IMPROVED FLOW STRAIGHTENERS REDUCE THROMBUS IN THE NASA DEBAKEY AXIAL-FLOW VENTRICULAR ASSIST DEVICE/

Citation
K. Kawahito et al., IMPROVED FLOW STRAIGHTENERS REDUCE THROMBUS IN THE NASA DEBAKEY AXIAL-FLOW VENTRICULAR ASSIST DEVICE/, Artificial organs, 21(4), 1997, pp. 339-343
Citations number
5
Categorie Soggetti
Engineering, Biomedical
Journal title
ISSN journal
0160564X
Volume
21
Issue
4
Year of publication
1997
Pages
339 - 343
Database
ISI
SICI code
0160-564X(1997)21:4<339:IFSRTI>2.0.ZU;2-F
Abstract
A small axial flow ventricular assist device (VAD) measuring 3 inches long and 1 inch in diameter is in development. The pump consists of a spinning inducer/impeller, a flow straightener (FLS), and a diffuser e nclosed in a cylindrical flow tube. The impeller has rod-shaped perman ent magnets embedded within its 6 blades and is activated magnetically by the motor stator which is positioned outside the flow tube. At the completion of a previous study, the FLS was identified as a thromboge nic area. The aim of the present study was to evaluate the thrombogeni city of redesigned FLSs (swept-back and bulbous types), compared with standard type (STD) FLS. A total of 15 pumps (STD, n = 7; swept-back, n = 4; and bulbous, n = 4) were sequentially implanted into 4 calves p aracorporeally in a short-term ex vivo test. The STD and bulbous FLSs experienced thrombus formation, but the swept-back FLS was thrombus fr ee during a 48 h screening test.