WO2014146938A1 - Process for producing a container from a preform having a portion to be superheated comprising a layer of material capable of being selectively superheated - Google Patents

Process for producing a container from a preform having a portion to be superheated comprising a layer of material capable of being selectively superheated Download PDF

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Publication number
WO2014146938A1
WO2014146938A1 PCT/EP2014/054787 EP2014054787W WO2014146938A1 WO 2014146938 A1 WO2014146938 A1 WO 2014146938A1 EP 2014054787 W EP2014054787 W EP 2014054787W WO 2014146938 A1 WO2014146938 A1 WO 2014146938A1
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WO
WIPO (PCT)
Prior art keywords
preform
layer
thermoplastic material
container
heating
Prior art date
Application number
PCT/EP2014/054787
Other languages
French (fr)
Inventor
Sébastien FEVRE
Original Assignee
Sidel Participations
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 Sidel Participations filed Critical Sidel Participations
Publication of WO2014146938A1 publication Critical patent/WO2014146938A1/en

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29BPREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B11/00Making preforms
    • B29B11/14Making preforms characterised by structure or composition
    • 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
    • B29C49/071Preforms or parisons characterised by their configuration, e.g. geometry, dimensions or physical properties
    • 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
    • B29C49/10Biaxial stretching during blow-moulding using mechanical means for prestretching
    • B29C49/12Stretching rods
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C49/00Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
    • B29C49/42Component parts, details or accessories; Auxiliary operations
    • B29C49/64Heating or cooling preforms, parisons or blown articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C49/00Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
    • B29C49/42Component parts, details or accessories; Auxiliary operations
    • B29C49/64Heating or cooling preforms, parisons or blown articles
    • B29C49/6409Thermal conditioning of preforms
    • B29C49/6436Thermal conditioning of preforms characterised by temperature differential
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/07Preforms or parisons characterised by their configuration
    • B29C2949/0715Preforms or parisons characterised by their configuration the preform having one end closed
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2949/00Indexing scheme relating to blow-moulding
    • B29C2949/20Preforms or parisons whereby a specific part is made of only one component, e.g. only one layer
    • B29C2949/22Preforms or parisons whereby a specific part is made of only one component, e.g. only one layer at neck portion
    • 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
    • B29C2949/20Preforms or parisons whereby a specific part is made of only one component, e.g. only one layer
    • B29C2949/24Preforms or parisons whereby a specific part is made of only one component, e.g. only one layer at flange portion
    • 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
    • B29C2949/30Preforms or parisons made of several components
    • B29C2949/3016Preforms or parisons made of several components at body portion
    • B29C2949/3018Preforms or parisons made of several components at body portion partially
    • 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
    • B29C2949/30Preforms or parisons made of several components
    • B29C2949/302Preforms or parisons made of several components at bottom portion
    • 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
    • B29C2949/30Preforms or parisons made of several components
    • B29C2949/3032Preforms or parisons made of several components having components being injected
    • 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
    • B29C2949/30Preforms or parisons made of several components
    • B29C2949/3032Preforms or parisons made of several components having components being injected
    • B29C2949/3034Preforms or parisons made of several components having components being injected having two or more components being injected
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C49/00Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
    • B29C49/42Component parts, details or accessories; Auxiliary operations
    • B29C49/64Heating or cooling preforms, parisons or blown articles
    • B29C49/6409Thermal conditioning of preforms
    • B29C49/6436Thermal conditioning of preforms characterised by temperature differential
    • B29C49/6462Thermal conditioning of preforms characterised by temperature differential by masking
    • 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
    • B29K2995/00Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0018Properties of moulding materials, reinforcements, fillers, preformed parts or moulds having particular optical properties, e.g. fluorescent or phosphorescent

Definitions

  • the invention relates to a method for producing a container, such as a bottle, made of thermoplastic material by forming, such as blowing or stretch-blow molding, the body of a preform preheated by heating radiation.
  • the invention more particularly relates to a method of producing a container, such as a bottle, made of thermoplastic material by blowing or stretch-blow molding the body of a preform preheated by heating radiation, the method comprising a final step of forming the container by blow molding or stretch blow molding in which the container is obtained by stretching the body of the preform, at least a portion of the body of the preform being stretched more rapidly relative to the portions forming the remainder of the body;
  • a preform in which the portion of the body intended to undergo a faster drawing has a coefficient of absorption of the heating radiation greater than that of the rest of the body, the body of the preform being made at the means of a first thermoplastic material, each portion intended to undergo a faster drawing during the forming step being made by superposition of a first layer of said first material and a second layer of a second thermoplastic material having a coefficient absorbing the heating radiation greater than that of the first material;
  • Thermoplastic preforms are obtained by injection into a mold during an initial manufacturing step.
  • the preforms generally have a substantially cylindrical body of revolution with a thick tubular wall which is closed at one of its axial ends by a thick-walled bottom, and which is extended at its other end by a collar, also tubular.
  • the neck is shaped according to its shape and its final dimensions while the body of the preform is called to undergo a relatively large deformation to form the final container during a final forming step.
  • the body of the preform is made malleable by heating beyond a glass transition temperature.
  • the preform thus heated is placed in a mold which has a mold cavity corresponding to the final container to obtain.
  • a pressurized fluid such as air, is then injected into the malleable body of the preform so as to press the wall against the cavity of the mold.
  • the body of the preform is heated homogeneously during the heating step. As a result, it undergoes expansion that is homogeneous in all radial directions.
  • the mold is generally maintained at a cold temperature relative to that of the preform.
  • the wall of the preform comes into contact with the mold, it is cooled suddenly so as to be fixed in a semi-crystalline state.
  • This cooling phenomenon makes it difficult to produce containers, especially bottles, having a cross section that is not approximately symmetrical with respect to the axis of the neck from the preform.
  • FIGS. 1A to 1C This last case is illustrated in FIGS. 1A to 1C.
  • the body of a preform 10 which is arranged in a mold 12 is thus shown in cross-section.
  • the body of the preform 10 is homogeneously heated.
  • proximal portions 14 of the preform 10 are arranged radially near the cavity of the mold 12, while other portions 16 distal of the preform 10 are relatively more radially distant. of the mold cavity 12.
  • the injection of the fluid under pressure into the body of the homogeneously heated preform 10 causes a homogeneous expansion of the body in all radial directions.
  • the proximal portions 14 contact the mold 12 before the distal portions 16.
  • the proximal portions 14 are thus frozen in a state of stretch much less important than the distal portions 16.
  • a method has already been proposed, in particular in said document FR-A1 -2,703,944, to obtain a container of non-symmetrical section of revolution with a wall of homogeneous thickness obtained by blow molding or stretch-blow molding.
  • portions 14 proximal to the body of the preform 10 at a temperature above the glass transition temperature, without however reaching the crystallization temperature of the material. Subsequently, the proximal portions 14 will be referred to as “portions 14 to be overheated” or “portions 14 superheated”.
  • such a method commonly known as the "preferential heating method” makes it possible to give the superheated portions 14 mechanical characteristics that make drawing, in particular circumferential, more rapid compared to the distal portions 16.
  • the superheated portions 14 have greater elasticity than the distal portions 16.
  • the shape and distribution of superheated portions 14 and distal portions define a heating profile of the preform.
  • the heating profile is adapted according to the shape of the final container to obtain.
  • the implementation of the method disclosed in this document requires an oven provided with means for restricting the heating of the distal portions.
  • This is for example shield to protect the distal portions of a heating radiation, or means to temporarily disengage the preform revolution.
  • Such means are very expensive to manufacture.
  • the present invention provides a method of the type described above, characterized in that the first layer of each portion to be heated has a thickness less than the rest of the body of the preform.
  • the second layer of each portion to be superheated has a thickness proportional to the heating temperature to be obtained in the portion to be superheated
  • the preform has a wall of uniform thickness, including in the portion to be overheated;
  • the first layer of each portion to be overheated is made integrally with the rest of the body; the second layer is produced by injection molding;
  • the first layer is produced by overmoulding on the second layer previously obtained by injection molding;
  • the second material has the same composition as the first material to which an additive is added which promotes the absorption of the heating radiation;
  • the second thermoplastic material has a composition different from the first thermoplastic material
  • the second layer of at least one portion to be superheated is arranged outside the preform
  • the second layer of at least one portion to be overheated is arranged inside the preform.
  • FIGS. 1A, 1B and 1C show different state of expansion of a preform during a forming step belonging to a process carried out according to the state of the art without preferential heating;
  • FIGS. 2A, 2B and 2C are views similar to those of FIGS. 1A, 1B, 1C which represent different states of expansion of a preform during a forming step belonging to a process carried out according to the teachings of FIG. invention;
  • FIG. 3 is a front view which shows a preform made at the end of a first step of manufacturing the process carried out according to the teachings of the invention
  • FIG. 4 is a front view showing the final container obtained from the preform of FIG. 3 after implementation of the method produced according to the teachings of the invention;
  • - Figure 5 is a top view which shows the container of Figure 4;
  • FIG. 6 is an axial sectional view which shows the preform of Figure 3 obtained according to a first embodiment of the invention
  • FIG. 7 is a perspective view showing a preform at the end of a first phase of the initial manufacturing step carried out according to a second embodiment of the invention.
  • Figure 8 shows the preform of Figure 7 at the end of the initial step of manufacturing.
  • the portions 14 of the body of the preform which are heated to a temperature greater than that of the distal portions 16 during the heating step will be indifferently called:
  • FIG. 3 shows a preform 10 made of thermoplastic material made according to the teachings of the invention.
  • the preform 10 comprises a substantially cylindrical body 18 of revolution with thick tubular wall 20 which is closed at one of its axial ends by a thick walled bottom 22.
  • the body 18 is extended at its open end by a neck 24, also tubular.
  • the axis "A" of the neck 18 also forms the axis of the body 18 of the preform 10.
  • the neck 24 is shaped in its shape and its final dimensions while the body 18 of the preform 10 is called to undergo a relatively large deformation to form a final container 26 during a forming step.
  • FIGS. 4 and 5 show the final container 26 that must be obtained from said preform 10. It can be seen that this container 26 is asymmetrical with respect to the "A" axis of the neck 24. Thus, a distal portion 16 of the body 18 of the container 26 arranged on the left in Figures 4 and 5 is substantially eccentric with respect to the portion of the body 12 arranged on the right. A proximal portion 14 of the body 18 of the container shown on the right in FIGS. 4 and 5 is arranged near the axis "A" with respect to the distal portion 16.
  • a container 26 is for example intended to contain a household product such as a detergent product.
  • the distal portion 16 of the container 26 corresponds to the distal portion 16 of the preform 10 which has been arranged at a distance from the cavity of the mold 12 during the forming operation, while the portion 14 proximal of the container 26 corresponds to the superheated portion 14 which has been arranged near the cavity of the mold 12.
  • the superheated portion 14 is delimited with respect to the distal portion 16 by a boundary 28.
  • the bottom 22 of the preform 10 is considered as an integral part of the superheated portion 14. Indeed, it is known that obtaining the bottom of the container 26 requires stretching greater than that of the distal portions 16, especially when the preform is stretched axially by an elongation rod during the forming step, thus conferring proximity between the bottom 22 of the preform and the cavity of the mold 12.
  • the body 18 of the preform 10 and the container 26 has only one portion 14 to overheat and a single distal portion 16. It will be understood, however, that the invention is applicable to preforms and containers having a plurality of unrelated superheating and / or distal portions.
  • the invention proposes a method for producing an asymmetrical container made of thermoplastic material, such as the container 26 shown in FIGS. 4 and 5.
  • the method comprises an initial step "E0" for manufacturing the preform 10 in which the portion 14 of the body 18 for faster drawing has a higher heating radiation absorption coefficient than that of the rest of the body 18.
  • the body 18 of the preform 10 is made by means of a first thermoplastic material and a second thermoplastic material, the second thermoplastic material having an absorption coefficient heating radiation greater than that of the first thermoplastic material.
  • Each portion 14 to be overheated is made by superposition of a first layer 30 of said first material and a second layer 32 of said second material .
  • the second material does not enter the constitution of the distal portions 16.
  • the portions 14 to be overheated comprise the second more absorbent thermoplastic material.
  • the distal portion 16 consists of a single layer of the first thermoplastic material.
  • the neck 24 of the preform 10 is made of the same material as the distal portion 16.
  • first layer 30 of each portion 14 to be overheated is formed integrally with the rest of the body 18 and with the neck 24.
  • the second thermoplastic material is selected to have a greater heating radiation absorption coefficient than that of the first thermoplastic material.
  • a wall made with the second thermoplastic material will increase its temperature faster than a wall made with the first thermoplastic material.
  • the second material is for example made according to the same formula as the first thermoplastic material, to which is added an additive that promotes the absorption of heating radiation. This is for example an additive that is not transparent in the wavelength of the heating radiation.
  • the second thermoplastic material is a thermoplastic material which has a composition totally different from the first thermoplastic material
  • the second thermoplastic material advantageously has mechanical characteristics substantially similar to those of the first material, at least at room temperature.
  • FIG. 10 A first embodiment of the preform 10 is illustrated in FIG.
  • the first layer 30 which is arranged outside the preform 10 while the second layer 32 is arranged on the inside of the wall of the preform 10.
  • the wall of the portion 14 to be superheated has a thickness identical to that of the distal portion 16 equal to the axis "A".
  • the body 18 of the preform has a wall of uniform thickness along the axis "A”.
  • the first layer 30 of each portion 14 to be superheated has a thickness less than that of the wall of the distal portions 16.
  • the thickness of the first layer 30 is equal to that of the second layer 32.
  • the second layer of each portion to be heated has a thickness greater than that of the first layer.
  • the second layer of each superheating portion has a thickness less than that of the first layer.
  • the second layer of each portion to be overheated has a variable thickness depending on the heating temperature gradient to be obtained in the portion to be superheated itself.
  • the thickness of the second layer is proportional to the final temperature to be obtained at the end of the heating step.
  • This first embodiment of the preform 10 can be obtained by an overmoulding process.
  • Such a method is well known to those skilled in the art, and reference can be made to EP-2.159.031 which describes an example of implementation of such a method.
  • the process described in this document is a so-called "bi-injection" process comprising:
  • FIGS. 7 and 8 show a second embodiment of the preform 10.
  • the portion 14 to be overheated is essentially formed by the bottom 22 of the preform 10.
  • the difference with respect to the first embodiment lies in the fact that the second layer 32 of the portion 14 to be overheated is here arranged outside the preform 10 while the first layer 30 is arranged towards the inside of the preform 10.
  • the first layer 30, the distal portion 16 and the neck 24 are first produced by injection molding of the first plastic material.
  • An incomplete preform is thus obtained, as shown in FIG. 7, in which a recess has been formed in the thickness of the portion 14 to be superheated in order to allow the second layer 32 to be overmoulded on the outside of the first layer.
  • the preform 10 thus manufactured according to any one of the embodiments undergoes a step "E1" intermediate heating.
  • the body 18 of the preform 10 is heated by uniform exposure of the entire body 18 of the preform 10 to electromagnetic heating radiation.
  • electromagnetic heating radiation This is for example infrared radiation or microwave radiation.
  • the heating is performed by scrolling the preforms 10 in a furnace (not shown) having at least one heating side wall, for example constituted by heating tubes attached to the wall of the furnace, with simultaneous rotation of the preforms on themselves to homogenize the exposure time of all the portions 14, 16 of the body 18 of the preform 10.
  • Protection means provide thermal protection of the neck 18.
  • a reflective panel can preferably be arranged opposite the tubes to reflect towards the bodies 18 of the preforms 10 the fraction of the passing heating radiation between two successive 18 bodies.
  • Such an implementation device is particularly suitable for mass production of containers 26.
  • the portion 14 to be overheated and the distal portion 16 are exposed to identical heating radiation, both in terms of exposure time and power of the radiation.
  • the entire body 18 of the preform is heated to a temperature above the softening temperature, or glass transition temperature, of the material by the electromagnetic radiation heating.
  • the second layer 32 of the portion 14 to be overheated will have absorbed more energy than the distal portion 16. This results in a faster increase of the temperature of the second layer 32 of the portion 14 to overheat relative to the distal portion 16. Due to the large contact surface between the first layer 30 and the second layer 32, the heat stored in the second layer 32 is transmitted by conduction to the first layer 30. Thus, the temperature of the portion 14 to be superheated is homogeneous in its entire thickness and is greater than the glass transition temperature reached by the distal portion 16.
  • each portion 14 to be heated is heated to a temperature even higher than that of the remainder of the body 18 because of the absorption coefficient of the second layer 32.
  • this disparity in temperature between the portion 14 to be heated and the distal portion 16 makes it possible, after a final step "E2" forming, for example by blowing or by stretching blowing, to an asymmetrical container 26 having a homogeneous wall thickness, as illustrated in Figures 2A, 2B and 2C.
  • All preforms can be uniformly exposed to the heating radiation regardless of the shape of the final container, including a symmetrical shape of revolution.
  • the heating profile of the preforms is in fact now determined by the structure of the preform itself, in particular by the distribution of the second absorbent thermoplastic material, and not by its exposure time to the heating radiation.

Abstract

The invention relates to a process for producing a container (26), made of a thermoplastic material, the process comprising a final step (E2) of forming the container (26) by blow moulding or stretch-blow moulding during which at least one portion (14) of the body (18) of the preform (10) undergoes a more rapid stretching than the rest of the body (18), characterized in that it comprises: - an initial step (E0) of manufacturing the preform (10) during which the body (18) is made using a first thermoplastic material, each portion (14) to be stretched more rapidly comprising a second layer (32) of a second thermoplastic material that has a higher coefficient for absorption of the heating radiation than that of the first material; - an intermediate step (E1) of heating via uniform exposure of the body (18) of the preform to the electromagnetic heating radiation.

Description

"Procédé de réalisation d'un récipient à partir d'une préforme comportant une portion à surchauffer comportant une couche de matériau susceptible d'être surchauffé sélectivement" "Process for producing a container from a preform comprising an overheating portion comprising a layer of material that can be selectively superheated"
L'invention concerne un procédé de réalisation d'un récipient, tel qu'une bouteille, en matériau thermoplastique par formage, tel que soufflage ou étirage-soufflage, du corps d'une préforme préchauffée par un rayonnement de chauffage. The invention relates to a method for producing a container, such as a bottle, made of thermoplastic material by forming, such as blowing or stretch-blow molding, the body of a preform preheated by heating radiation.
L'invention concerne plus particulièrement un procédé de réalisation d'un récipient, tel qu'une bouteille, en matériau thermoplastique par soufflage ou étirage-soufflage du corps d'une préforme préchauffée par un rayonnement de chauffage, le procédé comportant une étape finale de formage du récipient par soufflage ou étirage-soufflage au cours de laquelle le récipient est obtenu par étirement du corps de la préforme, au moins une portion du corps de la préforme subissant un étirage plus rapide par rapport aux portions formant le reste du corps ;  The invention more particularly relates to a method of producing a container, such as a bottle, made of thermoplastic material by blowing or stretch-blow molding the body of a preform preheated by heating radiation, the method comprising a final step of forming the container by blow molding or stretch blow molding in which the container is obtained by stretching the body of the preform, at least a portion of the body of the preform being stretched more rapidly relative to the portions forming the remainder of the body;
le procédé comportant :  the process comprising:
- une étape initiale de fabrication d'une préforme dans laquelle la portion du corps destinée à subir un étirage plus rapide présente un coefficient d'absorption du rayonnement de chauffage plus grand que celui du reste du corps, le corps de la préforme étant réalisé au moyen d'un premier matériau thermoplastique, chaque portion destinée à subir un étirage plus rapide durant l'étape de formage étant réalisée par superposition d'une première couche dudit premier matériau et d'une deuxième couche d'un deuxième matériau thermoplastique présentant un coefficient d'absorption du rayonnement de chauffage plus grand que celui du premier matériau ;  an initial step of manufacturing a preform in which the portion of the body intended to undergo a faster drawing has a coefficient of absorption of the heating radiation greater than that of the rest of the body, the body of the preform being made at the means of a first thermoplastic material, each portion intended to undergo a faster drawing during the forming step being made by superposition of a first layer of said first material and a second layer of a second thermoplastic material having a coefficient absorbing the heating radiation greater than that of the first material;
- une étape intermédiaire de chauffage du corps de la préforme par exposition uniforme du corps entier de la préforme au rayonnement électromagnétique de chauffage, à l'issue de laquelle l'ensemble du corps de la préforme est chauffé à une température supérieure à la température de ramollissement des matériaux la constituant par le rayonnement électromagnétique de chauffage, chaque portion destinée à subir un étirage plus rapide au cours de l'étape de formage étant surchauffée à une température encore supérieure à celle du reste du corps du fait de son coefficient d'absorption. an intermediate step of heating the body of the preform by uniformly exposing the whole body of the preform to the electromagnetic heating radiation, at the end of which the entire body of the preform is heated to a temperature above the temperature of softening materials constituting it by electromagnetic radiation heating, each portion intended to undergo a faster stretching during the forming step being superheated at a temperature still higher than that of the rest of the body because of its absorption coefficient.
Les préformes en matériau thermoplastique sont obtenues par injection dans un moule lors d'une étape initiale de fabrication.  Thermoplastic preforms are obtained by injection into a mold during an initial manufacturing step.
Les préformes présentent généralement un corps sensiblement cylindrique de révolution à paroi tubulaire épaisse qui est fermé à l'une de ses extrémités axiales par un fond à paroi épaisse, et qui est prolongé à son autre extrémité par un col, lui aussi tubulaire. Le col est conformé à sa forme et à ses dimensions définitives tandis que le corps de la préforme est appelé à subir une déformation relativement importante pour former le récipient final lors d'une étape finale de formage.  The preforms generally have a substantially cylindrical body of revolution with a thick tubular wall which is closed at one of its axial ends by a thick-walled bottom, and which is extended at its other end by a collar, also tubular. The neck is shaped according to its shape and its final dimensions while the body of the preform is called to undergo a relatively large deformation to form the final container during a final forming step.
Lors d'une étape intermédiaire de chauffage, le corps de la préforme est rendu malléable par chauffage au-delà d'une température de transition vitreuse.  During an intermediate heating step, the body of the preform is made malleable by heating beyond a glass transition temperature.
Ensuite, lors de l'étape finale de formage, la préforme ainsi chauffée est placée dans un moule qui présente une empreinte de moulage conforme au récipient final à obtenir. Un fluide sous pression, tel que de l'air, est alors injecté dans le corps malléable de la préforme afin d'en plaquer la paroi contre l'empreinte du moule.  Then, during the final forming step, the preform thus heated is placed in a mold which has a mold cavity corresponding to the final container to obtain. A pressurized fluid, such as air, is then injected into the malleable body of the preform so as to press the wall against the cavity of the mold.
Traditionnellement, le corps de la préforme est chauffé de manière homogène lors de l'étape de chauffage. De ce fait, il subit une expansion qui est homogène dans toutes les directions radiales.  Traditionally, the body of the preform is heated homogeneously during the heating step. As a result, it undergoes expansion that is homogeneous in all radial directions.
Le moule est généralement maintenu à une température froide relativement à celle de la préforme. Ainsi, lorsque la paroi de la préforme entre en contact avec le moule, elle est refroidie brutalement de manière à être figée dans un état semi-cristallin. Ce phénomène de refroidissement rend difficile la réalisation de récipients, notamment des bouteilles, présentant une section transversale qui n'est pas approximativement symétrique de révolution par rapport à l'axe du col à partir de la préforme. Il s'agit par exemple des récipients de section transversale polygonale dans lesquels chaque face approximativement plane s'écarte sensiblement d'une surface cylindrique enveloppant les arêtes, ou des récipients à corps aplatis tels que les flacons pour produits lessiviels. The mold is generally maintained at a cold temperature relative to that of the preform. Thus, when the wall of the preform comes into contact with the mold, it is cooled suddenly so as to be fixed in a semi-crystalline state. This cooling phenomenon makes it difficult to produce containers, especially bottles, having a cross section that is not approximately symmetrical with respect to the axis of the neck from the preform. For example, containers of polygonal cross-section in which each approximately planar face deviates substantially from a cylindrical surface surrounding the edges, or containers with flattened bodies such as detergent bottles.
Ce dernier cas est illustré aux figures 1A à 1C. On a ainsi représenté en section transversale le corps d'une préforme 10 qui est agencé dans un moule 12. Le corps de la préforme 10 est chauffé de manière homogène.  This last case is illustrated in FIGS. 1A to 1C. The body of a preform 10 which is arranged in a mold 12 is thus shown in cross-section. The body of the preform 10 is homogeneously heated.
Du fait de la forme asymétrique de révolution du récipient final, certaines portions 14 proximales de la préforme 10 sont agencées radialement à proximité de l'empreinte du moule 12, tandis que d'autres portions 16 distales de la préforme 10 sont relativement plus éloignées radialement de l'empreinte du moule 12.  Because of the asymmetrical shape of the final container revolution, some proximal portions 14 of the preform 10 are arranged radially near the cavity of the mold 12, while other portions 16 distal of the preform 10 are relatively more radially distant. of the mold cavity 12.
Comme illustré à la figure 1B, l'injection du fluide sous pression dans le corps de la préforme 10, chauffé de manière homogène, provoque une expansion homogène du corps dans toutes les directions radiales. Cependant, les portions 14 proximales entrent en contact avec le moule 12 avant les portions 16 distales. Les portions 14 proximales sont donc figées dans un état d'étirement bien moins important que les portions 16 distales.  As illustrated in FIG. 1B, the injection of the fluid under pressure into the body of the homogeneously heated preform 10 causes a homogeneous expansion of the body in all radial directions. However, the proximal portions 14 contact the mold 12 before the distal portions 16. The proximal portions 14 are thus frozen in a state of stretch much less important than the distal portions 16.
Du fait que le chauffage homogène confère au matériau les mêmes caractéristiques d'étirement quelles que soient les portions 14, 16 du corps de la préforme 10, l'étirement supérieur des portions 16 distales du corps de la préforme 10 s'accompagne d'un amincissement accru de cette portion 16 de paroi. Comme cela est représenté à la figure 1C, on obtient, finalement, un récipient à paroi d'épaisseur non constante, plus mince dans les portions 16 distales du corps de la préforme 10 de départ et plus épaisse dans les portions 14 proximales de la préforme 10 de départ. Since the homogeneous heating gives the material the same stretching characteristics regardless of the portions 14, 16 of the body of the preform 10, the upper stretch of the distal portions 16 of the body of the preform 10 is accompanied by a increased thinning of this portion 16 of the wall. As shown in FIG. 1C, there is finally obtained a container with a wall of non-constant thickness, which is thinner in the portions 16 distal to the body of the preform 10 starting and thicker in the proximal portions 14 of the preform 10 starting.
Ceci entraîne de nombreux inconvénients qui sont cités dans le document FR-A1-2.703.944.  This entails many drawbacks which are cited in the document FR-A1-2.703.944.
On a déjà proposé un procédé, notamment dans ledit document FR-A1 -2.703.944, pour obtenir un récipient de section non symétrique de révolution à paroi d'épaisseur homogène obtenu par soufflage ou étirage-soufflage.  A method has already been proposed, in particular in said document FR-A1 -2,703,944, to obtain a container of non-symmetrical section of revolution with a wall of homogeneous thickness obtained by blow molding or stretch-blow molding.
Ce document propose notamment de chauffer les portions This document proposes, in particular, to heat the portions
14 proximales du corps de la préforme 10 à une température supérieure à la température de transition vitreuse, sans toutefois atteindre la température de cristallisation du matériau. Par la suite, les portions 14 proximale seront donc appelées "portions 14 à surchauffer" ou "portions 14 surchauffées". 14 proximal to the body of the preform 10 at a temperature above the glass transition temperature, without however reaching the crystallization temperature of the material. Subsequently, the proximal portions 14 will be referred to as "portions 14 to be overheated" or "portions 14 superheated".
Comme illustré aux figures 2A à 2C, un tel procédé, appelé couramment "procédé de chauffe préférentielle", permet de conférer aux portions 14 surchauffées des caractéristiques mécaniques permettant un étirage, notamment circonférentiel, plus rapide par rapport aux portions 16 distales. Par exemple, les portions 14 surchauffées présentent une plus grande élasticité que celle des portions 16 distales.  As illustrated in FIGS. 2A to 2C, such a method, commonly known as the "preferential heating method", makes it possible to give the superheated portions 14 mechanical characteristics that make drawing, in particular circumferential, more rapid compared to the distal portions 16. For example, the superheated portions 14 have greater elasticity than the distal portions 16.
La forme et la répartition des portions 14 surchauffées et des portions distales définissent un profil de chauffage de la préforme. Le profil de chauffage est adapté en fonction de la forme du récipient final à obtenir.  The shape and distribution of superheated portions 14 and distal portions define a heating profile of the preform. The heating profile is adapted according to the shape of the final container to obtain.
Comme illustré à la figure 2B, lorsque le fluide sous pression est injecté dans le corps de la préforme 10, les portions 14 surchauffées sont étirées plus rapidement que les portions 16 distales sous l'effet de la pression du fluide. Ainsi, à l'instant où les portions 14 surchauffées entrent en contact avec le moule 12, elles présentent une épaisseur inférieure à celle des portions 16 distales. Les portions 14 surchauffées sont alors refroidies et figées dans leur état, permettant d'étirer progressivement le reste du corps de la préforme 10 jusqu'à épouser l'empreinte du moule 12. En réglant la température de chaque portion 14, 16, cela permet d'obtenir un récipient final à paroi d'épaisseur homogène, comme représenté à la figure 2C. As illustrated in FIG. 2B, when the pressurized fluid is injected into the body of the preform 10, the superheated portions 14 are stretched more rapidly than the distal portions 16 under the effect of the fluid pressure. Thus, at the instant when the superheated portions 14 come into contact with the mold 12, they have a thickness less than that of the distal portions 16. The superheated portions 14 are then cooled and fixed in their state, making it possible to progressively stretch the rest of the body of the preform 10 to match the mold cavity 12. By adjusting the temperature of each portion 14, 16, this allows to obtain a final container wall homogeneous thickness, as shown in Figure 2C.
Bien entendu, pour obtenir un récipient final satisfaisant, il est nécessaire d'indexer la position angulaire autour de son axe principal par rapport au moule afin d'orienter correctement les portions surchauffées vers les portions proximales correspondantes de l'empreinte du moule.  Of course, to obtain a satisfactory final container, it is necessary to index the angular position around its main axis relative to the mold in order to correctly orient the superheated portions to the corresponding proximal portions of the mold cavity.
Cependant, la mise en œuvre du procédé divulgué dans ce document nécessite un four muni de moyens pour restreindre le chauffage des portions distales. Il s'agit par exemple de bouclier pour protéger les portions distales d'un rayonnement chauffant, ou encore de moyens pour débrayer temporairement la révolution des préformes. De tels moyens sont très onéreux à fabriquer.  However, the implementation of the method disclosed in this document requires an oven provided with means for restricting the heating of the distal portions. This is for example shield to protect the distal portions of a heating radiation, or means to temporarily disengage the preform revolution. Such means are very expensive to manufacture.
En outre, il est très délicat de procéder au réglage du four pour obtenir des profils de chauffage précis en fonction de la forme du récipient à obtenir.  In addition, it is very difficult to adjust the oven to obtain accurate heating profiles depending on the shape of the container to obtain.
Pour résoudre notamment ces problèmes, la présente invention propose un procédé du type décrit précédemment, caractérisé en ce que la première couche de chaque portion à surchauffer présente une épaisseur inférieure au reste du corps de la préforme.  To solve these problems in particular, the present invention provides a method of the type described above, characterized in that the first layer of each portion to be heated has a thickness less than the rest of the body of the preform.
Selon d'autres caractéristiques de l'invention :  According to other features of the invention:
- la deuxième couche de chaque portion à surchauffer présente une épaisseur proportionnelle à la température de chauffage à obtenir dans la portion à surchauffer ;  the second layer of each portion to be superheated has a thickness proportional to the heating temperature to be obtained in the portion to be superheated;
- la préforme présente une paroi d'épaisseur uniforme, y compris dans la portion à surchauffer ;  the preform has a wall of uniform thickness, including in the portion to be overheated;
- la première couche de chaque portion à surchauffer est réalisée venue de matière avec le reste du corps ; - la deuxième couche est réalisée par moulage par injection ; the first layer of each portion to be overheated is made integrally with the rest of the body; the second layer is produced by injection molding;
- la première couche est réalisée par surmoulage sur la deuxième couche préalablement obtenue par moulage par injection ;  the first layer is produced by overmoulding on the second layer previously obtained by injection molding;
- le deuxième matériau présente la même composition que le premier matériau à laquelle est ajouté un additif qui favorise l'absorption du rayonnement de chauffage ;  the second material has the same composition as the first material to which an additive is added which promotes the absorption of the heating radiation;
- le deuxième matériau thermoplastique présente une composition différente du premier matériau thermoplastique ;  the second thermoplastic material has a composition different from the first thermoplastic material;
- la deuxième couche d'au moins une portion à surchauffer est agencée à l'extérieur de la préforme ;  the second layer of at least one portion to be superheated is arranged outside the preform;
- la deuxième couche d'au moins une portion à surchauffer est agencée à l'intérieur de la préforme.  the second layer of at least one portion to be overheated is arranged inside the preform.
D'autres caractéristiques et avantages de l'invention apparaîtront au cours de la lecture de la description détaillée qui va suivre pour la compréhension de laquelle on se reportera aux dessins annexés, parmi lesquels :  Other characteristics and advantages of the invention will appear during the reading of the detailed description which follows for the understanding of which reference will be made to the appended drawings, among which:
- les figures 1A, 1B et 1C représentent différents état d'expansion d'une préforme lors d'une étape de formage appartenant à un procédé réalisé selon l'état de la technique sans chauffe préférentielle ;  FIGS. 1A, 1B and 1C show different state of expansion of a preform during a forming step belonging to a process carried out according to the state of the art without preferential heating;
- les figures 2A, 2B et 2C sont des vues similaires à celles des figures 1A, 1B, 1C qui représentent différents états d'expansion d'une préforme lors d'une étape de formage appartenant à un procédé réalisé selon les enseignements de l'invention ;  FIGS. 2A, 2B and 2C are views similar to those of FIGS. 1A, 1B, 1C which represent different states of expansion of a preform during a forming step belonging to a process carried out according to the teachings of FIG. invention;
- la figure 3 est une vue de face qui représente une préforme réalisée à l'issue d'une première étape de fabrication du procédé réalisé selon les enseignements de l'invention ;  - Figure 3 is a front view which shows a preform made at the end of a first step of manufacturing the process carried out according to the teachings of the invention;
- la figure 4 est une vue de face qui représente le récipient final obtenue à partir de la préforme de la figure 3 après mise en œuvre du procédé réalisé selon les enseignements de l'invention ; - la figure 5 est une vue de dessus qui représente le récipient de la figure 4 ; FIG. 4 is a front view showing the final container obtained from the preform of FIG. 3 after implementation of the method produced according to the teachings of the invention; - Figure 5 is a top view which shows the container of Figure 4;
- la figure 6 est une vue en coupe axiale qui représente la préforme de la figure 3 obtenue selon un premier mode de réalisation de l'invention ;  - Figure 6 is an axial sectional view which shows the preform of Figure 3 obtained according to a first embodiment of the invention;
- la figure 7 est une vue en perspective qui représente une préforme à l'issue d'une première phase de l'étape initiale de fabrication réalisée selon un deuxième mode de réalisation de l'invention ;  FIG. 7 is a perspective view showing a preform at the end of a first phase of the initial manufacturing step carried out according to a second embodiment of the invention;
- la figure 8 représente la préforme de la figure 7 à l'issue de l'étape initiale de fabrication.  - Figure 8 shows the preform of Figure 7 at the end of the initial step of manufacturing.
Dans la description et dans les revendications, les portions 14 du corps de la préforme qui sont chauffées à une température supérieure à celle des portions 16 distales lors de l'étape de chauffage seront appelées indifféremment :  In the description and in the claims, the portions 14 of the body of the preform which are heated to a temperature greater than that of the distal portions 16 during the heating step will be indifferently called:
- "portions 14 surchauffées" après l'étape de chauffage, ou - "superheated portions 14" after the heating step, or
- "portion 14 à surchauffer" avant l'étape de chauffage. - "portion 14 to overheat" before the heating step.
On a représenté à la figure 3, une préforme 10 en matériau thermoplastique réalisée selon les enseignements de l'invention. Classiquement, la préforme 10 comporte un corps 18 sensiblement cylindrique de révolution à paroi 20 tubulaire épaisse qui est fermé à l'une de ses extrémités axiales par un fond 22 à paroi épaisse. Le corps 18 est prolongé à son extrémité ouverte par un col 24, lui aussi tubulaire. L'axe "A" du col 18 forme aussi l'axe du corps 18 de la préforme 10.  FIG. 3 shows a preform 10 made of thermoplastic material made according to the teachings of the invention. Conventionally, the preform 10 comprises a substantially cylindrical body 18 of revolution with thick tubular wall 20 which is closed at one of its axial ends by a thick walled bottom 22. The body 18 is extended at its open end by a neck 24, also tubular. The axis "A" of the neck 18 also forms the axis of the body 18 of the preform 10.
Le col 24 est conformé à sa forme et à ses dimensions définitives tandis que le corps 18 de la préforme 10 est appelé à subir une déformation relativement importante pour former un récipient 26 final lors d'une étape de formage.  The neck 24 is shaped in its shape and its final dimensions while the body 18 of the preform 10 is called to undergo a relatively large deformation to form a final container 26 during a forming step.
On a représenté aux figures 4 et 5 le récipient 26 final qui doit être obtenu à partir de ladite préforme 10. On constate que ce récipient 26 est asymétrique par rapport à l'axe "A" du col 24. Ainsi, une portion 16 distale du corps 18 du récipient 26 agencée à gauche aux figures 4 et 5 est sensiblement excentrée par rapport à la portion du corps 12 agencé à droite. Une portion 14 proximale du corps 18 du récipient représentée à droite aux figures 4 et 5 est agencée à proximité de l'axe "A" par rapport à la portion 16 distale. Un tel récipient 26 est par exemple destiné à contenir un produit ménager tel qu'un produit lessiviel. FIGS. 4 and 5 show the final container 26 that must be obtained from said preform 10. It can be seen that this container 26 is asymmetrical with respect to the "A" axis of the neck 24. Thus, a distal portion 16 of the body 18 of the container 26 arranged on the left in Figures 4 and 5 is substantially eccentric with respect to the portion of the body 12 arranged on the right. A proximal portion 14 of the body 18 of the container shown on the right in FIGS. 4 and 5 is arranged near the axis "A" with respect to the distal portion 16. Such a container 26 is for example intended to contain a household product such as a detergent product.
Comme expliqué en préambule de la description, la portion 16 distale du récipient 26 correspond à la portion 16 distale de la préforme 10 qui a été agencée à distance de l'empreinte du moule 12 lors de l'opération de formage, tandis que la portion 14 proximale du récipient 26 correspond à la portion 14 surchauffée qui a été agencée à proximité de l'empreinte du moule 12.  As explained in the preamble of the description, the distal portion 16 of the container 26 corresponds to the distal portion 16 of the preform 10 which has been arranged at a distance from the cavity of the mold 12 during the forming operation, while the portion 14 proximal of the container 26 corresponds to the superheated portion 14 which has been arranged near the cavity of the mold 12.
Sur les figures 3 à 5, la portion 14 surchauffée est délimitée par rapport à la portion 16 distale par une frontière 28.  In FIGS. 3 to 5, the superheated portion 14 is delimited with respect to the distal portion 16 by a boundary 28.
On constate aux figures 3 à 5 que le fond 22 de la préforme 10 est considéré comme une partie intégrante de la portion 14 surchauffée. En effet, il est connu que l'obtention du fond du récipient 26 nécessite un étirage supérieur à celui des portions 16 distales, notamment lorsque la préforme est étirée axialement par une tige d'élongation pendant l'étape de formage, conférant ainsi une proximité entre le fond 22 de la préforme et l'empreinte du moule 12.  It can be seen in FIGS. 3 to 5 that the bottom 22 of the preform 10 is considered as an integral part of the superheated portion 14. Indeed, it is known that obtaining the bottom of the container 26 requires stretching greater than that of the distal portions 16, especially when the preform is stretched axially by an elongation rod during the forming step, thus conferring proximity between the bottom 22 of the preform and the cavity of the mold 12.
Dans l'exemple représenté aux figures, le corps 18 de la préforme 10 et du récipient 26 ne comporte qu'une unique portion 14 à surchauffer et une unique portion 16 distale. On comprendra néanmoins que l'invention est applicable à des préformes et à des récipients comportant plusieurs portions à surchauffer et/ou distales non connexes.  In the example shown in the figures, the body 18 of the preform 10 and the container 26 has only one portion 14 to overheat and a single distal portion 16. It will be understood, however, that the invention is applicable to preforms and containers having a plurality of unrelated superheating and / or distal portions.
L'invention propose un procédé pour la réalisation d'un récipient asymétrique en matériau thermoplastique, tel que le récipient 26 représenté aux figures 4 et 5.  The invention proposes a method for producing an asymmetrical container made of thermoplastic material, such as the container 26 shown in FIGS. 4 and 5.
Le procédé comporte une étape "E0" initiale de fabrication de la préforme 10 dans laquelle la portion 14 du corps 18 destinée à subir un étirage plus rapide présente un coefficient d'absorption du rayonnement de chauffage plus grand que celui du reste du corps 18. The method comprises an initial step "E0" for manufacturing the preform 10 in which the portion 14 of the body 18 for faster drawing has a higher heating radiation absorption coefficient than that of the rest of the body 18.
Plus particulièrement, au cours de l'étape "E0" de fabrication, le corps 18 de la préforme 10 est réalisé au moyen d'un premier matériau thermoplastique et d'un deuxième matériau thermoplastique, le deuxième matériau thermoplastique présentant un coefficient d'absorption du rayonnement de chauffage plus grand que celui du premier matériau thermo- plastique.  More particularly, during the step "E0" of manufacture, the body 18 of the preform 10 is made by means of a first thermoplastic material and a second thermoplastic material, the second thermoplastic material having an absorption coefficient heating radiation greater than that of the first thermoplastic material.
Chaque portion 14 à surchauffer, c'est-à-dire destinée à subir un étirage plus rapide durant l'étape de formage, est réalisée par superposition d'une première couche 30 dudit premier matériau et d'une deuxième couche 32 dudit deuxième matériau.  Each portion 14 to be overheated, that is to say destined to undergo a faster drawing during the forming step, is made by superposition of a first layer 30 of said first material and a second layer 32 of said second material .
Le deuxième matériau n'entre pas dans la constitution des portions 16 distales. En d'autres termes, seules les portions 14 à surchauffer comportent le deuxième matériau thermoplastique plus absorbant. Dans l'exemple représenté aux figures, la portion 16 distale est constituée d'une unique couche du premier matériau thermoplastique.  The second material does not enter the constitution of the distal portions 16. In other words, only the portions 14 to be overheated comprise the second more absorbent thermoplastic material. In the example shown in the figures, the distal portion 16 consists of a single layer of the first thermoplastic material.
Le col 24 de la préforme 10 est constitué du même matériau que la portion 16 distale.  The neck 24 of the preform 10 is made of the same material as the distal portion 16.
Ainsi, la première couche 30 de chaque portion 14 à surchauffer est réalisée venue de matière avec le reste du corps 18 et avec le col 24.  Thus, the first layer 30 of each portion 14 to be overheated is formed integrally with the rest of the body 18 and with the neck 24.
Le deuxième matériau thermoplastique est sélectionné de manière à présenter un coefficient d'absorption du rayonnement de chauffage plus grand que celui du premier matériau thermoplastique. En d'autres termes, lors d'une exposition à un rayonnement de chauffage identique, une paroi réalisée avec le deuxième matériau thermoplastique verra sa température augmenter plus vite qu'une paroi réalisée avec le premier matériau thermoplastique. Pour ce faire, le deuxième matériau est par exemple réalisé selon la même formule que le premier matériau thermoplastique, à laquelle est ajouté un additif qui favorise l'absorption du rayonnement de chauffage. Il s'agit par exemple d'un additif qui n'est pas transparent dans la longueur d'onde du rayonnement chauffant. The second thermoplastic material is selected to have a greater heating radiation absorption coefficient than that of the first thermoplastic material. In other words, during exposure to identical heating radiation, a wall made with the second thermoplastic material will increase its temperature faster than a wall made with the first thermoplastic material. To do this, the second material is for example made according to the same formula as the first thermoplastic material, to which is added an additive that promotes the absorption of heating radiation. This is for example an additive that is not transparent in the wavelength of the heating radiation.
En variante, le deuxième matériau thermoplastique est un matériau thermoplastique qui présente une composition totalement différente du premier matériau thermoplastique,  In a variant, the second thermoplastic material is a thermoplastic material which has a composition totally different from the first thermoplastic material,
Quelle que soit la solution retenue, le deuxième matériau thermoplastique présente avantageusement des caractéristiques mécaniques sensiblement analogues à celles du premier matériau, tout au moins à température ambiante.  Whatever the chosen solution, the second thermoplastic material advantageously has mechanical characteristics substantially similar to those of the first material, at least at room temperature.
Un premier mode de réalisation de la préforme 10 est illustré à la figure 6.  A first embodiment of the preform 10 is illustrated in FIG.
Dans ce premier mode de réalisation, la première couche 30 qui est agencée à l'extérieur de la préforme 10 tandis que la deuxième couche 32 est agencée côté intérieur de la paroi de la préforme 10.  In this first embodiment, the first layer 30 which is arranged outside the preform 10 while the second layer 32 is arranged on the inside of the wall of the preform 10.
La paroi de la portion 14 à surchauffer présente une épaisseur identique à celle de la portion 16 distale à hauteur égale par rapport à l'axe "A". Dans cet exemple, le corps 18 de la préforme présente une paroi d'épaisseur uniforme tout le long de l'axe "A".  The wall of the portion 14 to be superheated has a thickness identical to that of the distal portion 16 equal to the axis "A". In this example, the body 18 of the preform has a wall of uniform thickness along the axis "A".
Ainsi, la première couche 30 de chaque portion 14 à surchauffer présente une épaisseur inférieure à celle de la paroi des portions 16 distales.  Thus, the first layer 30 of each portion 14 to be superheated has a thickness less than that of the wall of the distal portions 16.
Dans la portion 14 à surchauffer, l'épaisseur de la première couche 30 est égale à celle de la deuxième couche 32.  In the portion 14 to be overheated, the thickness of the first layer 30 is equal to that of the second layer 32.
En variante non représentée, la deuxième couche de chaque portion à surchauffer présente une épaisseur supérieure à celle de la première couche. Selon une autre variante non représentée, la deuxième couche de chaque portion à surchauffer présente une épaisseur inférieure à celle de la première couche. In variant not shown, the second layer of each portion to be heated has a thickness greater than that of the first layer. According to another variant not shown, the second layer of each superheating portion has a thickness less than that of the first layer.
Selon encore une autre variante non représentée de l'invention, la deuxième couche de chaque portion à surchauffer présente une épaisseur variable en fonction du gradient de température de chauffage à obtenir dans la portion à surchauffer elle-même. Par exemple, l'épaisseur de la deuxième couche est proportionnelle à la température finale à obtenir à l'issue de l'étape de chauffage. Ainsi, au sein même de la portion à surchauffer, une zone à surchauffer modérément présentera une deuxième couche de faible épaisseur par rapport à une zone à surchauffer plus intensément.  According to yet another variant not shown of the invention, the second layer of each portion to be overheated has a variable thickness depending on the heating temperature gradient to be obtained in the portion to be superheated itself. For example, the thickness of the second layer is proportional to the final temperature to be obtained at the end of the heating step. Thus, even within the portion to be overheated, an area to be moderately overheated will have a second thin layer relative to an area to be overheated more intensely.
Ce premier mode de réalisation de la préforme 10 peut être obtenu par un procédé de surmoulage. Un tel procédé est bien connu de l'homme du métier, et l'on pourra se reporter au document EP-2.159.031 qui décrit un exemple de mise en œuvre d'un tel procédé. Le procédé décrit dans ce document est un procédé dit "bi-injection" comportant :  This first embodiment of the preform 10 can be obtained by an overmoulding process. Such a method is well known to those skilled in the art, and reference can be made to EP-2.159.031 which describes an example of implementation of such a method. The process described in this document is a so-called "bi-injection" process comprising:
- une première phase au cours de laquelle la deuxième couche 32 est tout d'abord réalisée par moulage par injection du deuxième matériau thermoplastique,  a first phase during which the second layer 32 is firstly produced by injection molding of the second thermoplastic material,
- puis, une deuxième phase au cours de laquelle la première couche 30 ainsi que le reste du corps 18 et le col 24 de la préforme 10 sont surmoulés par injection du premier matériau thermoplastique autour de cette deuxième couche 32.  - Then, a second phase during which the first layer 30 and the remainder of the body 18 and the neck 24 of the preform 10 are overmoulded by injection of the first thermoplastic material around this second layer 32.
Pour une explication plus détaillée de ce procédé "bi-injection", on se reportera directement au document cité.  For a more detailed explanation of this "bi-injection" process, reference will be made directly to the document cited.
On a représenté aux figures 7 et 8 un deuxième mode de réalisation de la préforme 10. Dans cet exemple, la portion 14 à surchauffer est formée essentiellement par le fond 22 de la préforme 10. La différence par rapport au premier mode de réalisation réside dans le fait que la deuxième couche 32 de la portion 14 à surchauffer est ici agencée à l'extérieur de la préforme 10 tandis que la première couche 30 est agencée vers l'intérieur de la préforme 10. FIGS. 7 and 8 show a second embodiment of the preform 10. In this example, the portion 14 to be overheated is essentially formed by the bottom 22 of the preform 10. The difference with respect to the first embodiment lies in the fact that the second layer 32 of the portion 14 to be overheated is here arranged outside the preform 10 while the first layer 30 is arranged towards the inside of the preform 10.
Pour réaliser une telle préforme, on réalise tout d'abord la première couche 30, la portion 16 distale et le col 24 par moulage par injection du premier matériau plastique. On obtient ainsi une préforme incomplète, comme représentée à la figure 7, dans laquelle un évidemment a été ménagé dans l'épaisseur de la portion 14 à surchauffer pour permettre de surmouler par la suite la deuxième couche 32 à l'extérieur de la première couche 30 par injection du deuxième matériau thermoplastique, comme représenté à la figure 8.  To produce such a preform, the first layer 30, the distal portion 16 and the neck 24 are first produced by injection molding of the first plastic material. An incomplete preform is thus obtained, as shown in FIG. 7, in which a recess has been formed in the thickness of the portion 14 to be superheated in order to allow the second layer 32 to be overmoulded on the outside of the first layer. By injection of the second thermoplastic material, as shown in FIG.
Lors de la suite du procédé de réalisation, la préforme 10 ainsi fabriquée selon l'un quelconque des modes de réalisation subit une étape "E1" intermédiaire de chauffage.  In the following embodiment of the process, the preform 10 thus manufactured according to any one of the embodiments undergoes a step "E1" intermediate heating.
Au cours de cette étape "E1" de chauffage, le corps 18 de la préforme 10 est chauffé par exposition uniforme du corps 18 entier de la préforme 10 à un rayonnement électromagnétique de chauffage. Il s'agit par exemple d'un rayonnement infrarouge ou d'un rayonnement micro-onde.  During this heating step "E1", the body 18 of the preform 10 is heated by uniform exposure of the entire body 18 of the preform 10 to electromagnetic heating radiation. This is for example infrared radiation or microwave radiation.
Selon un exemple non limitatif de mise en œuvre, le chauffage est effectué en faisant défiler les préformes 10 dans un four (non représenté) comportant au moins une paroi latérale chauffante, par exemple constituée par des tubes de chauffage fixés à la paroi du four, avec simultanément mise en rotation des préformes sur elles-mêmes pour homogénéiser le temps d'exposition de toutes les portions 14, 16 du corps 18 de la préforme 10. Des moyens de protection assurent la protection thermique du col 18. Un panneau réfléchissant peut de préférence être disposé en regard des tubes pour réfléchir vers les corps 18 des préformes 10 la fraction du rayonnement chauffant passant entre deux corps 18 successifs. Un tel dispositif de mise en œuvre est particulièrement adapté aux productions en grande série de récipients 26. According to a nonlimiting example of implementation, the heating is performed by scrolling the preforms 10 in a furnace (not shown) having at least one heating side wall, for example constituted by heating tubes attached to the wall of the furnace, with simultaneous rotation of the preforms on themselves to homogenize the exposure time of all the portions 14, 16 of the body 18 of the preform 10. Protection means provide thermal protection of the neck 18. A reflective panel can preferably be arranged opposite the tubes to reflect towards the bodies 18 of the preforms 10 the fraction of the passing heating radiation between two successive 18 bodies. Such an implementation device is particularly suitable for mass production of containers 26.
Ainsi, la portion 14 à surchauffer et la portion 16 distale sont exposées à un rayonnement chauffant identique, aussi bien en terme de temps d'exposition que de puissance du rayonnement.  Thus, the portion 14 to be overheated and the distal portion 16 are exposed to identical heating radiation, both in terms of exposure time and power of the radiation.
A l'issue de cette étape "E1" de chauffage, l'ensemble du corps 18 de la préforme est chauffé à une température supérieure à la température de ramollissement, ou température de transition vitreuse, du matériau par le rayonnement électromagnétique de chauffage.  At the end of this step "E1" of heating, the entire body 18 of the preform is heated to a temperature above the softening temperature, or glass transition temperature, of the material by the electromagnetic radiation heating.
Néanmoins, la deuxième couche 32 de la portion 14 à surchauffer aura absorbé une énergie plus importante que la portion 16 distale. Ceci se traduit par une augmentation plus rapide de la température de la deuxième couche 32 de la portion 14 à surchauffer par rapport à la portion 16 distale. Du fait de la surface de contact importante entre la première couche 30 et la deuxième couche 32, la chaleur emmagasinée dans la deuxième couche 32 est transmise par conduction à la première couche 30. Ainsi, la température de la portion 14 à surchauffer est homogène dans toute son épaisseur et elle est supérieure à la température de transition vitreuse atteinte par la portion 16 distale.  Nevertheless, the second layer 32 of the portion 14 to be overheated will have absorbed more energy than the distal portion 16. This results in a faster increase of the temperature of the second layer 32 of the portion 14 to overheat relative to the distal portion 16. Due to the large contact surface between the first layer 30 and the second layer 32, the heat stored in the second layer 32 is transmitted by conduction to the first layer 30. Thus, the temperature of the portion 14 to be superheated is homogeneous in its entire thickness and is greater than the glass transition temperature reached by the distal portion 16.
Ainsi, à la fin de l'étape "E1" de chauffage, chaque portion 14 à surchauffer est chauffée à une température encore supérieure à celle du reste du corps 18 du fait du coefficient d'absorption de la deuxième couche 32.  Thus, at the end of the heating step "E1", each portion 14 to be heated is heated to a temperature even higher than that of the remainder of the body 18 because of the absorption coefficient of the second layer 32.
Comme expliqué en préambule de la description, cette disparité de température entre la portion 14 à surchauffer et la portion 16 distale permet d'aboutir, à l'issue d'une étape "E2" finale de formage, par exemple par soufflage ou par étirage-soufflage, à un récipient 26 asymétrique présentant une épaisseur de paroi homogène, comme cela est illustré aux figures 2A, 2B et 2C. As explained in the preamble of the description, this disparity in temperature between the portion 14 to be heated and the distal portion 16 makes it possible, after a final step "E2" forming, for example by blowing or by stretching blowing, to an asymmetrical container 26 having a homogeneous wall thickness, as illustrated in Figures 2A, 2B and 2C.
Le procédé réalisé selon les enseignements de l'invention permet avantageusement de simplifier les fours de chauffage pour la mise en œuvre de l'étape "E1" intermédiaire de chauffage.  The process carried out according to the teachings of the invention advantageously makes it possible to simplify the heating furnaces for the implementation of the intermediate "E1" heating stage.
Les fours comportant moins de pièces sont ainsi moins onéreux à fabriquer.  Furnaces with fewer parts are thus less expensive to manufacture.
En outre, il est possible de réaliser des récipients de formes différentes sans perdre de temps en réglage du four, Toutes les préformes peuvent être exposées uniformément au rayonnement chauffant quelle que soit la forme du récipient final, y compris une forme symétrique de révolution. Le profil de chauffage des préformes est en effet désormais déterminé par la structure de la préforme elle-même, notamment par la répartition du deuxième matériau thermoplastique absorbant, et non par son temps d'exposition au rayonnement de chauffage.  In addition, it is possible to produce containers of different shapes without losing time in setting the oven, All preforms can be uniformly exposed to the heating radiation regardless of the shape of the final container, including a symmetrical shape of revolution. The heating profile of the preforms is in fact now determined by the structure of the preform itself, in particular by the distribution of the second absorbent thermoplastic material, and not by its exposure time to the heating radiation.
De plus, il est possible de réaliser des profils de chauffage très précis car les portions 14 à surchauffer sont désormais déterminées structurellement.  In addition, it is possible to achieve very precise heating profiles because the portions 14 to be overheated are now determined structurally.

Claims

REVENDICATIONS
1. Procédé de réalisation d'un récipient (26), tel qu'une bouteille, en matériau thermoplastique par soufflage ou étirage-soufflage du corps (18) d'une préforme (10) préchauffée par un rayonnement de chauffage, le procédé comportant une étape (E2) finale de formage du récipient (26) par soufflage ou étirage-soufflage au cours de laquelle le récipient (26) est obtenu par étirement du corps (18) de la préforme (10), au moins une portion (14) du corps (18) de la préforme (10) subissant un étirage plus rapide par rapport aux portions (16) formant le reste du corps (18) ;  1. A method of producing a container (26), such as a bottle, of thermoplastic material by blow molding or stretch blow molding of the body (18) of a preform (10) preheated by heating radiation, the method comprising a final step (E2) for forming the container (26) by blow molding or stretch-blow molding during which the container (26) is obtained by stretching the body (18) of the preform (10), at least a portion (14) ) the body (18) of the preform (10) being stretched more rapidly relative to the portions (16) forming the remainder of the body (18);
le procédé comportant :  the process comprising:
- une étape (E0) initiale de fabrication d'une préforme (10) dans laquelle la portion (14) du corps (18) destinée à subir un étirage plus rapide présente un coefficient d'absorption du rayonnement de chauffage plus grand que celui du reste du corps, le corps (18) de la préforme étant réalisé au moyen d'un premier matériau thermoplastique, chaque portion (14) destinée à subir un étirage plus rapide durant l'étape (E2) de formage étant réalisée par superposition d'une première couche (30) dudit premier matériau et d'une deuxième couche (32) d'un deuxième matériau thermoplastique présentant un coefficient d'absorption du rayonnement de chauffage plus grand que celui du premier matériau ;  an initial step (E0) of manufacture of a preform (10) in which the portion (14) of the body (18) intended to undergo a faster drawing has a coefficient of absorption of the heating radiation greater than that of the remainder of the body, the body (18) of the preform being made by means of a first thermoplastic material, each portion (14) intended to undergo a more rapid drawing during the forming step (E2) being carried out by superposition of a first layer (30) of said first material and a second layer (32) of a second thermoplastic material having a greater heating radiation absorption coefficient than that of the first material;
- une étape (E1) intermédiaire de chauffage du corps (18) de la préforme par exposition uniforme du corps (18) entier de la préforme au rayonnement électromagnétique de chauffage, à l'issue de laquelle l'ensemble du corps (18) de la préforme (10) est chauffé à une température supérieure à la température de ramollissement des matériaux la constituant par le rayonnement électromagnétique de chauffage, chaque portion (14) destinée à subir un étirage plus rapide au cours de l'étape (E2) de formage étant surchauffée à une température encore supérieure à celle du reste du corps (18) du fait de son coefficient d'absorption ; an intermediate step (E1) for heating the body (18) of the preform by uniform exposure of the entire body (18) of the preform to the electromagnetic heating radiation, at the end of which the entire body (18) of the preform (10) is heated to a temperature above the softening temperature of the materials constituting it by the electromagnetic heating radiation, each portion (14) intended to undergo a faster stretching during the forming step (E2) being superheated to a temperature still higher than that of the rest of the body (18) due to its absorption coefficient;
caractérisé en ce que la première couche (30) de chaque portion (14) à surchauffer présente une épaisseur inférieure au reste du corps (18) de la préforme (10).  characterized in that the first layer (30) of each portion (14) to be superheated has a thickness less than the rest of the body (18) of the preform (10).
2. Procédé selon la revendication précédente, caractérisé en ce que la deuxième couche (32) de chaque portion (14) à surchauffer présente une épaisseur proportionnelle à la température de chauffage à obtenir dans la portion (14) à surchauffer.  2. Method according to the preceding claim, characterized in that the second layer (32) of each portion (14) to superheat has a thickness proportional to the heating temperature to be obtained in the portion (14) to overheat.
3. Procédé selon l'une quelconque des revendications précédentes, caractérisé en ce que la préforme (10) présente une paroi d'épaisseur uniforme, y compris dans la portion (14) à surchauffer.  3. Method according to any one of the preceding claims, characterized in that the preform (10) has a wall of uniform thickness, including the portion (14) to overheat.
4. Procédé selon l'une quelconque des revendications précédentes, caractérisé en ce que la première couche (30) de chaque portion à surchauffer est réalisée venue de matière avec le reste du corps (18).  4. Method according to any one of the preceding claims, characterized in that the first layer (30) of each portion to be overheated is made integral with the rest of the body (18).
5. Procédé selon la revendication précédente, caractérisé en ce que la deuxième couche (32) est réalisée par moulage par injection.  5. Method according to the preceding claim, characterized in that the second layer (32) is produced by injection molding.
6. Procédé selon la revendication précédente, caractérisé en ce que la première couche (30) est réalisée par surmoulage sur la deuxième couche (32) préalablement obtenue par moulage par injection.  6. Method according to the preceding claim, characterized in that the first layer (30) is formed by overmoulding on the second layer (32) previously obtained by injection molding.
7. Procédé selon l'une quelconque des revendications précédentes, caractérisé en ce que le deuxième matériau présente la même composition que le premier matériau à laquelle est ajouté un additif qui favorise l'absorption du rayonnement de chauffage.  7. Method according to any one of the preceding claims, characterized in that the second material has the same composition as the first material to which is added an additive that promotes the absorption of the heating radiation.
8. Procédé selon l'une quelconque des revendications 1 à 6, caractérisé en ce que le deuxième matériau thermoplastique présente une composition différente du premier matériau thermoplastique. 8. Method according to any one of claims 1 to 6, characterized in that the second thermoplastic material has a different composition of the first thermoplastic material.
9. Procédé selon l'une quelconque des revendications précédentes, caractérisé en ce que la deuxième couche (32) d'au moins une portion (14) à surchauffer est agencée à l'extérieur de la préforme (10).  9. Method according to any one of the preceding claims, characterized in that the second layer (32) of at least one portion (14) to be heated is arranged outside the preform (10).
10. Procédé selon l'une quelconque des revendications 1 à 8, caractérisé en ce que la deuxième couche (32) d'au moins une portion à surchauffer est agencée à l'intérieur de la préforme (10).  10. Process according to any one of claims 1 to 8, characterized in that the second layer (32) of at least one superheating portion is arranged inside the preform (10).
PCT/EP2014/054787 2013-03-19 2014-03-12 Process for producing a container from a preform having a portion to be superheated comprising a layer of material capable of being selectively superheated WO2014146938A1 (en)

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FR1352431 2013-03-19
FR1352431A FR3003505B1 (en) 2013-03-19 2013-03-19 "METHOD OF MAKING A CONTAINER FROM A PREFORM COMPRISING AN OVERHEATING PORTION COMPRISING A LAYER OF MATERIAL THAT CAN BE SELECTIVELY OVERHEATED"

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Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5681521A (en) * 1993-04-15 1997-10-28 Sidel Process and equipment for heat treatment of the body of a preform or of an intermediate-stage container made of a thermoplastic material
WO2001047688A2 (en) * 1999-12-24 2001-07-05 Resilux Process and apparatus for treating plastic preforms
DE102010015019A1 (en) * 2010-04-14 2011-10-20 Krones Ag Premold for producing e.g. polyethylene terephthalate bottle, utilized for filling beverage, has hollow body comprising outer and inner surfaces, where region with absorption or reflection for thermal radiation is arranged on surfaces

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5681521A (en) * 1993-04-15 1997-10-28 Sidel Process and equipment for heat treatment of the body of a preform or of an intermediate-stage container made of a thermoplastic material
WO2001047688A2 (en) * 1999-12-24 2001-07-05 Resilux Process and apparatus for treating plastic preforms
DE102010015019A1 (en) * 2010-04-14 2011-10-20 Krones Ag Premold for producing e.g. polyethylene terephthalate bottle, utilized for filling beverage, has hollow body comprising outer and inner surfaces, where region with absorption or reflection for thermal radiation is arranged on surfaces

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FR3003505A1 (en) 2014-09-26

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