GB2301308A - Parison moulding including cooling of the parison - Google Patents

Parison moulding including cooling of the parison Download PDF

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Publication number
GB2301308A
GB2301308A GB9614845A GB9614845A GB2301308A GB 2301308 A GB2301308 A GB 2301308A GB 9614845 A GB9614845 A GB 9614845A GB 9614845 A GB9614845 A GB 9614845A GB 2301308 A GB2301308 A GB 2301308A
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United Kingdom
Prior art keywords
cooling
parison
core rod
station
mould
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB9614845A
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GB9614845D0 (en
GB2301308B (en
Inventor
Paul Marcus
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Individual
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Individual
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Filing date
Publication date
Priority claimed from US08/282,530 external-priority patent/US5501593A/en
Application filed by Individual filed Critical Individual
Publication of GB9614845D0 publication Critical patent/GB9614845D0/en
Publication of GB2301308A publication Critical patent/GB2301308A/en
Application granted granted Critical
Publication of GB2301308B publication Critical patent/GB2301308B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C45/00Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
    • B29C45/03Injection moulding apparatus
    • B29C45/04Injection moulding apparatus using movable moulds or mould halves
    • B29C45/0408Injection moulding apparatus using movable moulds or mould halves involving at least a linear movement
    • B29C45/0416Injection moulding apparatus using movable moulds or mould halves involving at least a linear movement co-operating with fixed mould halves
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C45/00Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
    • B29C45/17Component parts, details or accessories; Auxiliary operations
    • B29C45/72Heating or cooling
    • B29C45/7207Heating or cooling of the moulded articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C49/00Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
    • B29C49/42Component parts, details or accessories; Auxiliary operations
    • B29C49/64Heating or cooling preforms, parisons or blown articles
    • B29C49/6409Thermal conditioning of preforms
    • B29C49/6427Cooling of preforms
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/07Preforms or parisons characterised by their configuration
    • B29C2949/0715Preforms or parisons characterised by their configuration the preform having one end closed
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C49/00Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
    • B29C49/02Combined blow-moulding and manufacture of the preform or the parison
    • B29C49/06Injection blow-moulding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2067/00Use of polyesters or derivatives thereof, as moulding material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/25Solid
    • B29K2105/253Preform

Landscapes

  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)

Abstract

A parison moulding apparatus includes an injection-moulding station 12 at which a first core rod assembly 22 a /22 b defines, with an injection-mould 18, a cavity into which molten resin under pressure is injected to form the parison, a cooling station 14 a /14 b with a cooling mould 36 a /36 b , indexing means 24 for moving the parison from mould 18 to cooling mould 36 a ,36 b and leaving it there to be cooled, an ejection station 16 a ,16 b for further cooling the parison and with means for ejecting the cooled parison and a further core rod assembly 22 b /22 a movable by means 24 to a cooling station 14 b ,14 a , when first assembly 22 a /22 b is returned to station 12, for further cooling of the parison and to remove it from a cooling station 14 b /14 a and transfer it to ejecting station 16 a /16 b when first assembly 22 a /22 b is moved to station 14 b /14 a . The first and second core rod assemblies have cooling means.

Description

Parison Mouldina Apparatus and Method The present invention is applicable to a two-staqe process by which parisons are produced in an injection mouldinq machine, cooled to room temperature, stored and later conveyed in bulk to a reheat, orientation - stretch and blow mouldinq machine. In this manner, oriented hollow plastic bottles are formed. Polyethylene teraphthalate (PET) is typical of the plastic material used.
Heretofore coolinq of parisons durinq the first staqe has been time consuminq, resultinq in inefficiency and poor productivity. However, sufficient coolinq is indispensable if the parisons are to maintain their shape durinq later handling operations. Techniques proposed to date for cooling parisons often times created bottlenecks downstream from the injection moulds thereby severely hamperinq productivity. Obviously, a high rate of production of parisons is important in commercial operation, and the rate at which the injection molding cycle can produce the parisons has been limited by the time taken to cool the parisons sufficient-ly to allow post molding handling without damage to the parison.
Typically, the hollow plastic parisons produced in the injection molding cycle have relatively thick walls and are molded with PET resin at relatively high temperatures. Consequently, after removal from the injection mold, the hollow parison must be cooled sufficiently to prevent deformation or adhesion to one another. However, the thick parison wall tends to trap heat. Cooling the parison in the injection mold by means of its contact with the cool mold surfaces quickly chills the inner and outer skin, but mold cooling will remove the heat trapped within the wall only by keeping the parison in the injection mold for an extended period of time. Naturally, this is economically prohibitive because high parison production is not feasible unless cooling in the injection mold is held at a minimum.
Initial cooling of the molded parison following formation may be sufficient to permit ejection from the injection mold, but additional cooling is then immediately required to remove additional heat as it is conducted to the skin. If the additional cooling were omitted the skin temperature would rise and cause the molded parisons to stick together, to become prone to surface damage, or to bend or warp.
Naturally this is unacceptable.
Many approaches have been proposed to alleviate these problems but they either were cost prohibitive, did not optimize injection molding cycles, required excessive parison handling or required cumbersome or highly inefficient dedicated equipment.
Summary of the Invention A principal object of the present invention is to provide a parison molding apparatus and method that is highly efficient, low in cost and that optimizes injection molding cycles thereby increasing parison production while at the same time providing adequate cooling of the molded parisons.
Another object is to provide a parison molding apparatus and method of the foregoing type that enables rapid operating cycles by parison injection molding without the necessity for extended cooling time in the injection mold but with extended cooling times outside the injection mold that may be increased many fold to arrive at the desired degree of parison cooling without affecting or detracting from the molding cycle or time.
In accordance with the proposed parison molding system a first parison is initially injection molded at an injection molding station about a first core rod assembly in an injection mold cavity defined with a female mold and a neck mold. This female mold, neck mold and core rod assembly possesses cooling means for cooling the molded parison. The first core rod assembly and neck mold then transports the slightly cooled parison to a first cooling station having a first cooling female mold and at which the first core rod assembly and neck mold remain with the first parison which is subject to further cooling. In this regard, the first core rod assembly may place the parison in intimate contact with the first cooling mold by a form of compression molding or by blowing the parison off the core rod into intimate contact with a slightly enlarged cavity wall of the cooling mold.A second core rod assembly and neck mold which were associated with a previously molded second parison at a second cooling station will be withdrawn from this second parison which will remain in a second cooling mold half and then moved to the injection molding station and associated with the injection mold. The withdrawal of the second core rod assembly and neck mold and insertion into the injection mold will occur simultaneously with retraction of the first core rod assembly and neck mold with the first molded parison and its transport and insertion into the first cooling mold at the first cooling station. The second-parison at the second cooling station then receives a third core rod assembly for further cooling of the second parison.
Upon the completion of the injection molding of the third parison at the injection molding station, the third core rod assembly is retracted with the second parison and moved to an ejection station at which the second parison is yet further cooled. The second core rod assembly and neck mold will transport the third parison to the second cooling station while the first core rod assembly and neck mold retracts from the first parison at the first cooling station and moves back to the injection molding station to mold a further parison. A fourth core rod assembly is inserted into the first parison at the first cooling station.Upon or shortly before completion of the injection molding of the fourth parison, the second cooled parison may be moved to yet another cooling station if needed or simply discharged or ejected at the ejection station if adequately cooled and deposited at a collection station. Simultaneously, the first parison will be placed at another ejection station for further cooling by the fourth core rod assembly. Thus, with all of the cooling steps established (at least 4) the injection molding cycle may be shortened to increase parison production several fold.
Other objects and advantages will become apparent from the following detailed description which is to be taken in conjunction with the accompanying drawings.
Brief Description of the Figures Figure 1 is a top plan view of a parison molding and cooling apparatus showing the press in a closed or clamped position; Figure 2 is a similar top plan view of the press opened; Figure 3 is a similar plan view with the press still opened but linearly shifted and indexed to the left to align a core rod assembly with the injection mold and align the other core rod assemblies as shown; Figure 4 is a similar plan view with the press clamped and the aligned core rod assembly inserted into the injection mold to start the next parison injection molding cycle.
Detailed Description of the Preferred Enibodiments In the drawings, a parison molding machine 10 is illustrated with one of a plurality of in-line stations, namely, a parison molding station 12, a pair of parison cooling stations 14a and 14b on opposite sides of the parison molding station 12 and a pair of parison cooling and ejection stations 16a and 16b spaced outwardly of the respective cooling stations 14a and 14b. As will be readily apparent one or more additional cooling stations may be interposed between stations 14a,b and 16a,b to increase the cooling time of the parison while maintaining the molding cycle constant and at a minimum timewise.
The parison molding station 12 includes a parison mold 18 mounted on clamping plate 20 and that cooperates with a pair of core rod assemblies 22a and 22b mounted on an axially and laterally shiftable indexing plate 24 in forming a parison. In each molding cycle, one of the core rod assemblies is disposed within the cavity of mold 18 for purposes of receiving the injected plastic shot from nozzle 26.
The core rod assemblies 22a and 22b include core rods 28a and 28b and associated split neck molds 30a and 30b. The mold 18, core rods 28a and 28b and neck molds 30a and 30b are temperature controlled and preferably cooled in a manner well known in the art by fluid (air, water or oil). For certain types of containers, a one-piece neck mold could be employed.
The choice of neck mold depends on the size and shape of containers being formed. The selected neck mold will remain in a closed position except at such time as it is desired to disassociate the core assembly 22a or 22b from the parison at the cooling stations 14a and 14b so that the free core assembly may be in a position to return to the parison injection molding station 12 to form another parison.
Upon reciprocation of the indexing plate 24 and assuming the relative position of the parts as shown in Figure 1, the parison mold 18 will be disposed about the core rod 28a into engagement with the closed neck mold 30a also disposed about the core rod 28a to define the parison forming cavity. The parison 34a is formed upon the injection through nozzle 26 into the cavity at the injection molding station 12 of the selected plastic under controlled pressure and temperature and with uniform density in a manner well known in the art.
The mold 18 is temperature controlled and preferably cooled by fluid (water or oil) in a manner well known in the art. The neck mold 30a is also cooled by fluid to set the configuration of the neck of the parison. The core rod 28a is similarly cooled by fluid. In this manner, a skin is formed on the outer and inner surfaces of the parison 34a. The cooling cycle time at the parison injection station 12 is held to a minimum to optimize the production of parisons.
At the relative disposition of the indexing plate 24 as shown in Figure 1, the previously molded parison 34b on core rod assembly 22b is disposed at the cooling station 14b. At this station, parison 34b is placed in cooling mold 36b which is cooled by fluid (water or oil). Thus, at cooling station 14b the parison 34b will be cooled by mold 36b and will continue to be cooled by core rod 28b and neck mold 30b for the duration of the injection molding cycle.
In this regard, the parison 34b may be in intimate contact with the core rod 28b and cooling mold 36b similar to a form of compression molding. However, as shown, the parison 36b is blown off the core rod 28b into intimate contact with the slightly enlarged core cavity surfaces of cooling mold 36b at the beginning of the cooling cycle. The previously molded and cooled parison 34c at the cooling station 14a will have been disassociated earlier from core rod assembly 22a and neck mold 30a. At the station 14a, parison 34c will continue to be cooled in mold 36a and by the engaged transfer core rod assembly 38a which can also be cooled by fluid (water or oil) in a manner similar to core rod assemblies 22a and 22b.
Again, the cooling at station 14a about core rod assembly 38a will be for the duration of the injection molding cycle. The core rod assembly 38a can be on indexing plate 24 or on a separate plate if it desired to remove the parisons further away from molding station 12 and cooling station 14a and 14b when they are transferred to ejection stations 16a and 16b. The earlier cooled and transferred parison 34d on transfer core rod assembly 38b will be at ejection station 16b at which the parison will be further cooled in mold 40b which is cooled by fluid (water or oil) while also being cooled on core rod assembly 38b. The previous parison 34e at ejection station 16a will be disassociated from core rod assembly 38a but further cooled in mold.At or near the end of the injection molding cycle, or certainly before core rod assembly 38a transfers parison 34c to station 16a, an ejection mechanism 42a will push or otherwise eject the parison 34e to a collection bin or station (not shown). As stated, one or more additional cooling stations similar to stations 14a and 14b may be interposed between these stations and ejection stations 16a and 16b to provide for further cooling of the parisons.
At the completion of the injection molding cycle, the indexing plate 24 is retracted to the position shown in Figure 2. As shown, parison 34a will be retracted with core rod assembly 22a and closed neck mold 30a. Prior to the retraction of plate 24, the neck mold 30b will have opened thereby permitting the open neck mold and core rod 28b to be retracted and leave remaining in mold 36b the parison 34b. In this regard, the core rod 28b may have air jets, ports or longitudinal channels or spaces as shown that with a blast of air, will free the parison 34b from the core rod 28b or suction through port 44b may be used for this purpose or be used in conjunction with the air jets. When the cooling mold is slightly larger than the outer dimensions of the parison, this freeing of the parison from the core rod into contact with the shield will occur at the beginning of the cooling cycle. The parison 34c is removed from mold 36a and retracted with transfer core rod assembly 38a. In this instance, pressurized air through port 44a, may be used to free parison 34c from mold 36a or even suction ports on core rod assembly 38a may be used for this purpose alone or in conjunction with air pressure through port 44a. The parison 34d will remain at station 16b and in mold 40b and be free of core rod assembly 38b; and this removal could be achieved or facilitated by air pressure passing through core rod assembly 38b or a plunger activated abutment 46b, shown in phantom, which is activated immediately before retraction of the indexing plate 24 and retracted thereafter. The parison 34e can be ejected at any time prior to transfer of parison 34c by core rod assembly 38a to station 16a.
The indexing plate 24 will then be shifted laterally so that core rod assembly 22b will be axially aligned with mold 18 at the injection molding station 12 and the other core rods will be aligned as shown in Figure 3. Even during this indexing step, the various parisons will be further cooled.
The indexing plate 24 will thereafter be reciprocated axially to place core rod assembly 22b with closed neck mold 30b in association with injection mold 18 as shown in Figure 4. Parison 34a will be placed in cooling mold 36a at station 14a while on core rod 28a and closed neck mold 30a. Core rod assembly 38b will be inserted in parison 34b while core rod assembly 38a will transfer parison 34c to ejection station 16a. During this indexing step, the various parisons will be further cooled. The next parison injection molding cycle will commence to form parison 34f. The indexing sequence previously described will be repeated to eventually associate core rod assembly 22a once again with the mold 18 of injection molding station 12.
As explained, at stations 14a and 14b, the space between the cooling cavity and outer parison wall allows the preform parison to be blown off the associated core rods 28a, 28b or separated from the core rods 28a, 28b. The blow air forces the parison against the wall of the cooling cavity to remove the heat from the plastic parison while freeing it from the core rod.
In those applications that do not have the parison blown off the core rod, the plastic parison is forced against the cooling cavity wall by the core rod by a form of compression molding. In this case, both the core rod and cooling cavity remove heat from parison. In this embodiment, the cooling cavity walls may not be tapered. They could be straight or have undercut rings to hold the parison in the cooling cavity when the core rod is withdrawing.
In a further embodiment, the present invention contemplates the cooling molds 36a and 36b being split or in two halves. In this case, the cooling cavity grabs and locks the parison to thereby cool it while allowing the core to be removed.
In all cases, a further cooling core assembly 38a, 38b enters the parison while it is cooling in the cooling cavity. This is a form of compression molding as well. The cooling core rod assembly 38a, 38b also remove heat. The cooling core rod assemblies 38a, 38b may have undercut rings or may be straight.
This allows the core rod assemblies 38a, 38b to grip the inside of the parison to pull it from cooling cavity. As the process proceeds, adequately cooled parisons will be collected without fear or concern over them sticking or distorting.
Although a single row of stations are illustrated in the drawings, it should be understood that multiple rows of such stations may be on the plates 20 and 24 not only in a horizontally disposed line as illustrated, but vertical or in parallel lines; and similarly, the plates 20 and 24 could be horizontally disposed rather than being vertical as shown where desired or necessary.
The cooled parisons may be transported to a blow-molding location where the parisons are reheated, seasoned, oriented and stretched and blow molded into the desired configuration.
Thus, the several aforenoted objects and advantages are more effectively attained. Although a single somewhat preferred embodiment has been disclosed in detail herein, it should be understood that the invention is in no sense limited thereby but its scope is to be determined by that of the appended claims.

Claims (9)

1. A parison injection mouldinq apparatus havinq shortened injection mouldinq cycles with extended cooling for increased parison production, comprisinq: a parison injection moulding station havinq a parison injection mould and a first core rod assembly defininq with the injection mould a cavity for forming the parison, means for introducinq into the cavity molten resin under pressure to form the parison, the injection mould and core rod assembly havinq cooling means for cooling the parison; at least one cooling station havinq a cooling mould;; indexing means for movinq the parison on the core rod assembly to the cooling station at which the parison is placed in the cooling mould by the core rod assembly for cooling the parison; the indexing means being operable to thereafter remove the core rod assembly from the parison and leave the parison in the cooling mould for further cooling and move the core rod assembly back to the injection mouldinq station; an injection station havinq a cooling mould for further cooling the parison and havinq means for ejectinq the cooled parison; another core rod assembly havinq cooling means; the indexing means being operable to move said another core rod assembly to the cooling station when the first core rod assembly is returned to the injection mouldinq station for further cooling of the parison and to remove the parison from the cooling station and transfer it to the ejection station when the first core rod is moved to the cooling station.
2. The invention in accordance with claim 1 wherein the mould cavity is further defined by a neck mould associated with the first core rod assembly for forming a neck on the parisons.
3. The invention in accordance with claim 2 wherein the injection mould, neck mould and core rod assembly havinq cooling means for cooling the parison at the injection mouldinq station.
4. The invention in accordance with claim 3 wherein the core rod assemblies and associated neck mould operate to cool the parisons thereon when moved to and while at the cooling station.
5. The invention in accordance with claim 1 wherein each of the cooling stations havinq a cooling mould for receivinq the parisons moved to the cooling stations by the respective core rod assemblies, the cooling moulds at each cooling station havinq cooling means for cooling the parisons at the cooling stations.
6. The invention in accordance with claim 1 wherein each of the ejection stations include means for ejectinq the parison from the respective ejection stations.
7. The invention in accordance with claim 6 wherein the mould cavity is further defined by a neck mould associated with the first core rod assembly for forming a neck on the parisons; the injection mould, neck mould and core rod assembly havinq cooling means for cooling the parison at the injection mouldinq station; the core rod assemblies and associated neck mould operate to cool the parisons thereon when moved to and while at the cooling stations; each of the cooling stations havinq a cooling mould for receivinq the parisons moved to the cooling stations by the respective core rod assemblies, the cooling mould at each cooling station havinq cooling means for cooling the parisons at the cooling stations.
8. The invention in accordance with claim 1 wherein a plurality of cooling stations are interposed between the injection mouldinq station and each of the ejection stations to increase parison cooling time while minimizinq the parison injection mouldinq cycle times.
9. The invention in accordance with claim 1 wherein the cooling mould is not substantially larqer than the parisons and the respective core rod assemblies blow the parison into intimate contact with the cooling mould and free the parison from the respective core rod assemblies.
GB9614845A 1994-07-28 1995-07-27 Parison moulding apparatus and method Expired - Fee Related GB2301308B (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/282,530 US5501593A (en) 1994-04-07 1994-07-28 Parison molding apparatus
GB9515426A GB2292108B (en) 1994-07-28 1995-07-27 Parison molding apparatus and method

Publications (3)

Publication Number Publication Date
GB9614845D0 GB9614845D0 (en) 1996-09-04
GB2301308A true GB2301308A (en) 1996-12-04
GB2301308B GB2301308B (en) 1997-12-17

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GB9614845A Expired - Fee Related GB2301308B (en) 1994-07-28 1995-07-27 Parison moulding apparatus and method

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0873840A1 (en) * 1997-04-22 1998-10-28 Inter Tooling Services B.V. Injection molding machine for manufacturing hollow plastic articles.
EP0982113A2 (en) * 1998-08-18 2000-03-01 Ventax Robot Inc. Handling and cooling system for plastic container preforms

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1592746A (en) * 1977-05-21 1981-07-08 Linde Ag Injection moulding
US4352777A (en) * 1979-01-24 1982-10-05 Valyi Emery I Method for forming hollow plastic objects
US4472131A (en) * 1979-12-03 1984-09-18 Ryder Leonard B Apparatus for injection molding of plastic preform
EP0167660A2 (en) * 1984-06-11 1986-01-15 Canada Cup, Inc. Injection blow molding process
US4950152A (en) * 1988-12-05 1990-08-21 Electra Form, Inc. Apparatus for producing preforms and blow molded articles
US5051227A (en) * 1988-12-05 1991-09-24 Electra Form, Inc. Production of preforms and blow molded articles

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1592746A (en) * 1977-05-21 1981-07-08 Linde Ag Injection moulding
US4352777A (en) * 1979-01-24 1982-10-05 Valyi Emery I Method for forming hollow plastic objects
US4472131A (en) * 1979-12-03 1984-09-18 Ryder Leonard B Apparatus for injection molding of plastic preform
EP0167660A2 (en) * 1984-06-11 1986-01-15 Canada Cup, Inc. Injection blow molding process
US4950152A (en) * 1988-12-05 1990-08-21 Electra Form, Inc. Apparatus for producing preforms and blow molded articles
US5051227A (en) * 1988-12-05 1991-09-24 Electra Form, Inc. Production of preforms and blow molded articles

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0873840A1 (en) * 1997-04-22 1998-10-28 Inter Tooling Services B.V. Injection molding machine for manufacturing hollow plastic articles.
NL1005872C2 (en) * 1997-04-22 1998-10-29 Inter Tooling Services Bv Injection molding machine for injection molding preforms for plastic bottles and similar containers.
US6095788A (en) * 1997-04-22 2000-08-01 Inter Tooling Services B.V. Injection molding machine for manufacturing hollow plastic articles
EP0982113A2 (en) * 1998-08-18 2000-03-01 Ventax Robot Inc. Handling and cooling system for plastic container preforms
EP0982113A3 (en) * 1998-08-18 2001-07-11 Ventax Robot Inc. Handling and cooling system for plastic container preforms
US6296473B1 (en) 1998-08-18 2001-10-02 Ventax Robot Inc. Handling and cooling system for plastic container preforms

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Publication number Publication date
GB9614845D0 (en) 1996-09-04
GB2301308B (en) 1997-12-17

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