IP Library Granted Patent US 11,754,075
Granted Patent B2
US 11,754,075 · App. 17/258,853 · Granted Sep 12, 2023

Impeller for an implantable, vascular support system

Inventors: Armin Schuelke (Aidlingen, DE); Ingo Stotz (Ditzingen, DE); Johannes Bette (Leonberg, DE); David Minzenmay (Stuttgart, DE)
Assignee: KARDION GMBH
F04D13/024A61M60/174A61M60/237A61M60/408A61M60/416A61M60/419A61M60/804A61M60/82A61M60/857F04D3/02F04D29/181F04D29/20F04D29/60A61M2207/00
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 11,754,075
App. No.
17/258,853
Granted
Sep 12, 2023
Kind
B2
Abstract

An impeller ( 1 ) for an implantable vascular support system ( 2 ) is provided. The impeller includes an impeller body ( 3 ) having a first longitudinal portion ( 4 ) and a second longitudinal portion ( 5 ) forming a first inner rotor ( 12 ) having at least one magnet encapsulated in the second longitudinal portion ( 5 ). At least one blade ( 6 ) formed in the first longitudinal portion ( 4 ) is configured to axially convey a fluid upon rotation. A second outer rotor ( 13 ) extends axially and includes at least one magnet. The first rotor ( 12 ) and the second rotor ( 13 ) form a magnetic coupling ( 14 ). The magnets of the first and second rotor being arranged to partially axially overlap with an axial offset and are entirely radially offset.

Claims (36)

1. A cardiac support system, comprising:

an impeller comprising:

an impeller body comprising:

a first longitudinal portion comprising at least one blade configured to axially convey a fluid by a rotational movement; and

a second longitudinal portion comprising a first rotor extending axially; and

at least one magnet disposed and encapsulated in the second longitudinal portion; and

a second rotor extending axially and comprising at least one magnet, wherein the first rotor and the second rotor are configured to form a magnetic coupling, wherein the at least one magnet of the impeller and the at least one magnet of the second rotor partially axially overlap and are partially axially offset, and wherein the at least one magnet of the impeller and the at least one magnet of the second rotor are entirely radially offset.

2. The cardiac support system according to claim 1 , wherein the impeller body is a single piece.

3. The cardiac support system according to claim 1 , wherein the impeller body comprises multiple pieces.

4. The cardiac support system according to claim 1 , further comprising a drive shaft, wherein the drive shaft comprises the second rotor.

5. The cardiac support system according to claim 1 , wherein the magnetic coupling comprises a radial coupling.

6. The cardiac support system according to claim 1 , wherein the first rotor is an outer rotor and the second rotor is an inner rotor positioned at least partially in a cavity within the impeller body.

7. The cardiac support system according to claim 1 , wherein the second longitudinal portion further comprises a magnetic return.

8. The cardiac support system according to claim 1 , further comprising a cover configured to at least partially encapsulate the at least one magnet of the second longitudinal portion.

9. The cardiac support system according to claim 1 , wherein the at least one magnet of the impeller comprises a plurality of magnets offset from one another axially.

10. The cardiac support system according to claim 1 , wherein the at least one magnet of the second rotor comprises a plurality of magnets offset from one another axially.

11. The cardiac support system according to claim 1 , wherein:

the second longitudinal portion of the impeller is disposed in a proximal direction with respect to the first longitudinal portion of the impeller; and

the at least one magnet of the second rotor is partially axially offset in the proximal direction with respect to the at least one magnet of the impeller.

12. The cardiac support system according to claim 11 , wherein said at least one blade of the first longitudinal portion is configured to axially convey said fluid in the proximal direction.

13. A method for producing a cardiac support system, comprising:

disposing and encapsulating at least one magnet in a second longitudinal portion of an impeller body of an impeller of the cardiac support system, wherein the impeller body further comprises a first longitudinal portion comprising at least one blade configured to axially convey a fluid by a rotational movement,

wherein the second longitudinal portion comprises a first rotor extending axially, and

wherein the cardiac support system comprises a second rotor extending axially and comprising at least one magnet, wherein the first rotor and the second rotor are configured to form a magnetic coupling, wherein the at least one magnet of the impeller and the at least one magnet of the second rotor partially axially overlap and are partially axially offset, and wherein the at least one magnet of the impeller and the at least one magnet of the second rotor are entirely radially offset.

14. The method according to claim 13 , wherein the impeller body is a single piece.

15. The method according to claim 13 , wherein the impeller body comprises multiple pieces.

16. The method according to claim 13 , wherein the second longitudinal portion further comprises a magnetic return.

17. The method according to claim 13 , wherein encapsulating the at least one magnet comprises encapsulating the at least one magnet of the second longitudinal portion with a cover.

18. The method according to claim 17 , wherein encapsulating the at least one magnet of the second longitudinal portion with the cover comprises thermally joining the cover to the second longitudinal portion.

19. The method according to claim 13 , wherein the first rotor is an outer rotor and the second rotor is an inner rotor positioned at least partially in a cavity within the impeller body.

20. The method according to claim 13 , wherein the at least one magnet of the impeller comprises a plurality of magnets offset from one another axially.

21. The method according to claim 13 , wherein the at least one magnet of the second rotor comprises a plurality of magnets offset from one another axially.

22. The method according to claim 13 , wherein:

the second longitudinal portion of the impeller is disposed in a proximal direction with respect to the first longitudinal portion of the impeller; and

the at least one magnet of the second rotor is partially axially offset in the proximal direction with respect to the at least one magnet of the impeller.

23. The method according to claim 22 , wherein said at least one blade of the first longitudinal portion is configured to axially convey said fluid in the proximal direction.

Assignments (4)
CORRECTIVE ASSIGNMENT TO CORRECT THE APPLICATION NO. 17055502 TO READ 17055023 PREVIOUSLY RECORDED AT REEL: 062896 FRAME: 0150. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded Mar 17, 2023
From: ROBERT BOSCH GMBH
To: KARDION GMBH
Reel/Frame 063116/0438 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 6, 2023
From: ROBERT BOSCH GMBH
To: KARDION GMBH
Reel/Frame 062896/0150 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 21, 2022
From: SCHUELKE, ARMIN; STOTZ, INGO; BETTE, JOHANNES; MINZENMAY, DAVID
To: ROBERT BOSCH GMBH
Reel/Frame 058731/0417 →
SECURITY INTEREST Recorded Apr 26, 2021
From: KARDION GMBH
To: EDWARDS LIFESCIENCES HOLDING, INC.
Reel/Frame 056046/0422 →
Continuity (1)
Related Publication 20210379358A1 · Dec 9, 2021
Cited By (23)
US 12,194,287 US 12,201,823 US 12,263,333 US 12,383,727 US 12,390,633 US 12,397,146 US 12,409,312 US 12,447,327 US 12,465,744 US 12,478,775 US 12,478,776 US 12,491,355 US 12,508,416 US 12,515,036 US 12,515,038 US 12,523,228 US 12,576,262 US 12,589,237 US 12,589,238 US 12,667,714 US 12,685,856 US 12,691,275 US 12,714,848