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Axial PumpA rotary blood pump includes a pump housing for receiving a flow straightener, a rotor mounted on rotor bearings and having an inducer portion and an impeller portion, and a diffuser. The entrance angle, outlet angle, axial and radial clearances of blades associated with the flow straightener, inducer portion, impeller portion and diffuser are optimized to minimize hemolysis while maintaining pump efficiency. The rotor bearing includes a bearing chamber that is filled with cross-linked blood or other bio-compatible material. A back emf integrated circuit regulates rotor operation and a microcomputer may be used to control one or more back emf integrated circuits. A plurality of magnets are disposed in each of a plurality of impeller blades with a small air gap. A stator may be axially adjusted on the pump housing to absorb bearing load and maximize pump efficiency.
Document ID
19980037704
Acquisition Source
Johnson Space Center
Document Type
Other - Patent
Authors
Bozeman, Richard J., Jr.
(NASA Johnson Space Center Houston, TX United States)
Akkerman, James W.
(NASA Johnson Space Center Houston, TX United States)
Aber, Gregory S.
(NASA Johnson Space Center Houston, TX United States)
VanDamm, George Arthur
(NASA Johnson Space Center Houston, TX United States)
Bacak, James W.
(NASA Johnson Space Center Houston, TX United States)
Svejkovsky, Paul A.
(NASA Johnson Space Center Houston, TX United States)
Benkowski, Robert J.
(NASA Johnson Space Center Houston, TX United States)
Date Acquired
August 18, 2013
Publication Date
December 2, 1997
Subject Category
Mechanical Engineering
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-153595
Patent Application Number: US-Patent-Appl-SN-653929
Patent Number: US-Patent-5,692,882
Patent Number: NASA-Case-MSC-22424-3
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-5,692,882|NASA-Case-MSC-22424-3
Patent Application
US-Patent-Appl-SN-153595|US-Patent-Appl-SN-653929
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