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耦合热、动载荷的超超临界汽轮机迷宫密封动力特性

司和勇 曹丽华 李盼

司和勇, 曹丽华, 李盼. 耦合热、动载荷的超超临界汽轮机迷宫密封动力特性[J]. 航空动力学报, 2019, 34(9): 1905-1913. doi: 10.13224/j.cnki.jasp.2019.09.007
引用本文: 司和勇, 曹丽华, 李盼. 耦合热、动载荷的超超临界汽轮机迷宫密封动力特性[J]. 航空动力学报, 2019, 34(9): 1905-1913. doi: 10.13224/j.cnki.jasp.2019.09.007
Dynamic characteristics coupled thermal and dynamic loads for labyrinth seal in ultra-supercritical steam turbine[J]. Journal of Aerospace Power, 2019, 34(9): 1905-1913. doi: 10.13224/j.cnki.jasp.2019.09.007
Citation: Dynamic characteristics coupled thermal and dynamic loads for labyrinth seal in ultra-supercritical steam turbine[J]. Journal of Aerospace Power, 2019, 34(9): 1905-1913. doi: 10.13224/j.cnki.jasp.2019.09.007

耦合热、动载荷的超超临界汽轮机迷宫密封动力特性

doi: 10.13224/j.cnki.jasp.2019.09.007
基金项目: 国家自然科学基金(51576036)

Dynamic characteristics coupled thermal and dynamic loads for labyrinth seal in ultra-supercritical steam turbine

  • 摘要: 密封汽流激振严重影响超超临界汽轮机的安全运行,采用DEFINE_CG_MOTION和DEFINE_PROFILE控制宏建立转子的涡动方程,通过Workbench流固耦合方法计算热、动载荷下密封齿形变,根据快速傅里叶变化得到机组运行时的密封动力特性,并对转子稳定性进行分析。结果表明:蒸汽可导致密封齿膨胀变形,温度对密封齿长度变化影响可达1%~1.5%,压力和离心作用对其影响较小。热、动载荷使迷宫密封直接刚度减小,直接阻尼先增加后减小,交叉刚度先减小后增加,动力系数的最大变化为原来的2倍。35~55 Hz内转子稳定裕度急剧下降,转子对密封汽流激振更敏感。热、动载荷引起的压力波动集中在低频范围,密封周向压力波动可增高18.5 kPa。密封高压区的压力波幅剧增是汽流激振显著的主要原因。

     

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出版历程
  • 收稿日期:  2019-04-15
  • 刊出日期:  2019-09-28

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