Axial-flow pump for a ventricular assist device and method for producing an axial-flow pump for a ventricular assist device
The invention relates to an axial flow pump ( 102 ) for a ventricular assist device. The axial flow pump ( 102 ) comprises a pump housing ( 104 ) for arranging in a blood vessel and a pump rotor ( 108 ), which is or can be mounted in the pump housing ( 104 ) for rotation about an axis of rotation and which consists of a hub ( 200 ) and at least one blade element ( 110 ) which is helically wound around the hub ( 200 ), at least in portions, and is provided for conveying, in the direction of the axis of rotation ( 302 ), a medium to be conveyed. In order to increase the pump efficiency, the blade element ( 110 ) has at least one blade section ( 202 ) having an undulating blade curvature.
1. A cardiac support system for insertion through a catheter into a blood vessel, comprising:
an axial flow pump comprising:
a tube-shaped pump housing having an axis of rotation extending therethrough; and
a pump rotor extending in the pump housing and being rotatable about the axis of rotation, the pump rotor comprising a hub and at least one blade element, the at least one blade element being wound at least in sections helically around the hub and configured to axially draw blood into the pump housing in a direction toward the hub;
wherein the pump housing further comprises:
a pump intake section upstream of the pump rotor and configured to receive the blood drawn into the pump housing, the pump intake section being penetrated by the axis of rotation; and
at least one peripheral outlet opening configured to laterally discharge the blood drawn into the pump housing;
wherein at least a portion of the at least one blade element is disposed downstream of an upstream edge of the at least one peripheral outlet opening; and
wherein the at least one blade element has a profile with camber lines, wherein a curvature of each of the camber lines when unwound into a plane increases along the axis of rotation in a direction starting from the pump intake section towards the at least one peripheral outlet opening to an inflection point at which a blade angle (ß) of the blade element is at a maximum, and wherein the curvature of each of the camber lines decreases after the inflection point; and
wherein, in a region of the pump rotor located radially relative to the axis of rotation and having a blade height SH of the at least one blade element defined relative to a maximum blade height SHMAX so that 25%≤SH/SHMAX≤100%, the inflection point of each of the camber lines is located in a region of an upstream edge of the at least one peripheral outlet opening.
2. The cardiac support system according to claim 1 , wherein the at least one blade element comprises at least one blade section having a wavy blade curvature.
3. The cardiac support system according to claim 2 , wherein the at least one blade section having the wavy blade curvature is configured in a section of the pump rotor at least partially located in a housing section of the pump housing open to the at least one outlet opening.
4. The cardiac support system according to claim 2 , wherein the wavy blade curvature varies in a direction of a radial extension of the at least one blade section.
5. The cardiac support system according to claim 2 , wherein the wavy blade curvature increases with increasing radial distance from the axis of rotation.
6. The cardiac support system according to claim 2 , wherein the at least one blade element has a thickness that changes along the axis of rotation in the at least one blade section having the wavy blade curvature.
7. The cardiac support system according to claim 1 , wherein the hub faces a distal end of the cardiac support system.
8. The cardiac support system according to claim 1 , wherein the hub has a diameter that increases along the axis of rotation in the direction starting from the pump intake region towards the outlet opening.
9. The cardiac support system according to claim 1 , wherein the blade angle (B) is measured relative to a line perpendicular to the axis of rotation.
10. A cardiac support system for insertion through a catheter into a blood vessel, comprising:
an axial flow pump comprising:
a pump rotor being rotatable about an axis of rotation, the pump rotor comprising a hub and at least one blade element, the at least one blade element being wound at least in sections helically around the hub and configured to axially draw blood into the pump in a direction toward the hub;
at least one peripheral outlet opening configured to laterally discharge the blood drawn into the pump;
wherein at least a portion of the at least one blade element is disposed downstream of an upstream edge of the at least one peripheral outlet opening; and
wherein the at least one blade element has a profile with camber lines, wherein a curvature of each of the camber lines when unwound into a plane increases along the axis of rotation in a direction starting from an upstream end of the rotor towards the at least one peripheral outlet opening to an inflection point at which a blade angle (ß) of the blade element is at a maximum, and wherein the curvature of each of the camber lines decreases after the inflection point;
wherein, in a region of the pump rotor located radially relative to the axis of rotation and having a blade height SH of the at least one blade element defined relative to a maximum blade height SHMAX so that 25%≤SH/SHMAX≤100%, the inflection point of each of the camber lines is located in a region of an upstream edge of the at least one peripheral outlet opening.
11. The cardiac support system according to claim 10 , wherein the at least one blade element comprises at least one blade section having a wavy blade curvature.
12. The cardiac support system according to claim 11 , wherein the at least one blade section having the wavy blade curvature is configured in a section of the pump rotor at least partially located in a section of the pump open to the at least one outlet opening.
13. The cardiac support system according to claim 11 , wherein the wavy blade curvature varies in a direction of a radial extension of the at least one blade section.
14. The cardiac support system according to claim 11 , wherein the wavy blade curvature increases with increasing radial distance from the axis of rotation.
15. The cardiac support system according to claim 11 , wherein the at least one blade element has a thickness that changes along the axis of rotation in the at least one blade section having the wavy blade curvature.
16. The cardiac support system according to claim 10 , wherein the hub faces a distal end of the cardiac support system.
17. The cardiac support system according to claim 10 , wherein the hub has a diameter that increases along the axis of rotation in the direction starting from the upstream end of the rotor towards the outlet opening.
18. The cardiac support system according to claim 10 , wherein the blade angle (ß) is measured relative to a line perpendicular to the axis of rotation.