CN111300763A

CN111300763A - Mold, mold assembly and stack member

Info

Publication number: CN111300763A
Application number: CN201911232803.9A
Authority: CN
Inventors: 德里克·罗伯逊·麦克里迪; 马丁·丹尼尔·比津斯基
Original assignee: Husky Injection Molding Systems Ltd
Current assignee: Husky Injection Molding Systems Ltd
Priority date: 2018-12-11
Filing date: 2019-12-05
Publication date: 2020-06-19
Anticipated expiration: 2039-12-05
Also published as: CN111300763B; CN212920269U; WO2020118414A1

Abstract

A preform core coolant diverter (260) includes a body defining supply and return channels (261, 262, 263) and a snap-fit connector (267) engaging a seat (215) defined in a punch (210). The snap-fit connector (267) retains the flow splitter (260) in the boss (215) such that the supply channel (261, 262) of the body redirects cooling fluid from the lateral cooling circuit outlet (214a) of the boss (215) into the core (250) and the return channel (263) redirects cooling fluid from the core (250) into the lateral cooling circuit inlet (214b) of the boss (215). Also disclosed is a core cooling tube (270) that may be integrally formed with the coolant diverter (260).

Description

Mold, mold assembly and stack member

Technical Field

The present invention generally relates to molding apparatuses and related methods. More particularly, although not exclusively, the present invention relates to a mold stack, a mold assembly, a mold, a molding system for molding preforms and other articles (e.g., tubular articles), and to related methods.

Background

Molding is the process of forming a molded article from a molding material, such as a plastic material, by using a molding system, such as an injection molding system or a compression molding system. Various molded articles can be formed by using such molding processes, including preforms that can be formed, for example, from polyethylene terephthalate (PET) materials. Such preforms can then be blown into containers, such as beverage containers, bottles, cans, and the like.

By way of illustration, injection molding of preforms involves heating the PET material (or other suitable molding material for this purpose) to a homogeneous molten state, and injecting the thus-molten material under pressure into a molding cavity defined at least in part by a female cavity piece and a male core piece. Typically, the female core member is mounted on the female mold and the male core member is mounted on the male mold of the mold. The cavity and the core are urged together and are held together by a clamping force sufficient to hold the cavity and the core together against the pressure of the injection material. The molding cavity has a shape that generally corresponds to the final cold state shape of the molded article to be molded. The so-injected material is then cooled to a temperature sufficient to enable the so-formed molded article to be removed from the molding cavity. When cooled, the molded piece shrinks within the moulding cavity and therefore tends to remain associated with the core when the cavity and the punch are forced apart.

Thus, by urging the male mould away from the female mould, the moulded article can subsequently be demoulded by stripping it from the core. Stripping structures are known to assist in removing the molded article from the core half. Examples of ejector structures include ejector plates, ejector plate rings and neck rings, ejector pins, and the like.

One problem that needs to be addressed when process molding preforms that can be subsequently blown into beverage containers is the formation of a so-called "neck region". Typically and as an example, the neck region includes (i) an engagement feature, such as a thread (or other suitable structure), for receiving and retaining a closure assembly (e.g., a bottle cap), and (ii) a tamper-evident assembly for, for example, cooperating with the closure assembly to indicate whether the end product (i.e., a beverage container that has been filled with a beverage and shipped to a store) has been tampered with in any way. The neck region may contain other additional elements for various purposes, such as cooperating with portions of the molding system (e.g., support rails, etc.). As understood in the art, the neck region cannot be easily formed by using a cavity and a core half. Traditionally, split mold inserts (sometimes referred to by those skilled in the art as "neck rings") have been used to form the neck region.

A typical molding insert stack component that may be arranged (in use) in a molding machine includes a pair of split mold inserts that together with a cavity insert, a gate insert, and a core insert define a molding cavity. The molding material may be injected from a molding material source into the molding cavity via a receptacle or port in the gate insert to form a molded part. To facilitate forming a neck region of a molded article and subsequently removing the molded article therefrom, the split mold insert pair includes a pair of complementary split mold inserts mounted on adjacent slides of the slide pair. The slide pair is slidably mounted on the top surface of the stripper plate.

As is well known, the stripper plate is configured to be movable relative to the cavity insert and the core insert when the mold is disposed in the open configuration. Thus, the slide pair and the complementary split mold insert mounted thereon can be driven laterally via a cam arrangement or any other suitable known means for releasing a molded article from a molding cavity. One of the functions performed by the split mold insert pair is to assist in stripping the molded article from the core insert by "sliding" the molded article from the core insert.

Disclosure of Invention

The present invention seeks to provide an alternative cooling insert which is simpler and/or more cost effective to manufacture and assemble within a mould for moulding articles, particularly but not exclusively tubular articles (e.g. preforms). The invention relates particularly, but not exclusively, to a mold stack, a mold assembly, a molding system and an associated method. In the case of a tubular article, such as a preform, the article may have a base at the closed end, a neck finish at the open end, and a body portion therebetween. The neck-finish may comprise one or more radial flanges that may extend outwardly. The neck finish may include an engagement feature, such as a threaded or snap-fit finish. The preform and/or neck-finish may include any one or more of the other features defined above with respect to known preform designs. Additionally, any of the foregoing features defined with respect to known mold stacks, molds, and molding systems can be incorporated within a mold stack, a mold, and a molding system according to the present invention so long as they are consistent with the disclosure herein.

According to a first broad aspect of the present invention, there is provided a coolant diverter for a die (e.g. a preform die), the diverter being receivable, in use, in a seat defined in a punch, the diverter comprising a body bounding at least part of a first cooling channel and a second cooling channel, the first cooling channel comprising an inlet portion for receiving cooling fluid from a cooling circuit of the punch and an outlet portion extending, for example, at an angle, and a locator for engaging a locator of the punch seat. The second cooling channel includes an inlet for receiving cooling fluid from the core insert and an outlet for delivering the cooling fluid to the cooling circuit of the punch, wherein the positioner is configured to align, in use, an inlet portion of the first cooling channel with the cooling circuit of the punch and/or to inhibit removal of the diverter when the diverter is received in the punch shoe, in use.

The locator may comprise a snap-fit connector.

Another aspect of the invention provides a core coolant diverter for a mold (e.g., a preform mold), the diverter including a body defining supply and return channels and a snap-fit connector configured to engage a seat defined in a punch in use such that the supply channel of the body redirects cooling fluid from a lateral cooling circuit outlet of a base into a core insert and the return channel redirects cooling fluid from the core insert into a lateral cooling circuit inlet of the base.

The locator or snap-fit connector may comprise a protrusion, which may be located on or form part of the body. A locator or snap-fit connector may be received within the cooling circuit of the male die. The projection may comprise an annular projection receivable within the cooling circuit of the punch. The annular protrusion may comprise a lip, which may surround an opening of the inlet portion of the first cooling channel, for example for being received within a cooling circuit of the male die.

Alternatively, the retainer or snap-fit connector may contain a recess, such as a protrusion for receiving the die holder. In use, at least a portion of the second cooling channel can be defined between the exterior surface of the coolant diverter and the die base. The body may be substantially cylindrical in shape. The inlet portion of the first cooling passage may include a radial hole. The outlet portion of the first cooling passage may include an axial bore. At least a portion of the second cooling passage may be defined by a groove in the body. The first cooling passage may include a curved transition portion that may connect the radial bore to the axial bore.

The coolant diverter may include one or more spacers, for example, for engaging the die bed and/or centering the outlet portion of the first cooling passage therein. The outlet portion of the first cooling channel may be at least partially delimited by a tubular or partially tubular portion. At least one of the spacers may comprise a partial circumferential wall, which may surround and/or be spaced apart from at least a part of the tubular or partial tubular outlet portion of the first cooling channel.

Another aspect of the present invention provides a core cooling tube, such as for a preform mold. The core cooling tube may include a coolant diverter, for example as described above. The coolant diverter may, but need not, be integrally formed with the core cooling tube. The core cooling tube may be formed by an additive manufacturing process.

The core cooling tube may comprise an inlet portion, for example for receiving cooling fluid from a cooling circuit of the male mold.

The core cooling tube may include an open end, for example, for directing cooling fluid to an inner surface of the core insert. The core-cooling tube may include an outlet portion, which may include an open end. The open end may comprise an aperture. The aperture may define a flow area that may be less than a flow area through the outlet portion.

Another aspect of the invention provides a core cooling tube for a preform mold, the core cooling tube including an inlet portion for receiving cooling fluid from a cooling circuit of a male mold and an outlet portion having an open end for directing cooling fluid to an inner surface of a core insert, wherein the open end includes an orifice that depicts a flow area that is less than a flow area through the outlet portion.

The outlet portion may for example taper towards the open end. The outlet portion may be truncated, for example to define an aperture. The outlet portion may comprise a truncated cone or a dome, or the end portion may be defined by a truncated cone or a dome, which may define the aperture. The end portion may be used to direct cooling fluid to the conical or domed inner surface of the core insert. The end portion may comprise a conical or domed inner surface and/or a conical or domed outer surface.

The truncated outlet portion may be substantially spherical or elliptical. The aperture may be substantially circular or elliptical. The open end may be shaped and/or configured to be proximate an inner surface of the core insert, such as a conical or dome-shaped inner surface.

Another aspect of the invention provides a core assembly comprising a core insert and a core cooling tube, for example as described above. The core insert may include a molding portion defining a molding surface for molding a portion of the preform. The moulded part may be at least partially tubular with a closed end. The core-cooling tube may include an outlet portion, which may include an open end. The outlet portion or open end may be shaped and/or configured, for example, as a conical or dome-shaped inner surface proximate to the inner surface of the closed end of the core insert.

Additionally or alternatively, the core cooling tube may contain one or more (e.g., a plurality of) spacer elements that may protrude from an outer surface of the core cooling tube. The spacer element may be adapted or configured to center the core cooling tube within the core insert in use. One or more spacer elements may be located at or adjacent to the open end of the core cooling tube. One or more spacer elements may be located at one or more intermediate positions, for example between the open end and the coolant diverter. The or each spacer element may comprise a spacer blade.

At least two of the spacer elements or vanes may be axially spaced relative to one another, for example along the core cooling tube. The spacing elements or vanes may comprise a plurality of projections equally spaced around the circumference of the core cooling tube. The plurality of spacer elements or vanes may comprise one or more first spacer elements or vanes and one or more second spacer elements or vanes. The first spacer element or vane may be in a first axial position and/or the second spacer element or vane may be in a second axial position different from the first axial position. The plurality of equally spaced spacer elements or vanes may comprise alternating first and second spacer elements or vanes.

The core cooling tube may include an enlarged portion that may be shaped and/or configured to mate with a transition in an inner surface of the core insert. One or more, e.g. a plurality of spacer elements or vanes may protrude over and/or from the enlarged portion. The enlarged portion may be located at an intermediate position of the core cooling tube and/or between the open end of the core cooling tube and the coolant diverter.

Another aspect of the invention provides a method of making the above-described coolant splitter and/or core cooling tube. The method may include additional manufacturing processes.

Another aspect of the present invention provides a method of manufacturing a core cooling tube for a preform mold, the method comprising: forming a coolant diverter comprising a body defining at least a portion of first and second cooling channels for receipt within a seat in a punch, the first cooling channel comprising an inlet portion for receiving cooling fluid from a cooling circuit of the punch and an outlet portion extending at an angle relative to the inlet portion, the second cooling channel comprising an inlet for receiving cooling fluid from a core insert and an outlet for delivering the cooling fluid to the cooling circuit of the punch; and forming a core cooling tube comprising a first end connected to the outlet portion of the coolant diverter and a second open end for directing cooling fluid to the dome-shaped inner surface of the core insert; wherein the coolant splitter and the core cooling tube are integrally formed to provide a seamless, unitary monolithic structure.

The method may include forming a core cooling tube having one or more of the features of the coolant splitter or core cooling tube described above.

Another aspect of the invention provides a mold stack comprising a coolant diverter or core cooling tube as described above and at least one of a core insert, a cavity insert and a pair of split mold inserts.

Another aspect of the invention provides a mold assembly, such as a punch assembly, comprising one or more coolant diverters or core cooling tubes as described above.

Another aspect of the invention provides a mold comprising one or more coolant diverters or core cooling tubes as described above. The mold may comprise a preform mold or an injection mold, such as a preform injection mold.

Another aspect of the present invention provides a molding system including the mold as above. The molding system may include one or more of a melt dispenser, an injection molding machine, a material supply system, and a part removal and/or post-mold cooling apparatus.

Another aspect of the invention provides a computer program element comprising and/or defining a three-dimensional design for use with a simulation apparatus or a three-dimensional additive or subtractive manufacturing apparatus or device (e.g. a three-dimensional printer or CNC machine), the three-dimensional design comprising one or more embodiments of the above-described mold parts.

Another aspect of the invention provides a method of assembling a mold assembly or mold as above. Various steps and features of the method will be apparent to those skilled in the art.

Another aspect of the invention provides a method of molding an article. The method may include using one of the aforementioned mold stacks, molds, mold assemblies, or molding systems. The method may comprise any one or more features or steps associated with or relating to the use of any feature of any of the aforementioned mold stacks, molds, mold assemblies, or molding systems.

For the avoidance of doubt, any feature herein is equally applicable to any aspect of the invention. Within the scope of the present application, the various aspects, embodiments, examples and alternatives set forth in the preceding paragraphs, in the claims and/or in the following definitions and drawings, in particular in the individual features thereof, may be understood individually or in any combination. That is, all embodiments and/or features of any embodiment may be combined in any manner and/or combination unless such features are incompatible. For the avoidance of doubt, the terms "may", "and/or", "for example (e.g.)", "for example (for example)" and any similar terms as used herein should be construed as non-limiting, such that there need not be any features so defined. Indeed, any combination of optional features, whether explicitly claimed or not, is explicitly contemplated without departing from the scope of the present invention. The applicant reserves the right to change accordingly any originally filed claim or submit any new claim, including the right to amend any originally filed claim to depend from and/or incorporate any feature of any other claim, although not originally claimed in such a manner.

Drawings

Embodiments of the invention will now be defined, by way of example only, with reference to the accompanying drawings, in which:

FIG. 1 depicts a preform mold assembly according to an embodiment of the invention;

FIG. 2 depicts the preform mold assembly of FIG. 1 with the melt distributor omitted;

FIG. 3 depicts the male mold assembly of the preform mold assembly of FIGS. 1 and 2 with one core omitted and the other core assembly shown exploded;

FIG. 4 depicts an enlarged view of the area of FIG. 3 including an exploded core assembly;

figure 5 depicts a side view of a portion of the male die assembly of figures 3 and 4 showing the mounting of one of the cores to the male die;

FIG. 6 depicts a cross-sectional view through one of the core components and an adjacent portion of the male die to which the core component is secured;

FIG. 7 depicts a core cooling tube assembly of the core assembly of FIG. 6 shown from a first side;

FIG. 8 depicts the core cooling tube assembly of FIG. 7 shown from a second side;

FIG. 9 illustrates an alternative integral core cooling tube assembly shown from a first side;

FIG. 10 depicts the core cooling tube assembly of FIG. 9 shown from a second side;

FIG. 11 depicts a cross-sectional view along a central axial plane through the core cooling tube assembly of FIGS. 9 and 10;

FIG. 12 illustrates another alternative integral core cooling tube assembly shown from a first side;

FIG. 13 depicts the core cooling tube assembly of FIG. 12 shown from a second side;

FIG. 14 depicts a cross-sectional view along a central axial plane through the core cooling tube assembly of FIGS. 12 and 13;

FIG. 15 depicts a further alternative integral core cooling tube assembly shown from a first side;

FIG. 16 depicts the core cooling tube assembly of FIG. 15 shown from a second side;

FIG. 17 depicts a cross-sectional view along a central axial plane through the core cooling tube assembly of FIGS. 15 and 16;

FIG. 18 depicts an alternative two-piece core insert for use in the preform mold assembly of FIGS. 1 and 2;

FIG. 19 illustrates the two-piece core insert of FIG. 18 in an exploded view;

FIG. 20 depicts a cross-sectional view along a central axial plane of a stack component including the two-piece core insert of FIGS. 18 and 19;

FIG. 21 depicts moving parts of the preform mold assembly (including the punch assembly and stripper plate assembly) of FIGS. 1 and 2;

FIG. 22 shows a stripper plate of the stripper plate assembly of the moving part shown in FIG. 21;

FIG. 23 shows an exploded view of a pair of slides of the stripper plate assembly of FIG. 18;

FIG. 24 shows three neck ring halves and their associated retaining assemblies securing them to the slide;

FIG. 25 depicts an enlarged view of a portion of the stripper plate assembly of the moving half of FIG. 21 with the neck ring pair omitted to expose the slide;

fig. 26 depicts an enlarged view of fig. 25, wherein the connecting rods are omitted and insertion of the guide shaft is shown;

FIG. 27 depicts the female mold component of the preform mold assembly of FIGS. 1 and 2 with one of the cavity components removed therefrom;

FIG. 28 depicts one of the cavity assemblies of the female die assembly of FIG. 27;

FIG. 29 depicts a cavity insert of the cavity assembly of FIG. 28 with the gate insert omitted;

FIG. 30 shows a cooling channel in section A-A of the cavity insert of FIG. 29;

FIG. 31 depicts a gate insert of the cavity assembly of FIG. 28;

FIG. 32 shows one of the retaining pins of the cavity assembly of FIG. 28;

FIG. 33 depicts a partial cross-sectional view of the female die assembly through an array of cavity inserts of the female die assembly of FIG. 27;

FIG. 34 depicts a partial cross-sectional view of the female die assembly through a row of cavity inserts of the female die assembly of FIG. 27;

FIG. 35 depicts an enlarged view of the bypass and hold pin area of the partial cross-sectional view of FIG. 34;

FIG. 36 depicts a view similar to FIG. 35 showing an alternative bypass passage configuration;

FIG. 37 depicts a view similar to FIGS. 35 and 36, showing an alternative retention pin configuration in which a bypass channel is defined between the retention pin and the cavity insert;

FIG. 38 depicts a partial cross-sectional view of a gate area of an alternative cavity die assembly with a gate pad disposed between a nozzle tip and a gate insert;

FIG. 39 depicts an exploded view of the gate pad and gate insert of FIG. 38;

FIG. 40 depicts a partial cross-sectional view of the mold of FIG. 1 illustrating the mold stack, but omitting both the melt distributor and the core cooling tube assembly;

FIG. 41 depicts an enlarged view of region B of FIG. 39 illustrating the gap between the stripper plate and the punch;

FIG. 42 depicts the female die assembly of FIG. 27 lowered onto the moving parts illustrated in FIG. 21 during assembly; and

FIG. 43 depicts a portion of an alignment procedure for aligning the core and neck ring relative to the cavity of the female mold assembly.

Detailed Description

Referring to fig. 1 and 2, a non-limiting embodiment of a preform mold assembly 100 according to the present invention is depicted, which in this embodiment includes 48 cavities. The mold assembly 100 includes a first moving portion 110 for mounting to a moving platen (not shown) of an injection molding machine (not shown) and a second stationary portion 120 for mounting to a stationary platen (not shown) in a conventional manner. The first moving member 110 includes a punch assembly 200 and a stripper plate assembly 300. The second stationary portion 120 includes a female die assembly 400 and a melt distributor 500, commonly referred to as a hot runner. In this embodiment, the melt distributor 500 is of a conventional type. The present invention is particularly directed to the product specific assembly 130 shown in FIG. 2, generally referred to as the "cold half" 130. The cold half 130 includes a punch assembly 200, a stripper plate assembly 300, and a die assembly 400.

As shown more clearly in fig. 3 and 4, the punch assembly 200 includes a punch 210, a pair of cam plates 220, four guide pins 230 and a plurality of core assemblies 240. The male mold 210 is generally rectangular in plan, having a fan angle 211 for receiving tie bars (not shown) of an injection molding machine (not shown) in which the mold is mounted. The punch 210 also includes four guide pin holes 212 through its thickness, these guide pin holes 212 being horizontally inboard of each scalloped corner 211 and securely receiving a guide pin 230. The punch 210 also includes a plurality of ejection holes 213 through its thickness for receiving ejector pins (not shown).

A web of

cooling channels

214a, 214b is contained within the punch 210, which is fed into a plurality of cooling channel seats 215 in the front CRF of the punch 210 (as shown in fig. 6). The cooling gallery pockets 215 are arranged in an array of six vertical columns and eight horizontal rows. Each seat 215 is surrounded by three core mounting holes 216, said core mounting holes 216 extending through the thickness of the punch 210 and countersunk on the rear face CRR of the punch 210. An array of tie bolts 217 are also inserted into holes in the male 210, which are also countersunk on the rear face CRR. The cam plate 220 is bolted to the central lower region of the front CRF of the punch 210 and includes a pair of cam grooves 221 on its upper surface. Another cam plate 220 is bolted to the central upper region of the front CRF of the punch 210 and contains a similar pair of cam grooves 221 on its lower surface. The two cam disks 220 have the same configuration, varying only in their orientation. The cam slot 221 of each cam plate 220 extends perpendicularly from the front face CRF and converges towards the free end of the cam plate 220.

As shown more clearly in fig. 4-8, each core assembly 240 includes a hollow core insert 250 and a core

cooling tube assembly

260, 270. In this example, the core

cooling tube assemblies

260, 270 include a coolant flow splitter 260 received in one of the cooling channel seats 215 of the male mold 210 and a core cooling tube 270 releasably secured to the coolant flow splitter 260 and received within the hollow core insert 250.

Each core insert 250 includes a substantially cylindrical base 251 and a molded portion 252 joined to the base 251 by a taper 253. The molded portion 252 has: an outer molding surface 252a for molding the inner surface of the preform in the usual manner; a tapered transition region 252b for molding a transition region between the neck and body regions of the preform; and a top sealing surface portion TSS for molding a portion of the top sealing surface of the preform. The core cone 253 extends from the top sealing surface portion TSS to the front face 251a of the base 251 and includes a single male cone 253 for a stacked configuration known in the art as a so-called "cavity-locked" design. However, it should be understood that the core insert 250 may be of a so-called "core lock" design without departing from the scope of the present invention.

In this example, each core insert 250 includes a substantially planar mounting surface 254 and three blind threaded bores 255 extending from the mounting surface 254. The core insert 250 is thus mounted from the rear or rear, whereby the bolt 218 is inserted into the core mounting hole 216 from the rear CRR of the punch 210 and threadedly engages the threaded hole 255 of the core insert 250. This is shown in fig. 5. This rear mounting enables the core insert 250 to be secured from the rear of the punch 210. In this way, the pitch between core inserts 250 can be reduced without obstructing access to the bolts 218, as is the case with conventional core inserts having flanges with through holes for receiving the front mounted bolts 218.

As discussed in more detail below, this rear mounting in combination with the generally flat mounting surface 254 also enables the core insert 250 to be loosely mounted to the front CRF of the male mold 210 in a floating manner and securely fixed relative thereto after the mold 100 or cold half 130 is fully assembled. More specifically, by loosely tightening the bolts 218, the clearance between them and the core mounting holes 216 allows a degree of sliding movement between the mounting surface 254 of the core insert 250 and the front CRF. The mounting surface 254 defines an end of the core insert 250 and is devoid of any protrusions, thereby enabling the core insert 250 to slide relative to the punch 210. With the mold 100 or cold half 130 in the assembled state, the bolts 218 are still accessible from the back CRR of the punch 210 and thus can be torqued to securely fasten the core insert 250 to the punch 210.

However, it is also contemplated that the core insert 250 may be provided with a socket extending from the mounting surface 254. In some cases, the socket (not shown) may be smaller than the seat 215 in the punch 210 to allow some sliding movement therebetween. In other examples, the socket may be substantially the same size as the seat 215 in the punch 210.

Referring now to fig. 6, each core insert 250 includes a central bore 250a that extends from the mounting surface 254 to a semi-spherical or dome-shaped closed end adjacent the free end of the molded portion 252. The central bore 250a includes a cone intermediate region 250b corresponding to the tapered transition region 252b of the outer molded surface 252 a. In this manner, the wall thickness between central bore 250a and outer molding surface 252a remains substantially constant along the entire molded portion 252. The mounting surface 254 further includes a shallow recess 256 surrounding the central bore 250a and defining a shut-off surface 257 therebetween. The shut-off surface 257 also includes an O-ring groove 258 between the groove 256 and the central bore 250a, with an O-ring 259 received in the O-ring groove 258 for sealing the interface between the central bore 250a and the male die 210.

As shown in fig. 6-8, each coolant diverter 260 is substantially cylindrical and includes an axial blind bore 261, a radial bore 262 perpendicular to the axial bore 261, and a peripheral groove 263 parallel to the axial bore 261. An axial bore 261 extends from an upper surface 264 of the diverter 260 and terminates adjacent a lower surface 265 of the diverter 260. The axial bore 261 includes an enlarged portion 261a extending from the upper surface 264 and is threaded along a portion of its length to provide a connector for the core cooling tube 270. The radial bore 262 extends from the closed end of the axial bore 261 to a circumferential surface 266 of the diverter 260 opposite the peripheral groove 263. The axial bore 261 and the radial bore 262 together provide

first cooling passages

261, 262 of the coolant diverter 260.

The peripheral groove 263 extends from the upper surface 264 toward the lower surface 265 for approximately half of the circumference of the diverter 260, terminating on the opposite side of the axial bore 261, such that the circumferential surface 266 extends around the entire circumference of the lower end of the diverter 260. The peripheral groove 263 cooperates with the facing surface of the cooling channel seat 215 to define a second cooling channel of the coolant diverter 260, having an inlet defined at the front face CRF of the punch 210 and an outlet corresponding to the opening of the facing cooling channel 214b in the cooling channel seat 215.

Each coolant diverter 260 also includes a locator in the form of a retaining lip 267 that protrudes from the circumferential surface 266 around the perimeter of the opening of the radial bore 262. The coolant diverter 260 is formed from a resilient plastic material such that the retaining lip 267 is resiliently deformable. As such, insertion of the flow splitter 260 into the cooling passage seat 215 causes the retention lip 267 to elastically deform until the depth and orientation of the flow splitter 260 within the cooling passage seat 215 aligns the radial bore 262 with the facing cooling passage 214 a. When the radial bore 262 and the cooling channel 214a are aligned, the retaining lip 267 snaps into the cooling channel 214a and returns to its original shape. As a result, the retention lip 267 provides a snap-fit connector that serves both as a locating means to ensure proper alignment of the radial bore 262 and the cooling channel 214a, and as a retaining means for retaining the flow splitter 260 within the cooling channel seat 215. In this orientation, the peripheral groove 263 is aligned with the cooling channel 214b on the opposite side of the cooling channel seat 215. While the retaining lip 267 is a convenient and preferred configuration, it may be replaced by a groove for receiving a protrusion on the facing surface of the cooling gallery pocket 215.

Each core cooling tube 270 includes first, second and third

tubular segments

271, 272, 273. The first tubular section 271 has a first outer diameter, the second tubular section 272 has a second outer diameter greater than the first outer diameter, and the third tubular section 273 has a third outer diameter between the first and second outer diameters. The second tubular section 272 also includes tapered ends 272a, 272b that provide transitions between three diameters. The outer surfaces of the second and

third segments

272, 273 generally correspond to the profile of the central bore 250a of the core insert 250 in which the core cooling tube 270 is received, the central bore 250a being configured to provide a predetermined flow area between the outer surface of the core cooling tube 270 and the central bore 250a to maximize cooling efficiency.

The first tubular segment 271 includes an externally threaded lower end 271a that is received within the enlarged axial bore portion 261a of one of the coolant diverters 260 and is threadedly engaged with the internal thread of the enlarged axial bore portion 261a of one of the coolant diverters 260. The second tubular section 272 has an inner diameter greater than the inner diameter of the first tubular section 271, and the upper end of the first tubular section 271 is received in the second tubular section 272. The inner diameters of the second and third

tubular segments

272, 273 are substantially the same. The third tubular segment 273 is secured at its lower end to the second tubular segment 272 and includes an upper free end having a serrated profile including four tines 273 a. The third tubular segment 273 also includes a spacer lobe 273b in an intermediate portion thereof, the spacer lobe 273b being adjacent to the teeth 273a but spaced from the teeth 273a and aligned between each pair of teeth 273 a.

The teeth 273a ensure that any unintended forward movement of the core cooling tube 270 caused by fluid pressure flowing therethrough does not close off flow between the core cooling tube 270 and the inner domed end of the central bore 250a of the core insert 250. The spacer vanes 273b ensure that the core cooling tube 270 is also centrally located within the core insert 250. The spacer vanes 273b are configured to limit radial movement of the core cooling tube 270 by engaging facing surfaces of the central bore 250a of the core insert 250. This arrangement maintains the position of the core cooling tubes 270 within the central bore 250a, thereby ensuring that the flow profile of the cooling fluid is substantially evenly distributed along the central bore 250 a.

The flow direction of the cooling fluid from the

cooling channels

214a, 214b is indicated by arrows in fig. 6. As shown, the cooling fluid flows from the first inlet cooling passage 214a into the radial bore 262 of the coolant diverter 260, which serves as an inlet portion of the

first cooling passages

261, 262, and then flows upward and out of the axial bore 261, which serves as an outlet portion. The cooling fluid then flows through and out of the core cooling tube 270 to impinge on the center of the domed end of the central bore 250a of the core insert 250. The domed end of the core insert 250 then reverses the flow in an umbrella-like manner to the annular gap between the outer surface of the core cooling tube 270 and the central bore 250 a. However, it should be understood that the cooling fluid flow may flow in the opposite direction.

The outer surface of the core cooling tube 270 generally corresponds to the contour of the central bore 250a of the core insert 250 within the molded portion 252, thereby providing a predetermined annular flow area that is less than the flow area within the core cooling tube 270. In this manner, the cooling fluid is throttled along this annular flow region to create turbulence, thereby increasing the heat transfer between the mold portion 252 and the cooling fluid. The cooling fluid then flows into the peripheral groove 263 of the coolant diverter 260 and out of the cooling channel 214b on the opposite side of the cooling channel seat 215. Thus, the peripheral groove 263 serves as an outlet for the cooling fluid return to the network of

cooling channels

214a, 214 b.

The coolant diverter 260 is formed from a resilient plastic material, such as by molding or additive manufacturing. However, those skilled in the art will appreciate that coolant diverter 260 may also be formed from a different, more rigid plastic or metal material, with retaining lip 267 provided as an insert made of an elastomeric material or formed by overmolding the body of coolant diverter 260 with an elastomeric material. In addition, the core-cooling tube 270 is formed of stainless steel, and the

tubular sections

271, 272, 273 and the spacer fins 273b are brazed together. However, the core cooling tube 270 may alternatively be formed as a unitary body, such as by additive manufacturing techniques. The core cooling tube 270 may be formed from a different material, which may be a metal or plastic material, and/or may be formed by any other suitable process.

Fig. 9-11 illustrate alternative core

cooling tube assemblies

1260, 1270 which are similar to the core

cooling tube assemblies

260, 270 described above, wherein like features are labeled with like reference numerals plus the previous '1'. As shown, the core cooling tube 1270 differs, inter alia, in that the first, second and third

tubular segments

1271, 1272, 1273 and the coolant diverter 1260 are all integrally formed. The third tubular section 1273 of the core cooling tube 1270 also includes an open end 1273a defined by a truncated dome 1273a in place of the serrated end of the core cooling tube 270 described above.

Since core cooling tube 1270 and coolant flow splitter 1260 are integral in this example and have little risk of separation, there is no need to provide serrated ends in this example. Further, truncated dome 1273a includes an aperture a having a smaller diameter than the apertures in third tubular section 1273, thereby defining a flow area that is less than the flow area through third tubular section 1273. As a result, the cooling fluid flowing through the core cooling tube 1270 is accelerated as it exits through the aperture A. This configuration also concentrates the flow directly to the central region of the domed end of the central bore 250a of the core insert 250 before reversing the flow as described above. It has been found that reducing the flow area to provide accelerated directional flow can improve cooling performance.

Conversely, the teeth 273a in the core cooling tube 270 described above provide an effective increase in flow area as compared to the flow area through the third tubular section 273. Indeed, some flow of coolant fluid from the third tubular segment 273 will exit through the spaces between the teeth 273a and be entrained to flow in a reverse direction through the annular gap between the outer surface of the core cooling tube 270 and the central bore 250a of the core insert 250, thereby avoiding the domed end of the central bore 250a of the core insert 250.

It will be appreciated by those skilled in the art that this end region of the core insert 250 is exposed to the highest temperatures because molten plastic introduced into the cavity during molding directly impinges thereon. As such, the reduction in flow area and directional flow toward this region of the core insert 250 provided by the core cooling tube 1270 according to this example is particularly advantageous.

The coolant flow splitter 1260 is a continuation of the first tubular section 1271 with a gradually curved tubular transition 1263 between the axial bore 1261 and the radial bore 1262. The coolant flow diverter 1260 also includes three spacer fins 1266 that center it within the cooling channel seat 215 of the punch 210. The radial bore 1262 and the curved transition connecting it to the axial bore 1261 are formed by a tubular transition 1263, the tubular transition 1263 having a substantially constant thickness to maximize the flow area around the coolant flow splitter 1260 as compared to the shallow groove 263 of the coolant flow splitter 260 shown in FIGS. 6-8. This alleviates the flow restriction created by the flutes 263, thereby reducing the pressure drop as the cooling fluid exits the core insert 250 back into the network of

cooling channels

214a, 214 b.

Retaining lip 1267 is formed by the tapered end of tubular transition 1263, which functions in a similar manner to retaining lip 267 described above. The unitary structure is formed of a suitable plastic material having sufficient resiliency to enable the retention lip 1267 to elastically deform when the coolant diverter 1260 is inserted into the cooling channel seat 215, snapping into the cooling channel 214a and returning to its original shape. However, the core cooling tube 1270 should be formed of a material that is also sufficiently rigid so that it retains its shape under the pressure of the cooling fluid. In an effort to mitigate the effects of any deformation of the core cooling tube 1270, the second tubular section 1272 includes three spaced vanes 1272c equally spaced about its periphery, and the third tubular section 1273 includes six spaced vanes 1273b equally spaced about its periphery, with every other spaced vane 1273b being axially staggered relative to adjacent spaced vanes 1273 b. Of course, different portions of the overall structure may also be formed of different materials to provide additional rigidity when desired. Preferably, the coolant diverter 2260 and the core cooling tube 2270 are integrally formed to provide a seamless, unitary monolithic structure. This may be accomplished by, for example, but not limited to, additive manufacturing processes.

Turning now to fig. 12-14, another alternative core cooling

tube assembly

2260, 2270 is shown, which is similar to the core cooling

tube assembly

1260, 1270 just defined above, with like features labeled with like reference numerals and the foregoing '1' replaced with the foregoing '2'. As shown, the core cooling tube 2270 differs in that the third tubular section 2273 contains only three spacer vanes 2273b that are axially aligned and evenly distributed around the circumference of the third tubular section 2273.

Further, the coolant diverter 2260 includes a partial circumferential wall 2268 having an outer surface similar to the circumferential surface 266 of the core cooling tube 270 according to the first example, but without the retaining lip shown. This partial circumferential wall 2268 is spaced from the body of the coolant diverter 2260, which defines the axial bore 2261 and cooperates with the facing surface of the cooling channel seat 215 of the punch 210 to provide a substantially sealed connection between the radial bore 2262 and the facing cooling channel 214 a. Although no retaining lip is shown in fig. 12-14, those skilled in the art will appreciate that such a retaining lip may be incorporated in this example.

Coolant diverter 2260 also includes spaced fins 2266 on opposite sides of partial circumferential wall 2268. In this way, the spacing fins 2266 and the partial circumferential wall 2268 together center the coolant flow divider 2260 within the cooling channel seat 215 of the punch 210. Further, the bottom of the coolant diverter 2260 is provided with a locating socket 2265, the locating socket 2265 having a recess 2265a in its lower surface. The locating sockets 2265 are received in locating grooves (not shown) in the base of a variation of the cooling channel seat 215 of the punch 210 shown in figure 6. The locating grooves (not shown) also include projections that engage the notches 2265a to ensure directional alignment between the radial holes 2262 and the facing cooling passages 214 a. Although the notch 2265a does not provide a retaining means in this example, it may be replaced by a radial projection that engages a facing one of the locating grooves (not shown) to provide both a locating means and a retaining means.

A tubular transition 2263 connects to a partial circumferential wall 2268 around the entrance of the radial bore 2262. As such, the coolant diverter 2260 according to this example more rigidly secures the core cooling tube 2270 in the cooling channel seat 215 of the punch 210, while minimizing the reduction in flow area around the tubular transition 2263, as compared to the coolant diverter 1260 according to the second example. In this way, this arrangement substantially maintains the above-described advantages over the coolant flow splitter 1260 according to the second example, namely, a reduced pressure drop as the cooling fluid flows out of the core insert 250 back into the network of

cooling channels

214a, 214 b.

Fig. 15-17 illustrate yet another alternative core cooling

tube assembly

3260, 3270 that is similar to the core cooling

tube assembly

2260, 2270 just defined above, wherein like features are labeled with like reference numerals, with the former '2' being replaced with the former '3'. As shown, the core

cooling tube assemblies

3260, 3270 differ only in that a partial circumferential wall 3268 of the coolant splitter 3260 is joined to the body defining the axial bore 3261 by

webs

3264a, 3264b around its periphery. More specifically, an upper edge of the partial circumferential wall 3268 is joined to the body by an annular web 3264a, and axial side edges of the partial circumferential wall 3268 are joined to the body by respective axial webs 3264 b. This creates a cavity between the partial circumferential wall 3268, the body and the

webs

3264a, 3264 b.

This arrangement further increases the rigidity of the joint between the core cooling tube 3270 and the cooling channel seat 215 of the male mold 210. However, the resulting reduction in flow area around the tubular transition 3263 increases the pressure drop as the cooling fluid flows out of the core insert 250 back into the network of

cooling channels

214a, 214b as compared to the

core cooling tubes

1270, 2270 according to the second and third examples. As with the core cooling tube 2270 according to the third example, a retaining lip may be incorporated in this example.

An alternative two-piece core insert 1250 is shown in fig. 18-20 that may be used in preform mold assembly 100 in place of core insert 250 previously described. The two-piece core insert 1250 is similar to the core insert 250 described above, with like features being labeled with like reference numerals plus the previous '1'. As shown, the two-piece core insert 1250 differs from the core insert 250 described above in that it includes a primary core insert 1250a and a core ring 1250 b.

In this example, the forwardmost portion of the base 1251 of the main core insert 1250a is recessed to provide a front face 1251a and an interface portion 1251b that protrudes from the front face 1251 a. Core ring 1250b includes a base 1251' or flange 1251' having a front face 1251a ' corresponding to front face 251a of core insert 250 described above. The core ring 1250b also includes an inner interface 1251b' and a male taper 1253 that corresponds to the male taper 253 of the core insert 250 described above. The interface portion 1251b is received by the core ring 1250b and contacts the inner interface surface 1251b' of the core ring 1250b in a press-fit condition.

As more clearly illustrated in fig. 20, the provision of the core ring 1250b provides a vent path from the inside corner of the neck opening of the preform cavity between the primary core insert 1250a and the core ring 1250 b. This enables the parting line between the two-piece core insert 1250 and the split mold insert 350 or neck ring 350 to move from the top sealing surface to the outer corner of the neck opening. The reason for this and the meaning thereof will be apparent to those skilled in the art. In this example, the core ring 1250b contains a pair of exhaust passages CRV that extend from the inner interface 1251b' to the collector groove CG defined by the outer surface of the male cone 1253. In operation, exhaust through the exhaust passage is directed by the collector groove CG which is aligned with the lower exhaust passage LNRV defined on the mating face through the collar 350. As shown, the collar 350 also includes an upper vent passage UNRV defined on a mating surface thereof.

Turning now to fig. 21, the moving portion 110 of the mold assembly 100 is shown in isolation with the female mold assembly 400 omitted to expose features of the stripper plate assembly 300. The stripper plate assembly 300 includes a stripper plate 310, six slide pairs 320 slidably mounted to the stripper plate 310, upper and lower guide assemblies 330 that guide the slide pairs 320 for movement along the stripper plate 310, and four connecting rods 340. In this example, the mold stack includes a plurality of split mold inserts 350 or neck rings 350, the split mold inserts 350 or neck rings 350 being arranged in pairs and mounted on the slide 320 for movement therewith.

The stripper plate 310, shown more clearly in figure 22, is substantially rectangular in plan, having a fan angle 311, the fan angle 311 being aligned with the fan angle 211 of the punch 210 for receiving tie bars (not shown) of an injection molding machine (not shown) in which the mold is mounted. The stripper plate 310 also includes four guide pin bushings 312 having associated holes (not shown) through its thickness, the guide pin bushings 312 being horizontally located inboard of each scalloped corner 311 for receiving the guide pins 230 of the punch 210. The stripper plate 310 also includes a plurality of core insertion holes 313, upper and lower cam disk holes 314, 314 and ten wear or support plates 315 (hereinafter support plates 315) through its thickness that provide bearing surfaces against which the slides 320 move along the stripper plate 310.

Each guide pin bushing 312 is in the form of a hollow cylinder and is bolted to the stripper plate 310 by four bolts 312 a. Each guide pin bushing 312 also includes a grease nipple 312b for introducing grease onto its inner surface in the usual manner. The inner diameter of the guide pin bushing 312 provides a small gap between the guide pin 230 and the guide pin bushing 312 within which grease introduced via the grease nipple 312b is received so that the guide pin 230 is free to slide within the guide pin bushing 312 to support the stripper plate 310 during movement between the stripper plate 310 and the punch 210 in the usual manner.

The core insert holes 313 are arranged in an array of six vertical columns and four horizontal rows, and each is configured to receive the base 251 of one of the core inserts 250. Each core insertion hole 313 is sized to provide clearance between it and the core insert base 251 to prevent contact between the stripper plate 310 as it moves along the guide pins 230 toward and away from the punch 210. The cam plate aperture 314 is oblong and configured to receive the cam plate 220. Each cam plate aperture 314 is sized to provide clearance between the cam plate aperture 314 and the cam plate 220 to prevent contact between the stripper plate 310 as it moves along the guide pins 230 toward and away from the punch 210. A pair of threaded guide bracket mounting holes 330a are included between each row of punch insertion holes 313 at the top and bottom of the punch 310. A pair of guide bracket pins 330b is also included between each pair of guide bracket mounting holes 330 a.

The support plate 315, which may also be referred to as a wear plate 315, is formed of a wear resistant material. Each support plate 315 is substantially rectangular in plan and includes two holes 316 and four partial

circular cutouts

317a, 317b through its thickness. The spacing of the support plate holes 316 corresponds to the spacing of the core insertion holes 313 along each vertical column. Two of the partial circular cutouts 317a are located at the centers of the short edges of the support plates 315, and the pitch of each partial circular cutout 317a and its adjacent support plate hole 316 also corresponds to the pitch of the core insertion holes 313 along each vertical column. Two further part-circular cutouts 317b are located in the centre of the long edges of the support plate 315. Thus, the support plate 315 is symmetrical about the central longitudinal axis.

The support plate 315 is placed longitudinally along the vertical column thereof with the support plate hole 316 and the partial circular cutout 317a aligned with the core insertion hole 313. Three support plates 315 are installed along each of two central columns of the core insertion holes 313, and a single support plate 315 is installed at the vertical center of the four outermost columns. In a mold according to the present disclosure, the support plates 315 are selectively positioned to provide balanced support for the slide pairs 320 during ejection, while minimizing their number to reduce cost. This is made possible by the load path created by the overall design of the mold assembly 100, as will be discussed below.

Each slide pair 320, shown more clearly in fig. 23, comprises a first slide 320a and a second slide 320b having substantially the same design. Each

slider

320a, 320b is in the form of a rod having a generally square or near square cross-section, with a plurality of semi-circular cutouts 321 along one side thereof and a guide hole 322 at each of its

ends

323a, 323b, the guide holes 322 extending through from one side to the other. A guide bushing 322a is received in each guide bore 322 and is retained therein by an interference fit, although other arrangements are also contemplated. The centermost slides 320a, 320b also include a cam follower 324 (shown in fig. 25) at each

end

323a, 323 b. Each cam follower 324 is in the form of a roller rotatably mounted to a sliding

end

323a, 323b for receipt within one of the cam slots 221 of one of the cam plates 220.

Each

slide

320a, 320b also includes in its front face a first pair of link mounting holes 325a at the first end 323a, a second pair of link mounting holes 325b adjacent to but spaced from the second end 323b, a series of neck ring mounting holes 326 and a series of cooling channel ports 327. One of the neck ring mounting holes 326 is located between each of the semi-circular cutouts 321, and the other neck ring mounting hole 326 is located outside each of the semi-circular cutouts 321, adjacent the

end

323a, 323b of the

slides

320a, 320 b. In use, the neck rings 350 are mounted to the

slides

320a, 320b through the neck ring mounting holes 326 such that the cooling channel ports 327 align with cooling channel ports (not shown) on facing surfaces of the neck rings 350. Each cooling channel port 327 contains an O-ring 327a (shown in fig. 26) for sealing the neck ring 350. The cooling channel ports 327 are connected to a cooling channel network (not shown) that is connected to a cooling fluid source in the usual manner.

In this example, the neck ring 350 is floatingly secured to the

slides

320a, 320b by a retainer assembly of the type defined in our co-pending application No. PCT/CA2018/050693, which is incorporated herein by reference. More specifically, as shown in fig. 24, each neck ring 350 is formed from a pair of

neck ring halves

350a, 350 b. A plurality of neck ring halves 350a are positioned longitudinally adjacent to each other on the slide 320a, and a corresponding plurality of neck ring halves 350b are positioned longitudinally adjacent to each other on the opposing slide 320 b. Each

neck ring half

350a, 350b is generally conventionally configured, but is configured to be secured to the

slides

320a, 320b by two retainer mechanisms 351.

Each retainer mechanism 351 includes a retainer member in the form of a bolt 352 and an insert member 353. Each bolt 352 has a head portion 352a and a threaded shaft portion 352 b. Each insert member 353 has an upper annular flange portion 353a, a cylindrical body portion 353b extending axially from the flange portion 353a, and a cylindrical opening extending axially through the flange portion 353a and the body portion 353 b. The bolt 352 is received within the cylindrical opening of the insert member 353 and is in threaded engagement with the collar mounting aperture 326 to retain the insert member 353 between the bolt 352 and the facing surfaces of the

slides

320a, 320 b. This results in a fixed spacing between the flange portion 353a of the insertion member 353 and the facing surfaces of the

sliders

320a, 320 b.

Each

neck ring half

350a, 350b has a semi-cylindrical central opening 354 such that when a pair of

neck ring halves

350a, 350b are brought together during operation of the injection molding system, the inward surfaces of the openings 354 providing the

neck ring halves

350a, 350b will define the contour of the neck region of the preform to be molded. Each

neck ring half

350a, 350b will be retained to the

respective slider

320a, 320b by a pair of retainer mechanisms 351 located on each longitudinal side of the

neck ring halves

350a, 350 b. Each

neck ring half

350a, 350b includes a generally arcuate upper half ring portion 355a and a flange portion 355 b. The half ring portion 355a has a tapered side surface 355c and the flange portion 355b has a lower surface 355d and an inner tapered surface 355 e.

Each

neck ring half

350a, 350b also has a pair of longitudinally opposed, generally stepped, semi-cylindrical side apertures 356. Each aperture 356 has a passageway all the way through the flange portion 355b of the

neck ring halves

350a, 350 b. When a pair of

neck ring halves

350a, 350b are positioned longitudinally adjacent to each other on the

slides

320a, 320b, a cylindrical opening is formed by two adjacent facing apertures 356. The opening is configured to receive one of the retaining mechanisms 351 and includes a recessed platform defined by a step in the facing aperture 356. The depth of the recessed platform is specifically set to position the flange portion 353a of the insert member 353 such that a gap is formed between the lower surface of the flange portion 353a and the upwardly facing opposing surface of the recessed platform. For example, the gap may be in the range of 0.01 to 0.03 mm.

When the

neck ring halves

350a, 350b are mounted to the slides, pressure exerted on the flange portion 355b by the O-ring 327a urges the flange portion 355b away from the

slides

320a, 320 b. The aforementioned clearance between the lower surface of the flange portion 353a and the upwardly facing opposing surface of the recessed platform formed by the stepped side aperture 356 allows for a small amount (e.g., 0.01 to 0.03mm) of clearance to be formed between the

neck ring halves

350a, 350b and the forward faces of the

slides

320a, 320 b. This clearance enables the

neck ring halves

350a, 350b to slide or float to some extent relative to the

slides

320a, 320b while applying sufficient compression to the O-ring 327a to maintain a sealed interface between the cooling channel ports 327 and the facing cooling channel ports (not shown) of the

neck ring halves

350a, 350 b.

As such, the

neck ring halves

350a, 350b are able to slide to some extent relative to their

respective slides

320a, 320b when the halves are brought together. This allows the

neck ring halves

350a, 350b in pairs to be repositioned to facilitate proper alignment with the rest of the mold stack. However, it is also contemplated that a conventional non-floating neck ring (not shown) may be used, as will be defined in more detail below.

Fig. 25 and 26 illustrate the interconnection between the slide pair 320 and the stripper plate 310, including one of the guide assemblies 330 and a pair of connecting rods 340. The guide assembly 330 includes a guide shaft 331 having a circular cross-section and fastened to the stripper plate 310 by seven guide brackets 332. The upper guide assembly 330 is mounted across the upper region of the stripper plate 310 directly below the upper scalloped corner 311 and the guide pin bushing 312. The lower guide assembly 330 is similarly mounted across the lower region of the stripper plate 310, directly above the lower scalloped corner 311 and the guide pin bushing 312.

Each of the upper and

lower guide assemblies

330, 330 includes a guide bracket 332 mounted between each sliding pair 320 and an end guide bracket 332 mounted adjacent each scalloped corner 311. The guide bracket 332 fixes the guide shaft 331 in place. Each guide bracket 332 includes a base 333, a clamping member 334, and a pair of bolts 335 received within respective bolt holes 336 in each of the base 333 and the clamping member 334. As shown in fig. 26, each guide assembly 330 is assembled by inserting the guide shaft 331 through the guide bushing 322a at one

end

323a, 323b of the

slider

320a, 320b with the guide frame base 333 held in place by the guide frame pin 330 b. The guide frame clamping member 334 is then placed on the guide shaft 331, and a bolt 335 is inserted into a bolt hole 336 in each of the guide frame base 333 and the clamping member 334. The bolt 335 is threadedly engaged with the guide bracket mounting hole 330a to fasten the guide bracket clamping member 334 to the stripper plate 310 and clamp the guide shaft 331 between the guide bracket clamping member 334 and the base 333. As a result, the

sliders

320a, 320b are held against the support plate 315 of the stripper plate 310 so that they can slide along the guide shaft 331 and the support plate 315.

In this example, the connecting rods 340 are elongate, have a square cross-section, and each have six pairs of bolt holes 341 spaced along its length. Although only bolt 342 is shown in each pair of bolt holes 341 in fig. 25, bolt 342 is received in each bolt hole 341 and secures connecting rod 340 to one of the

sliders

320a, 320b of each slider pair 320. One of the connecting rods 340 is connected to the first slider 320a of each slider pair 320, and the other of the connecting rods 340 is connected to the second side 320b of each slider pair 320. Thus, the sliding motion of one of the first sliders 320a causes all of the first sliders 320a to move therewith. Similarly, sliding movement of one of the second slides 320b causes all of the second slides 320b to move therewith.

In use, forward movement of the stripper plate 310 away from the punch 210 causes the cam follower 324 to move along the cam groove 221, which causes the

slides

320a, 320b carrying the cam follower 324 to slide toward each other along the guide shaft 331 and the support plate 315. This in turn causes each of the sliding pairs 320 to move away from each other, sliding along the guide shaft 331 and the support plate 315 to open the neck rings and, in doing so, eject the preform from the core in the usual manner. Similarly, the rearward movement of the stripper plate 310 toward the punch 210 causes the cam followers 324 to travel along the cam grooves 221 along a reverse path, thereby closing the neck rings.

Turning now to fig. 27, the die assembly 400 includes a die 410, four guide bushings 420 and a plurality of cavity assemblies 430. The female mold 410 is substantially rectangular in plan, having a front face CVF, a rear face CVR and scalloped corners 411. When the mold 100 is in the assembled state, the scalloped corners 411 are aligned with the scalloped

corners

211, 311 of the punch 210 and stripper plate 310 for receiving tie bars (not shown) of an injection molding machine (not shown) in which the mold is mounted. The female die 410 includes guide pin holes (not shown) through its thickness that are aligned with the guide pin bushings 420 and are horizontally located inboard of each scalloped corner 411 for receiving the guide pins 230 of the male die 210.

The female die 410 also includes a plurality of seats 412 through its thickness, a web of

cooling channels

413a, 413b, 413c in communication with the seats 412, and upper and lower cam disc holes 414, 414 through its thickness. The sockets 412 are arranged in an array of six vertical columns and eight horizontal rows arranged to mate with the core inserts 250. Each seat 412 is surrounded by four threaded cavity mounting holes 415, with one of the cavity inserts 430 received in each seat 412 and secured to the female die 410 by bolts 416, the bolts 416 being in threaded engagement with the cavity mounting holes 415. The cam plate aperture 414 is oblong and configured to receive the cam plate 220. Each cam plate aperture 414 is sized to provide clearance between cam plate aperture 414 and cam plate 220 to prevent contact therebetween when mold 100 is closed. The female die 410 also includes an array of tie bolt holes 417 for receiving the above-described tie bolts 217 to secure the female die 410 to the male die 210, as will be further defined below.

Each guide pin bushing 420 is in the form of a hollow cylinder and is bolted to the female mold 410 by four bolts 421. Each guide pin bushing 420 also includes a grease nipple 422 for introducing grease onto its inner surface in the usual manner. The inner diameter of the guide pin bushing 420 provides a small clearance between the guide pin 230 and the guide pin bushing 420 within which grease introduced via the grease nipple 422 is received such that the guide pin 230 is free to slide within the guide pin bushing 420 to ensure proper alignment between the punch 210 and the matrix 410 during operation in the usual manner.

As shown more clearly in fig. 28-35, each cavity assembly 430 includes a cavity insert 440, a gate insert 450, and a pair of retaining pins 460. In this example, cavity insert 440 and gate insert 450 are separate components, but in other variations they may be formed as a single unitary structure. The cavity insert 440 includes a generally cylindrical body 441 having flat sides 442 to provide a generally circular cross-section. The cavity insert 440 also includes a socket 443 projecting from the mounting face 441a at one end of the body 441, four axial mounting holes 444 adjacent the outer corners of the substantially elliptical cross-section, the four axial mounting holes 444 extending from the mounting face 441a to the front face 441b at the opposite end of the body 441, and a network of cooling channels 445.

The socket 443 is hollow with a stepped gate insert seat 446 for receiving the gate insert 450. The body 441 of the cavity insert 440 is also hollow and includes a concave taper 447 that extends from the front face 441b to the molding surface 448. Body 441 includes an annular step 447a that joins cone 447 to a molding surface 448, which molding surface 448 extends from annular step 447a to gate insert seat 446. The gate insert seat 446 comprises a cylindrical first portion 446a and a cylindrical second portion 446b, the first portion 446a extending from the end face 443a of the socket 443 to a first internal shoulder 443b, the second portion 446b having a smaller diameter than the first portion 446a, extending from the first internal shoulder 443b to a second internal shoulder 443 c. The first internal shoulder 443b provides a transition from the first portion 446a of the gate insert seat 446 to the second portion 446b thereof, while the second shoulder 443c provides a transition from the second portion 446b of the gate insert seat 446 to the molding surface 448 of the body 441.

The socket 443 includes a pair of threaded radial holes 449 that extend from the first portion 446a of the gate insert base 446 to the outer circumferential surface of the socket 443. The axes of radial bores 449 are parallel to flat side 442 and their bases are substantially flush with first inner shoulder 443b of gate insert seat 446. The receptacle 443 also includes a circumferential groove 443d in its outer peripheral surface below the radial hole 449 for receiving an O-ring seal (not shown).

The network of cooling channels 445 includes a coolant inlet 445a and a coolant outlet 445b, each fluidly connected to two different circuits. One of the circuits is shown in the schematic diagram of fig. 30, which corresponds to one half of the cavity insert 440 depicted by line a-a in fig. 29. The other circuit (not shown in fig. 30) mirrors that shown in fig. 30, and both coolant inlet 445a and outlet 445b are fluidly connected to both circuits. Each circuit includes a pair of first axial channels 445c, a pair of transverse or cross channels 445d, and a pair of second axial channels 445 e. The coolant inlet 445a is defined by an axial slot 445a through the socket 443, the axial slot 445a extending from its end face 443a to the first interior shoulder 443 b. The coolant outlet 445b is also defined by an axial slot 445b through the socket 443, similar to the axial slot of the coolant inlet 445a, but on the opposite side thereof. The coolant inlet 445a, coolant outlet 445b, and radial holes 449 are equally spaced around the circumference of the receptacle 443 such that the radial holes 449 are located between the coolant inlet 445a and the coolant outlet 445 b. The flow path through each of the coolant inlet 445a and the coolant outlet 445b is perpendicular to the axis of the radial hole 449.

The

axial passages

445c, 445e are provided by blind bores equally spaced around the socket 443 and the body 441 and extending from the end face 443a of the socket 443 to the transverse passage 445 d. As best shown in fig. 29, the diameter of first portion 446a of gate insert seat 446 is such that the portion of each of these bore holes extending from end surface 443a to first internal shoulder 443b opens into first portion 446 a. The transverse channel 445d of each circuit is also provided by a blind bore extending from the circumferential surface 441c of the cylinder 441 towards a respective one of the flat sides 442 such that they extend orthogonally to one another. The intersecting passages 445d intersect each other and with a respective pair of

axial passages

445c, 445e to provide fluid communication between the first and second

axial passages

445c, 445 e.

Referring now to fig. 31-33, gate insert 450 is generally cylindrical having a first nozzle tip receiving portion 451, a second molding cavity portion 452, and a third gate portion 453 joining first portion 451 to second portion 452. The first portion 451 includes a groove 451a extending from an end face 451b thereof, the groove 451a being shaped to receive the tip of a valve gated injection nozzle (not shown) and an associated tip insulator (not shown) in the usual manner. The first portion 451 also includes a circumferential groove 451c in its outer circumferential surface and spaced from the end surface 451b for receiving an O-ring seal (not shown).

Second portion 452 defines a dome-shaped molding surface 452a extending from an end surface 452b thereof that is shaped to define an outer surface of a base of a preform to be molded in a conventional manner. The second portion 452 further includes a circumferential groove 452c in its outer circumferential surface and spaced from the end face 452b for receiving an O-ring seal (not shown). The third portion 453 defines a central cylindrical gate 453a that connects the groove 451a of the first portion 451 to the molding surface 452a of the second portion 452 in a conventional manner.

The second section 452 has a diameter less than the diameter of the first section 451 and the third section 453 has a diameter less than the diameters of the first and

second sections

451, 452. Thus, the third section 453 provides a necked transition between the first and

second sections

451, 452, thereby providing a circumferential cooling groove 454 therebetween. In addition, the third portion 453 further includes a circumferential bypass groove 455 in the recessed cooling groove 454. In this example, the bypass channel 455 is narrower than the cooling channel 454 such that a pair of shoulders 454a are defined in the base of the cooling channel 454. As such, the cooling trough 454 provides a main trough 454, and the bypass trough 455 provides a bypass trough 455 in the base of the main trough 454.

Referring now to fig. 32, each retaining pin 460 includes a cylindrical body 461 having an externally threaded portion 462 and a plug portion 463. The threaded portion 462 includes a driving end 464 having a hexagonal recess 465, the hexagonal recess 465 being configured to receive a driving tool, such as a hexagonal key (not shown). Plug portion 463 extends from threaded portion 462 and includes a smooth circumferential surface 466 and a flat end 467.

Referring to fig. 33 and 34, the web of

cooling channels

413a, 413b, 413c of the female die 410 comprises: a feed channel 413a extending through the female die 410 and parallel to the row of seats 412; and a series of

branch channels

413b, 413c extending between each of the columns of seats 412, connecting the seats 412 in each column together in series. In FIG. 33, the branch cooling channel section 413b on the left side of each seat 412 provides an inlet 413b to the seat 412, while the branch cooling channel section 413c on the right side of each seat 412 provides an outlet 413c, or vice versa. In this example, the inlet 413b and the outlet 413c are aligned at the same depth in the female die 410, and are also on opposite sides of the female die 410. It is also contemplated that the inlet 413b and the outlet 413c may extend at an angle (e.g., a right angle) with respect to each other.

The feed passage 413a has a first diameter D₁And the inlet 413b and the outlet 413c have a diameter smaller than the first diameter D₁Second diameter D₂. Each seat 412 of the female mold 410 comprises a stepped bore having a first cavity insert receiving portion 412a, a second gate insert receiving portion 412b having a smaller diameter than the first portion 412a, and a step 412c providing a transition therebetween. The female mold 410 has a depth D or thickness, as described from the anterior CVF to the posterior CVR, that is much thinner than a conventional female mold (not shown).

The bodies of conventional cavity inserts (not shown) are almost completely received within the holes in such conventional dies (not shown) such that most or all of their molding surfaces are within the plate, and cooling channels are formed around the outer surface of each body, which define paths with the holes along which the cooling fluid flows. Instead, the female mold 410 of mold 100 only receives socket 443 so that the same female mold 410 can be used with different cavity inserts 440 for molding different preform designs. This also minimizes the thickness of the female mold 410. In this example, the first diameter D₁About half the depth D, the second diameter D₂About one third of the depth D. It has been found that this provides a female mold 410 that is sufficiently rigid in operation while minimizing the depth D. It is contemplated that in some applications, some of the

cooling channels

413a, 413b, 413c may be sized up to 75% of the depth D of the female mold 410 without compromising its rigidity. However, preferably, the

cooling channels

413a, 413b, 413c have a dimension D₁、D₂At most 60% of the depth D of the female mold 410. Also preferably, the dimension D of the inlet 413b and the outlet 413c₁、D₂Is at least 15%, more preferably at least 25% of the depth D of the female mold 410. It should also be noted that the

cooling channels

413a, 413b, 413c need not have a circular cross-section, in which case the dimension D mentioned above₁、D₂May represent the dimension of the cooling channel across the thickness of the female die 410.

Additionally, in this example, the molding surface 448 of the cavity insert 440 is located entirely between the concave taper 447 of the cavity insert 440 and the mounting surface 441a of the body 441. However, the foregoing is not necessary in all cases, as the location of this split line may be affected by the depth of the gate insert seat 446, the length of the socket 443, the thickness of the cavity die 410, and the shape and size of the base molding portion defined in the gate insert 450. Sufficient to state that a portion of the molding surface 448 may be received within the die holder 412. It is contemplated that up to one third, but preferably 10% or less, of the molding surface 448 can be received within the die holder 412.

As shown in fig. 28 and 33, gate insert 450 is received within stepped gate insert seat 446 of cavity insert 440. More specifically, molding cavity portion 452 of gate insert 450 is received within second portion 446b of gate insert seat 446 with an O-ring (not shown) received within circumferential groove 452c, thereby providing a seal therebetween. The end surface 452b of the mold cavity portion 452 abuts the second shoulder 443c such that the dome-shaped molding surface 452a provides an extension of the molding surface 448 of the cavity insert 440. A lower portion of nozzle tip receiving portion 451 is received within an upper portion of first portion 446a of gate insert seat 446, with circumferential cooling groove 454 aligned with a lower portion of first portion 446a of gate insert seat 446 and with the bases of coolant inlet 445a and coolant outlet 445 b. A cooling channel 454b is defined between the circumferential cooling groove 454 and a lower facing surface of the first portion 446a of the gate insert seat 446.

As shown in fig. 28, 34 and 35, each retaining pin 460 is received within one of the radial holes 449 of the socket 443 of the cavity insert 440. Threaded portion 462 threadingly engages threads of radial bore 449, and plug portion 463 extends into receptacle 443, into circumferential cooling groove 454 and abuts shoulder 454 a. In this manner, the cooling channel 454b defined between the circumferential cooling groove 454 and the first portion 446a of the gate insert seat 446 is divided into two segments or halves, with the plug portion 463 of the retaining pin 460 acting as a flow splitter. As shown more clearly in fig. 35, the bypass trough 455, together with the flat end 467 of the plug portion 463, defines a bypass flow channel section 455a that allows some flow to pass between the two halves of the cooling channel 454 b. In addition to the above-described segmentation of the cooling channel 454b, the retaining pin 460 also retains the gate insert 450 within the socket 443 of the cavity insert 440 to retain the cavity assembly 430 in an assembled state.

The cavity assemblies 430 are mounted to the cavity die 410 by inserting the socket 443 of each cavity assembly 430 and the protruding portion of the gate insert 450 into one of the cavity die holders 412. More specifically, the socket 443 of each cavity insert 440 is received within the first cavity insert receiving portion 412a and an upper portion of the nozzle tip receiving portion 451 is received within the second gate insert receiving portion 412 b. O-rings (not shown) are received within the

circumferential grooves

451c, 443d to provide a sealed connection with the cavity insert seats 412 on either side of the inlet 413b and outlet 413 c. Although not explicitly shown in the drawings, the end surface 451b of the nozzle tip receiving portion 451 of the gate insert 450 is slightly recessed with respect to the rear face CVR of the female die 410.

The cavity inserts 440 are oriented such that the flat sides 442 of the body 441 face each other along a vertical column, as shown in fig. 27 and 33. In this orientation, the coolant inlet 445a and outlet 445b in the socket 443 are aligned with the inlet 413b and outlet 413c in the female die 410. The bolts 416 are inserted into the mounting holes 444 of the body 441 of each cavity insert 440 and threadedly engaged with the cavity mounting holes 415 to fasten the cavity inserts 440 to the female die 410. The torsion bolt 416 forces the mounting surface 441a of the body 441 against the front face CVF of the die 410. The twist bolt 416 also forces the end face 443a of each socket 443 against the step 412c of the die holder 412, thereby closing the upper ends of the inlet 445a and outlet 445b and the bore forming the

axial passage

445c, 445 e. As a result, the network of cooling channels 445 of each cavity insert 440 is sealingly connected to the network of

cooling channels

413a, 413b, 413c of the female die 410.

In use, cooling fluid flows from the supply passage 413a through the inlet 413b of the seat 412 into the inlet 445a of the first cavity assembly 430 in each vertical column. The majority of the cooling fluid flows from the inlet 445a into the first axial passage 445c of each cooling circuit, through the crossover passage 445d, into the second axial passage 445e, and out the outlet 445b into the outlet 413c of the seat 412. However, some cooling fluid also flows through bypass channel section 455a, which provides more balanced flow through cavity assembly 430 and simultaneously cools the area of gate insert 450 surrounding gate 453 a. The cooling fluid then enters the inlet 413b of the next seat 412 in the column and passes through the cavity assembly 430 received therein. It should be noted, however, that this is only one possible implementation. Other configurations of

cooling passages

413a, 413b, 413c, 445 are contemplated without departing from the scope of the present invention.

Indeed, it is expressly contemplated that the configuration of bypass channel segment 455a may be changed, such as by one or more modifications to bypass slot 455 or retaining pin 460. Fig. 36 shows a variation in which each bypass channel segment 1455a is located adjacent to the mold cavity portion 452 of gate insert 450 so as to provide only a shoulder 1454 a. The retaining pin 460 in the arrangement of fig. 36 corresponds to the arrangement of fig. 35. Fig. 37 shows another variation, in which

bypass passage sections

455a, 1455a are omitted, and retaining pin 2460 includes a plug portion 2463 having a tapered end 2467. The tapered end 2467 cooperates with the circumferential cooling groove 454 to provide a bifurcated bypass passage section 2455 a. Other arrangements are also contemplated and understood by those skilled in the art. For example, the cut provided by the tapered end 2467 may be replaced by a hole through the pin or some other arrangement.

Figures 38 and 39 show an alternative die assembly 3400 which is similar to the die assembly 400 described above, with like features being labelled with like reference numerals plus the previous '3'. As shown, the die assembly 3400 differs, inter alia, in that gate insert 450 is replaced by a two-part assembly that includes gate insert 3450 and gate pad 3457. Each seat 3412 of female die 3410 includes a first cavity insert receiving portion 3412a, a second gate insert receiving portion 3412b having a diameter slightly smaller than first portion 3412a, and a tapered transition 3412c therebetween.

Gate insert 3450 includes a gate pad receiving portion 3451 in place of first nozzle tip receiving portion 451, which gate pad receiving portion 3451 is longer and stepped to provide an enlarged end 3456 that abuts end face 3443a of socket 3443 instead of step 412c of die holder 412 in the previous example. The sprue pad-receiving portion 3451 includes a frustoconical groove 3456a for receiving the sprue pad 3457, the frustoconical groove 3456a tapering at an included angle of between 30 and 40 degrees (about 35 degrees in this example). The gate 3453a engages the receiver 3451 with the dome-shaped molding surface 3452 a. The enlarged end 3456 also includes a lip 3456b adjacent the step, which in the assembled state is adjacent the tapered transition 3412c of the seat 3412 of the female die 3410. A circumferential groove 3451c is also located on the outer peripheral surface of the enlarged end 3456 for receiving an O-ring seal (not shown).

The gate pad 3457 is hollow and defines therein a nozzle holder 3451 a. Sprue pad 3457 includes a first threaded end 3457a, a second frustoconical outlet end 3457b, a flange 3457c between first and

second ends

3457a, 3457b, and a shoulder 3457d between flange 3457c and first end 3457 a. Both the flange 3457c and the shoulder 3457d protrude outward. The flange 3457c is hexagonal in this example for engaging an installation tool in use. Like the groove 3456a of the sprue pad-receiving portion 3451, the exit end 3457b tapers at an included angle of between 30 and 40 degrees, in this embodiment about 35 degrees. Nozzle mount 3451a terminates at a central cylindrical gate 3459 at an exit end 3457b of gate pad 3457, which gate 3459 forms an orifice through the tip of exit end 3457 b.

In the assembled state, threaded end 3457a of gate pad 3457 is received within and threadedly engaged with threaded bore 3501 of melt distributor 3500 such that a nozzle tip (not shown) extends from within melt distributor 3500 into nozzle seat 3451 a. The bore 3501 of the melt distributor 3500 is stepped, with an enlarged pocket 3501a at the end of the threaded bore 3501, with a shoulder 3457d received within the enlarged pocket 3501 a. Shoulder 3457d is annular and sized to provide a tight fit with pocket 3501 to maintain alignment of gate pad 3457 relative to melt distributor 3500.

When melt distributor 3500 is mounted to female die 3410, outlet end 3457b of gate pad 3457 is received within gate pad receiving portion 3451 of gate insert 3450 and

gates

3453a, 3459 thereof are aligned to receive molten material. It has been found that this split gate insert arrangement reduces wear that may otherwise occur due to misalignment between the nozzle tip (not shown) and the gate insert 450. It also facilitates separation of melt dispenser 3500 from a cold half (not shown) incorporated into female mold assembly 3400 without the need to allow melt dispenser 3500 to cool, thereby enabling faster mold transitions. Gate pad 3457 can be configured to act as a sacrificial component, thereby reducing wear on gate insert 3450 and extending its useful life.

As shown in fig. 38, the combined depth of socket 3443, gate insert 3450 and flange 3457c is slightly less than the depth of cavity die 3410 for reasons that will be further defined below.

Fig. 40 and 41 show partial cross-sectional views of one of the mold stacks MS through the assembled cold half 130 shown in fig. 2, with the mold stack MS shown in the molding configuration. In this molding configuration, the top sealing surface of the preform is defined in part by the top sealing surface portion TSS of the core insert 250 and in part by the neck ring 350. The components of each mold stack MS engage one another in a design commonly referred to in the art as a "cavity lock" design. The inner tapered surface 355e of the collar 350 surrounds the taper 253 of the core insert 250, and the lower surface 355d of the flange portion 355b of the collar 350 abuts the front face 251a of the base 251 of the core insert 250. In this example, the front face 251a provides an annular bearing surface 251a that engages a portion of the flange portion 355b of the collar 350. The tapered side surface 355c of the neck ring 350 is received within the female taper 447 of the cavity insert 440, and the half-ring portion 355a of the neck ring 350 abuts or is otherwise spaced from the annular step 447a to define a narrow vent opening, allowing air to escape the molding cavity but preventing the molding material (i.e., flash) from flowing out during injection molding.

A significant difference from conventional molds is that the mold stack MS in this example has a stack height that is configured such that an applied clamping load CL (illustrated by the arrow in fig. 40) applied to each of the male and female molds 210, 410 (via the melt distributor 500) is substantially fully directed through the mold stack. More specifically, the distance between the neck ring 350 and the punch 210 is greater than the thickness of the stripper plate assembly 300 received between the neck ring 350 and the punch 210, thereby preventing the clamping load CL from being directed through the stripper plate assembly 300. In this example, this difference results in a gap provided by the gap G between the stripper plate 310 and the punch 210. While this arrangement is preferred, it is also contemplated that in some variations, a gap G may be provided between the slide 320 and the stripper plate 310.

Further, the mold stack MS in this example is configured such that the clamping load CL applied therethrough is balanced. For example, the portion of the neck ring 350 that engages the cavity insert 440, i.e., the tapered side surface 355c and the radial end surface of each half-ring portion 355a, has a similar projected area in the direction of the clamping load CL as the portion of the inner tapered surface 355e and the lower surface 355d of the flange portion 355b that engages the annular bearing surface 251a of the core insert 250. In this example, the mold stack MS is configured such that substantially all of the clamping load CL is transmitted through the tapered side surface 355c and the radial end surface of each half ring portion 355a, and is not between the flange portion 355b of the neck ring 350 and the facing surface of the cavity insert 440.

It will be apparent to those skilled in the art that substantially all of the clamping load CL passes through the mold stacks MS, thereby providing a separate load path through each mold stack MS. This ensures a more even and predictable distribution of the clamping load CL over the mould 100. Routing substantially all of the clamp load CL through the mold stack MS may also eliminate the need for tonnage blocks and the need to tightly control the thickness of the stripper plate 310 and support plate 315, as is required in conventional preform molds. Another result of eliminating the load path through the support plate 315 and stripper plate 310 is that the distribution and configuration of the support plates 315 is less critical because they no longer function to evenly distribute the clamping load on the mold assembly 100. Therefore, their number, distribution and manufacturing tolerances are less critical.

Further, as described above, the end surface 451b of the nozzle tip receiving portion 451 of the gate insert 450 is slightly recessed with respect to the rear surface CVR of the female die 410. This ensures that most, if not all, of the clamping load CL is transferred through the female mold 410, avoiding any load transfer via the gate insert 450. In the case of the alternative die assembly 3400, a similar effect is achieved by the aforementioned combined depth of socket 3443, gate insert 3450 and flange 3457 being slightly less than the depth of die 3410.

It should be noted, however, that a tonnage block (not shown) may be provided at a predetermined location between the male mold 210 and the female mold 410 in order to protect the mold stack MS from inadvertent application of an over-clamp load CL. Those skilled in the art will also appreciate that the gap G need not be provided between the punch 210 and the stripper plate 310. Other configurations are possible without departing from the disclosure herein. A non-limiting example would be to dimension the core insert 250, the neck ring 350, and the cavity insert 450 such that they are in contact with small gaps between other surrounding components of the mold shoe.

The mold 100 may also be configured to protect the mold stack MS from excessive stress. For example, the mold 100 may be configured such that if a predetermined threshold clamping load CL is exceeded, only a portion of the clamping load CL is directed through the mold stack MS. In this example, this may be accomplished by configuring the gap G such that a portion of the clamping load CL is directed through the stripper plate assembly 300 when a predetermined clamping load CL is exceeded. More specifically, the gap G may be configured such that once a predetermined compression of the mold stack MS is achieved, the gap G closes and a portion of the clamping load CL is directed from the neck rings 350 through the stripper plate assembly 300 to the female mold 410. More preferably, however, the mold 100 may include one or more posts or tonnage blocks (not shown) between the male 210 and female 410 through which a portion of the clamping load CL is directed when a predetermined clamping load CL is exceeded.

Referring to fig. 42 and 43, the mold 100 enables a novel method of aligning the mold stack MS of the mold 100. The method of aligning a mold stack MS comprises the steps of:

i) assembling the die assembly 400 as described above, ensuring that the proper torque is applied to the bolt 416 to ensure that the cavity assembly 430 is properly secured to the die 410;

ii) assembling the stripper plate assembly 300 as described above with the neck ring 350 floatingly mounted to the slide 320;

iii) assembling the punch assembly 200 as described above, with the punch 210 in a vertical position on the base plate and ensuring that the bolts 218 are only loosely tightened so that the punch insert 250 is loosely mounted to the front CRF in a floating manner;

iv) rotating the male die assembly 200 so that its rear face CRR rests on the substrate;

v) lowering the stripper plate assembly 300 onto the punch assembly 200 to form the moving part 110 shown in figure 21;

vi) rotating the die assembly 400 such that the cavity assembly 430 is at a minimum;

vii) lowering the die assembly 400 onto the moving part 110 (see fig. 42);

viii) installing a latch (not shown) to hold the core, stripping and die

assembly

200, 300, 400 or the cold half 130 together, rotating the cold half 130 so that the rear CVR of the die 410 rests on the substrate, and removing the latch (not shown);

ix) repeatedly raising and lowering the punch assembly 200 relative to the stripper plate and die assembly 300, 400 (see fig. 43) using suitable lifting gears (not shown) to align the core insert 250 relative to the neck ring 350 and the cavity insert 450;

x) mounting and torqueing the tie bolt 217 to engage with the tie bolt hole 417 of the female die 410, thereby securing the male die 210 to the female die 410 and the mold stack MS in the closed configuration, starting with the innermost bolt 217 and expanding;

xi) torqueing the bolts 218 from the back side of the male die 210 to secure the core inserts 250 to the male die 210 in a fixed, aligned condition, wherein the core inserts are immovable relative to the male die 210 and are aligned with the neck rings 350 and cavity inserts 450;

xii) reinstall the latches (not shown) and rotate the cold half 130 to the vertical position; and

xiii) remove the coupling bolt 217 so that the cold half 130 is ready for installation.

In the above method, the cavity insert 440 is the only stacked component that is initially secured in place. The neck ring 350 is secured to the slide 320 in a floating manner by means of a retainer mechanism 351. Similarly, the core insert 250 is initially mounted in a floating manner. Thus, in step ix) above, the raising and lowering of the male mold assembly 200 causes the female taper 447 of the fixed cavity insert 440 to engage the tapered side surface 355c of the half-ring portion 355a, thereby aligning the collar 350 relative to the cavity insert 440. In addition, the inner tapered surface 355e of the collar 350 engages the core taper 253 of the core insert 250, thereby aligning the core insert 250 relative to the collar 350.

While the rear-mounted bolts 218 provide a simple and effective means to secure the core inserts 250, 1250 from their floating condition while the mold 100 is in the assembled condition, other arrangements are contemplated. For example, the bolts 218 may be replaced by another fastening device, which may preferably be operated without access to the front of at least some of the core inserts 250, 1250. When in the assembled state, the fastening means may be operated from the back side of the punch 210 or from some other accessible region of the mold 100 (e.g., the side, top, or bottom). In addition and as described above, although the mounting surface 254 is devoid of any protrusions, the core insert 250 may be provided with a socket extending from the mounting surface 254 that is smaller than the seat 215 in the male mold 210 to allow some sliding movement therebetween. Indeed, in some examples, the socket may be substantially the same size as the seat 215 in the punch 210.

It will be appreciated by those skilled in the art that the floating collar 350 may be replaced with a conventional collar 350. Conventional neck rings (not shown) may be loosely mounted to the slides 320 so that they are free floating during the above-described process. The neck ring bolts can then be torqued to secure them in place after the mold 100 is installed in a machine (not shown). Other configurations and methods are also contemplated. For example, the procedure outlined in CA2741937 may be employed, wherein the cavity mounting holes 444 are aligned with mounting holes of a conventional neck ring (not shown), and some of the cavity mounting bolts 416 are omitted during the alignment procedure. This enables a tool (not shown) to be inserted through the cavity mounting hole 444 to twist the neck ring mounting bolts (not shown) before removing the attachment bolts 217 at step xiii of the alignment process described previously.

It should be understood that the configuration of the elements of the molding system 100 may vary, particularly (but not exclusively) as defined above. For example, the annular bearing surface 251a of the core insert 250 may be angled or tapered when it is perpendicular to the longitudinal axis of the core. It is particularly advantageous that the annular bearing surface 251a is angled or tapered, for example to provide a recess, such as a conical recess. This can be configured to provide an inward force to the neck rings 350 under a clamping load CL, for example, to prevent the neck rings 350 from separating due to the pressure of the molten plastic during injection molding. This may be a shallow recess, for example at an angle of less than 10 degrees. Further, the closed end of the core insert 250 may be conical or any other suitable shape. The shape of the

core cooling tubes

1270, 2270, 3270 may also be shaped to approximate the different shapes.

It will also be appreciated by those of ordinary skill in the art that several variations in the configuration and/or use of the above examples may be contemplated without departing from the scope of the present invention. It will also be appreciated by those skilled in the art that any number of combinations of the above-described features and/or features shown in the accompanying drawings provide significant advantages over the prior art and are therefore within the scope of the invention as defined herein.

Claims

1. A coolant diverter (260, 1260) for a preform mold (100), the preform mold (100) receivable in use in a seat (215) defined in a punch (210), the diverter (260, 1260) comprising a body defining at least a portion of first and second cooling channels (261, 262, 263, 1261, 1262, 1263), and a locator (267, 1267) for engaging the locator (214a) of the punch seat (215), the first cooling channel (261, 262, 1261, 1262) comprising an inlet portion (262, 1262) for receiving cooling fluid from a cooling circuit (214a, 214b) of the punch (210) and an outlet portion (261, 1262) extending at an angle relative to the inlet portion for supplying the cooling fluid to a core insert (250), 1261) The second cooling channel (263, 1263) including an inlet for receiving cooling fluid from the core insert (250) and an outlet for delivering the cooling fluid to the cooling circuit (214a, 214b) of the punch (210), wherein the positioner (267, 1267) is configured to align, in use, the inlet portion (262, 1262) of the first cooling channel (261, 262, 1261, 1262) with the cooling circuit (214a, 214b) of the punch (210) and inhibit removal of the diverter (260, 1260) when the diverter (260, 1260) is received within the punch shoe (215).

2. The coolant diverter (260, 1260) of claim 1, wherein the locator (267, 1267) includes a snap-fit connector (267, 1267).

3. The coolant diverter (260, 1260) of claim 1 or 2, wherein the locator (267, 1267) includes a projection (267, 1267) on the body, the projection (267, 1267) being receivable within the cooling circuit (214a, 214b) of the male die (210).

4. The coolant diverter (260, 1260) of claim 3, wherein the projection (267, 1267) includes an annular projection (267, 1267), the annular projection (267, 1267) being receivable within the cooling circuit (214a, 214b) of the male die (210).

5. The coolant diverter (260, 1260) of claim 4, wherein the annular protrusion (267, 1267) includes a lip (267, 1267) surrounding an opening of the inlet portion (262, 1262) of the first cooling channel (261, 262, 1261, 1262) for receipt within the cooling circuit (214a, 214b) of the punch (210).

6. The coolant diverter (260, 1260) of claim 1 or 2, wherein the locator includes a groove for receiving a protrusion of the die holder (215).

7. The coolant diverter (260, 1260) of any of the preceding claims, wherein at least a portion of the second cooling channel (263, 1263) is defined, in use, between an outer surface of the coolant diverter (260, 1260) and the boss die (215).

8. The coolant diverter (260, 1260) of claim 7, wherein the body is substantially cylindrical in shape, an inlet portion (262, 1262) of the first cooling channel (261, 262, 1261, 1262) including a radial bore (262, 1262), an outlet portion (261, 1261) of the first cooling channel (261, 262, 1261) including an axial bore (261, 1261) and at least a portion of a second cooling channel (263, 1263) defined by a groove (263, 1263) in the body.

9. The coolant diverter (260, 1260) of claim 8, wherein the first cooling channel (261, 262, 1261, 1262) includes a curved transition (1263, 2263, 3263) connecting the radial bore (262, 1262) to the axial bore (261, 1261).

10. The coolant diverter (260, 1260) of any of claims 7-9, including one or more spacers (266, 1266, 2266, 2268, 3266, 3268) for engaging the boss base (215) to center the outlet portion (261, 262, 1261, 1262) of the first cooling channel (261, 262, 1261, 1262) therein.

11. The coolant diverter (260, 1260) of claim 10, wherein the outlet portion (261, 1261) of the first cooling channel (261, 262, 1261, 1262) is defined by a tubular or partially tubular portion.

12. The coolant diverter (260, 1260) of claim 11, wherein at least one of the spacers (266, 1266, 2266, 2268, 3266, 3268) includes a partial circumferential wall (266, 2268, 3268) surrounding at least a portion of the tubular or partial tubular outlet portion (261, 1261) of the first cooling channel (261, 262, 1261, 1262) and spaced apart from at least a portion of the tubular or partial tubular outlet portion (261, 1261) of the first cooling channel (261, 262, 1261, 1262).

13. The coolant diverter (260, 1260) of any one of claims 10-12, wherein at least one of the spacers (266, 1266, 2266, 2268, 3266, 3268) includes a fin (1266, 2266, 3266) projecting radially relative to the outlet portion (261, 1261) of the first cooling channel (261, 262, 1261, 1262).

14. The coolant diverter (260) of any of the preceding claims, including a connector (261a) for joining a core cooling tube (270) thereto.

15. The coolant diverter (260) of claim 14, wherein the connector (261a) includes a threaded hole (261 a).

16. A core cooling tube (1270) for a preform mold, said core cooling tube comprising a coolant diverter (1260) according to any one of claims 1-13 integrally formed therewith.

17. The core cooling tube (1270) according to claim 16, including an open end (1273a), said open end (1273a) being shaped and configured to access a conical or dome-shaped inner surface of a core insert (250, 1250).

18. The core cooling tube (1270) according to claim 16, including an open end (1273a, 2273a) defined by a frustoconical or domed shape for directing cooling fluid to a conical or domed shaped inner surface of a core insert (250, 1250).

19. The core cooling tube (1270) according to any one of claims 16 to 18, comprising a plurality of spacer elements (1272c, 1273b, 2272c, 2273b, 3272c, 3273b) protruding from an outer surface of said core cooling tube (1270) for centering said core cooling tube (1270) within a core insert (250, 1250), wherein said spacer elements (1272c, 1273b, 2272c, 2273b, 3272c, 3273b) are axially spaced relative to each other along said core cooling tube (1270).

20. A core cooling tube (1270) according to any of claims 16 to 19 formed by an additive manufacturing process.

21. A core cooling tube (1270, 2270, 3270) for a preform mold (100), the core cooling tube (1270, 2270, 3270) comprising an inlet portion (1271, 2271, 3271) for receiving cooling fluid from a cooling circuit of a punch (210) and an outlet portion (1273, 2273, 3273a) having an open end (1273a, 2273a, 3273a) for directing cooling fluid to an inner surface of a core insert (250, 1250), wherein the open end (1273a, 2273a, 3273a) comprises an aperture (a) defining a flow area that is smaller than a flow area through the outlet portion (1273, 2273, 3273).

22. The core-cooling tube (1270, 2270, 3270) of claim 19, wherein said outlet portion (1273, 2273, 3273) tapers toward said open end (1273a, 2273a, 3273a) and is truncated to define said aperture (a).

23. The core cooling tube (1270, 2270, 3270) of claim 19 or 20, wherein said outlet portion (1273, 2273, 3273) comprises a truncated cone defining said aperture (a).

24. The core-cooling tube (1270, 2270, 3270) of claim 19 or 20, wherein said outlet portion (1273, 2273, 3273) includes a truncated dome (1273a, 2273a, 3273a) defining said aperture (a).

25. The core-cooling tube (1270, 2270, 3270) of claim 24, wherein said truncated dome (1273a, 2273a, 3273a) is substantially spherical or elliptical.

26. The core cooling tube (1270, 2270, 3270) according to any one of claims 21 to 25, wherein said aperture (a) is substantially circular or elliptical.

27. The core cooling tube (1270, 2270, 3270) of any of claims 21-26, wherein said open end (1273a, 2273a, 3273a) is shaped and configured to approximate a conical or dome-shaped inner surface of a core insert (250, 1250).

28. A core assembly comprising a core insert (250, 1250) and a core cooling tube (1270, 2270, 3270), the core insert (250, 1250) comprising a tubular molding portion (252, 1252), the tubular molding portion (252, 1252) defining a molding surface (252a) for molding a portion of a preform and having a closed end, wherein the core cooling tube (1270, 2270, 3270) comprises an outlet portion (1273, 2273, 3273) having an open end (1273a, 2273a, 3273a), the open end (1273a, 2273a, 3273a) being shaped and/or configured to approximate an inner surface of the closed end of the core insert (250, 1250).

29. The core assembly of claim 28, wherein the open end (1273a, 2273a, 3273a) includes an aperture (a) having a smaller flow area than a flow area through the outlet portion (1273, 2273, 3273).

30. The core assembly of claim 29, wherein the outlet portion (1273, 2273, 3273) tapers towards the open end (1273a, 2273a, 3273a) and is truncated to define the aperture (a).

31. The core assembly of any one of claims 28 to 30, wherein the outlet portion (1273, 2273, 3273) comprises a truncated cone defining the aperture (a).

32. The core assembly of any one of claims 28 to 30, wherein the outlet portion (1273, 2273, 3273) comprises a truncated dome (1273a, 2273a, 3273a) defining the aperture (a).

33. The core assembly of claim 32, wherein said truncated dome (1273a, 2273a, 3273a) is substantially spherical or elliptical.

34. The core assembly of any of claims 28 to 33, wherein the aperture (a) is substantially circular or elliptical.

35. A method of manufacturing a core cooling tube (1270, 2270, 3270) for a preform mold (100), the method comprising:

forming a coolant diverter (1260, 2260, 3260) comprising a body defining at least a portion of first and second cooling channels (261, 262, 263, 1261, 1262, 1263) for being received within a seat (215) in a punch (210), the first cooling channel (261, 262, 1261, 1262) comprising an inlet portion (262, 1262) for receiving cooling fluid from a cooling circuit (214a, 214b) of the punch (210) and an outlet portion (261, 1261) extending at an angle relative to the inlet portion (262, 1262), the second cooling channel (263, 1263) comprising an inlet for receiving cooling fluid from a core insert (250) and an outlet for delivering the cooling fluid to the cooling circuit (214a, 214b) of the punch (210); and

forming a core cooling tube (1271, 1272, 1273, 2271, 2272, 2273, 3271, 3272, 3273) including a first end connected to the outlet portion (261, 1261) of the coolant diverter (260, 1260, 2260, 3260) and a second open end (1273a, 2273a, 3273a) for directing the cooling fluid to a dome-shaped inner surface of the core insert (250);

wherein the coolant diverter (260, 1260, 2260, 3260) and the core cooling tube (1271, 1272, 1273, 2271, 2272, 2273, 3271, 3272, 3273) are integrally formed to provide a seamless unitary structure (1270, 2270, 3270).

36. The method of claim 35 including forming the coolant diverter (1260) with a locator (1267) for engaging a locator (214a) of the punch shoe (215) to align, in use, the inlet portion (1262) of the first cooling channel (1261, 1262) with the cooling circuit (214a, 214b) of the punch (210) when the diverter (1260) is received within the punch shoe (215).

37. The method of claim 36, wherein the locator (1267) includes a snap-fit connector (1267).

38. The method of any of claims 35-37, comprising forming the core cooling tube (1270, 2270, 3270) with a truncated dome to form the second open end (1273a, 2273a, 3273 a).

39. The method of any of claims 35 to 38, wherein the core cooling tube (1270) comprises a core cooling tube (1270) of any of claims 16 to 19.

40. The method of any of claims 35 to 39, including forming the coolant diverter (1260) as one or more spacers (1266, 2266, 2268, 3266, 3268) for engaging the boss (215) to center the outlet portion (1261, 2261, 3262) of the first cooling gallery (1261, 1262, 2261, 2262, 3261, 3262) therein.

41. The method according to claim 40, wherein the outlet portion (2261, 3261) of the first cooling channel (2261, 2262, 3261, 3262) is defined by a tubular or partially tubular portion (2263, 3263), and at least one of the spacers (2266, 2268, 3268, 3266) comprises a partial circumferential wall (2268, 3268) surrounding and spaced apart from at least a portion of the tubular or partially tubular outlet portion (2261, 3261) of the first cooling channel (2261, 2262, 3261, 3262).

42. The method of claim 40 or 41, wherein at least one of the spacers (1266, 2266, 2268, 3268, 3266) includes a fin (1266, 2266, 3266) protruding radially with respect to an outlet portion (1261, 2261, 3261, 3262) of the first cooling channel (1261, 1262, 2261, 2262, 3261).