Heating sleeve for injection molding nozzle

Patent metadata

Field	Value
Publication number	US-2016339618-A1
Application number	US-201615228066-A
Country	US
Kind code	A1
Filing date	Aug 4, 2016
Priority date	Mar 4, 2014
Publication date	Nov 24, 2016
Grant date	—

Abstract

An injection molding system comprising:
a manifold, a nozzle comprising a nozzle body having an outer circumferential surface that reduces in cross-sectional diameter or radial length beginning from a selected upstream point to a selected downstream point, a sleeve having a hollow bore having an inner surface complementary to the outer circumferential surface of the nozzle body such that the downstream end of the nozzle body is insertable into the upstream end of the hollow bore and further insertable downstream through the hollow bore to a point of maximum downstream travel at which the outside circumferential surface of the nozzle body engages the inside surface of the hollow bore, the engaged surfaces preventing further downstream travel of the sleeve body through the hollow bore.

First claim

What is claimed is:

1 . An injection molding system comprising:
a manifold having a flow channel receiving a stream of injection fluid, a comprising a nozzle body having an upstream end, a downstream end and a flow passage having an axial length sealably communicating at the upstream end with the flow channel of the manifold for delivering the injection fluid downstream to the cavity of a mold, the nozzle body having an outer circumferential surface that reduces in cross-sectional diameter or radial length beginning from a selected upstream point to a selected downstream point along at least a portion of the axial length of the flow passage, a sleeve heatable to an elevated temperature, the sleeve being comprised of a sleeve body having a hollow bore having an upstream end, a downstream end and an axial length, the hollow bore having an inner surface complementary to the outer circumferential surface of the nozzle body such that the downstream end of the nozzle body is insertable into the upstream end of the hollow bore and further insertable downstream through the hollow bore to a point of maximum downstream travel at which the outside circumferential surface of the nozzle body engages the inside surface of the hollow bore, the engaged surfaces preventing or opposing further downstream travel of the nozzle body through the hollow bore, a spring adapted to constantly urge the sleeve body in an upstream direction with an upstream directed force relative to the nozzle body to maintain the inner surface of the sleeve body in mating contact with the outer circumferential surface of the nozzle body.

2 . The system of claim 1 wherein the inner surface of the sleeve body that is complementary to the outer surface reduces in diameter beginning from a selected upstream point downstream to a selected downstream point along the axial length of the hollow bore.

3 . The system of claim 1 wherein the spring is adapted to bear against the nozzle in a downstream direction to exert a downstream directed force against the nozzle body.

4 . The system of claim 3 wherein the spring is compressed to exert the upstream directed force.

5 . The system of claim 2 wherein the spring is mounted between opposing surfaces of or fixedly interconnected to the nozzle body and the sleeve such that the spring can be compressed to exert an upstream directed force against the sleeve body and an opposing downstream directed force against the nozzle body.

6 . The system of claim 1 wherein the outer circumferential surface of the nozzle body that reduces in diameter or radial length is generally conical in configuration.

7 . The system of claim 1 wherein the inside surface of the sleeve body that reduces in diameter or radial length is generally conical in configuration.

8 . The system of claim 1 further comprising a heating element disposed helically around the flow passage of the nozzle body in contact with at least one of the sleeve body or the nozzle body along a selected axial distance.

9 . The system of claim 8 wherein the heating element is disposed a radial distance apart from a central axis of the flow passage that reduces in radial distance going from upstream toward downstream along the axial distance.

10 . The system of claim 8 wherein the heating element is disposed a uniform radial distance apart from a central axis of the flow passage along the axial distance.

11 . The system of claim 8 wherein the heating element is embedded within either the sleeve body or the nozzle body.

12 . The system of claim 8 further comprising a thermocouple element disposed helically around the flow passage of the nozzle body.

13 . The system of claim 12 wherein the heating element and the thermocouple element are disposed within a tube that is disposed helically around the flow passage of the nozzle body in contact with at least one of the sleeve body or the nozzle body along the selected axial distance, the terminus of the heating element and the terminus of the thermocouple element being disposed at least about 0.125 inches axially apart from each other.

14 . The system of claim 13 wherein the tube is embedded within either the sleeve body or the nozzle body.

15 . A method of heating a nozzle of a system according to claim 1 comprising mating the outer circumferential surface of the nozzle body with the inside surface of the sleeve body and heating the sleeve body to an elevated temperature.

16 . A method of heating a nozzle in an injection molding apparatus comprised of:
a manifold having a flow channel receiving a stream of injection fluid, a nozzle comprising a nozzle body having an upstream end, a downstream end and a flow passage having an axial length sealably communicating at the upstream end with the flow channel of the manifold for delivering the injection fluid downstream to the cavity of a mold, the nozzle body having an outer circumferential surface that reduces in cross-sectional diameter or radial length beginning from a selected upstream point to a selected downstream point along at least a portion of the axial length of the flow passage, a sleeve heatable to an elevated temperature, the sleeve comprising a sleeve body having a hollow bore having an upstream end, a downstream end and an axial length, the hollow bore having an inner surface complementary to the outer circumferential surface of the nozzle body such that the downstream end of the nozzle body is insertable into the upstream end of the hollow bore and further insertable downstream through the hollow bore to a point of maximum downstream travel at which the outside circumferential surface of the nozzle body engages the inside surface of the hollow bore, the engaged surfaces preventing further downstream travel of the sleeve body through the hollow bore, wherein the method comprises: inserting the downstream end of the nozzle body axially into the upstream end of the hollow bore of the sleeve, moving the sleeve axially upstream to surround the outer circumferential surface of the nozzle body along a predetermined axial length of the nozzle body extending up to an upstream position where the inner surface of the hollow bore mates or engages with the outer circumferential surface of the nozzle body such that the sleeve is prevented from further upstream movement.

17 . The method of claim 16 further comprising heating the sleeve body to an elevated temperature.

18 . The method of claim 16 further comprising constantly urging the sleeve body in an upstream direction with an upstream force to maintain the inner surface of the sleeve in mating contact with the outer circumferential surface of the nozzle.

19 . The method of claim 16 further comprising helically winding a heating element around the outside surface of the nozzle and extending the helically wound heating element along a selected axial length of the nozzle.

20 . The method of claim 16 further comprising helically winding a thermocouple element around the outside surface of the nozzle and extending the helically wound thermocouple element along a selected axial length of the nozzle.

21 . The method of claim 16 further comprising forming the outer circumferential surface that reduces in cross-sectional diameter or radial length to be generally conical.

22 . The method of claim 16 further comprising forming the inner surface that reduces in cross-sectional diameter or radial length to be generally conical.

23 . Th

Assignees

• Synventive Molding Solutions Inc

Inventors

• Galati Vito

Classifications

• B29C45/1782 Primary

  Mounting or clamping means for heating elements or thermocouples · CPC title

• B29C45/7613

  the termination of flow of material into the mould · CPC title

• B29K2105/0067

  Melt · CPC title

• B29C45/03

  Injection moulding apparatus (transfer moulding B29C45/02) · CPC title

• B29C45/74

  of the injection unit · CPC title