( k = 26W/mK) and stainless steel (k =14.9W/mK). It has been found that, under similar experimental conditions of the flame jet, the maximum local heat flux obtained with the brass plate(which has the highest thermal conductivity), is much higher than that obtained with the stainless steel plate(which has the lowest thermal conductivity). Such a phenomenon is quite obvious at the stagnation region but becomes less significant in the wall jet region of the impingement plate.; It is also found that the use of a low-conductivity impingement plate would lead to a larger suppression of heat transfer and a higher collection of unburned fuel at the stagnation point, as well as an outward shift of the location of maximum heat flux from there. More unburned fuel being consumed progressively beyond the stagnation region would lead to further shift of the location of the maximum heat flux. It has found that conduction, usually thought to be less significant in this kind of heat transfer, was actually playing a rather important role in the overall heat transfer from an impinging flame jet to the impingement plate.; Experimental investigation has been conducted to study the thermal effect of the impingement plate surface emissivity, a parameter normally assumed to affect directly radiation heat transfer. Three brass plates of different surface emissivites (0.10, 0.38 and 0.98) were tested using the same premixed impinging flame jet. The phenomena of the occurrence of a cold region around the stagnation region and the outward shift of the location of maximum heat flux have also been observed. Although the surface emissivities are quite different, viz. 0.1, 0.38 and 0.98, the differences among maximum local heat fluxes of the impingement plates were found to be rather small, especially at the wall jet region (where the maximum difference was only 8%). It is therefore concluded that the effect of surface emissivity, and hence radiation, on both heat flux and temperature distribution on an impingement plate is rather insignificant, especially at the wall jet region. This implies that non-luminous radiation has insignificant influence on the thermal performance of the gas-fired premixed impingement flame jet system.; To investigate the effect of surface roughness of the impingement plate on convective heat transfer of the flame jet system, three brass plates of significantly different surface roughness (1.035 mum, 100 mu m and 500 mum) have been tested using the same premixed impinging flame jet. A difference in the stagnation point heat flux of 40% was found between the smoothest and the roughest plates. It shows that a rough surface is able to act as a turbulence promoter. In view of the dominant role of convection in the flame jet system, a variation in plate surface roughness can generate quite a significant effect on the overall heat transfer from a premixed flame jet to the impingement plate.; Multivariate regression models have been developed for the prediction of the area-averaged heat flux received in terms of each of three important plate characteristics, viz. thermal conductivity, surface emissivity and surface roughness. By means of a full factorial design, the integrated effect of each of these plate characteristics and the three test variables (i.e. Reynolds number, equivalence ratio, and nozzle-to-plate distance) on heat flux received can be estimated. At a confidence level of 95%, predictions given by all three area-averaged heat flux models have been found to agree closely with the experimental results.; A numerical study was conducted to simulate conduction heat transfer through the impingement plates. Assuming heat loss from the heated plate to the surroundi
机译:已经进行了实验以研究冲击板对冲击火焰喷射系统的传热特性的影响。对于本研究,冲击板是用三种材料制成的。黄铜(k = 61W / mK),青铜(k = 26W / mK)和不锈钢(k = 14.9W / mK)。已经发现,在类似的火焰喷射实验条件下,用黄铜板(导热率最高)获得的最大局部热通量要比用不锈钢板(最低导热率)获得的最大局部热通量高得多。导热系数)。这种现象在停滞区域相当明显,但在冲击板的壁射流区域变得不那么明显。还发现使用低电导率的撞击板将导致更大程度的热传递抑制,并在停滞点处收集更多未燃烧的燃料,以及最大热通量位置从此处向外移动。在停滞区域之外逐渐消耗更多未燃烧的燃料将导致最大热通量的位置进一步偏移。已经发现通常被认为在这种热传递中不那么重要的传导实际上在从撞击火焰射流到撞击板的整个热传递中起着相当重要的作用。已经进行了实验研究以研究冲击板表面发射率的热效应,通常认为该参数直接影响辐射热传递。使用相同的预混合撞击火焰喷嘴测试了三个表面发射率分别为0.10、0.38和0.98的黄铜板。还观察到在停滞区周围出现冷区以及最大热通量位置向外移动的现象。尽管表面发射率有很大不同,即。在0.1、0.38和0.98之间,发现冲击板的最大局部热通量之间的差异很小,尤其是在壁射流区域(最大差异仅为8%)。因此得出结论,尤其是在壁射流区域,表面辐射率以及因此的辐射对冲击板上的热通量和温度分布的影响都很小。这意味着非发光辐射对燃气预混合冲击火焰喷射系统的热性能影响不大。为了研究冲击板的表面粗糙度对火焰喷射系统对流传热的影响,使用相同的预混合冲击火焰喷嘴测试了三块表面粗糙度明显不同的黄铜板(1.035μm,100μm和500 mm) 。在最光滑和最粗糙的板之间发现停滞点热通量相差40%。它表明粗糙的表面能够充当湍流促进剂。考虑到对流在火焰喷射系统中的主要作用,板表面粗糙度的变化会对从预混火焰喷射到冲击板的总热传递产生相当大的影响。已经开发出了多元回归模型,用于根据三个重要板块特性中的每个来预测接收到的面积平均热通量。导热率,表面发射率和表面粗糙度。通过全因子设计,可以估计这些板特性和三个测试变量(即雷诺数,当量比和喷嘴到板的距离)对接收到的热通量的综合影响。在95%的置信度下,已发现所有三个面积平均热通量模型给出的预测与实验结果非常吻合。进行了数值研究以模拟通过冲击板的传导热传递。假设热量从加热板流向周围

著录项

  • 作者

    Zhao, Zhen.;

  • 作者单位

    Hong Kong Polytechnic University (Hong Kong).;

  • 授予单位 Hong Kong Polytechnic University (Hong Kong).;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2006
  • 页码 226 p.
  • 总页数 226
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;
  • 关键词

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