WO1986003713A1 - Container, method and apparatus for manufacturing the same - Google Patents

Container, method and apparatus for manufacturing the same Download PDF

Info

Publication number
WO1986003713A1
WO1986003713A1 PCT/SE1985/000510 SE8500510W WO8603713A1 WO 1986003713 A1 WO1986003713 A1 WO 1986003713A1 SE 8500510 W SE8500510 W SE 8500510W WO 8603713 A1 WO8603713 A1 WO 8603713A1
Authority
WO
WIPO (PCT)
Prior art keywords
preform
hollow body
mandrel
region
forming
Prior art date
Application number
PCT/SE1985/000510
Other languages
French (fr)
Inventor
Torsten Nilsson
Original Assignee
Petainer S.A.
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Petainer S.A. filed Critical Petainer S.A.
Priority to DE8686900323T priority Critical patent/DE3572455D1/en
Priority to AT86900323T priority patent/ATE45700T1/en
Priority to IN356/CAL/86A priority patent/IN168171B/en
Publication of WO1986003713A1 publication Critical patent/WO1986003713A1/en
Priority to FI863260A priority patent/FI88373C/en
Priority to NO863238A priority patent/NO863238L/en
Priority to DK387086A priority patent/DK163970C/en
Priority to IN822/CAL/89A priority patent/IN171425B/en

Links

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
    • B29C57/00Shaping of tube ends, e.g. flanging, belling or closing; Apparatus therefor, e.g. collapsible mandrels
    • 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
    • B29C49/08Biaxial stretching during blow-moulding
    • 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
    • B29C49/18Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor using several blowing steps
    • 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
    • B29C49/48Moulds
    • 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
    • B29C49/76Neck calibration
    • 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
    • B29C55/00Shaping by stretching, e.g. drawing through a die; Apparatus therefor
    • B29C55/30Drawing through a die
    • 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
    • B29C49/48Moulds
    • B29C2049/4856Mounting, exchanging or centering moulds or parts thereof
    • B29C2049/4858Exchanging mould parts, e.g. for changing the mould size or geometry for making different products in the same mould
    • 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
    • B29C49/48Moulds
    • B29C2049/4879Moulds characterised by mould configurations
    • B29C2049/4892Mould halves consisting of an independent main and bottom part
    • 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
    • B29C2949/079Auxiliary parts or inserts
    • B29C2949/08Preforms made of several individual parts, e.g. by welding or gluing parts together
    • 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
    • B29K2105/258Tubular
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S264/00Plastic and nonmetallic article shaping or treating: processes
    • Y10S264/90Direct application of fluid pressure differential to shape, reshape, i.e. distort, or sustain an article or preform and heat-setting, i.e. crystallizing of stretched or molecularly oriented portion thereof
    • Y10S264/904Maintaining article in fixed shape during heat-setting

Definitions

  • The. present invention relates to a hollow body (e.g. a container) whose axially directed wall(s) comprise(s) oriented and/or crystal ⁇ lised plastics material, in addition to which the invention relates to a method and an apparatus for reshaping a primarily tubular pre- form of plastics material into the hollow body by means of mechanical shaping devices.
  • a hollow body e.g. a container
  • axially directed wall(s) comprise(s) oriented and/or crystal ⁇ lised plastics material
  • US Patent No. 4,372,908 reveals a technique where a stretched and oriented blank of thermoplastics material is reshaped into a con- tainer by means of one or more mechanical shaping processes.
  • the circum ⁇ ference of the body of the container is reduced during the reshaping of the blank into the container.
  • High-tempe ⁇ rature applications mean e.g. that the contents of filled and " sealed
  • containers are pasteurised (60-70OC), that the liquid is filled directly into the containers from boiling (warm filling) or that the contents of filled and sealed containers are sterilised (at least 1210C).
  • the mechanical strength of the containers is naturally also determined by the orientation of the material and/or its crystallisation. It is especially in the case of thermoplastics material that the thermal crystallisation is of importance.
  • a further requirement for containers of the kind envisaged here and 25 especially for a container intended for high-temperature applications is that the- shrinkage -which occurs during heating of stretched and .-- oriented thermoplastics material is eliminated or reduced to accept- . ' - ' able values. " .
  • the container In order to improve the strength of the material in the case of orientable thermoplastics material, the container is moulded in accordance with a known and generally applied technique, by means of a blowing process, at the same time as the temperature of the material is adapted to the properties of the material in ques ⁇ tion, in order to stretch the material during the blowing process and thereby orientate the same.
  • the blowing technique possesses the disadvantage that the distribu ⁇ tion of material during the moulding of the container is not fully 0 controllable since, during the expansion of the blank into the con ⁇ tainer, it is not possible to determine and control exactly where and how the stretching of the material, and thus its orientation, will proceed.
  • the stretching begins at a number of starting points, whose positions are determined by the prevailing temperature 5 distribution in the material, in addition to stretching forces aris ⁇ ing therein.
  • the propagation of expansion, and the stretch ratio ob ⁇ tained are furthermore temperature-dependent, which results in a vary ⁇ ing material thickness of the moulded container, i.e.
  • the thickness of the 0 container wall varies in the circumferential direction.
  • the addition ⁇ al heating of the material which takes place when it crystallises through the stretching, achieves in the material an additional uneven temperature distribution which results in an increase in variations in the thickness of the wall in the moulded container.
  • Corresponding 5 variations also occur in the axial direction of the container, i.e. in axial sections through regions of primarily equally large circum ⁇ ference, alternately thinner and thicker material portions are pre ⁇ sent.
  • the wall thickness of the blank is thus selected in accordance with known technique with regard to the aforementioned uncertainty in 0 the stretching and thinning out of the material, which implies an - - .
  • the present invention relates to a technique where all aforementioned disadvantages are eliminated.
  • the time re ⁇ quirement for the manufacture of each individual container is also reduced in comparison with that in previous known techniques, in addition to which the invention allows a simplified construction of the production equipment.
  • the quantity of material in each container is thus reduced, the desired temperature stability is achieved, and costs are reduced in comparison to pre ⁇ viously known and used techniques.
  • a preform of plastics material is reshaped, which has the property of being able to be oriented and/or crystallised by a mechanical processing, into a container in a number of consecutive reshaping processes which, in a preferred embodiment, take place in distinctly separate sub-stages.
  • the material is stretched (extended) ' in either the axial or the circumferential direction of the future container.
  • stretching (extending) the material every time to a controlled extent, the material accumulates a total stretching (extension) and a reduction in thickness equivalent to tha.t._which_ is required in order to supply the material with the desired and pre-determined orientation or crystallisation and thus the necessary strength properties.
  • the con ⁇ trolled stretching (extension) and the controlled reduction of the material thickness causes the moulded container to have the same material thickness in sections at right-angles to the axis of the container, thereby avoiding the variation in thickness, which con ⁇ tainers manufactured in accordance with known techniques have in axial sections through regions of primarily equally large circum ⁇ ference.
  • the tractive forces are supplemented by compressive forces which are applied in the vicinity of the bottom section of the preform, and which are directed towards the mouth of the preform. This technique is employed when the increase in the dimensions in the circumferential direction is large.
  • the pre ⁇ form is reshaped into the container in all sub-stages by use of mechanical reshaping devices.
  • the mechanical stretching takes place in every stage with the material at a specific and contrailed temperature which can be selected within a wide range.
  • the choice of temperature is determined however by the special effect which it is required to achieve in the moulding stage in question.
  • TG glass transition tempera ⁇ ture-, hereinafter abbreviated as TG, e.g. the temperature of the mate- rial is, in certain, and in general, the initial moulding stages, ilower than TG, while in the concluding stage or stages the .tempera ⁇ ture generally exceeds TG.
  • the material attains, in a preferred embodiment of the invention, temperatures within the range 70-160OC, in connection with the concluding shaping stages, while in the initial shaping stages it generally has a lower tempe ⁇ rature.
  • At least one of the shaping stages, and preferably the last one comprises a blow moulding stage.
  • the material is heated to a temperature close to or exceeding the maximum temperature at which the material was previously shaped mechanically.
  • Figs. 1-5 show the shaping of a preform into an intermediate preform by extension of the preform in its axial direction when the preform passes through a gap • .- that reduces the material thickness
  • Figs. 6-9 show expansion of the preform in its circ ⁇ .mferen- tial direction
  • Figs. 10-13 show reshaping of the expanded preform into a container.
  • Fig. 1 contains a preform 10 with a bottom section 11, a mouth 12, a ribbon-shaped, circumferential mouth edge region 13, a mouth edge 14, and an axially directed wall 15, located between the mouth and the bottom section.
  • the central axis of the preform is denoted by refer- ence numeral 16.
  • the preform is, in Fig. 2, placed in an apparatus for temperature setting of the preform material.
  • the apparatus in ⁇ cludes a sleeve 91, a mandrel 92 and a bottom support 93. All these devices are provided with channels 97 through which a fluid, such as a liquid passes for individual setting of each device to a certain working temperature.
  • the devices are adjustable to positions where there is formed between them a cavity whose shape substantially corresponds to that of the preform.
  • a preform which is placed in the cavity is thus enclosed on both the inside and the outside by the devices and assumes a temperature which in every part of the preform is determined by the temperatures of the adjoining devices and the time the preform stays in the cavity.
  • Figs. 3 and 4 show a basic apparatus for reduction of the material thickness of the preform during its simultaneous extension in the axial direction.
  • the apparatus includes a bottom support 94, a mandrel 95 and a traction device 96 which encloses the mandrel and is displaced in its axial direction by displacement devices (not shown in the Figures). Between the mandrel and the traction device there is located a slot 90 the breadth of which less than the material thick ⁇ ness of the axially directed wall of the preform.
  • the traction de- vices and/or the mandrel as well as the bottom support are, as a rule, provided with channels 98 through which fluid, such as a liquid passes for regulation of the temperature of the devices. Depending on the application, heat is either supplied or removed by means of the liquid.
  • a preform 10a located in the apparatus, and' its wall 15a,b undergoes, has undergone respectively an axial stretching (extension) and associated crystallisation.
  • FIG. 5 shows an intermediate preform 10b, formed by axial stretching of preform 10.
  • the intermediate preform has a bottom section lib, a mouth 12b, a ribbon-shaped mouth edge region 13b, a mouth edge ,14b, an axially directed wall 15b and a centre axis 16, i.e. the parts of the intermediate preform have reference numerals directly equivalent to those used for the preform 10 described in connection with Fig. 1.
  • FIGS. 6-9 show a basic embodiment of an apparatus in accordance with the invention. These Figures show an upper sleeve 30 and an lower sleeve 40 provided with channels 42 for temperature setting of the sleeve, and which sleeve is assumed to occupy a spatially fixed position, e.g. sleeve 40 is affixed to a frame (not shown).
  • the upper sleeve 30 is provided with channels 33 for flow of a fluid for tempe ⁇ rature setting of the sleeve, in addition to which there is disposed inside the sleeve a mandrel 50 which by drive means (not shown in the Figure) is displaceable relative to the upper sleeve in the axial direction of the sleeve.
  • the part 55 of the mandrel facing the lower sleeve 40 hereinafter termed the bottom section, has a shape mainly adapted to the shape of the bottom lib of the intermediate preform 10b, and is in the embodiment shown in the Figure thermally insulated from the rest of the mandrel, hereinafter termed the upper section 151 of the mandrel.
  • the bottom section has, in turn, a central sec ⁇ tion 56 which is thermally insulated from the outer circumferential portion 57 of the bottom section.
  • a central sec ⁇ tion 56 which is thermally insulated from the outer circumferential portion 57 of the bottom section.
  • channels 58,59 for temperature setting of the central sec ⁇ tion of the bottom section and its circumferential portion, respec ⁇ tively.
  • the upper section 151 of the mandrel is also provided with channels 53 for temperature setting.
  • the upper section of the mandrel, the central section of the bottom section, and its circum- ferential portion are thus indi idually adjustable to required tem ⁇ peratures.
  • a channel 52 for a pressure medium is disposed in the mandrel and is joined in the upper section of the mandrel via a con ⁇ nection device 54 to a pressure source 160, and is disposed in the lower section of the bottom section in order to open into the lower limiting surface 150 of the bottom section.
  • Channels 61 are provided for temperature setting of the inner sleeve.
  • a bottom support 75 is disposed inside the inner sleeve 60 for axial displacement therein by drive means (not shown in the Figures).
  • the bottom support is divided into a central section 78 and an outer circumferential section 79, thermally in- sulated from the former, corresponding to what has been shown in respect of the bottom section 55 of the mandrel.
  • Channels 76,77 for temperature setting of the bottom support are * disposed therein, for which reason the central section of the bottom support and its cir ⁇ cumferential section are also individually adjustable to required temperatures.
  • the upper sleeve 30 is provided with an upper stop device 32 which engages with an upper check (stop) device 99 e.g. adjustably affixed to the aforementioned frame and placed in a position such that when the upper stop device 32 abuts the upper check device 99 there is formed between the upper sleeve 30 and the lower sleeve 40 a columnar cavity 21a the breadth of which (the distance between the upper and the lower device in the Figure) exceeds the wall thickness of the circumferential mouth edge region 13b,c of the intermediate preform 10b,c. In the vicinity of the outer end region of the columnar cavity there is usually a device 23 which blocks cavity 21a entirely or partially.
  • an upper check (stop) device 99 e.g. adjustably affixed to the aforementioned frame and placed in a position such that when the upper stop device 32 abuts the upper check device 99 there is formed between the upper sleeve 30 and the lower sleeve 40 a columnar cavity 21a the breadth of which
  • the upper check device 99 can be displaced by the displacement devices (not shown in the Figures) to assume a position where it engages the stop device 32 and a position where the stop device 32 can at least partly travel therepast, whereby the upper sleeve 30 can be moved nearer to the lower sleeve 40 (cf. arrows A in Fig. 7).
  • the inner sleeve 60 is provided with stop devices 62 which in the upper position of the sleeve abut check (stop) devices 46 in the lower sleeve 40.
  • the stop device 62 and the check device 46 establish during abutment, that the upper limitation surface 63 of the inner sleeve 60, which surface has a shape substantially corresponding to that of the bottom section 55 of the mandrel, forms with said bottom section a columnar cavity 22 with a breadth somewhat exceeding the wall thickness in the mouth edge region.
  • the cavity 22 connects with the cavity 21a so that the two cavities together comprise a linked slot 21a-22 the width of which somewhat exceeds the thickness of the mouth edge region.
  • the bottom section 55 of the mandrel has a design such that ts lower limitation surface 150, in a region 51 adjacent the upper limitation surface 63 of the inner sleeve 60, has an down ⁇ wards and outwards directed location with the result that the limita ⁇ tion surface in this region comprises a guide surface delimitating the columnar cavity 22.
  • the guide surface is located on the circumferential outer portion 57 of the bottom section.
  • the upper sleeve 30 is provided with another stop device 31 which engages a check (stop) device 41 disposed on the lower sleeve 40.
  • the stop device 31 and the check device 41 have a mutual location such that when the stop device 31 abuts against the check device 41 a cavity 21b is formed between the upper sleeve and the lower sleeve, the cavity being of a slotlike shape having a width somewhat less than the wall thickness of the intermediate preform.
  • the stop device 31 also forms the device 23 which blocks the columnar cavity 21b outwards.
  • the intermediate preform has reference characters 10c to lOf, which refer to the actual reshaping stage of the preform.
  • Figs. 10-13 show a reshaped intermediate preform lOg which, compared with the intermediate preform 10c in Fig. 6, has an increased cross- -section.
  • Fig. 11 the ribbon-shaped mouth edge region 13g of the reshaped intermediate preform has been inserted into a slot-shaped recess 111 in a heating device 110.
  • Figures 12-13 show an outer sleeve 120 having an inner surface 127 which in the upper section 121 of the sleeve, continuously merges into an inner mouth surface 122 with a reduced circumference.
  • a bottom support 130 is supported for displacement within the sleeve by drive.means " (not shown in the Figures) in the axial direction of the sleeve.
  • Figures 12-13 show an upper mandrel 140 with a lower, primarily cylindrical section 141 and an upper section 142 with a greater circumference than the cylindrical section. The lower cylindrical section of the mandrel is adapted to the mouth surface
  • the outer surface 145 of the mandrel has, in the transition between the lower section 141 and the upper section 142, a shape adapted to the shape of the upper surface 126 of the outer sleeve 120 and forms after the transition a surface 146 primarily parallel to the upper surface of the sleeve in order to form a cavity or a slot 147 between the upper section 142 of the mandrel and the upper section 121 of the sleeve 120, when the mandrel is in its lower position; the cavity 147 forms a continuation of the slot 125, having a breadth that allows the edge region 13g of the reshaped intermediate preform to be inserted into the cavity.
  • the outer sleeve 120 and the mandrel 140 are provided with stop surfaces
  • the upper mandrel is, in certain embodiments, also provided with a channel 144 which, in cer ⁇ tain applications, is used in order to supply a pressure medium to the interior of the preform lOg during its reshaping.
  • the preform 10 is insert- ed in an apparatus 91-93 for setting of the material of the preform, at least in its primarily cylindrical section, to a suitable shaping temperature, preferably to a temperature exceeding the glass transi ⁇ tion temperature of the material (cf. Fig. 2).
  • the heated preform is then moved to the apparatus illustrated in Fig. 3 in which the wall thickness of the preform is reduced during simultaneous axial exten ⁇ sion of the wall as well as orientation and/or crystallisation of its material (cf. Figs. 3 and 4) for formation of the intermediate pre ⁇ form 10b, the primarily cylindrical section of which consists of stretched-and oriented and/or crystall sed material.
  • the material passes through the slot 90, by which means the material in a preferred embodiment of the inven ⁇ tion, obtains an orientation equivalent to that which occurs during material flow. As it moves into the slot, the material generally has a temperature exceeding its TG.
  • the intermediate preform 10b thus formed is then placed in the re ⁇ shaping device 30,40,50,60,75 illustrated in Figures 6-9.
  • the inter ⁇ mediate preform is reshaped into an expanded intermediate preform lOf in the reshaping device.
  • the intermedi ⁇ ate preform 10b is first placed in a position where it is enclosed by the inner sleeve 60 and abuts the bottom support 75.
  • a temperature conditioning of the intermediate preform 10b generally takes place, in that the inner sleeve has a temperature generally somewhat exceeding the glass transition temperature of the material (cf. Fig. 6).
  • the intermediate preform shrinks axially.
  • the intermediate preform has reference characters 10b and 10c, respec ⁇ tively, where 10c indicates that the intermediate preform has shrunk during the temperature conditioning.
  • the bottom support 75 is subsequently displaced upwards (cf. Fig. 7) at the same time as the interior of the intermediate preform is pres- surised by a pressure medium supplied via the channel 52 from the pressure source 160.
  • the pressure medium is heated in order to maintain or at least contribute towards maintain ⁇ ing the material of the intermediate preform at the required temper ⁇ ature.
  • the inner sleeve 60 and lower sleeve 40 thus have, relative to the mandrel 50 and upper sleeve 30 respectively, positions such that the previously described linked slot 21a,22 is formed.
  • Fig. 7 shows an embodiment of the invention where this positional setting is achieved by the upper stop device 32 when engaging with the upper check device 99 and by the lower stop device 62 when engaging the lower check device 46.
  • the relative locking between the devices means that during the upwards motion of the bottom support, the mouth edge 14b,14c of the intermediate preform as well as the adjoining mouth edge, region 13b,13c are displaced into the slot during simultaneous increase of the circumference of the intermediate preform in its mouth 12b,12c.
  • This displacement of the bottom support 75 and thus the intermediate preform continues until the mouth edge 14d reaches the stop device 31 of the upper sleeve 30.
  • the circumferential outer portion 57 of the bottom section has an elevated temperature (a temperature exceeding TG) in order to make the material more adapted to expand in the circumferential direction.
  • the upper check device 99 is subsequently displaced to the position where it can be passed by the stop device 32 (cf. Fig. 8), after which the upper sleeve 30 is displaced towards the lower sleeve 40 until the stop device 31 of the upper sleeve abuts against the check device 41 of the lower sleeve.
  • the material por ⁇ tions 13d are clamped in place next to the expanded mouth edge of the intermediate preform (i.e. equivalent to the ribbon-shaped circum ⁇ ferential mouth edge region 13d) between the upper sleeve and the lower sleeve.
  • the sleeves In the abutment regions for the material portions, the sleeves have .temperatures in excess of TG.
  • the inner sleeve 60 is subsequently displaced downwards in the Fig ⁇ ures at the same time as the mandrel 50 which successively expands the intermediate preform in its circumferential direction.
  • the mandrel thus has, at least in the region 51 where it abuts the ma ⁇ terial of the intermediate preform, a temperature above the TG of the material.
  • the downwards movements of the mandrel 50 and the inner sleeve 60 are synchronised so that the aforementioned slot 22 is maintained between the bottom section of the mandrel and the upper portions of the sleeve.
  • the intermediate preform By retaining the material in the mouth region of the intermediate preform in place, the intermediate preform is kept fixed between the upper sleeve 30 and the lower sleeve 40 whereby during the expansion the material in the intermediate pre- _. form is also subjected to axially directed stretching forces through the movement of the mandrel.
  • the bottom support 75 is simultaneously allowed to exert an upwardly directed force on the intermediate preform to reduce the magnitude of the stretching forces in the material of the intermediate preform, when this material is pressed upwards over and expanded by the mandrel. Practically, it has been shown that the retention of the edge portions of the intermedi ⁇ ate preform achieves a good result in production and a high produc ⁇ tion capacity.
  • FIG. 9 shows the shaping devices after a completed movement and the expanded intermediate preform lOf.
  • the expanded material of the inter edi- ate preform abuts against the outer surface of the mandrel 50, and as a rule also the inner surface of the lower sleeve 40.
  • These two sur ⁇ faces preferably have a temperature exceeding the TG of the material and as a rule one considerably exceeding the TG.
  • the materi ⁇ al is temperature-stabilised while retaining the shape that was de- termined by the lower sleeve 40 and the mandrel 50.
  • the selected temperature of both the sleeve and the mandrel and thus the temper ⁇ ature up to which temperature stability is achieved is determined by the maximum temperature at which the product which is being shaped is intended to be used.
  • con- tainers have been manufactured which are temperature-stable up to approximately 16QOC in that the inner surface had a temperature exceeding 160OC.
  • the mandrel 50 is also given a corresponding increased temperature.
  • the expanded intermediate preform lOf has in its mouth section an outwards-facing edge flange 17. In certain applications this is cut off, whereby the expanded intermediate preform lOg is formed (cf. Fig. 10).
  • the bottom section 55 of the mandrel 50 also includes both the central bottom section 56 and the circumferential outer portion 57, which are adjustable to specific temperatures independently of each other.
  • the bottom support 75 is likewise disposed with similarly separated sections 78,79. In certain applications this enables separate heat treatment of the mate ⁇ rial in the bottom section llf.llg of the expanded intermediate pre ⁇ form so that when the material has a low crystallisation it is pos ⁇ sible to thermally increase the same in order to achieve tempera- ture-stable and shape-stable material portions.
  • Figures 10-13 illustrate an embodiment of the invention where the expanded intermediate preform lOg with its mouth flange being cut is reshaped in its mouth section.
  • the ribbon-shaped circumferential mouth edge region 13g of the intermediate preform is inserted into the slot-shaped recesses 111 in the heating device 110.
  • the material is thus heated to a temperature somewhat exceeding the aforementioned maximum temperature at which the container which is being manufactured is intended to be used.
  • the intermediate preform expanded in this manner is subsequently introduced into the sleeve 120 for reshaping of the mouth 12g of the intermediate preform.
  • the heated material is pressed into the slot 125 between the mandrel 140 and the upper section 121 of the sleeve 120 with a reduced diameter, whereby the circumference of the expanded intermediate preform in the mouth section is reduced.

Landscapes

  • Mechanical Engineering (AREA)
  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)
  • Supplying Of Containers To The Packaging Station (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
  • Making Paper Articles (AREA)
  • Auxiliary Devices For And Details Of Packaging Control (AREA)
  • External Artificial Organs (AREA)
  • Shaping By String And By Release Of Stress In Plastics And The Like (AREA)
  • Detergent Compositions (AREA)
  • Food-Manufacturing Devices (AREA)
  • Separation Using Semi-Permeable Membranes (AREA)
  • Pens And Brushes (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)
  • Table Devices Or Equipment (AREA)
  • Artificial Filaments (AREA)
  • Containers And Plastic Fillers For Packaging (AREA)

Abstract

A hollow body (e.g. a container) as well as a method and an apparatus for its manufacture in which an axially directed wall of the body primarily comprises oriented and/or crystallised plastics material. A tubular preform (10d) is fixed in a circumferential region (13d) in the vicinity of the mouth edge (14d) of the preform between mechanical forming devices (30, 40), after which the devices, during continued clamping of the circumferential region, are displaced in the axial direction of the preform relative to a mandrel (50). Thus, the mandrel is displaced into the preform during simultaneous expansion thereof and the material is oriented and/or crystallised. In a preferred embodiment there is made a certain compensation of the stretching forces, which arise in the material when inserting the mandrel, by applying a force to the bottom of the preform by a bottom support (75).

Description

Container, method and apparatus for manufacturing the same
The. present invention relates to a hollow body (e.g. a container) whose axially directed wall(s) comprise(s) oriented and/or crystal¬ lised plastics material, in addition to which the invention relates to a method and an apparatus for reshaping a primarily tubular pre- form of plastics material into the hollow body by means of mechanical shaping devices.
It has been previously known to reshape blanks of thermoplastics material into a container, where the blank includes portions of axially oriented material. The reshaping takes place by means of a blowing process, during which the material of the blank is blown against mould walls whose shape corresponds to the shape of the con¬ tainer being produced. Patent publication GB 2.076.731 A describes such a technique for the manufacture of a bottle-shaped container.
US Patent No. 4,381,279 describes a technique where a blank of ori- ented thermoplastics material is remoulded by a blowing process into a container. Also this patent publication discloses a technique to remould an oriented blank into a container.
US Patent No. 4,372,908 reveals a technique where a stretched and oriented blank of thermoplastics material is reshaped into a con- tainer by means of one or more mechanical shaping processes. In accordance with the technique revealed in the patent the circum¬ ference of the body of the container is reduced during the reshaping of the blank into the container.
There is a considerable need for containers of plastic materials suitable for high-temperature applications and/or storage of liquids under pressure, e.g. storage of soft drinks, beer, etc. High-tempe¬ rature applications mean e.g. that the contents of filled and" sealed
Figure imgf000003_0001
containers are pasteurised (60-70OC), that the liquid is filled directly into the containers from boiling (warm filling) or that the contents of filled and sealed containers are sterilised (at least 1210C).
5 Further requirements in respect of containers of plastics material are that it should be possible to manufacture containers in which the body of the container and its mouth section have cross-sections independent of each other, e.g. the body has a polygonal cross-sec¬ tion whilst the mouth of the container is circular. The circular
10 shape of the mouth is, as a rule, desirable in order to facilitate sealing of the container.
In order to reduce the unit costs of the containers it is further necessary to adapt the distribution of material in the individual container to estimated mechanical stresses in various parts of the
15 container (mouth, container body and bottom). Additionally, it is also important that in each region (part) of the container material distribution should be as even as possible, since the thinnest and thus the weakest section of each such region is decisive of the stresses which the container is able to withstand. In addition to the
20 material thickness, the mechanical strength of the containers is naturally also determined by the orientation of the material and/or its crystallisation. It is especially in the case of thermoplastics material that the thermal crystallisation is of importance.
A further requirement for containers of the kind envisaged here and 25 especially for a container intended for high-temperature applications is that the- shrinkage -which occurs during heating of stretched and .-- oriented thermoplastics material is eliminated or reduced to accept- . '- ' able values. " .
- In storing liquids under pressure in a container of bottle or can -30 - type, it is true in purely physical terms that wit an inner pressure in the container its wall material is 'subjected to a stress that is approximately twice as large in the circumferential direction than in the axial direction. In order to improve the strength of the material in the case of orientable thermoplastics material, the container is moulded in accordance with a known and generally applied technique, by means of a blowing process, at the same time as the temperature of the material is adapted to the properties of the material in ques¬ tion, in order to stretch the material during the blowing process and thereby orientate the same.
The blowing technique possesses the disadvantage that the distribu¬ tion of material during the moulding of the container is not fully 0 controllable since, during the expansion of the blank into the con¬ tainer, it is not possible to determine and control exactly where and how the stretching of the material, and thus its orientation, will proceed. Normally, the stretching begins at a number of starting points, whose positions are determined by the prevailing temperature 5 distribution in the material, in addition to stretching forces aris¬ ing therein. The propagation of expansion, and the stretch ratio ob¬ tained are furthermore temperature-dependent, which results in a vary¬ ing material thickness of the moulded container, i.e. even in a sec¬ tion at right-angles to the axial direction the thickness of the 0 container wall varies in the circumferential direction. The addition¬ al heating of the material which takes place when it crystallises through the stretching, achieves in the material an additional uneven temperature distribution which results in an increase in variations in the thickness of the wall in the moulded container. Corresponding 5 variations also occur in the axial direction of the container, i.e. in axial sections through regions of primarily equally large circum¬ ference, alternately thinner and thicker material portions are pre¬ sent. The wall thickness of the blank is thus selected in accordance with known technique with regard to the aforementioned uncertainty in 0 the stretching and thinning out of the material, which implies an - - . 'cαrer-dimens oning of the blank-,, and thus also a surplus of material in the moulded container. In order to attain temperature stability in containers of orientable thermoplastics material, it is known to temperature-stabilise the containers in that during the blowing of the containers the container material is allowed to touch hot mould walls against which the mate- rial abuts for a relatively long period (of the order of magnitude of 1-2 minutes). This abutment is realised in that after blowing, an inner overpressure is maintained inside the blown container, whereby the wall material is pressed against the walls of the mould. Long cycle times, however, make this an expensive technique.
The present invention relates to a technique where all aforementioned disadvantages are eliminated. In accordance with the invention one starts with a preform of orientable and/or crystalusable material from which a container is manufactured with high mechanical strength and temperature stability and with a considerably improved material distribution, compared with previously known techniques, in that this is fully controlled. In accordance with the invention, the time re¬ quirement for the manufacture of each individual container is also reduced in comparison with that in previous known techniques, in addition to which the invention allows a simplified construction of the production equipment. By means of the invention the quantity of material in each container is thus reduced, the desired temperature stability is achieved, and costs are reduced in comparison to pre¬ viously known and used techniques.
In accordance with the invention, a preform of plastics material is reshaped, which has the property of being able to be oriented and/or crystallised by a mechanical processing, into a container in a number of consecutive reshaping processes which, in a preferred embodiment, take place in distinctly separate sub-stages. In every such process or stage the material is stretched (extended)' in either the axial or the circumferential direction of the future container. By stretching (extending) the material every time to a controlled extent, the material accumulates a total stretching (extension) and a reduction in thickness equivalent to tha.t._which_ is required in order to supply the material with the desired and pre-determined orientation or crystallisation and thus the necessary strength properties. The con¬ trolled stretching (extension) and the controlled reduction of the material thickness causes the moulded container to have the same material thickness in sections at right-angles to the axis of the container, thereby avoiding the variation in thickness, which con¬ tainers manufactured in accordance with known techniques have in axial sections through regions of primarily equally large circum¬ ference.
In mechanical stretching (expansion) of the preform in the circum- ferential direction, there are certain difficulties present in achieving a required degree of stretching (degree of expansion) in each individual stage of stretching, unless special measures are taken. In accordance with the invention, a primarily ribbon-shaped, circumferential region in the vicinity of the mouth edge of the pre- form is fixed between mechanical devices which displace the preform in its axial direction across a mandrel during simultaneous expansion of the preform. Since the material of the preform is thus subjected to stretching forces, the tendencies towards folding of the material, when the preform expands in its circumferential direction, are avoid- ed. It is, in accordance with the invention, thus possible in many applications to achieve a required increase of the dimensions in the circumferential direction in a single reshaping stage.
In a preferred embodiment, the tractive forces are supplemented by compressive forces which are applied in the vicinity of the bottom section of the preform, and which are directed towards the mouth of the preform. This technique is employed when the increase in the dimensions in the circumferential direction is large.
In accordance with a preferred embodiment of the invention, the pre¬ form is reshaped into the container in all sub-stages by use of mechanical reshaping devices. The mechanical stretching (extension or expansion, respectively) takes place in every stage with the material at a specific and contrailed temperature which can be selected within a wide range. The choice of temperature is determined however by the special effect which it is required to achieve in the moulding stage in question. For materials with a distinct glass transition tempera¬ ture-, hereinafter abbreviated as TG, e.g. the temperature of the mate- rial is, in certain, and in general, the initial moulding stages, ilower than TG, while in the concluding stage or stages the .tempera¬ ture generally exceeds TG. In the case of the material, polyethylene terephthalate, hereinafter abbreviated as PET, the material attains, in a preferred embodiment of the invention, temperatures within the range 70-160OC, in connection with the concluding shaping stages, while in the initial shaping stages it generally has a lower tempe¬ rature.
In certain applications of the invention, e.g. where one intends to obtain a container with a shape which is difficult to achieve by means of mechanical shaping devices, at least one of the shaping stages, and preferably the last one, comprises a blow moulding stage. In connection herewith the material is heated to a temperature close to or exceeding the maximum temperature at which the material was previously shaped mechanically.
in the dependent claims further appropriate embodiments of the invention are stated.
The invention is described in greater detail in connection with a number of figures, where
Figs. 1-5 show the shaping of a preform into an intermediate preform by extension of the preform in its axial direction when the preform passes through a gap .- that reduces the material thickness,
Figs. 6-9 show expansion of the preform in its circύ.mferen- tial direction, and
Figs. 10-13 show reshaping of the expanded preform into a container. Fig. 1 contains a preform 10 with a bottom section 11, a mouth 12, a ribbon-shaped, circumferential mouth edge region 13, a mouth edge 14, and an axially directed wall 15, located between the mouth and the bottom section. The central axis of the preform is denoted by refer- ence numeral 16. The preform is, in Fig. 2, placed in an apparatus for temperature setting of the preform material. The apparatus in¬ cludes a sleeve 91, a mandrel 92 and a bottom support 93. All these devices are provided with channels 97 through which a fluid, such as a liquid passes for individual setting of each device to a certain working temperature. The devices are adjustable to positions where there is formed between them a cavity whose shape substantially corresponds to that of the preform. A preform which is placed in the cavity is thus enclosed on both the inside and the outside by the devices and assumes a temperature which in every part of the preform is determined by the temperatures of the adjoining devices and the time the preform stays in the cavity.
Figs. 3 and 4 show a basic apparatus for reduction of the material thickness of the preform during its simultaneous extension in the axial direction. The apparatus includes a bottom support 94, a mandrel 95 and a traction device 96 which encloses the mandrel and is displaced in its axial direction by displacement devices (not shown in the Figures). Between the mandrel and the traction device there is located a slot 90 the breadth of which less than the material thick¬ ness of the axially directed wall of the preform. The traction de- vices and/or the mandrel as well as the bottom support are, as a rule, provided with channels 98 through which fluid, such as a liquid passes for regulation of the temperature of the devices. Depending on the application, heat is either supplied or removed by means of the liquid. There is a preform 10a, located in the apparatus, and' its wall 15a,b undergoes, has undergone respectively an axial stretching (extension) and associated crystallisation.
'/ Fig. 5 shows an intermediate preform 10b, formed by axial stretching of preform 10. The intermediate preform has a bottom section lib, a mouth 12b, a ribbon-shaped mouth edge region 13b, a mouth edge ,14b, an axially directed wall 15b and a centre axis 16, i.e. the parts of the intermediate preform have reference numerals directly equivalent to those used for the preform 10 described in connection with Fig. 1.
The Figures 6-9 show a basic embodiment of an apparatus in accordance with the invention. These Figures show an upper sleeve 30 and an lower sleeve 40 provided with channels 42 for temperature setting of the sleeve, and which sleeve is assumed to occupy a spatially fixed position, e.g. sleeve 40 is affixed to a frame (not shown). The upper sleeve 30 is provided with channels 33 for flow of a fluid for tempe¬ rature setting of the sleeve, in addition to which there is disposed inside the sleeve a mandrel 50 which by drive means (not shown in the Figure) is displaceable relative to the upper sleeve in the axial direction of the sleeve. The part 55 of the mandrel facing the lower sleeve 40, hereinafter termed the bottom section, has a shape mainly adapted to the shape of the bottom lib of the intermediate preform 10b, and is in the embodiment shown in the Figure thermally insulated from the rest of the mandrel, hereinafter termed the upper section 151 of the mandrel. The bottom section has, in turn, a central sec¬ tion 56 which is thermally insulated from the outer circumferential portion 57 of the bottom section. In the bottom section there are disposed channels 58,59 for temperature setting of the central sec¬ tion of the bottom section and its circumferential portion, respec¬ tively. The upper section 151 of the mandrel is also provided with channels 53 for temperature setting. The upper section of the mandrel, the central section of the bottom section, and its circum- ferential portion are thus indi idually adjustable to required tem¬ peratures. A channel 52 for a pressure medium is disposed in the mandrel and is joined in the upper section of the mandrel via a con¬ nection device 54 to a pressure source 160, and is disposed in the lower section of the bottom section in order to open into the lower limiting surface 150 of the bottom section. Inside the lower sleeve 40 there is disposed an inner sleeve 60, displaceable in the axial direction of the sleeve 40 by drive means (not shown in the Figures), the inner surface 64 of which has a shape primarily in correspondence with the outer surface of the intermediate preform. Channels 61 are provided for temperature setting of the inner sleeve. A bottom support 75 is disposed inside the inner sleeve 60 for axial displacement therein by drive means (not shown in the Figures). In certain embodiments the bottom support is divided into a central section 78 and an outer circumferential section 79, thermally in- sulated from the former, corresponding to what has been shown in respect of the bottom section 55 of the mandrel. Channels 76,77 for temperature setting of the bottom support are* disposed therein, for which reason the central section of the bottom support and its cir¬ cumferential section are also individually adjustable to required temperatures.
The upper sleeve 30 is provided with an upper stop device 32 which engages with an upper check (stop) device 99 e.g. adjustably affixed to the aforementioned frame and placed in a position such that when the upper stop device 32 abuts the upper check device 99 there is formed between the upper sleeve 30 and the lower sleeve 40 a columnar cavity 21a the breadth of which (the distance between the upper and the lower device in the Figure) exceeds the wall thickness of the circumferential mouth edge region 13b,c of the intermediate preform 10b,c. In the vicinity of the outer end region of the columnar cavity there is usually a device 23 which blocks cavity 21a entirely or partially.
The upper check device 99 can be displaced by the displacement devices (not shown in the Figures) to assume a position where it engages the stop device 32 and a position where the stop device 32 can at least partly travel therepast, whereby the upper sleeve 30 can be moved nearer to the lower sleeve 40 (cf. arrows A in Fig. 7).
The inner sleeve 60 is provided with stop devices 62 which in the upper position of the sleeve abut check (stop) devices 46 in the lower sleeve 40. The stop device 62 and the check device 46 establish during abutment, that the upper limitation surface 63 of the inner sleeve 60, which surface has a shape substantially corresponding to that of the bottom section 55 of the mandrel, forms with said bottom section a columnar cavity 22 with a breadth somewhat exceeding the wall thickness in the mouth edge region. The cavity 22 connects with the cavity 21a so that the two cavities together comprise a linked slot 21a-22 the width of which somewhat exceeds the thickness of the mouth edge region. The bottom section 55 of the mandrel has a design such that ts lower limitation surface 150, in a region 51 adjacent the upper limitation surface 63 of the inner sleeve 60, has an down¬ wards and outwards directed location with the result that the limita¬ tion surface in this region comprises a guide surface delimitating the columnar cavity 22. In the case of a divided bottom section the guide surface is located on the circumferential outer portion 57 of the bottom section.
The upper sleeve 30 is provided with another stop device 31 which engages a check (stop) device 41 disposed on the lower sleeve 40. The stop device 31 and the check device 41 have a mutual location such that when the stop device 31 abuts against the check device 41 a cavity 21b is formed between the upper sleeve and the lower sleeve, the cavity being of a slotlike shape having a width somewhat less than the wall thickness of the intermediate preform. In Figures 6-9, the stop device 31 also forms the device 23 which blocks the columnar cavity 21b outwards. Finally, it should be mentioned that in Figs. 6-9 the intermediate preform has reference characters 10c to lOf, which refer to the actual reshaping stage of the preform.
Figs. 10-13 show a reshaped intermediate preform lOg which, compared with the intermediate preform 10c in Fig. 6, has an increased cross- -section. In Fig. 11 the ribbon-shaped mouth edge region 13g of the reshaped intermediate preform has been inserted into a slot-shaped recess 111 in a heating device 110.
Figures 12-13 show an outer sleeve 120 having an inner surface 127 which in the upper section 121 of the sleeve, continuously merges into an inner mouth surface 122 with a reduced circumference. A bottom support 130 is supported for displacement within the sleeve by drive.means" (not shown in the Figures) in the axial direction of the sleeve. In addition, Figures 12-13 show an upper mandrel 140 with a lower, primarily cylindrical section 141 and an upper section 142 with a greater circumference than the cylindrical section. The lower cylindrical section of the mandrel is adapted to the mouth surface
122 of the outer sleeve such that there is formed between the outer limitation surface 145 of the mandrel an inner mouth surface 122, a slot 125 with a breadth somewhat exceeding the material thickness of the mouth edge region 13g of the preform. The outer surface 145 of the mandrel has, in the transition between the lower section 141 and the upper section 142, a shape adapted to the shape of the upper surface 126 of the outer sleeve 120 and forms after the transition a surface 146 primarily parallel to the upper surface of the sleeve in order to form a cavity or a slot 147 between the upper section 142 of the mandrel and the upper section 121 of the sleeve 120, when the mandrel is in its lower position; the cavity 147 forms a continuation of the slot 125, having a breadth that allows the edge region 13g of the reshaped intermediate preform to be inserted into the cavity. The outer sleeve 120 and the mandrel 140 are provided with stop surfaces
123 and 143 respectively, which guarantee the intended distance in the axial direction between the sleeve and the mandrel and thus the intended breadth of the cavity or slot 146. The upper mandrel is, in certain embodiments, also provided with a channel 144 which, in cer¬ tain applications, is used in order to supply a pressure medium to the interior of the preform lOg during its reshaping.
In a preferred embodiment of the invention, the preform 10 is insert- ed in an apparatus 91-93 for setting of the material of the preform, at least in its primarily cylindrical section, to a suitable shaping temperature, preferably to a temperature exceeding the glass transi¬ tion temperature of the material (cf. Fig. 2). The heated preform is then moved to the apparatus illustrated in Fig. 3 in which the wall thickness of the preform is reduced during simultaneous axial exten¬ sion of the wall as well as orientation and/or crystallisation of its material (cf. Figs. 3 and 4) for formation of the intermediate pre¬ form 10b, the primarily cylindrical section of which consists of stretched-and oriented and/or crystall sed material. Fig. 3 shows the preform during reshaping into the intermediate preform 10b. In the orientation/crystallisation, the material passes through the slot 90, by which means the material in a preferred embodiment of the inven¬ tion, obtains an orientation equivalent to that which occurs during material flow. As it moves into the slot, the material generally has a temperature exceeding its TG.
The intermediate preform 10b thus formed is then placed in the re¬ shaping device 30,40,50,60,75 illustrated in Figures 6-9. The inter¬ mediate preform is reshaped into an expanded intermediate preform lOf in the reshaping device. In order to allow reshaping, the intermedi¬ ate preform 10b is first placed in a position where it is enclosed by the inner sleeve 60 and abuts the bottom support 75. In this posi¬ tion, a temperature conditioning of the intermediate preform 10b generally takes place, in that the inner sleeve has a temperature generally somewhat exceeding the glass transition temperature of the material (cf. Fig. 6). If this temperature conditioning is performed at a temperature which exceeds the temperature which the material has when passing through the slot 90, the intermediate preform shrinks axially. In Fig. 6 these two alternatives are denoted in that the intermediate preform has reference characters 10b and 10c, respec¬ tively, where 10c indicates that the intermediate preform has shrunk during the temperature conditioning.
The bottom support 75 is subsequently displaced upwards (cf. Fig. 7) at the same time as the interior of the intermediate preform is pres- surised by a pressure medium supplied via the channel 52 from the pressure source 160. In certain applications, the pressure medium is heated in order to maintain or at least contribute towards maintain¬ ing the material of the intermediate preform at the required temper¬ ature. The inner sleeve 60 and lower sleeve 40 thus have, relative to the mandrel 50 and upper sleeve 30 respectively, positions such that the previously described linked slot 21a,22 is formed. Fig. 7 shows an embodiment of the invention where this positional setting is achieved by the upper stop device 32 when engaging with the upper check device 99 and by the lower stop device 62 when engaging the lower check device 46. The relative locking between the devices means that during the upwards motion of the bottom support, the mouth edge 14b,14c of the intermediate preform as well as the adjoining mouth edge, region 13b,13c are displaced into the slot during simultaneous increase of the circumference of the intermediate preform in its mouth 12b,12c. This displacement of the bottom support 75 and thus the intermediate preform continues until the mouth edge 14d reaches the stop device 31 of the upper sleeve 30. In certain embodiments, the circumferential outer portion 57 of the bottom section has an elevated temperature (a temperature exceeding TG) in order to make the material more adapted to expand in the circumferential direction.
The upper check device 99 is subsequently displaced to the position where it can be passed by the stop device 32 (cf. Fig. 8), after which the upper sleeve 30 is displaced towards the lower sleeve 40 until the stop device 31 of the upper sleeve abuts against the check device 41 of the lower sleeve. In this position, the material por¬ tions 13d are clamped in place next to the expanded mouth edge of the intermediate preform (i.e. equivalent to the ribbon-shaped circum¬ ferential mouth edge region 13d) between the upper sleeve and the lower sleeve. In the abutment regions for the material portions, the sleeves have .temperatures in excess of TG.
The inner sleeve 60 is subsequently displaced downwards in the Fig¬ ures at the same time as the mandrel 50 which successively expands the intermediate preform in its circumferential direction. The mandrel thus has, at least in the region 51 where it abuts the ma¬ terial of the intermediate preform, a temperature above the TG of the material. As a rule, the downwards movements of the mandrel 50 and the inner sleeve 60 are synchronised so that the aforementioned slot 22 is maintained between the bottom section of the mandrel and the upper portions of the sleeve. By retaining the material in the mouth region of the intermediate preform in place, the intermediate preform is kept fixed between the upper sleeve 30 and the lower sleeve 40 whereby during the expansion the material in the intermediate pre- _. form is also subjected to axially directed stretching forces through the movement of the mandrel. As a rule, the bottom support 75 is simultaneously allowed to exert an upwardly directed force on the intermediate preform to reduce the magnitude of the stretching forces in the material of the intermediate preform, when this material is pressed upwards over and expanded by the mandrel. Practically, it has been shown that the retention of the edge portions of the intermedi¬ ate preform achieves a good result in production and a high produc¬ tion capacity. In those applications where the retention effect is supplemented by an upwardly directed pressing force from the bottom support 75, both a further improved result and a shortened cycle time are generally achieved. Fig. 9 shows the shaping devices after a completed movement and the expanded intermediate preform lOf.
Immediately after expansion, the expanded material of the inter edi- ate preform abuts against the outer surface of the mandrel 50, and as a rule also the inner surface of the lower sleeve 40. These two sur¬ faces preferably have a temperature exceeding the TG of the material and as a rule one considerably exceeding the TG. Whereby, the materi¬ al is temperature-stabilised while retaining the shape that was de- termined by the lower sleeve 40 and the mandrel 50. The selected temperature of both the sleeve and the mandrel and thus the temper¬ ature up to which temperature stability is achieved is determined by the maximum temperature at which the product which is being shaped is intended to be used. Thus, for polyethylene terephthalate (PET), con- tainers have been manufactured which are temperature-stable up to approximately 16QOC in that the inner surface had a temperature exceeding 160OC. In certain applications, the mandrel 50 is also given a corresponding increased temperature. As will be evident from Fig. 9 the expanded intermediate preform lOf has in its mouth section an outwards-facing edge flange 17. In certain applications this is cut off, whereby the expanded intermediate preform lOg is formed (cf. Fig. 10). As will be evident from the above description, the bottom section 55 of the mandrel 50 also includes both the central bottom section 56 and the circumferential outer portion 57, which are adjustable to specific temperatures independently of each other. The bottom support 75 is likewise disposed with similarly separated sections 78,79. In certain applications this enables separate heat treatment of the mate¬ rial in the bottom section llf.llg of the expanded intermediate pre¬ form so that when the material has a low crystallisation it is pos¬ sible to thermally increase the same in order to achieve tempera- ture-stable and shape-stable material portions. Thus, it is possible in accordance with the invention to obtain in the bottom section of the intermediate preform annular opaque material portions or disc¬ like ones.
Figures 10-13 illustrate an embodiment of the invention where the expanded intermediate preform lOg with its mouth flange being cut is reshaped in its mouth section. For this purpose, the ribbon-shaped circumferential mouth edge region 13g of the intermediate preform is inserted into the slot-shaped recesses 111 in the heating device 110. The material is thus heated to a temperature somewhat exceeding the aforementioned maximum temperature at which the container which is being manufactured is intended to be used.
The intermediate preform expanded in this manner is subsequently introduced into the sleeve 120 for reshaping of the mouth 12g of the intermediate preform. By means of relative motion between the bottom support 130 and the sleeve 120 the heated material is pressed into the slot 125 between the mandrel 140 and the upper section 121 of the sleeve 120 with a reduced diameter, whereby the circumference of the expanded intermediate preform in the mouth section is reduced. By means of a subsequent relative movement between the mandrel 140 and the 'sleeve 120 while simultaneously supporting the intermediate preform by the bottom support 130 (with the interior of the inter¬ mediate preform being pressurised if necessary or required) upper edge portions of the intermediate preform are folded outwards and move into the slot 147 between the upper section 142 of the mandrel and the upper section 121 of the sleeve for the formation of an outwards-facing flange 18. Thus, an embodiment of a hollow body (container) 19 in accordance with the invention is completed.
In the above description the expressions upper, lower, vertical, etc. have been used, which should, however, be considered solely as a means of facilitating the description. It is evident that in accor¬ dance with the invention the apparatus can assume arbitrary orien¬ tations. It s also possible, within the scope of the invention, to allow the preform, intermediate preform, and the finished container to have an arbitrary cross-section which may also have a different shape in different sections of both preform, intermediate preform, and finished container. The reshaping of the mouth section described in the preceding paragraph is also applicable to intermediate pre¬ forms of non-circular cross-section. The technique is also applicable to shape non-circular into circular mouth portions.
The above detailed description has solely referred to a limited num¬ ber of embodiments of the invention, but it will be readily under¬ stood by those skilled in the art, that the invention includes a large number of embodiments within the scope of the following claims.

Claims

1. A hollow body (19) having an axis and comprising an axially directed wall of orienter and/or crystallised plastics material, said body being formed from a preform which is expanded both axially and circu ferentially, characterised in, that the walls of the body have an uniform thickness both in axial sections and in sections at righth angles to the axis, in regions of equal expansion in the circumferential direction.
2. A hollow body (19) as claimed in claim 1, characterised in, that said preform is mechanically expanded substantially without ax al stretching to form said body.
3. A hollow body (19) as claimed in claim 1, the body comprising a cylindrical mouth portion connected to a cylindrical body por¬ tion, and said mouth portion being of smaller diameter than said body portion, characterised in, that said mouth portion is formed by an inwardly deformation of a part of said body without axial stretching of said wall to form a mouth- portion wherein the thickness of the wall is larger than the thickness of the wall of the body portion.
4. A method of reforming a primarily tubular preform (10) of ori- entable and/or crystallisable plastics material into a hollow body, characterised in, that the preform in a circumferential region (13) adjacent to the mouth edge (14) of the preform is fixed between mechanical devices (30,40) and that while con¬ tinuously fixing the preform in said circumferential region displacing said circumferential region by effecting relative movement between the mechanical, devices (30,4,0) and a mandrel (50) in its axial direction for inserting thaimandrel in the __ preform during simultaneous expansion of said-'preform.
5. A method of forming a hollow body as claimed' in claim 4, charac- terised in, that the material in a primarily cylindrical section of the preform, prior'to the expansion-of the preform,- undergoes an extension in the swrraT direction of the preform during s mul- taneous reduction of the material thickness, for orientation and/or crystallisation of the material in the preform.
6. Method of forming a hollow body as claimed in claim 4 or 5, characterised in, that the material during the extension is oriented and/or crystallised corresponding to the orientation and/or crystallisation which the material would have obtained during stretching until material flow or yielding is obtained.
7. A method of forming a hollow body as claimed in any of claims 4-6, characterised in, that the c rcumferential region (13) for the fixing of the preform by the mechanical devices (30,40) is given the shape of an edge flange of thicker material and/or is formed as an edge flange (13d) facing outwards from the mouth (12) of the preform.
8. A method of forming a hollow body as claimed in claim 7, charac- terised, in that during the relative movement of the mandrel
(50) and the mechanical devices (30,40) a force which is directed ' towards the mouth (12) of the preform is applied to the bottom section (11) of the preform.
9. A method of forming a hollow body as claimed in claim 7, charac- terised in, that the expansion of the preform takes place in stages in that the mandrel (50) is provided with a number of suc- ' cessive portions of increasing circumference and/or that the ex¬ pansion of the preform takes place in stages by successivly intro¬ ducing mandrels (50) of increasingly greater circumference into the preform.
10. A method of forming a hollow body as claimed in claim 7, charac¬ terised in, that the mechanical devices (30,40) for fixing of the preform in the circumferential region (13) have abutment surfaces against the circumferential region, the temperature of said surfaces being increased to exceed the glass transition temperature (TG) of the plastics material.
11. A method of forming a hollow body as claimed in claim 7, charac¬ terised in, that the mandrel (50) is heated, at least in the region (51) where the mandrel and the material of the preform are brought into contact, to a temperature above the glass transition temperature (TG) of the material for expansion of the preform.
12. A method of forming a hollow body as claimed in claim 7, charac¬ terised in, that prior to the expansion of the preform the mate¬ rial thereof is enclosed by a sleeve (60) whose surfaces facing the preform have a temperature not less than about 30oc below TG or about 70OC more than TG.
13. A method of forming a hollow body as claimed in any of claims 7 or 12, characterised in, that the material of the preform after the expansion of the preform is enclosed by a sleeve (40) the temperature of which exceeds the glass transition temperature (TG) for temperature stabilisation of the material reformed during the expansion.
14. A method of forming a hollow body as claimed in any of the claims 4-13, characterised in, that the material in a circumferential region (13g) in the vicinity of and also including a mouth edge (14g) of the preform is heated to a temperature exceeding the glass transition temperature (TG) of the material and preferably to a temperature exceeding that at which thermostabilisation of the preform was performed and that the material in the circum¬ ferential region is given its final shape by mechanical forming devices (120,140).
15. A method as claimed in claim 14, characterised in, that the circumferential region (13) which is fixed between the mechanical devices (30,40) is detached from the preform, that the material in a second circumferential region (13g) comprising the mouth edge (14g) formed by the detaching is heated to a temperature exceeding the glass transi ion temperature (TG)- of the material and preferably to a temperature corresponding to that at which thermostabilisation of the preform was performed and that the material in the second circumferential region (13g) is gi.ven its final shape by the mechanical forming devices (120,140).
16. A method of forming a hollow body as claimed in claims 14 or 15, characterised in, that the circumference of the circumferential region (13,13g) is reduced by an axial displacement of said re¬ gion relative to a sleeve-shaped device (120), after which said region in an end region comprising the mouth edge (14g) is bent over to form a mouth flange (18) facing outwardly from the centre axis (16) of the preform.
17. A method of forming a hollow body as claimed in claim 15, charac¬ terised in, that the circumference of the second circumferential region (13g) is reduced by an axial displacement of said region relative to a sleeve-like device (120), after which said region in an end region comprising the mouth edge (14g) is bent over to form a mouth flange (18) facing outwardly from the centre axis (16) of the preform.
18. Apparatus for forming a hollow body from a hollow tubular preform in which the axially directed walls of the body comprise oriented and/or crystallised plastics material, characterised in, that the apparatus comprises mechanical devices (30,40,75) movable relative to each other to form a circumferential ribbon-shaped region in the vicinity of a mouth edge of the preform, and that said mechanical devices comprise a bottom support (75) which is disposed for axial displacement within at least one of said other mechanical devices (30,40) for movement relative to said other devices during simultaneous expansion of the preform to form said circumferential ribbon-shaped region.
19. Apparatus as claimed in claim 18, characterised in, that the _~ apparatus comprises- a mandrel (50) which is disposed for axial displacement within at east. one of said' other "mechanical devices -. (30,40) for movement .relati e to sai d, other devices^ (.30,40) to effect expansion of said preform when the preform- is secured by said other mechanical devices in- aid ribbon-shaped region.
20. Apparatus as claimed in claim 19, characterised in, that the apparatus comprises an axially displaceable sleeve (60) within at least one of said other mechanical devices (30,40) and facing said mandrel (50) to support the preform at the outer perifery thereof during expansion of said preform' and- that said sleeve (60) undergoes axial displacement in synchronism with said mandrel (50).
PCT/SE1985/000510 1984-07-05 1985-12-09 Container, method and apparatus for manufacturing the same WO1986003713A1 (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
DE8686900323T DE3572455D1 (en) 1984-12-14 1985-12-09 Container, method and apparatus for manufacturing the same
AT86900323T ATE45700T1 (en) 1984-12-14 1985-12-09 CONTAINER, METHOD AND APPARATUS FOR PRODUCTION THEREOF.
IN356/CAL/86A IN168171B (en) 1984-12-14 1986-05-08
FI863260A FI88373C (en) 1984-12-14 1986-08-11 FOERFARANDE OCH ANORDNING FOER FRAMSTAELLNING AV BEHAOLLARE
NO863238A NO863238L (en) 1984-12-14 1986-08-12 CONTAINER, PROCEDURE AND DEVICE FOR MANUFACTURING THIS.
DK387086A DK163970C (en) 1984-12-14 1986-08-14 METHOD AND APPARATUS FOR MANUFACTURING A CONTAINER
IN822/CAL/89A IN171425B (en) 1984-07-05 1989-10-03

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SE8406373-4 1984-12-14
SE8406373A SE450630B (en) 1984-12-14 1984-12-14 SET AND DEVICE FOR MANUFACTURING A PLASTIC CONTAINER THROUGH REFORMING A PRINCIPLES

Publications (1)

Publication Number Publication Date
WO1986003713A1 true WO1986003713A1 (en) 1986-07-03

Family

ID=20358173

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/SE1985/000510 WO1986003713A1 (en) 1984-07-05 1985-12-09 Container, method and apparatus for manufacturing the same

Country Status (21)

Country Link
US (2) US4927591A (en)
EP (1) EP0204810B1 (en)
JP (2) JPS62501138A (en)
AT (2) ATE107221T1 (en)
AU (2) AU597242B2 (en)
BE (1) BE903847A (en)
CA (2) CA1283064C (en)
CH (2) CH675225A5 (en)
DE (2) DE3572455D1 (en)
DK (1) DK163970C (en)
ES (1) ES8701589A1 (en)
FI (1) FI88373C (en)
FR (1) FR2574702B1 (en)
GB (2) GB2168315B (en)
IE (1) IE58167B1 (en)
IN (1) IN168171B (en)
IT (1) IT1184020B (en)
MX (1) MX162524A (en)
NO (1) NO863238L (en)
SE (1) SE450630B (en)
WO (1) WO1986003713A1 (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0280203A2 (en) * 1987-02-25 1988-08-31 Krupp Corpoplast Maschinenbau Gmbh Process and apparatus for making hollow articles of oriented thermoplastic material
EP0280204A2 (en) * 1987-02-25 1988-08-31 Krupp Corpoplast Maschinenbau Gmbh Process and apparatus for forming a flange on a hollow thermoplastics article
US5281387A (en) * 1992-07-07 1994-01-25 Continental Pet Technologies, Inc. Method of forming a container having a low crystallinity
US5474735A (en) * 1993-09-24 1995-12-12 Continental Pet Technologies, Inc. Pulse blow method for forming container with enhanced thermal stability
EP0739703A1 (en) * 1995-04-27 1996-10-30 Continental PET Deutschland GmbH Bottom shape of reuseable PET containers
US5829614A (en) * 1992-07-07 1998-11-03 Continental Pet Technologies, Inc. Method of forming container with high-crystallinity sidewall and low-crystallinity base

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE500363C2 (en) * 1988-11-14 1994-06-13 Plm Ab Process of reshaping a preform of plastic material with expandable mandrel
US5328655A (en) * 1989-03-08 1994-07-12 Fortex, Inc. Method and apparatus for the manufacture of shaped products of biaxially oriented polymeric material
US5262181A (en) * 1990-05-14 1993-11-16 Erca Holding Apparatus for forming hollow articles in thermoplastic material
IE68430B1 (en) * 1990-08-12 1996-06-12 Polysheet Ireland Ltd A method and apparatus for forming an article of PET material
SE468666B (en) * 1990-09-27 1993-03-01 Plm Ab SET AND DEVICE TO CRYSTALLIZE AMORFT PLASTIC MATERIAL IN A SUBSTANCE
US5374179A (en) * 1993-05-03 1994-12-20 Hewlett-Packard Company Multi-temperature film die
EP0669255B1 (en) * 1994-02-23 1999-03-24 Denki Kagaku Kogyo Kabushiki Kaisha Heat and pressure resistant container
SE523785C2 (en) 1995-02-07 2004-05-18 Plastech Aps Method and apparatus for producing a tubular container with closure means
US5633022A (en) * 1995-06-08 1997-05-27 Old Line Plastics, Inc. Differential temperature vacuum-forming tool
US5762854A (en) * 1996-03-05 1998-06-09 Valyi; Emery I. Compression molding process
FR2753648B1 (en) * 1996-09-26 1998-11-27 Alphacan Sa METHOD AND INSTALLATION FOR MANUFACTURING PLASTIC TUBES WITH BI-AXIAL DRAWING, AND PLASTIC TUBE THUS OBTAINED
CA2218262C (en) * 1996-10-17 2001-04-24 Kenji Kawano Ultra-high-speed semiconductor optical modulator with traveling-wave electrode
US6264050B1 (en) 1998-10-06 2001-07-24 Plastipak Packaging, Inc. Container with improved neck portion and method for making the same
RU2216447C1 (en) * 2002-12-05 2003-11-20 Закрытое акционерное общество "Бородино" Method of manufacture of hollow products from plastic material
US20050269744A1 (en) * 2004-06-07 2005-12-08 Lonsway Michael J Stretched container and method of manufacture
US7637733B2 (en) * 2004-12-02 2009-12-29 Graham Packaging Company, L.P. Method and apparatus for reforming a portion of a plastic container to include a three-dimensional feature or transferable element
US20070126152A1 (en) * 2005-12-06 2007-06-07 Graham Packaging Company, L.P. Methods and apparatuses for reforming an upper portion of a blow molded plastic container
US20080116620A1 (en) * 2006-11-21 2008-05-22 John Thomas Method and apparatus for blow molding in an injection molding machine
TWI329560B (en) * 2007-12-06 2010-09-01 Profile Tech Internat Co Ltd Film thermoforming method
US8734709B2 (en) * 2009-04-07 2014-05-27 Graham Packaging Company, L.P. Apparatus for reforming a portion of a plastic container
US8506285B2 (en) 2009-04-07 2013-08-13 Graham Packaging Company, L.P. Method and apparatus for reforming a portion of a plastic container using induction heating
GB201407573D0 (en) * 2014-04-30 2014-06-11 Smiths Medical Int Ltd Tubes and their manuacture
FR3020980B1 (en) * 2014-05-19 2016-07-01 Mohammed Seiffeddine Bou-Mezrag MOLD FOR CLIPSABLE BOTTLE

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NO124420B (en) * 1962-02-06 1900-01-01 Remington Arms Comp Inc
US3284560A (en) * 1963-09-18 1966-11-08 Fed Cartridge Corp Method of making plastic tubes
US3496597A (en) * 1966-08-24 1970-02-24 Dow Chemical Co Container forming apparatus
US3929960A (en) * 1973-10-01 1975-12-30 Canadian Ind Method for producing oriented plastic shotshells

Family Cites Families (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2854694A (en) * 1956-02-16 1958-10-07 Owens Illinois Glass Co Method and apparatus for forming bodies from plastic materials
FR1251528A (en) * 1960-02-18 1961-01-20 Bellofram Patents Inc Improvements made to waterproofing membranes for ball joints
NL254972A (en) * 1960-06-21
US3492387A (en) * 1961-10-13 1970-01-27 Plastic Ammunition Products In Plastic article making
US3359599A (en) * 1964-05-06 1967-12-26 Dore Co John L Liner flaring apparatus
US3757718A (en) * 1966-12-13 1973-09-11 Shell Oil Co Method for forming hollow articles of work-stengthenable plastic materials
DE1779384A1 (en) * 1968-08-05 1971-11-18 Conduco Ag Method and device for the production of hollow bodies made of thermoplastic material and provided with a neck-shaped opening in a blow molding process
US3849530A (en) * 1969-12-17 1974-11-19 Du Pont Process for producing a biaxially oriented thermoplastic article
US3812696A (en) * 1970-10-22 1974-05-28 Crown Cork & Seal Co Method of and apparatus for forming container bodies
JPS5034407Y2 (en) * 1971-09-08 1975-10-07
US4036514A (en) * 1972-06-26 1977-07-19 E. I. Du Pont De Nemours And Company Pipe fitting
NL7505421A (en) * 1974-05-13 1975-11-17 Continental Can Co PLASTIC RESERVOIR MADE FROM A COMPOSITE PLATE, METHOD OF MANUFACTURING A PLASTIC TANK, AND COMPOSITE PLATE THEREFORE.
JPS5150251A (en) * 1974-10-29 1976-05-01 Kawasaki Heavy Ind Ltd mig yosetsusochi
JPS5920992B2 (en) * 1976-03-10 1984-05-16 セイコーエプソン株式会社 Balance spring outer end fixed structure
SE424162B (en) * 1978-03-02 1982-07-05 Plm Ab SET AND DEVICE FOR SHAPING AN ANIMAL PART OF A PREFORM
SE424286B (en) * 1979-06-11 1982-07-12 Plm Ab PROCEDURE TO GET AN ARTICLE OF THERMOPLASTIC MATERIAL THROUGH TOWING, AND CONTAINERS MANUFACTURED AS SET
US4511322A (en) * 1979-06-11 1985-04-16 Plm Aktiebolag Apparatus for the manufacture of a cup-like article from polyethylene terephthalate or similar material
US4281979A (en) * 1979-10-26 1981-08-04 Owens-Illinois, Inc. Apparatus to form a flat-topped rim on a thin-walled foam plastic container
US4297306A (en) * 1979-11-07 1981-10-27 Yoshino Kogyosho Co., Ltd. Neck orienting method of bottles of saturated polyester resins
US4332766A (en) * 1980-02-01 1982-06-01 Federal Cartridge Corporation One-piece shotshell
NL8102376A (en) * 1980-05-29 1981-12-16 Plm Ab METHOD AND APPARATUS FOR FORMING A HOLDER
DE3020351A1 (en) * 1980-05-29 1981-12-03 Maja-Maschinenfabrik Hermann Schill Gmbh, 7640 Kehl MACHINE FOR BLEEDING OR SKINNING MEAT OR THE LIKE
US4358492A (en) * 1980-10-22 1982-11-09 The Goodyear Tire & Rubber Company Novel process for deep stretch forming of polyesters
GB2089276B (en) * 1980-11-19 1984-09-05 Metal Box Co Ltd Thermoplastics tubular articles
FR2510940A1 (en) * 1981-08-06 1983-02-11 Solvay PROCESS AND APPARATUS FOR THE MANUFACTURE OF MOLECULAR ORIENTED PLASTIC PIPES
SE428774B (en) * 1981-11-26 1983-07-25 Plm Ab SET TO ASTADCOMMA AND CONTAINER
SE428775B (en) * 1981-11-26 1983-07-25 Plm Ab CONTAINERS AND SETS AND APPARATUS FOR MAKING A SUGAR
US4420454A (en) * 1982-03-05 1983-12-13 Toyo Seikan Kaisha, Limited Method of making a plastic hollow article
JPS58159920A (en) * 1982-03-18 1983-09-22 Sumitomo Metal Ind Ltd Method and apparatus for making pipe by ironing
SE435596B (en) * 1982-10-14 1984-10-08 Plm Ab SET FOR THE PREPARATION OF AN ARTICLE THROUGH THE SHAPING AND CRYSTALLIZATION OF MATERIAL IN THE WALL WITH A THEME OF THERMOPLASTIC MATERIAL WHEN IT'S THICKNESS REDUCTION AND MECHANICAL FORMING ORGANIC
US4545953A (en) * 1982-10-20 1985-10-08 Hunt-Wesson Foods, Inc. Method for making an extrusion blow molded no drip lip
SE448967B (en) * 1983-03-10 1987-03-30 Petainer Sa SET AND DEVICE FOR MANUFACTURING THERMOPLASTIC CONTAINERS
US4563325A (en) * 1983-05-20 1986-01-07 Shell Oil Company Forming plastic articles in solid state
CA1252265A (en) * 1984-03-30 1989-04-11 Ian M. Ward Tubular materials
SE451969B (en) * 1984-07-05 1987-11-09 Petainer Sa SET TO MAKE A CONTAINER FROM A ROD SIZE AND IN THE BOTH CONNECTED SUBJECT OF ORIENTABLE PLASTIC MATERIAL
DE3705948A1 (en) * 1987-02-25 1988-09-08 Krupp Corpoplast Masch METHOD AND DEVICE FOR MOLDING A FLANGE ON A HOLLOW BODY MADE OF THERMOPLASTIC PLASTIC
DE3705947A1 (en) * 1987-02-25 1988-09-08 Krupp Corpoplast Masch METHOD AND DEVICE FOR PRODUCING HOLLOW BODIES FROM ORIENTED THERMOPLASTIC PLASTIC

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NO124420B (en) * 1962-02-06 1900-01-01 Remington Arms Comp Inc
US3284560A (en) * 1963-09-18 1966-11-08 Fed Cartridge Corp Method of making plastic tubes
US3496597A (en) * 1966-08-24 1970-02-24 Dow Chemical Co Container forming apparatus
US3929960A (en) * 1973-10-01 1975-12-30 Canadian Ind Method for producing oriented plastic shotshells

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0280204A2 (en) * 1987-02-25 1988-08-31 Krupp Corpoplast Maschinenbau Gmbh Process and apparatus for forming a flange on a hollow thermoplastics article
US4894198A (en) * 1987-02-25 1990-01-16 Krupp Corpoplast Process for producing hollow bodies of oriented thermoplastic material
EP0280203A3 (en) * 1987-02-25 1991-05-02 Krupp Corpoplast Maschinenbau Gmbh Process and apparatus for making hollow articles of oriented thermoplastic material
EP0280204A3 (en) * 1987-02-25 1991-05-02 Krupp Corpoplast Maschinenbau Gmbh Process and apparatus for forming a flange on a hollow thermoplastics article
EP0280203A2 (en) * 1987-02-25 1988-08-31 Krupp Corpoplast Maschinenbau Gmbh Process and apparatus for making hollow articles of oriented thermoplastic material
US6372318B1 (en) 1992-07-07 2002-04-16 Continental Pet Technologies, Inc. Method of forming container with high-crystallinity sidewall and low-crystallinity base
US5281387A (en) * 1992-07-07 1994-01-25 Continental Pet Technologies, Inc. Method of forming a container having a low crystallinity
US5520877A (en) * 1992-07-07 1996-05-28 Continental Pet Technologies, Inc. Method of forming container with high-crystallinity sidewall and low-crystallinity base
US7445826B2 (en) 1992-07-07 2008-11-04 Graham Packaging Pet Technologies Inc. Container with high-crystallinity sidewall and low-crystallinity base
US6926859B2 (en) 1992-07-07 2005-08-09 Graham Packaging Pet Technologies Inc. Method of forming container with high-crystallinity sidewall and low-crystallinity base
US5829614A (en) * 1992-07-07 1998-11-03 Continental Pet Technologies, Inc. Method of forming container with high-crystallinity sidewall and low-crystallinity base
US5474735A (en) * 1993-09-24 1995-12-12 Continental Pet Technologies, Inc. Pulse blow method for forming container with enhanced thermal stability
WO1996033857A1 (en) * 1995-04-27 1996-10-31 Continental Pet Deutschland Gmbh Base geometry of reusable pet containers
EP0739703A1 (en) * 1995-04-27 1996-10-30 Continental PET Deutschland GmbH Bottom shape of reuseable PET containers

Also Published As

Publication number Publication date
JPH0655617A (en) 1994-03-01
CH679470A5 (en) 1992-02-28
US4927591A (en) 1990-05-22
AU597242B2 (en) 1990-05-31
AU630402B2 (en) 1992-10-29
GB8818628D0 (en) 1988-09-07
CA1317726C (en) 1993-05-18
ES8701589A1 (en) 1986-12-16
CH675225A5 (en) 1990-09-14
AU4782990A (en) 1990-05-10
DK387086A (en) 1986-08-14
SE8406373L (en) 1986-06-15
DE3572455D1 (en) 1989-09-28
IT8568054A0 (en) 1985-12-13
JPH0669713B2 (en) 1994-09-07
DE3587856D1 (en) 1994-07-21
CA1283064C (en) 1991-04-16
DK163970B (en) 1992-04-27
DK387086D0 (en) 1986-08-14
GB2168315A (en) 1986-06-18
JPS62501138A (en) 1987-05-07
BE903847A (en) 1986-06-12
NO863238D0 (en) 1986-08-12
GB2207630B (en) 1989-07-12
GB8530828D0 (en) 1986-01-22
FR2574702A1 (en) 1986-06-20
FI863260A (en) 1986-08-11
DE3587856T2 (en) 1994-09-22
EP0204810B1 (en) 1989-08-23
EP0204810A1 (en) 1986-12-17
NO863238L (en) 1986-08-12
US5067888A (en) 1991-11-26
IT1184020B (en) 1987-10-22
FI88373B (en) 1993-01-29
ES549917A0 (en) 1986-12-16
DK163970C (en) 1992-09-21
SE450630B (en) 1987-07-13
IN168171B (en) 1991-02-16
ATE107221T1 (en) 1994-07-15
JPH0560411B2 (en) 1993-09-02
MX162524A (en) 1991-05-20
IE853157L (en) 1986-06-14
FR2574702B1 (en) 1987-11-20
SE8406373D0 (en) 1984-12-14
GB2168315B (en) 1989-07-05
IE58167B1 (en) 1993-07-28
AU5311286A (en) 1986-07-22
FI863260A0 (en) 1986-08-11
ATE45700T1 (en) 1989-09-15
FI88373C (en) 1993-05-10
GB2207630A (en) 1989-02-08

Similar Documents

Publication Publication Date Title
WO1986003713A1 (en) Container, method and apparatus for manufacturing the same
US4540544A (en) Method of producing a biaxially oriented container of polyethylene terephthalate or similar material
US4584158A (en) Method for producing a biaxially oriented container from a blank of thermoplastic material
KR100278011B1 (en) Thermoplastic container manufacturing method and manufacturing apparatus
JPH0124056B2 (en)
US4564495A (en) Method of producing a container
GB2067952A (en) Moulding an article from a parison of plastics material
JPS6129858B2 (en)
US4803024A (en) Method of producing a container
JP7532307B2 (en) Manufacturing method of resin container
US4007242A (en) Process for the manufacture of oriented hollow plastic articles
EP0308685A2 (en) A hollow body, and a method and apparatus for making such a hollow body
IE58169B1 (en) Shaping an open mouth of a substantially tubular preform
KR910003322B1 (en) Container method and apparatus for manufacturing the same
JPH051730B2 (en)
JPH04126206A (en) Preliminary molding of crystal plastic and manufacture thereof
CA1204259A (en) Method and apparatus of producing a biaxially oriented container of thermoplastics material

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A1

Designated state(s): AU CH DK FI JP NO US

AL Designated countries for regional patents

Kind code of ref document: A1

Designated state(s): AT BE CH DE FR GB IT LU NL SE

WWE Wipo information: entry into national phase

Ref document number: 1986900323

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 863260

Country of ref document: FI

WWP Wipo information: published in national office

Ref document number: 1986900323

Country of ref document: EP

WWG Wipo information: grant in national office

Ref document number: 1986900323

Country of ref document: EP

WWG Wipo information: grant in national office

Ref document number: 863260

Country of ref document: FI