Manufacture of an impeller

US12128227B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-12128227-B2
Application numberUS-202117528807-A
CountryUS
Kind codeB2
Filing dateNov 17, 2021
Priority dateApr 7, 2020
Publication dateOct 29, 2024
Grant dateOct 29, 2024

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

Apparatus and methods are described including manufacturing an impeller by forming a structure having first and second bushings at proximal and distal ends of the structure, the first and second bushings being connected to one another by at least one elongate element. The elongate element is caused to radially expand and form at least one helical elongate element, at least partially by axially compressing the structure. The helical elongate element is coated with a coupling agent configured to enhance bonding between the helical elongate element and an elastomeric layer. The coated helical elongate element is coated with the elastomeric layer. Subsequently, an elastomeric film is coupled to the helical elongate element, such that the helical elongate element with the elastomeric film coupled thereto defines a blade of the impeller. Other applications are also described.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method, comprising: manufacturing an impeller by: forming a structure having first and second bushings at proximal and distal ends of the structure, the first and second bushings being connected to one another by at least one elongate element; causing the at least one elongate element to radially expand and form at least one helical elongate element, at least partially by axially compressing the structure; coating the at least one helical elongate element with a coupling agent, the coupling agent configured to enhance bonding between the helical elongate element and an elastomeric layer; subsequently, coating the coupling-agent-coated helical elongate element with the elastomeric layer; and subsequently, coupling an elastomeric film to the at least one helical elongate element, such that the at least one helical elongate element with the elastomeric film coupled thereto defines a blade of the impeller. 2. The method according to claim 1 , wherein coupling the elastomeric film to the at least one helical elongate element, such that the at least one helical elongate element with the elastomeric film coupled thereto defines a blade of the impeller comprises dipping the helical elongate element into an elastomeric material from which the elastomeric film is made. 3. The method according to claim 1 , wherein the elastomeric film comprises an elastic material having an ultimate elongation of more than 300 percent. 4. The method according to claim 1 , wherein the elastomeric film comprises an elastic material having a melt flow index of at least 4. 5. The method according to claim 1 , wherein the elastomeric film comprises an elastic material having an ultimate tensile strength of more than 6000 psi. 6. The method according to claim 1 , wherein coating the at least one helical elongate element with the coupling agent comprises coating the at least one helical elongate element with a silane compound containing a first functional group which is configured to bond with the helical elongate element, and a second functional group which is configured to bond with the elastomeric layer. 7. The method according to claim 1 , wherein the elastomeric layer is made of a given elastomeric material and wherein the elastomeric film is made of the given elastomeric material. 8. The method according to claim 1 , wherein the elastomeric layer is made of a first elastomeric material and wherein the elastomeric film is made of a second elastomeric material that is different from the first elastomeric material. 9. The method according to claim 1 , wherein coating the coupling-agent-coated helical elongate element with the elastomeric layer comprises spraying an elastomer onto the coupling-agent-coated helical elongate element. 10. The method according to claim 1 , wherein coating the coupling-agent-coated helical elongate element with the elastomeric layer comprises at least partially rounding the coupling-agent-coated helical elongate element. 11. The method according to claim 1 , wherein coating the coupling-agent-coated helical elongate element with the elastomeric layer comprises coating the coupling-agent-coated helical elongate element with the elastomeric layer within a given time period of coating the at least one helical elongate element with the coupling agent. 12. The method according to claim 11 , wherein coating the coupling-agent-coated helical elongate element with the elastomeric layer further comprises spraying additional elastomeric material onto the coupling-agent-coated helical elongate element subsequent to coating the coupling-agent-coated helical elongate element with the elastomeric layer within the given time period of coating the at least one helical elongate element with the coupling agent. 13. The method according to claim 1 , wherein coating the at least one helical elongate element with the coupling agent comprises coating the at least one helical elongate element with a coupling agent containing a first functional group which is configured to bond with the helical elongate element, and a second functional group which is configured to bond with the elastomeric layer.

Assignees

Inventors

Classifications

  • Measuring · CPC title

  • Magnetic field sensors · CPC title

  • by means inserted into the body · CPC title

  • Details of apparatus construction, e.g. pump units or housings therefor, cuff pressurising systems, arrangements of fluid conduits or circuits (A61B5/02233, A61B5/0235 take precedence) · CPC title

  • drawing blood from a ventricle and returning the blood to the arterial system via a cannula external to the ventricle, e.g. left or right ventricular assist devices · CPC title

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US12128227B2 cover?
Apparatus and methods are described including manufacturing an impeller by forming a structure having first and second bushings at proximal and distal ends of the structure, the first and second bushings being connected to one another by at least one elongate element. The elongate element is caused to radially expand and form at least one helical elongate element, at least partially by axially …
Who is the assignee on this patent?
Magenta Medical Ltd
What technology area does this patent fall under?
Primary CPC classification A61M60/13. Mapped technology areas include Human Necessities.
When was this patent published?
Publication date Tue Oct 29 2024 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 12 related publications on this page (citations in our corpus or others sharing the same primary CPC).