Rotor for a fluid pump and method and mold for the production thereof

Patent metadata

Field	Value
Publication number	US-2018149165-A1
Application number	US-201615570128-A
Country	US
Kind code	A1
Filing date	Apr 29, 2016
Priority date	Apr 30, 2015
Publication date	May 31, 2018
Grant date	—

Abstract

The invention relates to a rotor for a compressible fluid pump, in particular a blood pump that can be introduced through a blood vessel into a patient's body, wherein said rotor comprises one or more conveying elements ( 15 ), is compressible and expandable between a first compressed state and a second radially expanded state, is made at least partially from a plastic reinforced with reinforcing elements, in particular fibers ( 10, 11, 13, 18, 19, 55, 56, 62, 63 ) and is provided for rotation about an axis of rotation ( 14 ). According to the invention, the rotor is tensioned in the first, compressed state and free from external stresses in the second, expanded state. A third state exists, which the rotor ( 42 ) occupies in the operating state under load. The reinforcing elements, in particular fibers, extend in the rotor in the third state at least in sections in a stretched manner.

First claim

1 . A rotor for a compressible fluid pump, which can be introduced through a blood vessel into a patient's body, the rotor comprising:
one or more impeller elements; wherein the rotor is configured to be radially compressed and expanded between a compressed state and an expanded state, the rotor further comprising, at least in part, a plastic material reinforced by strand-like reinforcement elements, wherein the rotor is intended to rotate about an axis of rotation, and wherein the rotor is tensioned in the compressed state and is free from external stresses in the expanded state, and wherein an operating state exists, which the rotor assumes while operating under load, wherein the reinforcement elements in the rotor in the operating state run in a stretched manner, at least sectionally.

2 . The rotor of claim 1 , wherein the reinforcement elements in the operating state of the rotor run in a stretched manner at least in part in regions of the rotor in which this experiences an elongation stress and run substantially in the direction of the elongation stress.

3 . The rotor of claim 1 , wherein more than half of the reinforcement elements are arranged in regions of the rotor experiencing elongation stresses in the operating state.

4 . The rotor of claim 1 , wherein there are substantially no differences between the expanded state and the operating state in respect of outer form.

5 . The rotor of claim 1 , wherein reinforcement elements are provided, which extend beyond the axis of rotation in a radial direction.

6 . The rotor of claim 1 , wherein, in the operating state, at least some of the reinforcement elements, run sectionally straight.

7 . The rotor of claim 1 , wherein, in the operating state, at least some of the reinforcement elements, run along a longitudinal direction of the one or more impeller elements with a smaller curvature than neutral fibers of the one or more impeller elements.

8 . The rotor of claim 1 , wherein the plastic material of the rotor has a Shore hardness <100 D.

9 . The rotor of claim 1 , wherein a first proportion of more than 30% of the reinforcement elements in the expanded state of the rotor runs substantially stretched from a portion disposed closest to the axis of rotation to a second portion disposed further from the axis of rotation.

10 . The rotor of claim 1 , wherein a first proportion of the reinforcement elements, the first proportion being more than 30% of the reinforcement elements, has a length corresponding to at least 30% of a maximum height of the one or more impeller elements, measured in a radial direction of the rotor in the expanded state.

11 . The rotor of claim 9 , wherein the first proportion of the reinforcement element runs substantially perpendicularly to the axis of rotation.

12 . The rotor of claim 1 , wherein a diameter of the reinforcement elements is less than 40 micrometers.

13 . The rotor of claim 1 , wherein a surface of the reinforcement elements having an adhesion promoter.

14 . The rotor of claim 1 , wherein a proportion of reinforcement elements in the expanded state of the rotor runs transversely to the reinforcement elements of a first proportion.

15 . The rotor of claim 1 , wherein the reinforcement elements are at least in part fabric portions with fibers running longitudinally and transversely.

16 . The rotor of claim 1 , wherein the reinforcement elements are film strips, wherein a length of the film strips is at least three times times greater than a width of the film strips.

17 . The rotor of claim 1 , wherein the reinforcement elements are surrounded by the plastic material from which the rotor is predominantly made, at least to a proportion of 90%.

18 . The rotor of claim 1 wherein the plastic material in which the reinforcement elements are embedded has different properties, at least in regions, on a side of the one or more impeller elements not loaded by a fluid counter pressure during operation compared to a side of the one or more impeller elements that is loaded by the fluid counter pressure.

19 . A rotor for a compressible fluid pump configured to be expanded and compressed radially between a first, compressed state and a second, expanded state, that the rotor comprising at least one element which is produced by injection molding with simultaneous addition of reinforcement elements in the expanded state, wherein the reinforcement elements are surrounded on all sides by an injection molding material and are present in a stretched form at least in part in the second, expanded state.

20 . The rotor of claim 1 , wherein the reinforcement elements in the expanded state of the rotor, without a fluid counter-pressure, are present in a form stretched to such an extent that when transitioning to a third state, which constitutes the operating state with the fluid counter-pressure, the reinforcement elements are lengthened by less than 5% wherein lengthening is measured as a distance between two ends of a reinforcement element.

21 . The rotor of claim 1 , wherein in the expanded state of the rotor with a fluid counter-pressure at least a portion of the reinforcement elements run in a stretched and straight manner in at least one region of an impeller element of the one or more impeller elements, wherein said impeller element is curved.

22 . The rotor of claim 21 , wherein in a cured region of an impeller element of the one or more impeller elements, at least two portions of reinforcement elements run in a stretched and straight manner, wherein directions in which the reinforcement elements of the portions run are parallel within the same portion, but are different between the two different portions.

23 . The rotor of claim 1 , wherein a length of at least 30% of the reinforcement elements is greater than an average thickness of the one or more impeller elements.

24 . The rotor of claim 1 , wherein the reinforcement elements are introduced into the plastic material in which said reinforcement elements are embedded in an injection molding method and, wherein the reinforcement elements have a partially curved course along a flow of the plastic material into the injection mold during a time for which the rotor is disposed in an injection mold.

25 . A method for producing the rotor of claim 1 by means of a molding method in which the material of the one or more impeller elements is introduced into volumes of the one or more impeller elements in a radial direction with respect to the axis of rotation, in such a way that a molding material flows into the volume of each individual impeller element of the one or more impeller elements in the radial direction.

26 . A method for producing the rotor of claim 1 , wherein the rotor is produced by molding wherein the molding is carried out in two successive phases with different injection directions.

27 . The method of claim 25 , wherein the rotor, after the molding, is subjected to a treatment which causes a different shrinkage of the molding material on an side of the one or more impeller elements loaded by a fluid counter-pressure during operation than on an opposite side.

28 . The method of claim 25 , wherein a shrinkable layer is applied to at least one of the one or more impeller elements on the side opposite the side of the one or more impeller elements exposed to a fluid counter-pressure during operation.

Assignees

• Ecp Entw Mbh

Inventors

• Siess Thorsten
• Scheckel Mario

Classifications

• F04D3/02

  of screw type · CPC title

• F04D29/181

  Axial flow rotors (F04D29/185 take precedence) · CPC title

• B29C45/2708

  Gates (B29C45/2703 takes precedence) · CPC title

• F04D29/026 Primary

  especially adapted for liquid pumps · CPC title

• B29C45/7207

  of the moulded articles · CPC title