WO2024047603A1 - Method for automatically determining the electrical energy to be supplied to a furnace for heating preforms, arranged upstream of a stretch-blow molding machine - Google Patents
Method for automatically determining the electrical energy to be supplied to a furnace for heating preforms, arranged upstream of a stretch-blow molding machine Download PDFInfo
- Publication number
- WO2024047603A1 WO2024047603A1 PCT/IB2023/058668 IB2023058668W WO2024047603A1 WO 2024047603 A1 WO2024047603 A1 WO 2024047603A1 IB 2023058668 W IB2023058668 W IB 2023058668W WO 2024047603 A1 WO2024047603 A1 WO 2024047603A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- heating
- stretching ratio
- preform
- heating elements
- electrical energy
- Prior art date
Links
- 238000010438 heat treatment Methods 0.000 title claims abstract description 181
- 238000000034 method Methods 0.000 title claims abstract description 37
- 238000000071 blow moulding Methods 0.000 title claims abstract description 12
- 238000011144 upstream manufacturing Methods 0.000 title claims abstract description 10
- 238000000465 moulding Methods 0.000 claims abstract description 21
- FGUUSXIOTUKUDN-IBGZPJMESA-N C1(=CC=CC=C1)N1C2=C(NC([C@H](C1)NC=1OC(=NN=1)C1=CC=CC=C1)=O)C=CC=C2 Chemical compound C1(=CC=CC=C1)N1C2=C(NC([C@H](C1)NC=1OC(=NN=1)C1=CC=CC=C1)=O)C=CC=C2 FGUUSXIOTUKUDN-IBGZPJMESA-N 0.000 claims description 7
- GNFTZDOKVXKIBK-UHFFFAOYSA-N 3-(2-methoxyethoxy)benzohydrazide Chemical compound COCCOC1=CC=CC(C(=O)NN)=C1 GNFTZDOKVXKIBK-UHFFFAOYSA-N 0.000 claims description 3
- 230000003213 activating effect Effects 0.000 claims description 2
- 238000007664 blowing Methods 0.000 description 5
- 238000004519 manufacturing process Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 230000009123 feedback regulation Effects 0.000 description 2
- 238000009423 ventilation Methods 0.000 description 2
- 230000004913 activation Effects 0.000 description 1
- 239000003570 air Substances 0.000 description 1
- WYTGDNHDOZPMIW-RCBQFDQVSA-N alstonine Natural products C1=CC2=C3C=CC=CC3=NC2=C2N1C[C@H]1[C@H](C)OC=C(C(=O)OC)[C@H]1C2 WYTGDNHDOZPMIW-RCBQFDQVSA-N 0.000 description 1
- 239000012080 ambient air Substances 0.000 description 1
- 230000033228 biological regulation Effects 0.000 description 1
- 230000002301 combined effect Effects 0.000 description 1
- 230000003750 conditioning effect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C49/00—Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
- B29C49/42—Component parts, details or accessories; Auxiliary operations
- B29C49/64—Heating or cooling preforms, parisons or blown articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C49/00—Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
- B29C49/42—Component parts, details or accessories; Auxiliary operations
- B29C49/42398—Simulation of the blow-moulding process
- B29C49/424—Simulation of the preform conditioning process
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C49/00—Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
- B29C49/42—Component parts, details or accessories; Auxiliary operations
- B29C49/64—Heating or cooling preforms, parisons or blown articles
- B29C49/6409—Thermal conditioning of preforms
- B29C49/6418—Heating of preforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C49/00—Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
- B29C49/42—Component parts, details or accessories; Auxiliary operations
- B29C49/64—Heating or cooling preforms, parisons or blown articles
- B29C49/68—Ovens specially adapted for heating preforms or parisons
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C49/00—Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
- B29C49/42—Component parts, details or accessories; Auxiliary operations
- B29C49/78—Measuring, controlling or regulating
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C49/00—Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
- B29C49/42—Component parts, details or accessories; Auxiliary operations
- B29C49/78—Measuring, controlling or regulating
- B29C2049/788—Controller type or interface
- B29C2049/78805—Computer or PLC control
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C49/00—Blow-moulding, i.e. blowing a preform or parison to a desired shape within a mould; Apparatus therefor
- B29C49/02—Combined blow-moulding and manufacture of the preform or the parison
- B29C49/06—Injection blow-moulding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/712—Containers; Packaging elements or accessories, Packages
- B29L2031/7158—Bottles
Definitions
- the present invention relates to a method for automatically determining the electrical energy in kWh to be supplied to a furnace provided with a plurality of heating modules arranged in at least one bench upstream of a stretch-blow molding machine.
- the stretch-blowing process must be preceded by a temperature conditioning step of the preforms, in which the preforms are heated to a predefined temperature for the blowing by means of specific heating modules which use a plurality of heating elements, e.g., infrared lamps.
- the heating modules are arranged symmetrically in two benches connected by a curved stretch.
- the heating elements in each module are arranged along a plane substantially parallel to the plane containing the axes of the preforms advancing along the respective bench.
- the neck of the preforms must remain substantially cold, i.e., at a temperature lower than the softening temperature so that the successive blowing operations do not deform it.
- This ventilation allows the ambient temperature of the heating module to be kept at a desirable level, eliminating the excessive heat, for example due to the infrared rays not captured by the preforms, and the temperature of the preform skin to be moderated.
- a desirable level of the inner temperature of the heating module is the one that allows the energy performance thereof to be optimized. It is well known that this energy performance is a function of the thickness of the preforms.
- the ventilation flow rate must be sufficient to perform this function, and it is desirable for it to be well-distributed in the heating module so that the whole surface of the preform wall, which must be heated, is treated homogeneously.
- a predictive-type method which allows automatically determining the optimal electrical energy in kWh to be supplied to the heating modules according to a predefined hourly productivity of the molding machine which blow molds specific containers starting from a specific preform, is not known.
- the present invention achieves at least one of such objects and other objects that will be apparent in light of the present description by means of a method for automatically determining the electrical energy in kWh to be supplied to a furnace provided with a plurality of heating modules arranged in at least one bench upstream of a stretch-blow molding machine provided with a plurality of molding cavities for molding containers, wherein each heating module is provided with a plurality of heating elements arranged along a plane substantially parallel to the plane containing the axes of the preforms advancing along the bench, the method comprising the following steps a) providing the following parameters as input data:
- said first range of total stretching ratio comprises values less than or equal to 8; said second range of total stretching ratio comprises values greater than 8 and less than 13.5; and said third range of total stretching ratio comprises values greater than or equal to 13.5; while coefficient “a” has a value from 0.45 to 0.58; coefficient “b” has a value from -0.25 to -0.35; coefficient “c” has a value from 0.60 to 0.75; coefficient “d” has a value from -0.36 to -0.50; coefficient “e” has a value from 0.75 to 0.86; and coefficient “f” has a value from -0.54 to - 0.60.
- the method of the invention also allows a quick and effective parameterization of the industrial stretch-blow process in few minutes with the goal of obtaining a product at 80% of its conformity.
- Figure 1 shows a diagrammatic layout of a heating module bench of a furnace arranged upstream of a molding machine
- Figure 2 shows a diagrammatic sectional view of a heating module crossed by the preforms
- Figure 3 diagrammatically shows an activation criterion of the heating elements close to the bottom of the preform
- Figure 3a shows a variant indicating the last and second-last heating element to be activated in a heating module
- Figure 4 shows a diagrammatic sectional view of a preform
- Figure 5 shows a diagrammatic side view of a container blown from the preform in Figure 4.
- Figure 6 shows a diagram with some input data for performing a method according to the invention
- Figure 7 shows three trend curves of the specific power W/g according to the net weight of the preform in grams.
- Figure 1 shows a generic furnace, indicated by reference numeral 1 , provided with a plurality of heating modules 2 arranged in a bench upstream of a stretch-blow molding machine 3 provided with a plurality of molding cavities (not shown) for molding containers.
- Arrow X indicates the advancement direction of the preforms 5 crossing the respective heating modules 2.
- the heating modules 2 can be arranged in at least two benches connected by a connection stretch, e.g., a curved or serpentine stretch.
- the molding machine 3 can be a linear-type machine or a rotary machine.
- each heating module 2 is provided with a plurality of heating elements 6 arranged along a plane substantially parallel to the plane containing the axes of the preforms 5 advancing along the bench on a transport line 4, for example, provided with chucks.
- the method of the present invention is a predictive method for automatically determining the optimal electrical energy in kWh for a predefined hourly productivity of a specific container blown from a specific preform.
- Such a method advantageously comprises the following steps: a) providing the following parameters as input data:
- step f the electrical energy in kWh required for said hourly productivity v is equal to:
- the first range of total stretching ratio comprises values less than or equal to 8; the second range of total stretching ratio comprises values greater than 8 and less than 13.5; and the third range of total stretching ratio comprises values greater than or equal to 13.5; while coefficient “a” has a value from 0.45 to 0.58; coefficient “b” has a value from -0.25 to -0.35; coefficient “c” has a value from 0.60 to 0.75; coefficient “d” has a value from -0.36 to -0.50; coefficient “e” has a value from 0.75 to 0.86; and coefficient “f” has a value from -0.54 to -0.60.
- coefficient “a” has a value from 0.45 to 0.55; coefficient “b” has a value from -0.27 to -0.35; coefficient “c” has a value from 0.60 to 0.72; coefficient “d” has a value from -0.40 to -0.48; coefficient “e” has a value from 0.78 to 0.86; coefficient “f” has a value from -0.54 to -0.60.
- the method of the invention allows the number of heating elements to be activated in each heating module to be automatically identified.
- step f) identifying the number of heating elements to be activated in each heating module ( Figure 3), always including all the heating elements 6 lying on a horizontal plane intersecting the body of the advancing preforms, and including the adjacent successive further heating element 6’ lying on a respective horizontal plane not intersecting the body of the preforms only in case, considering the center distance between the last of said heating elements 6 lying on a horizontal plane intersecting the body of the preforms and said successive further heating element 6’ proximal thereto, the height Y corresponding to the half-center distance of said center distance intersects the bottom of the preforms; h) activating, in each heating module 2, the heating elements identified in step g) by distributing said electrical energy in kWh on said identified heating elements.
- the last of the heating elements 6 lying on a horizontal plane intersecting the body of the preforms is the most distal one from the neck of the advancing preforms.
- the successive further heating element 6’ lying on a respective horizontal plane not intersecting the body of the preforms, is arranged below the last of said heating elements 6 lying on a horizontal plane intersecting the body of the preforms in case the transport line is configured to advance the preforms with the opening of the neck facing upwards, as shown in Figures 2 and 3.
- successive further heating element 6’ it is not excluded for the successive further heating element 6’ to be arranged above said last heating element 6 in case the transport line is configured to advance the preforms with the opening of the neck facing downwards.
- Figure 3 diagrammatically shows the criterion for identifying the heating elements to be activated according to the length of the preform (step g).
- the term “ON” indicates the heating elements to be activated, while the term “OFF” indicates the heating elements which remain switched off.
- the heating elements 6, 6’ can be infrared lamps arranged along a plane substantially parallel to said plane containing the axes of the preforms crossing the heating module.
- LED, NIR or laser lamps can be used, or another suitable heating element.
- Figures 4 and 5 respectively show an example of preform and container obtained by stretch-blow molding.
- H p height of the preform
- hp_ n height of the preform neck
- h p _ur height of the preform area under neck ring
- d O ut_max maximum outer diameter of the preform
- tmax maximum thickness of the preform
- H c height of the container
- h c _n height of the container neck
- h c _ur height of the container area under neck ring
- D O ut_max maximum outer diameter of the container.
- area under neck ring means the area immediately below the support ring 7 where there remains a greater thickness of the container due to the unstretched material after the blowing.
- Further input data can further comprise:
- the distribution of the electrical energy in kWh on the identified heating elements 6, 6’ is performed according to a first profile in case also the further heating element 6’ lying on a respective horizontal plane not intersecting the body of the preforms is to be activated, or, is performed according to a second profile in case also said further heating element 6’ is not to be activated.
- Profile means the distribution trend of the electrical energy in kWh on the identified heating elements 6, 6’ along a direction parallel to the axes of the preforms 5 advancing along the bench.
- an optimal and automated distribution of the electrical energy in kWh on the identified heating elements 6, 6’ is determined in the following manner:
- A being defined as the electrical energy in kWh, calculated in step f), divided by the number of identified heating elements 6, 6’ in all the plurality of heating modules 2, n being defined as the number of identified heating elements 6, 6’ in each heating module 2, in each heating module 2 - for the upper identified heating element, arranged in position most proximal to the support ring 7 of the advancing preforms, the electrical energy to be supplied is equal to
- Ai A + x*A, where coefficient x varies in a range from 1/9 to 3/4;
- Ai [(A*n)-Ai]/(n-1).
- A being defined as the electrical energy in kWh, calculated in step f), divided by the number of identified heating elements 6 in all the plurality of heating modules 2, n being defined as the number of identified heating elements 6 in each heating module 2, in each heating module 2
- the electrical energy to be supplied is equal to
- Ai A + x*A, where coefficient x varies in a range from 1/9 to 3/4;
- the electrical energy to be supplied is equal to An-1 — Ai - X*Ai.
- an optimal and automated distribution of the electrical energy in kWh on the identified heating elements 6, 6’ is determined in the following manner:
- A being defined as the electrical energy in kWh, calculated in step f), divided by the number of identified heating elements 6, 6’ in all the plurality of heating modules 2, n being defined as the number of identified heating elements 6, 6’ in each heating module 2, in each heating module 2
- the electrical energy to be supplied is equal to
- Ai A + x*A, where coefficient x varies in a range from 1/9 to 3/4;
- Ai [(A*n)-Ai]/(n-1).
- A being defined as the electrical energy in kWh, calculated in step f), divided by the number of identified heating elements 6 in all the plurality of heating modules 2, n being defined as the number of identified heating elements 6 in each heating module 2, in each heating module 2
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)
Abstract
A method for automatically determining the electrical energy in kWh to be supplied to a furnace provided with a plurality of heating modules arranged in at least one bench upstream of a stretch-blow molding machine provided with a plurality of molding cavities for molding containers, in which each heating module is provided with a plurality of heating elements arranged along a plane substantially parallel to the plane containing the axes of the preforms advancing along the bench, the method comprising the following steps a) providing the following parameters as input data: - hourly productivity (v) of the molding machine; - geometrical and weight data of the preform and preform neck; - geometrical data of the container to be molded; - number of heating modules; - number of heating elements in each heating module; b) providing a first range of total stretching ratio; a second range of total stretching ratio; and a third range of total stretching ratio; c) providing a first curve y=a*x-b, a second curve y=c*x-d, and a third curve y=e*x-f, where y is the specific power in W/g that the heating elements have to supply for each gram of net weight of the preform, and where x is the net weight of the preform in grams; d) calculating the total stretching ratio by multiplying the axial stretching ratio by the radial stretching ratio; e) extracting the value W/g from the first curve if the total stretching ratio calculated in step d) falls in the first range, from the second curve if said total stretching ratio falls in the second range, or from the third curve if the total stretching ratio falls in the third range; f) calculating the electrical energy in kWh required for said hourly productivity (v).
Description
METHOD FOR AUTOMATICALLY DETERMINING THE ELECTRICAL ENERGY TO BE SUPPLIED TO A FURNACE FOR HEATING PREFORMS, ARRANGED UPSTREAM OF A STRETCH-BLOW MOLDING MACHINE
★★★★★★★★★★★
Field of the invention
The present invention relates to a method for automatically determining the electrical energy in kWh to be supplied to a furnace provided with a plurality of heating modules arranged in at least one bench upstream of a stretch-blow molding machine.
Background art
It is known that the stretch-blowing process must be preceded by a temperature conditioning step of the preforms, in which the preforms are heated to a predefined temperature for the blowing by means of specific heating modules which use a plurality of heating elements, e.g., infrared lamps.
Generally, the heating modules are arranged symmetrically in two benches connected by a curved stretch. The heating elements in each module are arranged along a plane substantially parallel to the plane containing the axes of the preforms advancing along the respective bench.
During the passage of the preforms in these modules, the neck of the preforms must remain substantially cold, i.e., at a temperature lower than the softening temperature so that the successive blowing operations do not deform it.
It is also known that the heating of the body of the preforms is achieved due to the combined effect of:
- thermal radiation which penetrates into the thickness of the body of the preform (convection);
- contact with the ambient air heated inside the furnace (conduction);
- diffusion of the heat by conduction into the wall of the preform (stabilization/temperature inversion).
It also is important to ventilate the inside of the heating module and the outer surface of the preforms therein with a preset air flow so that the material of the outer surface of the preform is not brought to a too high temperature, which would cause it to crystalize while waiting for the material arranged inside the preform to
reach the blowing temperature. This ventilation allows the ambient temperature of the heating module to be kept at a desirable level, eliminating the excessive heat, for example due to the infrared rays not captured by the preforms, and the temperature of the preform skin to be moderated. Such a desirable level of the inner temperature of the heating module is the one that allows the energy performance thereof to be optimized. It is well known that this energy performance is a function of the thickness of the preforms. The ventilation flow rate must be sufficient to perform this function, and it is desirable for it to be well-distributed in the heating module so that the whole surface of the preform wall, which must be heated, is treated homogeneously.
Actually, it is still quite complex, in particular for operators with little experience, to optimally manage the heating elements of preforms in the heating modules arranged upstream of the stretch-blow molding machine according to the geometrical and weight data of the preform, the geometrical data of the container to be molded and the hourly productivity of the stretch-blow molding machine, expressed in containers per molding cavity per hour.
Known solutions exist which provide a feedback regulation of the electrical energy in kWh to be supplied to the heating elements of each module, said regulation being based on a control during the performance of the container production process. Disadvantageously, however, the production process proceeds prior to this feedback regulation, resulting in the arrival of not perfectly heated preforms at the stretch-blow molding machine.
In any case, a predictive-type method, which allows automatically determining the optimal electrical energy in kWh to be supplied to the heating modules according to a predefined hourly productivity of the molding machine which blow molds specific containers starting from a specific preform, is not known.
Therefore, the need is felt to provide an automated method of the predictive type. Summary of the invention
It is an object of the present invention to provide a predictive-type method for automatically determining, by means of computer, the optimal electrical energy in kWh to be supplied to the heating modules of a furnace arranged upstream of a stretch-blow molding machine having a predefined hourly productivity of a specific
container blown from a specific preform.
It is another object of the present invention to provide a predictive-type method for managing the heating elements of preforms in said heating modules.
It is another object of the present invention to provide a method which is also capable of automatically identifying the number of heating elements to be activated in each heating module.
It is a further object of the present invention to provide a predictive-type method for obtaining an optimal distribution of the electrical energy in kWh on the heating elements to be activated in each heating module.
The present invention achieves at least one of such objects and other objects that will be apparent in light of the present description by means of a method for automatically determining the electrical energy in kWh to be supplied to a furnace provided with a plurality of heating modules arranged in at least one bench upstream of a stretch-blow molding machine provided with a plurality of molding cavities for molding containers, wherein each heating module is provided with a plurality of heating elements arranged along a plane substantially parallel to the plane containing the axes of the preforms advancing along the bench, the method comprising the following steps a) providing the following parameters as input data:
- hourly productivity v of the molding machine, expressed in containers per molding cavity per hour;
- geometrical and weight data of the preform and preform neck;
- geometrical data of the container to be molded;
- number of heating modules;
- number of heating elements in each heating module; b) providing a first range of total stretching ratio; a second range of total stretching ratio comprising greater values than said first range; and a third range of total stretching ratio comprising greater values than said second range; c) providing a first curve y=a*x b, a second curve y=c*x d, and a third curve y=e*x f, where y is the specific power or power-to-mass ratio in W/g defining the power that the heating elements have to absorb for each gram of net weight of the preform, wherein said net weight of the preform is equal to the weight of the preform less
the weight of the preform neck, and where x is the net weight of the preform in grams; d) calculating the total stretching ratio by multiplying the axial stretching ratio by the radial stretching ratio; e) extracting the value W/g from the first curve if the total stretching ratio calculated in step d) falls in the first range, from the second curve if said total stretching ratio falls in the second range, or from the third curve if the total stretching ratio falls in the third range; f) calculating the electrical energy in kWh required for said hourly productivity v.
In a preferred variant, said first range of total stretching ratio comprises values less than or equal to 8; said second range of total stretching ratio comprises values greater than 8 and less than 13.5; and said third range of total stretching ratio comprises values greater than or equal to 13.5; while coefficient “a” has a value from 0.45 to 0.58; coefficient “b” has a value from -0.25 to -0.35; coefficient “c” has a value from 0.60 to 0.75; coefficient “d” has a value from -0.36 to -0.50; coefficient “e” has a value from 0.75 to 0.86; and coefficient “f” has a value from -0.54 to - 0.60.
Advantageously, the method of the invention also allows a quick and effective parameterization of the industrial stretch-blow process in few minutes with the goal of obtaining a product at 80% of its conformity.
By carrying out this method, the testing times are considerably shortened also in the presence of operators with little experience, for whom statistically it is complex to perform the first part (80%) of the industrial stretch-blow process, but it is simpler and more effective to complete the remaining 20% of the industrial process according to a final adjustment criterion.
Further features and advantages of the invention will become more apparent in light of the detailed description of exemplary, but non-exclusive embodiments thereof.
The dependent claims describe particular embodiments of the invention.
Brief description of the drawings
In the description of the invention, reference is made to the accompanying drawings, which are provided by way of non-limiting example, in which:
Figure 1 shows a diagrammatic layout of a heating module bench of a furnace arranged upstream of a molding machine;
Figure 2 shows a diagrammatic sectional view of a heating module crossed by the preforms;
Figure 3 diagrammatically shows an activation criterion of the heating elements close to the bottom of the preform;
Figure 3a shows a variant indicating the last and second-last heating element to be activated in a heating module;
Figure 4 shows a diagrammatic sectional view of a preform;
Figure 5 shows a diagrammatic side view of a container blown from the preform in Figure 4;
Figure 6 shows a diagram with some input data for performing a method according to the invention;
Figure 7 shows three trend curves of the specific power W/g according to the net weight of the preform in grams.
The same reference numerals and letters in the figures identify the same elements or components.
Description of embodiments of the invention
Figure 1 shows a generic furnace, indicated by reference numeral 1 , provided with a plurality of heating modules 2 arranged in a bench upstream of a stretch-blow molding machine 3 provided with a plurality of molding cavities (not shown) for molding containers.
Arrow X indicates the advancement direction of the preforms 5 crossing the respective heating modules 2.
Alternatively, the heating modules 2 can be arranged in at least two benches connected by a connection stretch, e.g., a curved or serpentine stretch.
The molding machine 3 can be a linear-type machine or a rotary machine.
As better shown in Figure 2, each heating module 2 is provided with a plurality of heating elements 6 arranged along a plane substantially parallel to the plane containing the axes of the preforms 5 advancing along the bench on a transport line 4, for example, provided with chucks.
The method of the present invention is a predictive method for automatically
determining the optimal electrical energy in kWh for a predefined hourly productivity of a specific container blown from a specific preform.
Such a method advantageously comprises the following steps: a) providing the following parameters as input data:
- hourly productivity v of the molding machine, expressed in containers per molding cavity per hour (containers/cavities per hour);
- geometrical and weight data of the preform and preform neck;
- geometrical data of the container to be molded;
- number of heating modules 2;
- number of heating elements in each heating module 2; b) providing a first range of total stretching ratio; a second range of total stretching ratio comprising greater values than said first range; and a third range of total stretching ratio comprising greater values than said second range; c) providing a first curve y=a*x b, a second curve y=c*x d, and a third curve y=e*x f, where y is the specific power or power-to-mass ratio in W/g defining the power that the heating elements have to absorb for each gram of net weight of the preform, wherein said net weight of the preform is equal to the weight of the preform minus the weight of the preform neck, and where x is the net weight of the preform in grams; d) calculating the total stretching ratio by multiplying the axial stretching ratio by the radial stretching ratio; e) extracting the value W/g from the first curve if the total stretching ratio calculated in step d) falls in the first range, from the second curve if said total stretching ratio falls in the second range, or from the third curve if the total stretching ratio falls in the third range; f) calculating the electrical energy in kWh required for said hourly productivity v.
In step f), the electrical energy in kWh required for said hourly productivity v is equal to:
(W/g * net weight of the preform * v * number of molding cavities) / 1000, where W/g is the value extracted in step e).
Surprisingly, after lengthy and complex technical considerations, the inventors discovered that by using predefined ranges of total stretching ratio and of
coefficients a, b, c, d, e, f of the three curves of step c) in combination with each other, the technical effect of automatically predicting the optimal electrical energy in kWh for a predefined hourly productivity of a specific container blown from a specific preform is reached in a simple, quick and highly efficient manner while considerably reducing consumption. This prediction is also useful for then automatically identifying the number of heating elements to be activated in each heating module.
In a preferred, but not exclusive variant, the first range of total stretching ratio comprises values less than or equal to 8; the second range of total stretching ratio comprises values greater than 8 and less than 13.5; and the third range of total stretching ratio comprises values greater than or equal to 13.5; while coefficient “a” has a value from 0.45 to 0.58; coefficient “b” has a value from -0.25 to -0.35; coefficient “c” has a value from 0.60 to 0.75; coefficient “d” has a value from -0.36 to -0.50; coefficient “e” has a value from 0.75 to 0.86; and coefficient “f” has a value from -0.54 to -0.60.
In a further variant of the invention, coefficient “a” has a value from 0.45 to 0.55; coefficient “b” has a value from -0.27 to -0.35; coefficient “c” has a value from 0.60 to 0.72; coefficient “d” has a value from -0.40 to -0.48; coefficient “e” has a value from 0.78 to 0.86; coefficient “f” has a value from -0.54 to -0.60.
Preferably, the method of the invention allows the number of heating elements to be activated in each heating module to be automatically identified.
To obtain this result, after step f), the following steps are provided: g) identifying the number of heating elements to be activated in each heating module (Figure 3), always including all the heating elements 6 lying on a horizontal plane intersecting the body of the advancing preforms, and including the adjacent successive further heating element 6’ lying on a respective horizontal plane not intersecting the body of the preforms only in case, considering the center distance between the last of said heating elements 6 lying on a horizontal plane intersecting the body of the preforms and said successive further heating element 6’ proximal thereto, the height Y corresponding to the half-center distance of said center distance intersects the bottom of the preforms;
h) activating, in each heating module 2, the heating elements identified in step g) by distributing said electrical energy in kWh on said identified heating elements. The last of the heating elements 6 lying on a horizontal plane intersecting the body of the preforms is the most distal one from the neck of the advancing preforms.
The successive further heating element 6’, lying on a respective horizontal plane not intersecting the body of the preforms, is arranged below the last of said heating elements 6 lying on a horizontal plane intersecting the body of the preforms in case the transport line is configured to advance the preforms with the opening of the neck facing upwards, as shown in Figures 2 and 3.
Alternatively, it is not excluded for the successive further heating element 6’ to be arranged above said last heating element 6 in case the transport line is configured to advance the preforms with the opening of the neck facing downwards.
Figure 3 diagrammatically shows the criterion for identifying the heating elements to be activated according to the length of the preform (step g). The term “ON” indicates the heating elements to be activated, while the term “OFF” indicates the heating elements which remain switched off.
In all the embodiments of the invention, the heating elements 6, 6’ can be infrared lamps arranged along a plane substantially parallel to said plane containing the axes of the preforms crossing the heating module. As an alternative to the infrared lamps, LED, NIR or laser lamps can be used, or another suitable heating element. Figures 4 and 5 respectively show an example of preform and container obtained by stretch-blow molding. These figures indicate geometrical data examples of the preform and container to be molded that are used by the method of the invention: Hp = height of the preform, hp_n = height of the preform neck, hp_ur = height of the preform area under neck ring, dOut_max = maximum outer diameter of the preform, tmax = maximum thickness of the preform, Hc = height of the container, hc_n = height of the container neck, hc_ur = height of the container area under neck ring, DOut_max = maximum outer diameter of the container.
As known in the field, the term “area under neck ring” means the area immediately below the support ring 7 where there remains a greater thickness of the container due to the unstretched material after the blowing.
Considering these geometrical data, the radial stretching ratio is calculated with the following ratio
Dout_max I (dout_ max " tmax) , while the axial stretching ratio is calculated with the following ratio (Hc_hc_n"hc_ur)/(Hp-hp_n-hp_ur).
Further input data can further comprise:
- the center distance of the heating elements, preferably equal in each heating module;
- the maximum power of the heating elements, preferably equal in each heating module.
Preferably, in step h), the distribution of the electrical energy in kWh on the identified heating elements 6, 6’ is performed according to a first profile in case also the further heating element 6’ lying on a respective horizontal plane not intersecting the body of the preforms is to be activated, or, is performed according to a second profile in case also said further heating element 6’ is not to be activated. “Profile” means the distribution trend of the electrical energy in kWh on the identified heating elements 6, 6’ along a direction parallel to the axes of the preforms 5 advancing along the bench.
More in detail, with the transport line configured to advance the preforms with the opening of the neck facing upwards as shown in Figures 2-3a, in case also said further heating element 6’ is to be activated, an optimal and automated distribution of the electrical energy in kWh on the identified heating elements 6, 6’ is determined in the following manner:
A being defined as the electrical energy in kWh, calculated in step f), divided by the number of identified heating elements 6, 6’ in all the plurality of heating modules 2, n being defined as the number of identified heating elements 6, 6’ in each heating module 2, in each heating module 2
- for the upper identified heating element, arranged in position most proximal to the support ring 7 of the advancing preforms, the electrical energy to be supplied is equal to
Ai = A + x*A, where coefficient x varies in a range from 1/9 to 3/4;
- while for the remaining identified heating elements, the electrical energy to be supplied is equal to
Ai = [(A*n)-Ai]/(n-1).
Instead, in case also said further heating element 6’ is not to be activated, an optimal and automated distribution of the electrical energy in kWh on the identified heating elements 6 is determined in the following manner:
A being defined as the electrical energy in kWh, calculated in step f), divided by the number of identified heating elements 6 in all the plurality of heating modules 2, n being defined as the number of identified heating elements 6 in each heating module 2, in each heating module 2
- for the upper identified heating element, arranged in position most proximal to the support ring 7 of the advancing preforms, the electrical energy to be supplied is equal to
Ai = A + x*A, where coefficient x varies in a range from 1/9 to 3/4;
- for the identified heating elements arranged in an intermediate position between said upper identified heating element and the underlying second-last identified heating element 6” (Figure 3a), the electrical energy to be supplied is equal to
Ai = [(A*n)-Ai]/(n-1),
- for said second-last identified heating element 6”, the electrical energy to be supplied is equal to
An-1 = Ai + X*Ai,
- and for the last identified heating element 6”’, or lower identified heating element, arranged in position proximal to the bottom of the advancing preforms, the electrical energy to be supplied is equal to
An-1 — Ai - X*Ai.
Instead, with the transport line configured to advance the preforms with the opening of the neck facing downwards (solution not shown), in case also said further heating element 6’ is to be activated, an optimal and automated distribution of the electrical energy in kWh on the identified heating elements 6, 6’ is determined in the following manner:
A being defined as the electrical energy in kWh, calculated in step f), divided by the number of identified heating elements 6, 6’ in all the plurality of heating modules 2, n being defined as the number of identified heating elements 6, 6’ in each heating module 2, in each heating module 2
- for the lower identified heating element, arranged in position most proximal to the support ring 7 of the advancing preforms, the electrical energy to be supplied is equal to
Ai = A + x*A, where coefficient x varies in a range from 1/9 to 3/4;
- while for the remaining identified heating elements, the electrical energy to be supplied is equal to
Ai = [(A*n)-Ai]/(n-1).
Instead, in case also said further heating element 6’ is not to be activated, an optimal and automated distribution of the electrical energy in kWh on the identified heating elements 6 is determined in the following manner:
A being defined as the electrical energy in kWh, calculated in step f), divided by the number of identified heating elements 6 in all the plurality of heating modules 2, n being defined as the number of identified heating elements 6 in each heating module 2, in each heating module 2
- for the lower identified heating element, arranged in position most proximal to the support ring 7 of the advancing preforms, the electrical energy to be supplied is equal to
Ai = A + x*A, where coefficient x varies in a range from 1/9 to 3/4;
- for the identified heating elements arranged in an intermediate position between said lower identified heating element and the overlying second-last identified heating element 6” (Figure 3a), the electrical energy to be supplied is equal to
Ai = [(A*n)-Ai]/(n-1),
- for said second-last identified heating element 6”, the electrical energy to be supplied is equal to
An-1 = Ai + X*Ai, - and for the last identified heating element 6”’, or upper identified heating element, arranged in position proximal to the bottom of the advancing preforms, the electrical energy to be supplied is equal to An-1 = Ai - X*Ai.
Therefore, with the method according to the invention, quickly determining an optimal distribution of the electrical energy in kWh on the identified heating elements that must be activated in each heating module 2 is also possible in automated manner.
Claims
1 . A method for automatically determining electrical energy in kWh to be supplied to a furnace (1 ) provided with a plurality of heating modules (2) arranged in at least one bench upstream of a stretch-blow molding machine (3) provided with a plurality of molding cavities for molding containers, wherein each heating module (2) is provided with a plurality of heating elements (6) arranged along a plane substantially parallel to the plane containing the axes of the preforms (5) advancing along the bench, the method comprising the following steps a) providing the following parameters as input data:
- hourly productivity (v) of the molding machine, expressed in containers per molding cavity per hour;
- geometrical and weight data of the preform and preform neck;
- geometrical data of the container to be molded;
- number of the heating modules (2);
- number of the heating elements (6) in each heating module (2); b) providing a first range of total stretching ratio; a second range of total stretching ratio comprising greater values than said first range; and a third range of total stretching ratio comprising greater values than said second range; c) providing a first curve y=a*x b, a second curve y=c*x d, and a third curve y=e*x f, wherein y is the specific power or power-to-mass ratio in W/g defining the power that the heating elements (6) have to absorb for each gram of net weight of the preform, wherein said net weight of the preform is equal to the weight of the preform minus the weight of the preform neck, and where x is the net weight of the preform in grams; d) calculating the total stretching ratio by multiplying the axial stretching ratio by the radial stretching ratio; e) extracting the value W/g from the first curve if the total stretching ratio calculated in step d) falls in the first range, from the second curve if said total stretching ratio falls in the second range, or from the third curve if the total stretching ratio falls in the third range; f) calculating the electrical energy in kWh required for said hourly productivity (v).
2. A method according to claim 1 , wherein said first range of total stretching ratio comprises values less than or equal to 8; said second range of total stretching ratio comprises values greater than 8 and less than 13.5; and said third range of total stretching ratio comprises values greater than or equal to 13.5; and wherein coefficient “a” has a value from 0.45 to 0.58; coefficient “b” has a value from -0.25 to -0.35; coefficient “c” has a value from 0.60 to 0.75; coefficient “d” has a value from -0.36 to -0.50; coefficient “e” has a value from 0.75 to 0.86; coefficient “f” has a value from -0.54 to -0.60; preferably wherein the electrical energy in kWh required for said hourly productivity (v) is equal to:
(W/g * net weight of the preform * v * number of molding cavities) / 1000, where W/g is the value extracted in step e).
3. A method according to claim 1 or 2, wherein after step f), the following steps for managing said heating elements (6) are provided: g) identifying the number of heating elements to be activated in each heating module (2), always including all the heating elements (6) lying on a horizontal plane intersecting the body of the advancing preforms, and including the adjacent successive further heating element (6’) lying on a respective horizontal plane not intersecting the body of the preforms only in case, considering the center distance between the last of said heating elements (6) lying on a horizontal plane intersecting the body of the preforms and said successive further heating element (6’) proximal thereto, the height (Y) corresponding to the half-center distance of said center distance intersects the bottom of the preforms; h) activating, in each heating module (2), the heating elements identified in step g) by distributing said electrical energy in kWh on said identified heating elements.
4. A method according to claim 2, wherein coefficient “a” has a value from 0.45 to 0.55; coefficient “b” has a value from -0.27 to -0.35; coefficient “c” has a value from 0.60 to 0.72; coefficient “d” has a value from -0.40 to -0.48; coefficient “e” has a value from 0.78 to 0.86; coefficient “f” has a value from -0.54 to -0.60.
5. A method according to claim 3, wherein in step h), the distribution of the electrical energy in kWh on said identified heating elements is performed according to a first profile in case also said further heating element (6’) lying on a
respective horizontal plane not intersecting the body of the preforms is to be activated, or it is performed according to a second profile in case also said further heating element (6’) is not to be activated.
6. A method according to claim 3 or 5, wherein in case also said further heating element (6’) is to be activated, the distribution of the electrical energy in kWh on said identified heating elements (6, 6’) is determined in the following manner:
A being defined as the electrical energy in kWh divided by the number of identified heating elements (6, 6’) in said plurality of heating modules (2), n being defined as the number of identified heating elements (6, 6’) in each heating module (2), in each heating module (2)
- for the identified heating element most proximal to the support ring (7) of the advancing preforms, the electrical energy to be supplied is equal to
Ai = A + x*A, where coefficient x varies in a range from 1/9 to 3/4;
- for the remaining identified heating elements, the electrical energy to be supplied is equal to
Ai = [(A*n)-Ai]/(n-1).
7. A method according to claim 3 or 5, wherein in case also said further heating element (6’) is not to be activated, the distribution of the electrical energy in kWh on said identified heating elements (6) is determined in the following manner:
A being defined as the electrical energy in kWh divided by the number of identified heating elements (6) in said plurality of heating modules (2), n being defined as the number of identified heating elements (6) in each heating module (2), in each heating module (2)
- for the identified heating element most proximal to the support ring (7) of the advancing preforms, the electrical energy to be supplied is equal to
Ai = A + x*A, where coefficient x varies in a range from 1/9 to 3/4;
- for the identified heating elements arranged in an intermediate position between said identified heating element most proximal to the support ring (7) and the
underlying, or overlying, second-last identified heating element, the electrical energy to be supplied is equal to
Ai = [(A*n)-Ai]/(n-1),
- for said second-last identified heating element, the electrical energy to be supplied is equal to
An-1 = Ai + X*Ai,
- and for the last identified heating element, or lower identified heating element or upper identified heating element, arranged in position proximal to the bottom of the advancing preforms, the electrical energy to be supplied is equal to
An-1 = Ai - X*Ai.
8. A method according to any one of the preceding claims, wherein the axial stretching ratio is calculated with the following ratio
(Hc-hc_n-hc_ur)/(Hp-hp_n-hp_ur), where
Hc = height of the container, hc_n = height of the container neck, hc_ur = height of the container area under neck ring,
Hp = height of the preform, hp_n = height of the preform neck, hp_ur = height of the preform area under neck ring, while the radial stretching ratio is calculated with the following ratio
Dout_max I (dout_ max " tmax ), where
Dout_max = maximum outer diameter of the container, dout_max = maximum outer diameter of the preform, tmax = maximum thickness of the preform.
9. A method according to any one of the preceding claims, wherein the heating elements in each heating module (2) are infrared lamps or NIR lamps or LED lamps or laser lamps.
10. A method according to any one of the preceding claims, wherein said geometrical data of the preform comprise
- height of the preform,
- height of the neck,
- height of the area under neck ring,
- maximum outer diameter,
- maximum thickness; and wherein said geometrical data of the container to be molded comprise
- height of the container, - height of the neck,
- height of the area under neck ring,
- maximum outer diameter.
11. A method according to any one of the preceding claims, wherein said input data further comprise - center distance of the heating elements, preferably equal in each heating module;
- maximum power of the heating elements, preferably equal in each heating module.
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IT102022000018045A IT202200018045A1 (en) | 2022-09-02 | 2022-09-02 | METHOD FOR AUTOMATICALLY DETERMINING THE ELECTRIC ENERGY TO BE SUPPLIED TO A PREFORM HEATING OVEN PLACED UPSTREAM OF A STRETCH-BLOW MOULDING MACHINE |
IT102022000018045 | 2022-09-02 |
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WO2024047603A1 true WO2024047603A1 (en) | 2024-03-07 |
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PCT/IB2023/058668 WO2024047603A1 (en) | 2022-09-02 | 2023-09-01 | Method for automatically determining the electrical energy to be supplied to a furnace for heating preforms, arranged upstream of a stretch-blow molding machine |
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Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4506144A (en) * | 1982-07-19 | 1985-03-19 | Cincinnati Milacron Inc. | Control for radiant heating |
US20060074614A1 (en) * | 2003-01-21 | 2006-04-06 | Chang Long F | Apparatus and method for virtual prototyping of blow molded objects |
US20180178438A1 (en) * | 2016-12-23 | 2018-06-28 | Sidel Participations | Method for parameterization of a station for heating a container production facility |
US20190061225A1 (en) * | 2017-08-24 | 2019-02-28 | Sidel Participations | Facility and method for production of containers, making possible production immediately upon start-up |
-
2022
- 2022-09-02 IT IT102022000018045A patent/IT202200018045A1/en unknown
-
2023
- 2023-09-01 WO PCT/IB2023/058668 patent/WO2024047603A1/en unknown
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4506144A (en) * | 1982-07-19 | 1985-03-19 | Cincinnati Milacron Inc. | Control for radiant heating |
US20060074614A1 (en) * | 2003-01-21 | 2006-04-06 | Chang Long F | Apparatus and method for virtual prototyping of blow molded objects |
US20180178438A1 (en) * | 2016-12-23 | 2018-06-28 | Sidel Participations | Method for parameterization of a station for heating a container production facility |
US20190061225A1 (en) * | 2017-08-24 | 2019-02-28 | Sidel Participations | Facility and method for production of containers, making possible production immediately upon start-up |
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