CA2303766A1 - Method for producing multi-layered preforms - Google Patents
Method for producing multi-layered preforms Download PDFInfo
- Publication number
- CA2303766A1 CA2303766A1 CA002303766A CA2303766A CA2303766A1 CA 2303766 A1 CA2303766 A1 CA 2303766A1 CA 002303766 A CA002303766 A CA 002303766A CA 2303766 A CA2303766 A CA 2303766A CA 2303766 A1 CA2303766 A1 CA 2303766A1
- Authority
- CA
- Canada
- Prior art keywords
- component
- jet chamber
- needle
- cycle
- shut
- 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.)
- Abandoned
Links
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 10
- 230000004888 barrier function Effects 0.000 claims abstract description 38
- 239000010410 layer Substances 0.000 claims abstract description 36
- 238000001746 injection moulding Methods 0.000 claims abstract description 16
- 239000004033 plastic Substances 0.000 claims abstract description 9
- 229920003023 plastic Polymers 0.000 claims abstract description 9
- 239000002344 surface layer Substances 0.000 claims abstract description 9
- 239000000463 material Substances 0.000 claims description 121
- 238000000034 method Methods 0.000 claims description 35
- 239000000945 filler Substances 0.000 claims description 22
- 230000007246 mechanism Effects 0.000 claims description 13
- 238000001816 cooling Methods 0.000 claims description 6
- 239000004677 Nylon Substances 0.000 claims description 5
- 229920001778 nylon Polymers 0.000 claims description 5
- 230000000903 blocking effect Effects 0.000 claims description 3
- 230000006835 compression Effects 0.000 claims 2
- 238000007906 compression Methods 0.000 claims 2
- 235000013361 beverage Nutrition 0.000 description 8
- 238000007796 conventional method Methods 0.000 description 5
- 238000002347 injection Methods 0.000 description 5
- 239000007924 injection Substances 0.000 description 5
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 4
- 229910052760 oxygen Inorganic materials 0.000 description 4
- 239000001301 oxygen Substances 0.000 description 4
- 230000009471 action Effects 0.000 description 3
- 230000035515 penetration Effects 0.000 description 3
- 230000002349 favourable effect Effects 0.000 description 2
- 239000008187 granular material Substances 0.000 description 2
- 230000000149 penetrating effect Effects 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 238000005303 weighing Methods 0.000 description 2
- 241000272470 Circus Species 0.000 description 1
- 229920000219 Ethylene vinyl alcohol Polymers 0.000 description 1
- 239000004952 Polyamide Substances 0.000 description 1
- 238000000071 blow moulding Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- UFRKOOWSQGXVKV-UHFFFAOYSA-N ethene;ethenol Chemical compound C=C.OC=C UFRKOOWSQGXVKV-UHFFFAOYSA-N 0.000 description 1
- 239000004715 ethylene vinyl alcohol Substances 0.000 description 1
- 238000010101 extrusion blow moulding Methods 0.000 description 1
- 239000010408 film Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000011065 in-situ storage Methods 0.000 description 1
- 229920003207 poly(ethylene-2,6-naphthalate) Polymers 0.000 description 1
- 229920002647 polyamide Polymers 0.000 description 1
- 239000004417 polycarbonate Substances 0.000 description 1
- 229920000515 polycarbonate Polymers 0.000 description 1
- 239000011112 polyethylene naphthalate Substances 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 239000012815 thermoplastic material Substances 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C45/00—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
- B29C45/16—Making multilayered or multicoloured articles
- B29C45/1642—Making multilayered or multicoloured articles having a "sandwich" structure
- B29C45/1646—Injecting parison-like articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C45/00—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
- B29C45/16—Making multilayered or multicoloured articles
- B29C45/1603—Multi-way nozzles specially adapted therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C45/00—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
- B29C45/16—Making multilayered or multicoloured articles
- B29C45/1642—Making multilayered or multicoloured articles having a "sandwich" structure
- B29C45/1643—Making multilayered or multicoloured articles having a "sandwich" structure from at least three different materials or with at least four layers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C45/00—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
- B29C45/16—Making multilayered or multicoloured articles
- B29C45/1642—Making multilayered or multicoloured articles having a "sandwich" structure
- B29C45/1646—Injecting parison-like articles
- B29C2045/1648—Injecting parison-like articles the parison core layer being a barrier material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C45/00—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
- B29C45/16—Making multilayered or multicoloured articles
- B29C45/1642—Making multilayered or multicoloured articles having a "sandwich" structure
- B29C2045/1656—Injecting the skin material through the central passage of the multiway nozzle
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C45/00—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
- B29C45/17—Component parts, details or accessories; Auxiliary operations
- B29C45/26—Moulds
- B29C45/27—Sprue channels ; Runner channels or runner nozzles
- B29C45/28—Closure devices therefor
- B29C45/2806—Closure devices therefor consisting of needle valve systems
- B29C2045/2872—Closure devices therefor consisting of needle valve systems with at least three positions, e.g. two different open positions to control the melt flow
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/07—Preforms or parisons characterised by their configuration
- B29C2949/081—Specified dimensions, e.g. values or ranges
- B29C2949/0811—Wall thickness
- B29C2949/0819—Wall thickness of a layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/07—Preforms or parisons characterised by their configuration
- B29C2949/0861—Other specified values, e.g. values or ranges
- B29C2949/0872—Weight
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/30—Preforms or parisons made of several components
- B29C2949/3008—Preforms or parisons made of several components at neck portion
- B29C2949/3009—Preforms or parisons made of several components at neck portion partially
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/30—Preforms or parisons made of several components
- B29C2949/3012—Preforms or parisons made of several components at flange portion
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/30—Preforms or parisons made of several components
- B29C2949/3016—Preforms or parisons made of several components at body portion
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/30—Preforms or parisons made of several components
- B29C2949/302—Preforms or parisons made of several components at bottom portion
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/30—Preforms or parisons made of several components
- B29C2949/3024—Preforms or parisons made of several components characterised by the number of components or by the manufacturing technique
- B29C2949/3026—Preforms or parisons made of several components characterised by the number of components or by the manufacturing technique having two or more components
- B29C2949/3028—Preforms or parisons made of several components characterised by the number of components or by the manufacturing technique having two or more components having three or more components
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/30—Preforms or parisons made of several components
- B29C2949/3024—Preforms or parisons made of several components characterised by the number of components or by the manufacturing technique
- B29C2949/3026—Preforms or parisons made of several components characterised by the number of components or by the manufacturing technique having two or more components
- B29C2949/3028—Preforms or parisons made of several components characterised by the number of components or by the manufacturing technique having two or more components having three or more components
- B29C2949/303—Preforms or parisons made of several components characterised by the number of components or by the manufacturing technique having two or more components having three or more components having more than three components
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2949/00—Indexing scheme relating to blow-moulding
- B29C2949/30—Preforms or parisons made of several components
- B29C2949/3032—Preforms or parisons made of several components having components being injected
- B29C2949/3034—Preforms or parisons made of several components having components being injected having two or more components being injected
- B29C2949/3036—Preforms or parisons made of several components having components being injected having two or more components being injected having three or more components being injected
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING 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
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/25—Solid
- B29K2105/253—Preform
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Mechanical Engineering (AREA)
- Injection Moulding Of Plastics Or The Like (AREA)
- Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)
Abstract
The inventive method for producing multilayered preforms makes it possible to create extremely thin layers, especially a thin surface layer and/or a thin barrier layer. These thin layers are at the most 35 % and 5 % respectively of the overall volume. They are produced using a multi-component injection moulding form tool which is operated in such a way that the plastic component provided for creating the thin layers is conveyed through the innermost jet chamber. Said plastic component has a slightly higher temperature and is therefore slightly viscous. Preforms produced in this way are characterised by a surface layer representing less than 35 vol. % or a barrier layer representing approx. 5 vol. %.
Description
(Certification copy]
Method for producing multi-layered preforms The invention under consideration concerns a method according to the preamble of Claim 1 and the preforms produced by said method.
Particularly, the invention under consideration concerns a method which is suitable for producing three-layered preforms which show an increased recycled material content, allowing preforms to be produced with an improved barrier action against oxygen penetration.
Multi-layered preforms have been known for some time now and find usage in, amongst others, the beverage industry which produces plastic bottles from these preforms in situ which are then filled with the beverage concerned. Chiefly, such beverage bottles are manufactured from PET, although they may be produced from other thermoplastic materials such as PEN, polyamide, polycarbonate, etc.. Manufacturing plants of this type today produce 48 three-layered preforms per operating cycle by means of sequential injection moulding, amounting to an annual capacity of approx. 50 million units. In producing such preforms, new material is injected into the mould of the form tool in the first instance, followed by cleaned, prepared recycled material and, during a third stage in production, new material is injected again in order to rid the injection moulding nozzle of recycled material. Care is taken here to ensure that the tolerance on metering out individual injection quantities is kept as low as possible. Such accuracy in metering is a prerequisite for producing beverage bottles which show a high recycled material content as recycled material may not come into direct contact with the bottled beverage itself.
Legal requirements stipulate this. When stretch blow moulding preforms into PET bottles, it must be ensured therefore that the inner layer of recycled material remains coated throughout by a layer of new material, a fact that places tough demands on Wn 99/2'2926 3 PCT/CA98/00471 both the construction of injection moulding tools and on preform manufacturing plants. Unfortunately, the injection moulding machines we know today do not show the high levels of metering accuracy required for producing PET preforms which show a high recycled material content. As EP 0'655'306 confirms, it is for these reasons that PET bottles in use today generally show a recycled material content of, at best, only 25 %.
It is the aim of the beverage industry, however, to achieve a higher recycled material content on principle, for reasons both of cost and cost stability. Particularly, as regards ecological balance, the costs involved in producing returnable bottles fabricated from PET with 35 % recycled material are nearing those for non-returnable disposable bottles ("breakeven point"). An increased recycled material content would thereby increase the economic efficiency of re-useable PET bottles.
Essentially, the level of economic efficiency depends on the wildly fluctuating price of new PET granules. If such granules are cheaper than recycled material, single-layer preforms fabricated from 100 % new material may be produced more cheaply, yet if the price rises above this breakeven point, three-layered preforms which show a recycled material content of 35 % and above are favourable. A higher recycled material content also results in improved price stability as the wild fluctuations seen in the price of new material will make a proportional difference only in those preforms using recycled PET. Cost implications for the manufacturer and the bottling firm are thus more favourable.
It is for this reason that is has already been suggested (Modern Plastics International, February 1997, page 29) that a co-extrusion blow moulding tool be used in the production of PET preforms and that product parts produced independently of one another be linked together. PET bottles which show a recycled material content of up to 80 % have been produced in this manner. A method of this type does, however, require additional tools and is proving to be complex and cost-intensive.
It is the aim of the beverage industry to produce formed bodies which meet with the law and show a high recycled material content without resorting to expensive technical measures.
The resulting technical problem is thus the way in which preforms can be produced with extremely thin layers of new material and without the use of expensive structures in order that the recycled material content of these preforms can be increased.
Particularly, the aim is to produce three-layered preforms which show at least one layer which is as thin as possible or a recycled material content of over 35 vol. %, particularly of 35.
to 65 vol. %, by means of a simple procedure.
According to Claim l, the solution to this problem lies in a surprisingly simple method for operating a multi-component injection moulding form tool and, particularly, in reversing the conventional arrangement for the supply of components A and B and operating the form tool in such a way that, in the first step in the cycle, the shut-off needle is brought into a position, wherein both the inner and the outer jet chambers are opened such that conveyance of component B through the outer jet chamber is stopped and only component A is injected into the mould cavity through the inner jet chamber.
In producing preforms which show a high recycled material content, the first component to be injected, component A (new material), is thus directed through the inner jet chamber to form a thin surface layer and the other component to be injected, component B (recycled material), is directed via the outer jet chamber to form a layer of filler. When injection moulding a three-layered preform of this type, in the first step in the cycle, the shut-off needle is brought into position I, wherein both the outer jet chamber containing component B
and the inner jet chamber containing component A are opened.
With the needle in this position, conveyance of component B is interrupted and component A is injected into the mould cavity.
WO 99/2x926 5 PCT/CH98/00471 In the second step in the cycle, the shut-off needle is brought into t~e outer jet chamber opened. With the needle in this position, conveyance of component A is interrupted and component B is inject into the mould cavity. The position of the shut-off needle re ins unchanged for the next step in the cycle, the so-called ho ing phase, during which time shrinkage of component H due to cooling is replaced. Once the holding phase is aver, the shut- ff needle is brought into closing position III, wherein both th inner and outer jet chambers are closed.
It proves surprising that, uring the next mould cycle, the first injection shot using co onent A is free from undesirable material H. This unexpected resu can be explained by the reversal of the admission channels, articularly, a small reduction in the viscosity of componen A (new material) is achieved through the specific manner in ich the individual components are conveyed, i.e. conveyance of omponent A through the slightly warmer inner jet chamber. Tn cont st to preforms produced using conventional methods of injection ulding, preforms with a thin surface layer (component A) can a created according to the inventive method and the relative prop tion of filler material can be increased by component B materia - 5~
(AMENDED SHEET J
(pg.4, 4aJ
... position I, wherein both the outer jet chamber containing component B and the inner jet chamber containing component A
are opened. With the needle in this position, conveyance of component B is interrupted and component A is injected into the mould cavity. In the second step in the cycle, the shut-off needle is brought into position II, wherein the inner jet chamber is closed and the outer jet chamber opened. With the needle in this position, conveyance of component A is interrupted and component B is injected into the mould cavity.
The position of the shut-off needle remains unchanged for the next step in the cycle, the so-called holding phase, during which time shrinkage of component B due to cooling is replaced.
Once the holding phase is over, the shut-off needle is brought into closing position III, wherein both the inner and outer jet chambers are closed.
It proves surprising that, during the next mould cycle, the first injection shot using component A is free from undesirable material B. As described bY way of example in EP 0 768 163 or EP 0 380 215 all methods known toda use material A in to in up, i.e. to replace material shrunk during cooling- This result, unexpected even to the specialist, can be explained by the reversal of the admission channels. Particularly, a small reduction in the viscosity of component A (new material) is achieved through the specific manner in which the individual components are conveyed, i.e. conveyance of component A through the slightly warmer inner jet chamber. In contrast to preforms produced using conventional methods of injection moulding, preforms with a thin surface layer (component A) can be created according to the inventive method and the relative proportion of filler material can be increased by component B material being loaded into the mould cavity during the holding pressure phase.
b Moreover, the inventive method also allows preforms which show an extremely thin barrier layer (e.g, of nylon or similar) to be produced. Harrier layers of this type serve the purpose of minimising the degree of oxygen penetration within the formed bodies (bottles) and are comparatively expensive. In order to create a preform with a thin barrier layer accarding to the invention, the conventional arrangement of admission channels is again reversed and the barrier material to be injected to form the thin barrier layer is directed through the innermost jet chamber and the plastic forming the surface layer is fed through the outer jet chamber. When injection moulding a preform of this type, in the first step in the cycle, again the shut-off needle is brought into position I, wherein both the w0 99/22926 6 PCT/CH98/00471 outer and inner jet chambers are opened and the component directed through the outer jet chamber is injected into the mould cavity in the first step in the procedure, while at the same time conveyance of the barrier material directed through the inner jet chamber is interrupted. The shut-off needle remains in position I for the next step in the cycle and the barrier material conveyed through the inner jet chamber is loaded into the mould cavity at the same time as the filler material fed through the outer or central jet chamber. During this phase in injection moulding, both components (filler and barrier material) are thus conveyed at the same time, i.e. by means of tubes lying inside one another, thereby ensuring that the proportion of conveyed barrier material remains extremely low, e.g. making up 5 ~ of the overall injected material volume. The filler material and the material forming the surface layer may therefore be one and the same. Preferably, a relatively inexpensive recycled material is used for the filler material. This may be achieved in a well-known and simple manner by controlling the supply of molten plastics. In a third step in the cycle, conveyance of the barrier material is stopped once more and the filled mould cavity is further loaded with the amount of filler material required to compensate for shrinkage. By throwing the shut-off needle forward into position III, both jet chambers are closed and the mould cycle completed. The thin barrier layer lies in the central wall structure of the preform in all preforms produced in this manner. It is observed that preforms and formed bodies with layers arranged in such a manner provide the required barrier action against oxygen penetration within such containers.
Other embodiments of the inventive method are characterised by the features cited in the subclaims. Preforms created according to the inventive method of operation show a recycled material content of over 35 vol. % and, where necessary, a barrier layer material content of less than 5 vol. o.
The invention shall be described in further detail hereinafter with reference to an example. The illustrations given hereinafter show:
Wb 99/22926 7 PCT/CH98/00471 Figure 1: cross section through a hot runner nozzle and associated needle shut-off mechanism thereof;
Figure 2a to 2d: positions and control of the needle shut-off arrangement;
Figure 3: longitudinal section through a preform produced in the conventional manner;
Figure 4: longitudinal section through a preform produced according to the inventive method showing a high recycled material content;
Figure 5: longitudinal section through a preform produced according to the inventive method showing a barrier layer.
Figure 1 shows a section taken from the structure of a co-injection form tool used for two different components, A and B, complete with a hot runner nozzle 34 and a needle shut-off mechanism 36. The material melted in the extruders lands in the hot runner manifold block 15 via separate runners, is ramified therein and fed into the individual hot runner nozzles 34. Each of these hot runner nozzles 34 features a removable nozzle holder 33 and is constructed from several nozzle inserts lying inside one another between which one inner jet chamber 3 and at least one outer jet chamber 5 are created, through which the various synthetic components are fed up to the nozzle point.
Heating elements keep both the hot runner manifold block 15 and the nozzle holder 33, and thereby the hot runner nozzle 34, at the required temperature. A pneumatic needle shut-off mechanism 36 controls a movable needle 37 located near the point of the hot runner nozzle 34 in order to release or block individual components A or B and/or C.
In the conventional method of operation, the shut-off needle 37 is brought into four different positions during the course of one mould cycle in order to, by way of example, fill a cavity with three layers. In the first position, the needle 37 is drawn backwards only as far as is required to load the cavity with the first component, particularly original PET or raw material, via the outer jet chamber 5. In the second position, the needle 37 is drawn further backwards such that the second component, e.g. recycled PET, can also be pressed into the mould cavity via the inner jet chamber 3 before the needle 37 is nudged back into its intitial position for the holding phase and then nudged all the way forward in order to close the nozzle 34. The shut-off needle is therefore brought into four different positions during the course of one mould cycle, that is in order to a) open the outer jet chamber 5, b) open the inner jet chamber 3, c) close the inner jet chamber 3 and d) close the outer jet chamber 5.
As shown in Figure 1, the needle shut-off mechanism 36 is lodged in a groove on the top plate 13 which acts as a pneumatic cylinder and comprises the first plunger 38 which guides the needle 37, above which a second, flexible plunger 39 is fitted. A hermetical cylinder cover 40 seals off this groove so that it is compression-proof. Suitably arranged pressure pipes 41, 43 and 44 allow the individual plungers, and therefore the needle 37, to be brought into the desired position. Each of the individual pressure pipes presents the pressure required to move the needle. Usually, the outer pressure pipe 44 is pressurized to 20 bar, the central pressure pipe 43 to 10 bar and the inner pressure pipe 41 to 5 bar. The positioning of the individual plungers 38 and 39 shown in Figure 1 is achieved when the individual pressure pipes are pressurized as stipulated above. Should the needle 37 be drawn backwards into its initial position in order to release the first synthetic component in the conventional manner, the pressure in the central pressure pipe 43 simply needs to be raised or reduced accordingly. With that, the first plunger 38 moves up to the stop of the second plunger 39 due to the force of the pressure in the~inner pressure pipe 41. To bring the needle 37 into the second position which opens up the supply of the second synthetic component via the inner jet chamber, the pressure in the outer pressure pipe 44 is raised or reduced analogously. This results in the two plungers 38, 39 moving together up to the cylinder cover 40. To stop the supply of material once more, first the outer pressure pipe 44 is re-pressurized and with that the two plungers 38, 39 move together in the closing direction. Likewise, only when the central pressure pipe 43 is re-pressurized also can the outer jet chamber be interrupted by the movement of the first plunger 38.
Compression-proof seals 51 and 52 are fitted on each individual plunger together with the seals 53 on the cylinder cover 40, ensuring that the pneumatic needle shut-off mechanism.36 works perfectly. An end seal 55 is also fitted in the nozzle holder 33 preventing pressure compensation occurring between the plunger arrangement 38, 39 and the nozzle arrangement 33, 34 and thus preventing pressurized steam penetrating along the needle 37 through the nozzle holder 33 from the individual, heated synthetic components, condensing on the walls of the plunger or on the nozzle needle and affecting or blocking the movability of the individual components in the needle shut-off mechanism 36. This is achieved in a well-known manner by the use of a gastight end seal 55 fabricated from temperature-resistant plastic.
According to the invention, to be able to produce multi-layered preforms which show an increased recycled material content or extremely thin layers using a multi-component injection moulding form tool of this type, the conventional arrangement for supplying components A and B is reversed and operated in such a way that component A is conveyed in the inner jet chamber 3 of the hot runner nozzle 34 together with only the material to be loaded to form a thin layer (new or barrier material) while component B is conveyed, together with the recycled material to be loaded, in the outer or central jet chamber 5 of the hot runner nozzle 34. Should a formed body be produced which shows a thin outer skin fabricated from new material as well as a thin barrier layer, new material is conveyed in the outermost of the three jet chambers, and the material forming the barrier layer in the innermost chamber, in such a manner that the material forming the barrier layer is squirted out of the central jet chamber at the same time as the filler material. When producing formed bodies which show a thin barrier layer fabricated from one single base material, in the first step an initial portion of base material is injected into the mould cavity through the outermost of the two jet chambers and, in the second step, both base material and barrier material are injected into the mould cavity at the same time, i.e. by means of tubes lying inside one another. The needle 37 is thus brought into the positions as explained in further detail hereinafter with reference to Figures 2a to 2d.
Figures 2a to 2d show partial sections through the hot runner nozzle 34, complete with the associated needle shut-off mechanism 36 thereof. As shown in Figure 2a, the needle 37 is drawn backwards as far as is required to release the inner jet chamber in order to load the original component A conveyed via this inner jet chamber 3. By interrupting conveyance of component B and conveying component A, the required quantity of the original material A can be loaded into the mould cavity. As the original material A inside the hot runner nozzle 34 is shown to be less viscous than the filler material B in the outer jet chamber 5, it is sufficient to load only a small portion of the original material A into the mould cavity. This position of the needle, position I, can be achieved by reducing the pressure in pressure pipes 44 and 43 above the second plunger 39, or between the first plunger 38 and the second plunger 39, to 0 bar, for example, while building up the pressure in the pressure pipe 41 below the first plunger 38 to 6 bar, for example. Using this distribution of compressive forces, the two plungers find their highest possible position and the needle 37 thereby releases the inner jet chamber 3.
In the second step in the cycle as shown in Figure 2b, the needle 37 is brought into position II, wherein the inner jet chamber 3 is closed but the outer jet chamber 5 remains open.
This is achieved by maintaining the pressure in the pressure pipe 41 at 6 bar, for example, while raising the pressure in the pressure pipe 44 above the second plunger 39 a little, to bar, for example. In this position, component B (filler material) is conveyed into the mould cavity through the outer jet chamber 5. This material is more viscous than that out of the inner jet chamber 3 and it thus displaces the previously injected component A forming a thin film on the outer surfaces of the mould cavity, without penetrating the film. This difference in viscosity allows preforms to be produced with a thin outer skin. In the third step in the cycle, the mould cavity filled with the filler material B remains pressurized for a period, i.e. during the so-called holding phase, in order to compensate for any material volume lost through shrinkage.
Figure 2c shows the hot runner nozzle 34 and the needle shut-off mechanism 36 thereof in position III, wherein both the inner jet chamber 3 and the outer jet chamber 5 are closed.
This is achieved by reducing the pressure in the pressure pipe 41 below the first plunger 38 to 0 bar, for example, and raising the pressure in the pressure pipe 43 between the two plungers to 6 bar, for example, at the same time while keeping the pressure in the pressure pipe 44 above the second plunger 39 at 10 bar, for example.
Conventionally, and without reversed delivery channels for components A and B, the mould cycle starts with the needle in the position shown in Figure 2b in order to load component A
(new material) into the mould cavity. The shut-off needle 37 is subsequently brought into position I to fill the mould cavity with component B (filler material). As shown in Figure 2d, the needle is brought back into position II for the holding phase in order to replace material shrunk due to cooling with component A and to ensure that component B (recycled material) does not land in the cavity first during the next mould cycle.
To complete the cycle the needle is brought into position III, as shown in Figure 2c.
\ WU 99/22926 12 PCT/CH98/00471 It is thus clear that in the method of operation under consideration, the mould cycle is completed when filler material shrinkage is replaced with the same component, while conventionally the volume of material shrinkage is replaced with whichever component is to be injected first during the next mould cycle. In the method under consideration, component B (recycled material) may be loaded repeatedly into the mould cavity but surprisingly it is observed that it is only component A, in fact, which lands in the mould cavity due to the lower viscosity of component A fed through the inner jet chamber and because conveyance of component B is interrupted at the beginning of the next mould cycle; it is in this manner that the tough requirements demanded by the beverage industry can be met as regards blow-moulded bodies which show an intact, outer or inner skin.
The longitudinal sections shown in Figures 3 and 4 make clear the distinction between the inventive method and the conventional method. Figure 3 shows a longitudinal section through a preform produced in the conventional manner with a threaded section 61 and a barrel section 62, the sprue 63 thereof lying in the bottom section 64. From this longitudinal section it is also evident that neither the inner skin 65 nor the outer skin 66 (except at sprue) is penetrated at any point by the filler material B. Particularly critical points here are the deformations in the threaded section 61 of the preform. In addition, this illustration makes clear the manner in which the volume of filler material shrunk during the holding phase is replaced with new material A. Particularly, the percentage of recycled material used is substantially reduced by this new material being additionally loaded into the bottom section 64.
In contrast, Figure 4 shows a longitudinal section through a preform produced according to the inventive method.
Essentially, this differs in the structure of the bottom section 64 which shows just three layers, namely an inner skin, filler material and an outer skin. Moreover, a fundamental distinction is shown in the thickness of the individual layers.
Conventional preforms weighing 48.0 g with an overall wall thickness of 4.37 mm which are suitable for 1.5 litre bottles have an outer skin with a thickness of 1.3 to 1.5 mm. This results in a volume percent of 25 to 33 vol. o as regards the innerlying filler material. In the case of preforms also weighing 48.0 g produced according to the inventive method as shown in Figure 4, the outer material 65, 66 shows a thickness of 1.2 to 0.6 mm, therefore allowing the percentage of filler material to be increased to 37 to 63 vol. s through the application of this particular method of manufacture.
By reversing the admission channels, preforms can also be produced with a barrier layer (e. g. of nylon, EVOH or similar) which shows an improved barrier action against oxygen. This shall be explained in further detail with reference to Figures 2a to 2c. According to the inventive method, during the production of preforms with a barrier layer, the needle 37 is brought into position II (Figure 2b) in the first step in the cycle in order to fill the cavity with material used for the surface layer. In the second step in the cycle, the shut-off needle 37 is brought into position I (Figure 2a) and the barrier material (e.g. nylon) conveyed through the inner jet chamber 3 is injected into the mould cavity together with the component fed through the outer jet chamber 5. Barrier material therefore ends up lying in the inner wall structure of the preform allowing the formed body to be provided with an extremely thin barrier layer of approx. 5 vol. o or less.
In a preferred embodiment, the barrier material is directed through the innermost jet chamber and the method allows the needle 37 to be brought into position I in the first step in the cycle, wherein both the inner and the outer jet chambers are opened but only the material directed through the outer jet chamber 5 is conveyed into the mould cavity while conveyance of the material directed through the inner jet chamber 3 is stopped. The needle 37 remains in position I for the second step in the cycle and material is conveyed through the outer jet chamber 5 at the same time as the barrier layer material conveyed through the inner jet chamber 3, resulting in a barrier material content of approx. 5 s or less of the overall injected material. To compensate for material shrinkage during the holding phase, the shut-off needle remains in position I
and conveyance of the barrier material conveyed through the inner jet chamber 3 is suspended. Following successful loading, the needle is brought into position III (Figure 2c) in order to close the inner and outer jet chambers. Preforms produced in this manner show a thin barrier layer which lies in the central wall structure of the preform.
The advantages shown by the inventive method and by the preforms created according to this method are immediately obvious to the specialist. Particularly, the conventional method requires four needle positions in succession for each mould cycle whereas the inventive method requires only two or three needle positions. This simplifies control of the needle shut-off mechanism. Moreover, according to the invention, shrinkage in component B is replaced with the same material, increasing the percentage of this component (recycled material) or lowering the percentage of the component fed through the innermost jet chamber. The acquisition of new and expensive machines or tools is not required to put the inventive method into practice.
Further developments, particularly those affecting the viscosity of individual components and those used in controlling the mould cycle, lie within the normal capacities of a person skilled in the art. It is understood that all plastics used in injection moulding technology, especially nylon, and not only PET material, may be processed using this method.
Method for producing multi-layered preforms The invention under consideration concerns a method according to the preamble of Claim 1 and the preforms produced by said method.
Particularly, the invention under consideration concerns a method which is suitable for producing three-layered preforms which show an increased recycled material content, allowing preforms to be produced with an improved barrier action against oxygen penetration.
Multi-layered preforms have been known for some time now and find usage in, amongst others, the beverage industry which produces plastic bottles from these preforms in situ which are then filled with the beverage concerned. Chiefly, such beverage bottles are manufactured from PET, although they may be produced from other thermoplastic materials such as PEN, polyamide, polycarbonate, etc.. Manufacturing plants of this type today produce 48 three-layered preforms per operating cycle by means of sequential injection moulding, amounting to an annual capacity of approx. 50 million units. In producing such preforms, new material is injected into the mould of the form tool in the first instance, followed by cleaned, prepared recycled material and, during a third stage in production, new material is injected again in order to rid the injection moulding nozzle of recycled material. Care is taken here to ensure that the tolerance on metering out individual injection quantities is kept as low as possible. Such accuracy in metering is a prerequisite for producing beverage bottles which show a high recycled material content as recycled material may not come into direct contact with the bottled beverage itself.
Legal requirements stipulate this. When stretch blow moulding preforms into PET bottles, it must be ensured therefore that the inner layer of recycled material remains coated throughout by a layer of new material, a fact that places tough demands on Wn 99/2'2926 3 PCT/CA98/00471 both the construction of injection moulding tools and on preform manufacturing plants. Unfortunately, the injection moulding machines we know today do not show the high levels of metering accuracy required for producing PET preforms which show a high recycled material content. As EP 0'655'306 confirms, it is for these reasons that PET bottles in use today generally show a recycled material content of, at best, only 25 %.
It is the aim of the beverage industry, however, to achieve a higher recycled material content on principle, for reasons both of cost and cost stability. Particularly, as regards ecological balance, the costs involved in producing returnable bottles fabricated from PET with 35 % recycled material are nearing those for non-returnable disposable bottles ("breakeven point"). An increased recycled material content would thereby increase the economic efficiency of re-useable PET bottles.
Essentially, the level of economic efficiency depends on the wildly fluctuating price of new PET granules. If such granules are cheaper than recycled material, single-layer preforms fabricated from 100 % new material may be produced more cheaply, yet if the price rises above this breakeven point, three-layered preforms which show a recycled material content of 35 % and above are favourable. A higher recycled material content also results in improved price stability as the wild fluctuations seen in the price of new material will make a proportional difference only in those preforms using recycled PET. Cost implications for the manufacturer and the bottling firm are thus more favourable.
It is for this reason that is has already been suggested (Modern Plastics International, February 1997, page 29) that a co-extrusion blow moulding tool be used in the production of PET preforms and that product parts produced independently of one another be linked together. PET bottles which show a recycled material content of up to 80 % have been produced in this manner. A method of this type does, however, require additional tools and is proving to be complex and cost-intensive.
It is the aim of the beverage industry to produce formed bodies which meet with the law and show a high recycled material content without resorting to expensive technical measures.
The resulting technical problem is thus the way in which preforms can be produced with extremely thin layers of new material and without the use of expensive structures in order that the recycled material content of these preforms can be increased.
Particularly, the aim is to produce three-layered preforms which show at least one layer which is as thin as possible or a recycled material content of over 35 vol. %, particularly of 35.
to 65 vol. %, by means of a simple procedure.
According to Claim l, the solution to this problem lies in a surprisingly simple method for operating a multi-component injection moulding form tool and, particularly, in reversing the conventional arrangement for the supply of components A and B and operating the form tool in such a way that, in the first step in the cycle, the shut-off needle is brought into a position, wherein both the inner and the outer jet chambers are opened such that conveyance of component B through the outer jet chamber is stopped and only component A is injected into the mould cavity through the inner jet chamber.
In producing preforms which show a high recycled material content, the first component to be injected, component A (new material), is thus directed through the inner jet chamber to form a thin surface layer and the other component to be injected, component B (recycled material), is directed via the outer jet chamber to form a layer of filler. When injection moulding a three-layered preform of this type, in the first step in the cycle, the shut-off needle is brought into position I, wherein both the outer jet chamber containing component B
and the inner jet chamber containing component A are opened.
With the needle in this position, conveyance of component B is interrupted and component A is injected into the mould cavity.
WO 99/2x926 5 PCT/CH98/00471 In the second step in the cycle, the shut-off needle is brought into t~e outer jet chamber opened. With the needle in this position, conveyance of component A is interrupted and component B is inject into the mould cavity. The position of the shut-off needle re ins unchanged for the next step in the cycle, the so-called ho ing phase, during which time shrinkage of component H due to cooling is replaced. Once the holding phase is aver, the shut- ff needle is brought into closing position III, wherein both th inner and outer jet chambers are closed.
It proves surprising that, uring the next mould cycle, the first injection shot using co onent A is free from undesirable material H. This unexpected resu can be explained by the reversal of the admission channels, articularly, a small reduction in the viscosity of componen A (new material) is achieved through the specific manner in ich the individual components are conveyed, i.e. conveyance of omponent A through the slightly warmer inner jet chamber. Tn cont st to preforms produced using conventional methods of injection ulding, preforms with a thin surface layer (component A) can a created according to the inventive method and the relative prop tion of filler material can be increased by component B materia - 5~
(AMENDED SHEET J
(pg.4, 4aJ
... position I, wherein both the outer jet chamber containing component B and the inner jet chamber containing component A
are opened. With the needle in this position, conveyance of component B is interrupted and component A is injected into the mould cavity. In the second step in the cycle, the shut-off needle is brought into position II, wherein the inner jet chamber is closed and the outer jet chamber opened. With the needle in this position, conveyance of component A is interrupted and component B is injected into the mould cavity.
The position of the shut-off needle remains unchanged for the next step in the cycle, the so-called holding phase, during which time shrinkage of component B due to cooling is replaced.
Once the holding phase is over, the shut-off needle is brought into closing position III, wherein both the inner and outer jet chambers are closed.
It proves surprising that, during the next mould cycle, the first injection shot using component A is free from undesirable material B. As described bY way of example in EP 0 768 163 or EP 0 380 215 all methods known toda use material A in to in up, i.e. to replace material shrunk during cooling- This result, unexpected even to the specialist, can be explained by the reversal of the admission channels. Particularly, a small reduction in the viscosity of component A (new material) is achieved through the specific manner in which the individual components are conveyed, i.e. conveyance of component A through the slightly warmer inner jet chamber. In contrast to preforms produced using conventional methods of injection moulding, preforms with a thin surface layer (component A) can be created according to the inventive method and the relative proportion of filler material can be increased by component B material being loaded into the mould cavity during the holding pressure phase.
b Moreover, the inventive method also allows preforms which show an extremely thin barrier layer (e.g, of nylon or similar) to be produced. Harrier layers of this type serve the purpose of minimising the degree of oxygen penetration within the formed bodies (bottles) and are comparatively expensive. In order to create a preform with a thin barrier layer accarding to the invention, the conventional arrangement of admission channels is again reversed and the barrier material to be injected to form the thin barrier layer is directed through the innermost jet chamber and the plastic forming the surface layer is fed through the outer jet chamber. When injection moulding a preform of this type, in the first step in the cycle, again the shut-off needle is brought into position I, wherein both the w0 99/22926 6 PCT/CH98/00471 outer and inner jet chambers are opened and the component directed through the outer jet chamber is injected into the mould cavity in the first step in the procedure, while at the same time conveyance of the barrier material directed through the inner jet chamber is interrupted. The shut-off needle remains in position I for the next step in the cycle and the barrier material conveyed through the inner jet chamber is loaded into the mould cavity at the same time as the filler material fed through the outer or central jet chamber. During this phase in injection moulding, both components (filler and barrier material) are thus conveyed at the same time, i.e. by means of tubes lying inside one another, thereby ensuring that the proportion of conveyed barrier material remains extremely low, e.g. making up 5 ~ of the overall injected material volume. The filler material and the material forming the surface layer may therefore be one and the same. Preferably, a relatively inexpensive recycled material is used for the filler material. This may be achieved in a well-known and simple manner by controlling the supply of molten plastics. In a third step in the cycle, conveyance of the barrier material is stopped once more and the filled mould cavity is further loaded with the amount of filler material required to compensate for shrinkage. By throwing the shut-off needle forward into position III, both jet chambers are closed and the mould cycle completed. The thin barrier layer lies in the central wall structure of the preform in all preforms produced in this manner. It is observed that preforms and formed bodies with layers arranged in such a manner provide the required barrier action against oxygen penetration within such containers.
Other embodiments of the inventive method are characterised by the features cited in the subclaims. Preforms created according to the inventive method of operation show a recycled material content of over 35 vol. % and, where necessary, a barrier layer material content of less than 5 vol. o.
The invention shall be described in further detail hereinafter with reference to an example. The illustrations given hereinafter show:
Wb 99/22926 7 PCT/CH98/00471 Figure 1: cross section through a hot runner nozzle and associated needle shut-off mechanism thereof;
Figure 2a to 2d: positions and control of the needle shut-off arrangement;
Figure 3: longitudinal section through a preform produced in the conventional manner;
Figure 4: longitudinal section through a preform produced according to the inventive method showing a high recycled material content;
Figure 5: longitudinal section through a preform produced according to the inventive method showing a barrier layer.
Figure 1 shows a section taken from the structure of a co-injection form tool used for two different components, A and B, complete with a hot runner nozzle 34 and a needle shut-off mechanism 36. The material melted in the extruders lands in the hot runner manifold block 15 via separate runners, is ramified therein and fed into the individual hot runner nozzles 34. Each of these hot runner nozzles 34 features a removable nozzle holder 33 and is constructed from several nozzle inserts lying inside one another between which one inner jet chamber 3 and at least one outer jet chamber 5 are created, through which the various synthetic components are fed up to the nozzle point.
Heating elements keep both the hot runner manifold block 15 and the nozzle holder 33, and thereby the hot runner nozzle 34, at the required temperature. A pneumatic needle shut-off mechanism 36 controls a movable needle 37 located near the point of the hot runner nozzle 34 in order to release or block individual components A or B and/or C.
In the conventional method of operation, the shut-off needle 37 is brought into four different positions during the course of one mould cycle in order to, by way of example, fill a cavity with three layers. In the first position, the needle 37 is drawn backwards only as far as is required to load the cavity with the first component, particularly original PET or raw material, via the outer jet chamber 5. In the second position, the needle 37 is drawn further backwards such that the second component, e.g. recycled PET, can also be pressed into the mould cavity via the inner jet chamber 3 before the needle 37 is nudged back into its intitial position for the holding phase and then nudged all the way forward in order to close the nozzle 34. The shut-off needle is therefore brought into four different positions during the course of one mould cycle, that is in order to a) open the outer jet chamber 5, b) open the inner jet chamber 3, c) close the inner jet chamber 3 and d) close the outer jet chamber 5.
As shown in Figure 1, the needle shut-off mechanism 36 is lodged in a groove on the top plate 13 which acts as a pneumatic cylinder and comprises the first plunger 38 which guides the needle 37, above which a second, flexible plunger 39 is fitted. A hermetical cylinder cover 40 seals off this groove so that it is compression-proof. Suitably arranged pressure pipes 41, 43 and 44 allow the individual plungers, and therefore the needle 37, to be brought into the desired position. Each of the individual pressure pipes presents the pressure required to move the needle. Usually, the outer pressure pipe 44 is pressurized to 20 bar, the central pressure pipe 43 to 10 bar and the inner pressure pipe 41 to 5 bar. The positioning of the individual plungers 38 and 39 shown in Figure 1 is achieved when the individual pressure pipes are pressurized as stipulated above. Should the needle 37 be drawn backwards into its initial position in order to release the first synthetic component in the conventional manner, the pressure in the central pressure pipe 43 simply needs to be raised or reduced accordingly. With that, the first plunger 38 moves up to the stop of the second plunger 39 due to the force of the pressure in the~inner pressure pipe 41. To bring the needle 37 into the second position which opens up the supply of the second synthetic component via the inner jet chamber, the pressure in the outer pressure pipe 44 is raised or reduced analogously. This results in the two plungers 38, 39 moving together up to the cylinder cover 40. To stop the supply of material once more, first the outer pressure pipe 44 is re-pressurized and with that the two plungers 38, 39 move together in the closing direction. Likewise, only when the central pressure pipe 43 is re-pressurized also can the outer jet chamber be interrupted by the movement of the first plunger 38.
Compression-proof seals 51 and 52 are fitted on each individual plunger together with the seals 53 on the cylinder cover 40, ensuring that the pneumatic needle shut-off mechanism.36 works perfectly. An end seal 55 is also fitted in the nozzle holder 33 preventing pressure compensation occurring between the plunger arrangement 38, 39 and the nozzle arrangement 33, 34 and thus preventing pressurized steam penetrating along the needle 37 through the nozzle holder 33 from the individual, heated synthetic components, condensing on the walls of the plunger or on the nozzle needle and affecting or blocking the movability of the individual components in the needle shut-off mechanism 36. This is achieved in a well-known manner by the use of a gastight end seal 55 fabricated from temperature-resistant plastic.
According to the invention, to be able to produce multi-layered preforms which show an increased recycled material content or extremely thin layers using a multi-component injection moulding form tool of this type, the conventional arrangement for supplying components A and B is reversed and operated in such a way that component A is conveyed in the inner jet chamber 3 of the hot runner nozzle 34 together with only the material to be loaded to form a thin layer (new or barrier material) while component B is conveyed, together with the recycled material to be loaded, in the outer or central jet chamber 5 of the hot runner nozzle 34. Should a formed body be produced which shows a thin outer skin fabricated from new material as well as a thin barrier layer, new material is conveyed in the outermost of the three jet chambers, and the material forming the barrier layer in the innermost chamber, in such a manner that the material forming the barrier layer is squirted out of the central jet chamber at the same time as the filler material. When producing formed bodies which show a thin barrier layer fabricated from one single base material, in the first step an initial portion of base material is injected into the mould cavity through the outermost of the two jet chambers and, in the second step, both base material and barrier material are injected into the mould cavity at the same time, i.e. by means of tubes lying inside one another. The needle 37 is thus brought into the positions as explained in further detail hereinafter with reference to Figures 2a to 2d.
Figures 2a to 2d show partial sections through the hot runner nozzle 34, complete with the associated needle shut-off mechanism 36 thereof. As shown in Figure 2a, the needle 37 is drawn backwards as far as is required to release the inner jet chamber in order to load the original component A conveyed via this inner jet chamber 3. By interrupting conveyance of component B and conveying component A, the required quantity of the original material A can be loaded into the mould cavity. As the original material A inside the hot runner nozzle 34 is shown to be less viscous than the filler material B in the outer jet chamber 5, it is sufficient to load only a small portion of the original material A into the mould cavity. This position of the needle, position I, can be achieved by reducing the pressure in pressure pipes 44 and 43 above the second plunger 39, or between the first plunger 38 and the second plunger 39, to 0 bar, for example, while building up the pressure in the pressure pipe 41 below the first plunger 38 to 6 bar, for example. Using this distribution of compressive forces, the two plungers find their highest possible position and the needle 37 thereby releases the inner jet chamber 3.
In the second step in the cycle as shown in Figure 2b, the needle 37 is brought into position II, wherein the inner jet chamber 3 is closed but the outer jet chamber 5 remains open.
This is achieved by maintaining the pressure in the pressure pipe 41 at 6 bar, for example, while raising the pressure in the pressure pipe 44 above the second plunger 39 a little, to bar, for example. In this position, component B (filler material) is conveyed into the mould cavity through the outer jet chamber 5. This material is more viscous than that out of the inner jet chamber 3 and it thus displaces the previously injected component A forming a thin film on the outer surfaces of the mould cavity, without penetrating the film. This difference in viscosity allows preforms to be produced with a thin outer skin. In the third step in the cycle, the mould cavity filled with the filler material B remains pressurized for a period, i.e. during the so-called holding phase, in order to compensate for any material volume lost through shrinkage.
Figure 2c shows the hot runner nozzle 34 and the needle shut-off mechanism 36 thereof in position III, wherein both the inner jet chamber 3 and the outer jet chamber 5 are closed.
This is achieved by reducing the pressure in the pressure pipe 41 below the first plunger 38 to 0 bar, for example, and raising the pressure in the pressure pipe 43 between the two plungers to 6 bar, for example, at the same time while keeping the pressure in the pressure pipe 44 above the second plunger 39 at 10 bar, for example.
Conventionally, and without reversed delivery channels for components A and B, the mould cycle starts with the needle in the position shown in Figure 2b in order to load component A
(new material) into the mould cavity. The shut-off needle 37 is subsequently brought into position I to fill the mould cavity with component B (filler material). As shown in Figure 2d, the needle is brought back into position II for the holding phase in order to replace material shrunk due to cooling with component A and to ensure that component B (recycled material) does not land in the cavity first during the next mould cycle.
To complete the cycle the needle is brought into position III, as shown in Figure 2c.
\ WU 99/22926 12 PCT/CH98/00471 It is thus clear that in the method of operation under consideration, the mould cycle is completed when filler material shrinkage is replaced with the same component, while conventionally the volume of material shrinkage is replaced with whichever component is to be injected first during the next mould cycle. In the method under consideration, component B (recycled material) may be loaded repeatedly into the mould cavity but surprisingly it is observed that it is only component A, in fact, which lands in the mould cavity due to the lower viscosity of component A fed through the inner jet chamber and because conveyance of component B is interrupted at the beginning of the next mould cycle; it is in this manner that the tough requirements demanded by the beverage industry can be met as regards blow-moulded bodies which show an intact, outer or inner skin.
The longitudinal sections shown in Figures 3 and 4 make clear the distinction between the inventive method and the conventional method. Figure 3 shows a longitudinal section through a preform produced in the conventional manner with a threaded section 61 and a barrel section 62, the sprue 63 thereof lying in the bottom section 64. From this longitudinal section it is also evident that neither the inner skin 65 nor the outer skin 66 (except at sprue) is penetrated at any point by the filler material B. Particularly critical points here are the deformations in the threaded section 61 of the preform. In addition, this illustration makes clear the manner in which the volume of filler material shrunk during the holding phase is replaced with new material A. Particularly, the percentage of recycled material used is substantially reduced by this new material being additionally loaded into the bottom section 64.
In contrast, Figure 4 shows a longitudinal section through a preform produced according to the inventive method.
Essentially, this differs in the structure of the bottom section 64 which shows just three layers, namely an inner skin, filler material and an outer skin. Moreover, a fundamental distinction is shown in the thickness of the individual layers.
Conventional preforms weighing 48.0 g with an overall wall thickness of 4.37 mm which are suitable for 1.5 litre bottles have an outer skin with a thickness of 1.3 to 1.5 mm. This results in a volume percent of 25 to 33 vol. o as regards the innerlying filler material. In the case of preforms also weighing 48.0 g produced according to the inventive method as shown in Figure 4, the outer material 65, 66 shows a thickness of 1.2 to 0.6 mm, therefore allowing the percentage of filler material to be increased to 37 to 63 vol. s through the application of this particular method of manufacture.
By reversing the admission channels, preforms can also be produced with a barrier layer (e. g. of nylon, EVOH or similar) which shows an improved barrier action against oxygen. This shall be explained in further detail with reference to Figures 2a to 2c. According to the inventive method, during the production of preforms with a barrier layer, the needle 37 is brought into position II (Figure 2b) in the first step in the cycle in order to fill the cavity with material used for the surface layer. In the second step in the cycle, the shut-off needle 37 is brought into position I (Figure 2a) and the barrier material (e.g. nylon) conveyed through the inner jet chamber 3 is injected into the mould cavity together with the component fed through the outer jet chamber 5. Barrier material therefore ends up lying in the inner wall structure of the preform allowing the formed body to be provided with an extremely thin barrier layer of approx. 5 vol. o or less.
In a preferred embodiment, the barrier material is directed through the innermost jet chamber and the method allows the needle 37 to be brought into position I in the first step in the cycle, wherein both the inner and the outer jet chambers are opened but only the material directed through the outer jet chamber 5 is conveyed into the mould cavity while conveyance of the material directed through the inner jet chamber 3 is stopped. The needle 37 remains in position I for the second step in the cycle and material is conveyed through the outer jet chamber 5 at the same time as the barrier layer material conveyed through the inner jet chamber 3, resulting in a barrier material content of approx. 5 s or less of the overall injected material. To compensate for material shrinkage during the holding phase, the shut-off needle remains in position I
and conveyance of the barrier material conveyed through the inner jet chamber 3 is suspended. Following successful loading, the needle is brought into position III (Figure 2c) in order to close the inner and outer jet chambers. Preforms produced in this manner show a thin barrier layer which lies in the central wall structure of the preform.
The advantages shown by the inventive method and by the preforms created according to this method are immediately obvious to the specialist. Particularly, the conventional method requires four needle positions in succession for each mould cycle whereas the inventive method requires only two or three needle positions. This simplifies control of the needle shut-off mechanism. Moreover, according to the invention, shrinkage in component B is replaced with the same material, increasing the percentage of this component (recycled material) or lowering the percentage of the component fed through the innermost jet chamber. The acquisition of new and expensive machines or tools is not required to put the inventive method into practice.
Further developments, particularly those affecting the viscosity of individual components and those used in controlling the mould cycle, lie within the normal capacities of a person skilled in the art. It is understood that all plastics used in injection moulding technology, especially nylon, and not only PET material, may be processed using this method.
Claims (8)
1. Method for. operating a multi-component injection moulding form tool in order to produce multi-layered formed bodies, whereby the multi-component injection moulding form tool features a hot runner nozzle with needle shut-off mechanism (36) used to release or block one inner jet chamber (3) and one outer jet chamber (5) of the nozzle needle (34) and, to that end, the needle shut-off mechanism (36) features a movable needle (37) and at least one first plunger (38) and one second plunger (39), arranged such that they are -movable within a cylindrical barrel, whereby either plunger (38, 39) may be shifted by means of compression in such a manner that the needle (37) connected to these plungers (38, 39) may be brought into the corresponding releasing/blocking positions (I, II, III, IV), where one component A to be injected to form a thin surface layer of new material is directed through the innermost jet chamber (3) and one component B to be injected as the filler material is directed through the one outer jet chamber (5), whereby, in the first step in the circle, the shut-off needle (37) is brought into a position (I), wherein the innermost jet chamber (3) containing component A and the outer jet chamber (5) containing component B are opened, whereby, in the first step in the cycle, only component A is conveyed through the innermost jet chamber (3) and conveyance of the other components through the one outer jet chamber (5) is stopped, and characterised in that, in order to produce a three-layered preform with a component B content of over 35 %, component B us conveyed through the one outer jet chamber (5) in the second step in the cycle and the material shrunk during cooling is replaced with component B in the third step in the cycle such that the component B
content amounts to over 35 vol. %, and, in order to complete the mould cycle, the shut-off needle (37) is brought into position III, wherein both the innermost bet chamber (3) and the one outer jet chamber (5) are closed
content amounts to over 35 vol. %, and, in order to complete the mould cycle, the shut-off needle (37) is brought into position III, wherein both the innermost bet chamber (3) and the one outer jet chamber (5) are closed
2. Method according to Claim 1, characterised in that, in the second step in the cycle, the shut-off needle (37) is brought into position II, wherein the innermost jet chamber (3) is blocked and the one outer jet chamber (5) opened.
3. Method for operating a multi-component injection moulding form tool in order to produce multi-layered formed bodies, whereby the multi-component injection moulding form tool features a hot runner nozzle with needle shut-off mechanism (36) used to release or block one inner jet chamber (3) and one outer jet chamber (5) of the nozzle needle (34) and, to that end, the needle shut-off mechanism (36) features a movable needle (37) and at least one initial plunger (38) and one second plunger (39), arranged such that they are movable within a cylindrical barrel, whereby either plunger (38, 39) may be shifted by means of compression in such a manner that the needle (37) connected to these plungers (38, 39) may be brought into the corresponding releasing/blocking positions (I, II, III, IV), whereby one component C to be injected to form a thin barrier layer of barrier material is directed through the innermost jet chamber (3) and one component B to be injected as the filler material is directed through the one outer jet chamber (5), whereby, in the first step in the cycle, the shut-off needle (37) is brought into a position (I) wherein the innermost jet chamber (3) containing component. C and the outer jet chamber (5) containing component. B are opened, whereby, in the first step in the cycle, only component C is conveyed through the innermost jet chamber (3) and conveyance of the other component through the one outer jet chamber (5) is stopped, characterised in that, in order to produce a three-layered preform with a barrier layer of material C, both component. C and component B are conveyed through the innermost jet chamber (3) and the outer jet chamber (5) respectively in the second step in the cycle such that the component C content amounts to 5 % or less of the overall volume and in that, in the third step in the cycle, conveyance of component C is interrupted in such a manner that only component B material is conveyed into the mould cavity from the outer jet chamber (5), and, in the fourth step in the cycle, the material shrunk during cooling is replaced with said component B, and, in order to complete the mould cycle, the shut-off needle (37) is brought into position III, wherein both the innermost jet chamber (3) and the one outer jet chamber (5) are closed.
4. Method as claimed in Claim 3, characterised in that the shut-off needle (37) is left in position I in the second and third steps in the cycle.
5. Method for producing a five-layered preform with an outer (66) and inner skim (65) fabricated from material A, a barrier layer fabricated from material C, particularly nylon, and a filler material B, particularly recycled material, in the first step in the cycle, the shut-off needle (37) is brought into position I, wherein the innermost jet chamber (3) containing component C and both the outer jet chamber containing component A and one jet chamber in between containing component B are opened, whereby conveyance of components B and C is stopped in the first step in the cycle and only component A is conveyed through the outer jet chamber, that conveyance of component A is stopped in the second step in the cycle and components B and C are conveyed at the same time, i.e. in the form of tubes, and, in the third step in the cycle, conveyance of component C is stopped and the plastic forming material shrunk during cooling is replaced with component B.
6. Method according to Claim 5, characterised in that a component C content of approx. 5 vol. % and a component B
content of over 30 % of the overall volume is conveyed in the second step in the cycle.
content of over 30 % of the overall volume is conveyed in the second step in the cycle.
7. Preform produced according to one of the methods as claimed in Claim 1 or 3, characterised in that it shows a component B content of over 35 vol. %.
8. Preform produced according to one of the methods as claimed in Claim 3 or 5, characterised in that it shows a barrier layer of material C of less than approx. 5 vol. %
and a material B content of over 35 vol. %.
and a material B content of over 35 vol. %.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH02540/97A CH692573A5 (en) | 1997-11-04 | 1997-11-04 | A method for producing multilayer preforms. |
CH2540/97 | 1997-11-04 | ||
PCT/CH1998/000471 WO1999022926A1 (en) | 1997-11-04 | 1998-11-04 | Method for producing multi-layered preforms |
Publications (1)
Publication Number | Publication Date |
---|---|
CA2303766A1 true CA2303766A1 (en) | 1999-05-14 |
Family
ID=4236097
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA002303766A Abandoned CA2303766A1 (en) | 1997-11-04 | 1998-11-04 | Method for producing multi-layered preforms |
Country Status (5)
Country | Link |
---|---|
EP (1) | EP1028838A1 (en) |
JP (1) | JP2001521837A (en) |
CA (1) | CA2303766A1 (en) |
CH (1) | CH692573A5 (en) |
WO (1) | WO1999022926A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2022082297A1 (en) * | 2020-10-21 | 2022-04-28 | Husky Injection Molding Systems Ltd. | Machine and method for injection molding multilayer articles having a high proportion of internal layer material |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
USRE38480E1 (en) * | 1999-06-04 | 2004-03-30 | Husky Injection Molding Systems Ltd. | Injection nozzle and method for injection molding |
US6214275B1 (en) * | 1999-06-04 | 2001-04-10 | Husky Injection Molding Systems Ltd. | Injection nozzle and method for injection molding |
CN100372740C (en) * | 2004-08-12 | 2008-03-05 | 珠海保税区中富聚酯啤酒瓶有限公司 | PET plastic container blank, method for manufacturing the same and equipment thereof |
DE102009035058A1 (en) | 2009-07-28 | 2011-02-10 | Gizeh Verpackungen Gmbh & Co. Kg | An injection molded thin-walled multilayer plastic packaging container having a barrier layer and method of making the same |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2342794C3 (en) * | 1973-08-24 | 1981-09-17 | Schloemann-Siemag AG, 4000 Düsseldorf | Method and device for the discontinuous production of multilayer molded parts from thermoplastic material |
JPS61235126A (en) * | 1985-04-12 | 1986-10-20 | Nissei Ee S B Kikai Kk | Multi-layer vessel and manufacture thereof |
US4808101A (en) * | 1986-05-12 | 1989-02-28 | Husky Injection Molding Systems Ltd. | Tri-injection of hollow articles |
US4957682A (en) * | 1988-01-19 | 1990-09-18 | Kamaya Kagaku Kogyo Co., Ltd. | Method of injection molding a three-layered container |
JPH0243017A (en) * | 1988-04-01 | 1990-02-13 | Kamaya Kagaku Kogyo Co Ltd | Method and device for injection molding of three-layer vessel, and three-layer vessel |
JPH0232813A (en) * | 1988-07-21 | 1990-02-02 | Mitsubishi Plastics Ind Ltd | Injection head for multi-layered parison molding |
US4990301A (en) * | 1989-01-25 | 1991-02-05 | Continental Pet Technologies, Inc. | Method and apparatus for injection molding of multilayer preforms |
EP0624449A3 (en) * | 1993-05-13 | 1994-12-28 | Husky Injection Molding | Method of molding plastic articles. |
NL1001417C2 (en) * | 1995-10-13 | 1997-04-15 | Inter Tooling Services Bv | Device for manufacturing hollow plastic objects. |
DE19613779C2 (en) * | 1996-04-04 | 1998-07-16 | Krupp Ag Hoesch Krupp | Process for the injection molding of three-layer moldings and device for carrying out the process |
DE19640662C1 (en) * | 1996-10-02 | 1998-03-05 | Krupp Ag Hoesch Krupp | Injection moulding of bottle preforms |
-
1997
- 1997-11-04 CH CH02540/97A patent/CH692573A5/en not_active IP Right Cessation
-
1998
- 1998-11-04 JP JP2000518830A patent/JP2001521837A/en active Pending
- 1998-11-04 WO PCT/CH1998/000471 patent/WO1999022926A1/en not_active Application Discontinuation
- 1998-11-04 CA CA002303766A patent/CA2303766A1/en not_active Abandoned
- 1998-11-04 EP EP98951147A patent/EP1028838A1/en not_active Withdrawn
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2022082297A1 (en) * | 2020-10-21 | 2022-04-28 | Husky Injection Molding Systems Ltd. | Machine and method for injection molding multilayer articles having a high proportion of internal layer material |
Also Published As
Publication number | Publication date |
---|---|
JP2001521837A (en) | 2001-11-13 |
CH692573A5 (en) | 2002-08-15 |
EP1028838A1 (en) | 2000-08-23 |
WO1999022926A1 (en) | 1999-05-14 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN1104319C (en) | Method of three layer injection molding with sequential and simultaneous coinjection | |
EP1412156B1 (en) | Injection molding of multi-layer plastic articles | |
EP0325440B2 (en) | Method and apparatus for the manufacture of three-layered containers | |
US6123211A (en) | Multilayer plastic container and method of making the same | |
AU2007307905B2 (en) | Method and apparatus for delivering sequential shots to multiple cavities to form multilayer articles | |
EP2781330B1 (en) | Injection moulding process | |
CA2248412C (en) | Injection molding apparatus for molding multi-layered article and method of injection-molding multi-layered article | |
US4950143A (en) | Injection mold manifold arrangement | |
AU721601B2 (en) | Molding multi-layered articles using coinjection techniques | |
CA2303766A1 (en) | Method for producing multi-layered preforms | |
CA1202459A (en) | Injection mold assembly | |
JP2003513820A (en) | Multilayer preform and method of manufacturing the same | |
KR19980076321A (en) | Injection Molding Machine for Thermoplastics | |
AU2001295835A1 (en) | Injection molding of multi-layer plastic articles |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
EEER | Examination request | ||
FZDE | Discontinued |