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Effect of Impeller Design and Spacing on Gas Exchange in a Percutaneous Respiratory Assist Catheter
Author(s) -
Jeffries R. Garrett,
Frankowski Brian J.,
Burgreen Greg W.,
Federspiel William J.
Publication year - 2014
Publication title -
artificial organs
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.684
H-Index - 76
eISSN - 1525-1594
pISSN - 0160-564X
DOI - 10.1111/aor.12308
Subject(s) - impeller , computational fluid dynamics , axial compressor , materials science , biomedical engineering , medicine , mechanical engineering , gas compressor , mechanics , engineering , physics
Providing partial respiratory assistance by removing carbon dioxide ( CO 2 ) can improve clinical outcomes in patients suffering from acute exacerbations of chronic obstructive pulmonary disease and acute respiratory distress syndrome. An intravenous respiratory assist device with a small (25 Fr ) insertion diameter eliminates the complexity and potential complications associated with external blood circuitry and can be inserted by nonspecialized surgeons. The impeller percutaneous respiratory assist catheter ( IPRAC ) is a highly efficient CO 2 removal device for percutaneous insertion to the vena cava via the right jugular or right femoral vein that utilizes an array of impellers rotating within a hollow‐fiber membrane bundle to enhance gas exchange. The objective of this study was to evaluate the effects of new impeller designs and impeller spacing on gas exchange in the IPRAC using computational fluid dynamics ( CFD ) and in vitro deionized water gas exchange testing. A CFD gas exchange and flow model was developed to guide a progressive impeller design process. Six impeller blade geometries were designed and tested in vitro in an IPRAC device with 2‐ or 10‐mm axial spacing and varying numbers of blades (2–5). The maximum CO 2 removal efficiency (exchange per unit surface area) achieved was 573 ± 8 mL /min/m 2 (40.1 mL /min absolute). The gas exchange rate was found to be largely independent of blade design and number of blades for the impellers tested but increased significantly (5–10%) with reduced axial spacing allowing for additional shaft impellers (23 vs. 14). CFD gas exchange predictions were within 2–13% of experimental values and accurately predicted the relative improvement with impellers at 2‐ versus 10‐mm axial spacing. The ability of CFD simulation to accurately forecast the effects of influential design parameters suggests it can be used to identify impeller traits that profoundly affect facilitated gas exchange.