Co-injection hot runner nozzle

US12194666B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-12194666-B2
Application numberUS-202217838915-A
CountryUS
Kind codeB2
Filing dateJun 13, 2022
Priority dateFeb 21, 2017
Publication dateJan 14, 2025
Grant dateJan 14, 2025

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A co-injection hot runner nozzle comprises an inner melt flow channel and an annular outer melt flow channel that surrounds the inner melt flow channel. The inner and outer melt flow channels have a first common source. The nozzle further comprises an annular intermediate melt flow channel disposed between the inner and outer melt flow channels. The annular intermediate melt flow channel is at least partly defined by a plurality of spiral grooves, each spiral groove having a respective inlet and defining a helical flow path. Lands between adjacent spiral grooves increase in clearance in a downstream direction. An annular axial flow path is defined over the lands. A plurality of feeder channels having a second common source is configured to supply melt to the plurality of inlets of the spiral grooves. The relationship of feeder channels to spiral grooves may be one-to-one. The inlets may be longitudinal channels.

First claim

Opening claim text (preview).

What is claimed is: 1. A co-injection molding method comprising: splitting a first melt flow between an inner channel and an outer channel of a co-injection hot runner nozzle, the outer channel forming an annular outer melt flow that surrounds an inner melt flow formed by the inner channel; and splitting a second melt flow among a plurality of feeder channels upstream of an annular intermediate channel of the co-injection hot runner nozzle, the intermediate channel being disposed between the inner and outer channels and being at least partly defined by a plurality of spiral grooves, each spiral groove having a respective inlet, the plurality of feeder channels supplying melt to the inlets of the plurality of spiral grooves, the intermediate channel being further defined by lands between adjacent spiral grooves that increase in clearance in a downstream direction, wherein melt comprising the second melt flow travels along helical paths defined by the respective spiral grooves and spills over the lands to form an annular axial flow, wherein the forming of the annular outer melt flow comprises passing melt through a plurality of flow transition channels arranged in a ring, each of the flow transition channels having an inlet, an outlet with a part-annulus shape, and a pair of opposing side walls that diverges in the downstream direction. 2. The co-injection molding method of claim 1 wherein the number of feeder channels matches the number of spiral grooves and wherein each feeder channel supplies melt to the inlet of a respective one of the spiral grooves. 3. The co-injection molding method of claim 2 wherein each inlet is a longitudinal channel and further comprising gradually redirecting longitudinally flowing melt from each inlet by about 70 degrees into its respective spiral groove.

Assignees

Inventors

Classifications

  • having two or more components being injected · CPC title

  • Controlling the flow of material of two or more nozzles or gates to a single mould cavity · CPC title

  • Nozzle tips (B29C45/2735 takes precedence) · CPC title

  • The moulding materials being injected simultaneously · CPC title

  • Injection moulding · CPC title

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What does patent US12194666B2 cover?
A co-injection hot runner nozzle comprises an inner melt flow channel and an annular outer melt flow channel that surrounds the inner melt flow channel. The inner and outer melt flow channels have a first common source. The nozzle further comprises an annular intermediate melt flow channel disposed between the inner and outer melt flow channels. The annular intermediate melt flow channel is at …
Who is the assignee on this patent?
Husky Injection Molding Systems Ltd
What technology area does this patent fall under?
Primary CPC classification B29C45/30. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Jan 14 2025 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 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).