Volume 36 Issue 6
Jun.  2021
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XIE Nan, TANG Yumeng, LIU Yangwei, ZHANG Yan. Numerical research on effects of blade tip clearances onthe hemocompatibility of artificial heart pump[J]. Journal of Aerospace Power, 2021, 36(6): 1304-1314. doi: 10.13224/j.cnki.jasp.2021.06.019
Citation: XIE Nan, TANG Yumeng, LIU Yangwei, ZHANG Yan. Numerical research on effects of blade tip clearances onthe hemocompatibility of artificial heart pump[J]. Journal of Aerospace Power, 2021, 36(6): 1304-1314. doi: 10.13224/j.cnki.jasp.2021.06.019

Numerical research on effects of blade tip clearances onthe hemocompatibility of artificial heart pump

doi: 10.13224/j.cnki.jasp.2021.06.019
  • Received Date: 2020-08-31
  • Publish Date: 2021-06-28
  • Steady and unsteady numerical simulations were carried out to systematically research the hemodynamic performance and hemocompatibility of four groups of centrifugal blood pumps with different blade tip clearance at 173 mmHg. The gaps studied were 5.0 mm, 2.0 mm, 1.0 mm and 0.2 mm, respectively, the distribution of parameters and the changes of normalized index of hemolysis with the size of blade tip clearance were researched. The results showed that the origin pump had good hemocompatibility at 3.0 L/min against a pressure head of 173 mmHg; with the decrease of blade tip clearance, the max stress and the normalized index of hemolysis showed a single peak and the minimum normalized index of hemolysis 0.000 5 g/100 L was obtained in the 1.0 mm clearance structure, which reduced the risk of thrombosis in the gap between the outer impeller walls and the lower housing cavity walls; compared with the results of the unsteady simulation: steady results were often too small to predict hemolysis, the transient normalized index of hemolysis changed periodically with the impeller rotation, and the difference between its mean and the steady results was within 5%.

     

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