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超超临界汽轮机汽封漏汽流动特性的数值模拟研究 被引量:3

The research of numerical simulation for steam vapor seal leakage
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摘要 利用ANSYS软件对梳齿型、侧齿型和蜂窝型汽封的内部气体流动特性进行数值模拟分析,其结果表明:在相同的特征尺寸和边界条件下,梳齿型汽封出口压力最高,蜂窝型汽封出口压力最低。在梳齿型汽封中,气流在汽封齿与凸台之间形成的蒸汽室内将产生漩涡;侧齿汽封由于增加了侧齿,产生的漩涡强度将增大;蜂窝汽封在每个小蜂窝中将产生漩涡,漩涡强度最小,节流效果最明显。蜂窝式汽封的漏汽量最小,梳齿型汽封漏汽量最大。当出口压力相同、入口压力不同时,随着入口压力的增加,3种汽封的漏汽量也随之增加;当出、入口压力相同时,随着汽封段长度的增加,3种汽封的漏汽量均减小。 The numerical simulation of internal vapor flow characteristics of the comb-type steam seal, side tooth steam vapor seal and honeycomb seal with ANSYS software shows that the outlet pressure of comb-type seal is the highest while the pressure of honeycomb seal outlet is the lowest under the same feature size, the same boundary con- ditions. In the comb type seal, airflow formed vortex in the steam room between the gland tooth and the convex plat- form. Due to the added lateral teeth, the vortex intensity in the lateral teeth gland is increased. For the honeycomb seal, the throttling effect is obvious each because each small cellular produces spiral. It can thus be seen that the steam leak- age from the cellular steam seal is minimum while that from comb-type steam seal is the largest. With the increasing steam inlet pressure, the steam leakage of all three seals increases under same outlet pressure and different inlet pres- sure. And with the increasing steam seal length, the steam leakage of all three seals decreases under same outlet and in- let pressure.
出处 《沈阳工程学院学报(自然科学版)》 2015年第1期35-38,共4页 Journal of Shenyang Institute of Engineering:Natural Science
关键词 蜂窝式汽封 梳齿型汽封 侧齿型汽封 数值模拟 漏汽量 Honeycomb seal Comb labyrinth seal Lateral teeth seal Numerical simulation Air leakage
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  • 1王旭,张文平,马胜远,诸振友.转子蜂窝密封封严特性的试验研究[J].热能动力工程,2004,19(5):521-525. 被引量:25
  • 2李军,邓清华,丰镇平.蜂窝汽封和迷宫式汽封流动性能比较的数值研究[J].中国电机工程学报,2005,25(16):108-111. 被引量:70
  • 3张延蜂,王绍民.蜂窝式密封及汽轮机相关节能技术的研究与应用[M].北京:中国电力出版社,2007.
  • 4Sehramm V,Wiilenborg K,Kim Set al.Influence of a hone; ycomb -facing on the flow through a stepped labyrinth seal[J].ASME J,Eng.Gas Turbine Power,2000,124:140-146.
  • 5Schlienger J,Pfau A,Kalfas A Let al.Effects of labyrinth seal variation on multistage axial turbine flow[A].GT2003-38270,Proceedings of ASME turbo Expo 2003,Power for Land,Sea,and Air[C].Atlanta,Georgia,USA:2003.
  • 6沈庆根.化工机器故障诊断技术.杭州:浙江大学出版社,1994
  • 7韩中合,康乐嘉.汽轮机直齿与斜齿汽封内部流场的数值计算与结构优化[J].动力工程,2007,27(4):473-476. 被引量:12
  • 8[1]Memmott E..Stability analysis and testing of a train of centrifugal compressors for high pressure gas injection[J] . Journal of Engineering for Gas Turbines and Power,1999, 121:509~514
  • 9[3]Soto E., Childs D..Experimental rotordynamic coefficient results for (a) a labyrinth seal with and without shunt injection and (b) a honeycomb seal [J] . Journal of Engineering for Gas Turbines and Power, 1999, 121:153 ~ 159
  • 10Dursun Eser,Yilmaz Dereli.Comparisons of rotordynamic coefficients in stepped labyrinth seals by using Colebrook-White friction factor model[J].Meccanica,2007,42:177-186.

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