首页|微肋几何因素对涡轮叶片冲击冷却性能的影响

微肋几何因素对涡轮叶片冲击冷却性能的影响

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为研究W型肋对冲击冷却的强化作用,采用数值模拟方法以光滑靶面为基准,研究冲击雷诺数Re在4 000~10 000范围内肋的宽度、高度和夹角对换热靶面的影响.所研究的肋宽W为0.05d,0.1d,0.2d,0.4d,高度H为0.1d,0.3d,0.4d,0.8d,夹角α为90°,120°,150°,180°.结果表明,随肋高度增加,换热总量和阻力整体增加,综合换热效果在H=0.3d时最佳.换热量随着肋宽度增大先增大后减小,在W=0.1d时最大;随着α增加,阻力先增大后减小,综合换热效果逐渐下降,α=90°时的综合换热效果最好,α=120°时总换热量最大;从整体而言,添加W=0.1d,H=0.3d及α=90°的W型肋的综合换热效果最好,换热量相比于光滑靶面可提升28.5%~33.5%.
Effect of Geometric Factors of Micro-ribs on Impingement Cooling Performance of Turbine Blades
In order to investigate the strengthening effect of W-shaped ribs on impingement cooling,this paper studied the effect of rib width,height and angle on the heat transfer target surface when the im-pingement Reynolds number Re is in the range of 4 000-10 000 based on the smooth target surface by u-sing the numerical simulation method.The studied rib width W is 0.05d,0.1d,0.2d,0.4d,height H is 0.1d,0.3d,0.4d,0.8d and angle α is 90°,120°,150°,180°.The results show that with the in-crease of rib height,the total heat transfer and the resistance increase as a whole,and the comprehensive thermal performance is the best at H=0.3d.The amount of heat transfer first increases and then decrea-ses with increasing rib width,reaching a maximum at W=0.1d.As the angle increases,the resistance first increases and then decreases,and the comprehensive thermal performance gradually decreases,with the best comprehensive thermal performance at α=90° and the maximum total heat transfer at α=120°.As a whole,the comprehensive thermal performance of the W-shaped rib is the best at W=0.1d,H=0.3d and α=90°.And the heat transfer capacity can be improved by 28.5%-33.5%compared with that of the smooth target surface.

impingement coolinggas turbineturbine bladeimpingement Reynolds numberW-shaped rib

栾佳铭、符昊、张华庆、栾一刚

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哈尔滨工程大学动力与能源工程学院,黑龙江哈尔滨 150001

中国船舶集团有限公司第七○三研究所,黑龙江哈尔滨 150078

冲击冷却 燃气轮机 涡轮叶片 冲击雷诺数 W型肋

2024

热能动力工程
中国 哈尔滨 第七0三研究所

热能动力工程

CSTPCD北大核心
影响因子:0.345
ISSN:1001-2060
年,卷(期):2024.39(11)