| タイトル | Method for Reducing Pumping Damage to Blood |
| 本文（外部サイト） | http://hdl.handle.net/2060/19980022703 |
| 著者（英） | Benkowski, Robert J.; Akkerman, James W.; Bozeman, Richard J., Jr.; Svejkovsky, Robert J.; Bacak, James W.; Aber, Gregory S.; VanDamm, George Arthur |
| 著者所属（英） | NASA Johnson Space Center |
| 発行日 | 1997-10-21 |
| 言語 | eng |
| 内容記述 | Methods are provided for minimizing damage to blood in a blood pump wherein the blood pump comprises a plurality of pump components that may affect blood damage such as clearance between pump blades and housing, number of impeller blades, rounded or flat blade edges, variations in entrance angles of blades, impeller length, and the like. The process comprises selecting a plurality of pump components believed to affect blood damage such as those listed herein before. Construction variations for each of the plurality of pump components are then selected. The pump components and variations are preferably listed in a matrix for easy visual comparison of test results. Blood is circulated through a pump configuration to test each variation of each pump component. After each test, total blood damage is determined for the blood pump. Preferably each pump component variation is tested at least three times to provide statistical results and check consistency of results. The least hemolytic variation for each pump component is preferably selected as an optimized component. If no statistical difference as to blood damage is produced for a variation of a pump component, then the variation that provides preferred hydrodynamic performance is selected. To compare the variation of pump components such as impeller and stator blade geometries, the preferred embodiment of the invention uses a stereolithography technique for realizing complex shapes within a short time period. |
| NASA分類 | Aerospace Medicine |
| 権利 | No Copyright |
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