EP3302846B1 - High speed blow forming process to shape aluminum containers using 3xxx alloys with high recycle content - Google Patents
High speed blow forming process to shape aluminum containers using 3xxx alloys with high recycle content Download PDFInfo
- Publication number
- EP3302846B1 EP3302846B1 EP16728186.4A EP16728186A EP3302846B1 EP 3302846 B1 EP3302846 B1 EP 3302846B1 EP 16728186 A EP16728186 A EP 16728186A EP 3302846 B1 EP3302846 B1 EP 3302846B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- preform
- bottle preform
- forming
- axial load
- mold cavity
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Revoked
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D26/00—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces
- B21D26/02—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure
- B21D26/033—Deforming tubular bodies
- B21D26/049—Deforming bodies having a closed end
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D26/00—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces
- B21D26/02—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure
- B21D26/053—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure characterised by the material of the blanks
Definitions
- This disclosure provides a high-speed blow forming process for shaping aluminium containers using 3xxx can body stock alloys with high recycled content.
- Metal cans are well known and widely used for beverages.
- Conventional beverage can bodies generally have simple upright cylindrical side walls. It is sometimes desired, however, for reasons of aesthetics, consumer appeal and/or product identification, to impart a different and more complex shape to the side wall and/or bottom of a metal beverage container, and in particular, to provide a metal container with the shape of a bottle rather than an ordinary cylindrical can shape.
- a method according to claim 1 provides a solution for rapid production of aluminium containers using metal with a high recycled content.
- the methods described herein provide an efficient, high-speed blow-forming process for shaping aluminium containers using conventional 3xxx can body stock alloys with high recycled content.
- the methods may be carried out on alloys having recycled content as high as 50 wt. % to 100 wt. %.
- a preform is a hollow workpiece typically having an open end opposite a closed end and a generally cylindrical wall.
- a D&I preform is a preform made by a D&I process.
- Preforms used in the methods described herein typically have a diameter of about 63.5 mm (2.5 inches (in)) to about 76.2 mm (3.0 in), a height of about 254.0 mm (10.0 in) to about 317.5 mm (12.5 in), a wall thickness of about 0.1524 mm (0.006 in) to about 0.508 mm (0.020 in), and a dome depth of about 10.16 mm (0.400 in) to about 25.4 mm (1.00 in).
- Preforms used in the methods described herein can be either coated or uncoated depending on the application.
- a conventional can coating system can be applied on the preforms.
- a conventional can coating system comprises inside spray, ink and over-varnish.
- This disclosure provides methods for aluminium forming at temperatures ranging from ambient temperature (i.e., between about 18 °C - about 25 °C) up to about 300 °C and provides methods for preform expansion to a diameter up to 40% larger than the original preform diameter.
- This disclosure provides methods for a low-pressure forming operation that operates up to 420 psi ( ⁇ 30 bars), with the use of a single segment split mold.
- the methods disclosed herein are commercially valuable because they use blow-forming to expand preforms made by a D&I process.
- the D&I process is more efficient than the alternative impact extrusion (IE) process.
- the D&I process is capable of running at a considerably higher production speed than the IE process, which makes the D&I process an economical option for a high-speed, large-volume production plant.
- the D&I process can be carried out on alloys having a high recycled content.
- the IE process requires the use of high-purity 1xxx series aluminium alloys, which are not recycle friendly.
- the disclosed methods are advantageous over conventional methods, at least because in those conventional methods aluminium bottles are manufactured by the impact extrusion (IE) process.
- blow-forming methods described herein use high pressure gas to expand an aluminium preform to fit a negative mold.
- the disclosed methods also could be applied to a product line employing hydroforming, which uses a liquid in place of the gas used in blow forming.
- a process for shaping aluminium containers includes the sequential steps of blanking out a disk from a sheet of a 3xxx series aluminium alloy; forming a bottle preform by drawing, redrawing, ironing, and doming the cup; placing the preform into a mold cavity; applying an axial load to the preform; and injecting an inert gas into the interior of the preform with sufficient pressure until the preform expands to fill the mold cavity.
- the sheet has a thickness in the range of about 0.381 mm (0.0150 in) to about 0.635 mm (0.0250 in).
- the disk has a diameter in the range of about 152.4 mm (6.0 in) to about 241.3 mm (9.5 in).
- the preform is heated to a forming temperature prior to injecting the inert gas.
- the forming temperature is about 200 °C to about 300 °C. In some cases, the forming temperature is about 250 °C to about 255 °C, or nominally 250 °C.
- the heating may be carried out while the preform is under the axial load. That is, the heating may be carried out while the axial load is applied. The axial load prevents the preform from expanding in the axial direction, but the axial load does not compress (i.e., reduce the length of) the preform.
- the inert gas is injected after a preset axial load is reached.
- the preset axial load is in the range of about 488.243 to 1220.61 kg/m 2 (100 to 250 lb/ft 2 ).
- the axial load decreases, so the injected gas applies pressure to the preform at a controlled rate.
- the preform may be annealed before it is placed in a mold cavity.
- the annealing temperature is from about 100 °C to about 400 °C. In some cases, the annealing temperature is from about 300 °C to about 400 °C.
- aluminium bottles made by any method disclosed herein.
- the methods described herein provide shaped aluminium bottles from conventional 3xxx can body stock alloys with up to 100% recycled content.
- the methods include manufacturing a preform having a wall, a closed end, and an open end by a D&I process and expanding the preform into a shaped container by high-speed blow forming.
- a disk is blanked out of an aluminium sheet.
- the blank may be formed by any method known in the art, such as by punching or cutting.
- an outer cutting tool cuts a 3xxx series aluminium sheet having a thickness ranging from about 0.381 mm (0.0150 in) to about 0.635 mm (0.0250 in) (e.g., 0.381 mm (0.0150 in) to 0.508 mm (0.0200 in), 0.4572 mm (0.0180 in) to 0.508 mm (0.0200 in), 0.4572 mm (0.0180 in) to 0.635 mm (0.0250 in), or 0.508 to 0.635 mm (0.0200 to 0.0250 in)), into a disk, and the disk is immediately drawn into a cup.
- the disk may be drawn into a cup with an inner cup forming tool.
- the cutting and drawing is carried out by a double action press, where the first action performs disk cutting and the second action performs cup forming in a continuous motion.
- the cut-out disk may have a diameter ranging from about 152.4 mm (6.0 in) to about 254.0 mm (10.0 in) (e.g., 152.4 mm (6.0 in), 157.48 mm (6.2 in), 165.1 mm (6.5 in), 170.18 mm (6.7 in), 177.8 mm (7.0 in), 182.88 mm (7.2 in), 190.5 mm (7.5 in), 195.58 mm (7.7 in), 203.2 mm (8.0 in), 208.28 mm (8.2 in), 215.9 mm (8.5 in), 220.98 mm (8.7 in), 228.6 mm (9.0 in), 233.68 mm (9.2 in), 241.3 mm (9.5 in), 246.38 mm (9
- the formed cup has a fairly large diameter that requires further operation to reduce its size to a smaller diameter to facilitate subsequent operations. This is accomplished by a redraw process.
- a suitable redraw process for the methods described herein includes, for example, the direct redraw process wherein the cup is drawn from inside of the cup base by using similar cup forming tools to reduce its diameter and displace the material to form a taller cup wall.
- Another suitable redraw process for use in the methods described herein is the reverse redraw process wherein the cup is drawn from the bottom of the cup and metal is folded in an opposite direction to form the taller cup wall.
- the methods disclosed herein may include either of these preform redraw processes, but are not limited to these redraw processes. Depending on machine requirements, limitations, and process requirements, there may be multiple redraw processes or combinations of redraw processes.
- an ironing tool will stretch and thin the cup wall to achieve the final preform wall thickness and length.
- a doming operation is performed wherein the bottom of the preform, i.e., the dome profile, is formed.
- the final preform may have a diameter ranging from about 50.8 mm (2.0 in) to about 88.9 mm (3.5 in) (e.g., 50.8 mm (2.0 in) to 76.2 mm (3.0 in), or 63.5 mm (2.5 in) to 88.9 mm (3.5 in)) and may be as tall as about 254.0 mm (10.0 in) to about 317.5 mm (12.5 in) (e.g., 254.0 mm (10.0 in), 266.7 mm (10.5 in), 279.4 mm (11.0 in), 292.1 mm (11.5 in), 304.8 mm (12.0 in), or 317.5 mm (12.5 in)).
- the preform wall has a thickness ranging from about 0.1524 mm (0.006 in) to about 0.508 mm (0.020 in) (e.g., 0.1524 mm (0.006 in), 0.1778 mm (0.007 in), 0.2032 mm (0.008 in), 0.2286 mm (0.009 in), 0.254 mm (0.010 in), 0.3048 mm (0.012 in), 0.3556 mm (0.014 in), 0.4064 mm (0.016 in), 0.4572 mm (0.018 in), or 0.508 mm (0.020 in)).
- 0.1524 mm (0.006 in) e.g., 0.1524 mm (0.006 in), 0.1778 mm (0.007 in), 0.2032 mm (0.008 in), 0.2286 mm (0.009 in), 0.254 mm (0.010 in), 0.3048 mm (0.012 in), 0.3556 mm (0.014 in), 0.4064 mm (0.016 in), 0.4572 mm (0.018 in), or 0.508
- the preform may have a constant wall thickness of about 0.254 mm (0.010 in) to about 0.508 mm (0.020 in) (e.g., 0.3048 mm (0.012 in), 0.3556 mm (0.014 in), 0.4064 mm (0.016 in), or 0.4572 mm (0.018 in)).
- the bottle preform may have a variable wall thickness with a thicker portion at the top of about 0.254 mm (0.010 in) to about 0.508 mm (0.020 in) (e.g., 0.254 mm (0.010 in), 0.3048 mm (0.012 in), 0.3556 mm (0.014 in), 0.4064 mm (0.016 in), 0.4572 mm (0.018 in), or 0.508 mm (0.020 in)) and a thinner portion in the middle of about 0.1524 mm (0.006 in) to about 0.3048 mm (0.012 in) (e.g., 0.1524 mm (0.006 in), 0.1778 mm (0.007 in), 0.2032 mm (0.008 in), 0.2286 mm (0.009 in), 0.254 mm (0.010 in), or 0.3048 mm (0.012 in)).
- a thinner portion in the middle of about 0.1524 mm (0.006 in) to about 0.3048 mm (0.012 in) e.g., 0.1524
- the preform dome has a depth from about 10.16 mm (0.400 in) to about 25.4 mm (1.00 in) (e.g., 10.16 mm (0.400 in), 12.7 mm (0.500 in), 15.24 mm (0.600 in), 17.78 mm (0.700 in), 20.32 mm (0.800 in), 22.86 mm (0.900 in), or 25.4 mm (1.00 in)).
- the preform may be subjected to an optional annealing operation with a temperature ranging from about 100 °C to about 400 °C (e.g., 100 °C - 300 °C, 100 °C - 200 °C, 200 °C - 400 °C, 200 °C - 300 °C, or 300 °C - 400 °C for a duration ranging from about 1 minute to about 3 hours (e.g., 1 minute - 1 hour, 1 minute - 30 minutes, 5 minutes - 20 minutes, 1 hour - 3 hours, 2 hours - 3 hours, or 1 hour - 2 hours).
- the annealing process may be performed to improve metal formability.
- the annealing process may have a duration ranging from about 1 hour to about 3 hours. In other cases, the annealing process may range from about 1 minute up to about 30 minutes.
- the annealing operation may be added during aluminium sheet production or during one or more preform production steps.
- the annealing process may be applied locally to a specific portion of the preform. For example, the annealing process may be applied to the neck portion of the bottle, to the body portion of the bottle, to the base portion of the bottle, or any combination thereof.
- the annealing process may also be applied to selective portions of the aluminium sheet before it is processed into a preform. Consequently, a gradient of mechanical properties is induced along the height of the sidewall of the preforms.
- the annealing step may be applied as an intermediate step in the necking and shaping progression operations.
- the methods provide high-speed blow forming processes for shaping D&I preforms of conventional 3xxx can body stock alloys with high recycled content.
- the recycled content may be present in an amount of up to 100 wt. % of the alloy. In some cases, the recycled content may be present from 50 wt. % to 100 wt. % of the alloy (e.g., 50 wt. %, 55 wt. %, 60 wt. %, 65 wt. %, 70 wt. %, 75 wt. %, 80 wt. %, 85 wt. %, 90 wt. %, 95 wt. %, or 100 wt. %).
- standard AA3104 can body stock alloys are used.
- Other non-limiting alloys that may be used in the methods disclosed herein are AA3003, AA3004, AA3105, and AA3204.
- a preform optionally is annealed in a box furnace prior to blow-forming. After optional annealing, the preform is placed in a mold cavity for blow forming.
- the mold cavity typically has a long axis.
- the preform also has a long axis and is disposed substantially coaxially within the mold cavity.
- the mold cavity is part of a split mold, i.e., a mold made up of two or more mating segments around the periphery of the mold cavity, separable for removal of the formed container. With a split mold, the defined shape may be asymmetric about the long axis of the cavity.
- a high-speed blow forming process uses an ambient or heated mold cavity.
- a controlled temperature gradient may be used, such that the temperature of the mold cavity varies about 5 °C to 10 °C (e.g., 5 °C, 6 °C, 7 °C, 8 °C, 9 °C, or 10 °C) from the top to the bottom of the perform.
- the top and bottom of the mold cavity are heated to temperatures from about 200 °C to 300 °C (e.g., 200 °C, 220 °C, 240 °C, 260 °C, 280 °C, or 300 °C), with the bottom being 5 °C to 10 °C higher than the top.
- a mold apparatus includes a split mold having two halves (left and right), a backing ram (bottom), and a preform seal (top).
- the backing ram and preform seal may also be heated.
- the backing ram is generally heated to a temperature from about 215 °C to about 335 °C (215 °C, 225 °C, 235 °C, 245 °C, 255 °C, 265 °C, 275 °C, 285 °C, 295 °C, 305 °C, 315 °C, 325 °C, or 335 °C), and the preform seal is generally heated to a temperature similar to the upper portion of the mold cavity, for example, to about 180 °C to 320 °C (e.g., 180 °C, 200 °C, 220 °C, 240 °C, 260 °C, 280 °C, 300 °
- Figure 2 is a schematic of a blow-forming process.
- a mold cavity 210, a backing ram 220, and a preform seal 230 enclose a preform 240 as shown in Fig. 2 , panel A.
- the backing ram 220 places an axial load indicated by arrow 250 on the preform 240 while the preform 240 is heated to its forming temperature, as shown in Fig. 2 , panel B.
- the axial load typically is in the range of 488.243 kg/m 2 (100 lb/ft 2 ) to 1220.61 kg/m 2 (250 lb/ft 2 ) (e.g., 488.243 kg/m 2 (100 lb/ft 2 ), 610.303 kg/m 2 (125 lb/ft 2 ), 732.364 kg/m 2 (150 lb/ft 2 ), 854.425 kg/m 2 (175 lb/ft 2 ), 976.486 kg/m 2 (200 lb/ft 2 ), 1098.55 kg/m 2 (225 lb/ft 2 ), or 1220.61 kg/m 2 (250 lb/ft 2 )).
- the displacement of the backing ram 220 is about 0 mm (0 in) to about 1.27 mm (0.050 in) (e.g., 0.635 mm (0.025 in) - 1.27 mm (0.05 in)).
- the backing ram 220 is essentially stationary once in place in contact with the preform dome and during the molding process.
- the preform 240 is pressurized with an inert gas 260, such as nitrogen, until the preform 240 expands to completely fill the mold cavity 210, as shown in Fig. 2 , panels C and D.
- the blowing pressure is applied to the preform at a controlled rate. As the preform 240 expands, the axial load decreases.
- the upper portion of the mold cavity is heated to 250 °C and the bottom portion of the mold cavity is heated to 255 °C.
- the seal is heated to 250 °C and the backing ram is heated to 275 °C.
- the four parts i.e., the two halves of the mold, the backing ram, and the seal
- An axial load of about 297.683 kg/m (200 lb/foot) is placed on the preform while the preform is heated to its forming temperature. Once the forming temperature is reached, the preform is pressurized with nitrogen until the mold cavity is filled.
- a blow forming method may be carried out at ambient temperatures, i.e., without heating the mold apparatus.
- ambient temperature conditions for example 23 °C
- the preform is immediately pressurized with an inert gas once the preset axial load is reached.
- the pressurization rate is approximately 1 second and the pressure is held until the blow formed preform completely fills the mold cavity.
- the split mold expansions increase in diameter up to 40% larger than the original diameter (e.g., 15 %, 20%, 25%, 30%, 35%, or 40%).
- the forming temperature ranges from ambient temperature, for example about 23 °C, to about 300 °C (e.g., 23 °C - 100 °C, 23 °C - 200 °C, 100 °C - 300 °C, or 200 °C - 300 °C).
- Figure 3 is a graph showing change in forming parameters over time as a D&I preform was expanded to a straight wall mold in a high-speed blow forming process.
- the fully formed bottle had a 40% expansion (to 2.933 in final diameter).
- This bottle was formed at a nominal temperature of 250 °C with a 5 °C temperature gradient from the top to the bottom of the preform, i.e., the temperature at the top of the preform was 250 °C and the temperature at the bottom of the preform was 255 °C.
- the entire forming process for making the straight wall container took approximately 5 seconds.
- the shaped aluminium containers described herein may be used for beverages including, but not limited to, soft drinks, water, beer, wine, energy drinks, and other beverages.
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Containers Having Bodies Formed In One Piece (AREA)
- Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)
Description
- This application claims the benefit of
.U.S. Provisional Patent Application No. 62/166,212, filed May 26, 2015 - This disclosure provides a high-speed blow forming process for shaping aluminium containers using 3xxx can body stock alloys with high recycled content.
- Metal cans are well known and widely used for beverages. Conventional beverage can bodies generally have simple upright cylindrical side walls. It is sometimes desired, however, for reasons of aesthetics, consumer appeal and/or product identification, to impart a different and more complex shape to the side wall and/or bottom of a metal beverage container, and in particular, to provide a metal container with the shape of a bottle rather than an ordinary cylindrical can shape.
- Methods of pressure forming metal containers from preforms are known in the art as described, for example, in
U.S. Patent No. 8,683,837 , which discloses a process for shaping aluminium containers comprising the sequential steps of: placing a bottle preform into a mold cavity; injecting gas into the preform to expand the preform into the mold; and applying an axial load to the bottle preform using a backing ram. A further similar process is disclosed byUS 3 896 648 A . There is a demand, however, for rapid production of aluminium containers using metal with a high recycled content. - A method according to claim 1 provides a solution for rapid production of aluminium containers using metal with a high recycled content.
- The methods described herein provide an efficient, high-speed blow-forming process for shaping aluminium containers using conventional 3xxx can body stock alloys with high recycled content. For example, the methods may be carried out on alloys having recycled content as high as 50 wt. % to 100 wt. %.
- This disclosure provides methods for high-temperature and low-temperature 3xxx series aluminium blow forming of fully or partially annealed aluminium alloy draw-and-iron (D&I) preforms. A preform is a hollow workpiece typically having an open end opposite a closed end and a generally cylindrical wall. A D&I preform is a preform made by a D&I process.
- Preforms used in the methods described herein typically have a diameter of about 63.5 mm (2.5 inches (in)) to about 76.2 mm (3.0 in), a height of about 254.0 mm (10.0 in) to about 317.5 mm (12.5 in), a wall thickness of about 0.1524 mm (0.006 in) to about 0.508 mm (0.020 in), and a dome depth of about 10.16 mm (0.400 in) to about 25.4 mm (1.00 in).
- Preforms used in the methods described herein can be either coated or uncoated depending on the application. For example, a conventional can coating system can be applied on the preforms. A conventional can coating system comprises inside spray, ink and over-varnish.
- This disclosure provides methods for aluminium forming at temperatures ranging from ambient temperature (i.e., between about 18 °C - about 25 °C) up to about 300 °C and provides methods for preform expansion to a diameter up to 40% larger than the original preform diameter. This disclosure provides methods for a low-pressure forming operation that operates up to 420 psi (≈30 bars), with the use of a single segment split mold.
- The methods disclosed herein are commercially valuable because they use blow-forming to expand preforms made by a D&I process. The D&I process is more efficient than the alternative impact extrusion (IE) process. The D&I process is capable of running at a considerably higher production speed than the IE process, which makes the D&I process an economical option for a high-speed, large-volume production plant. Moreover, the D&I process can be carried out on alloys having a high recycled content. Because of the large amount of deformation required, the IE process requires the use of high-purity 1xxx series aluminium alloys, which are not recycle friendly. Thus, the disclosed methods are advantageous over conventional methods, at least because in those conventional methods aluminium bottles are manufactured by the impact extrusion (IE) process.
- The blow-forming methods described herein use high pressure gas to expand an aluminium preform to fit a negative mold. The disclosed methods also could be applied to a product line employing hydroforming, which uses a liquid in place of the gas used in blow forming.
- In some examples, a process for shaping aluminium containers includes the sequential steps of blanking out a disk from a sheet of a 3xxx series aluminium alloy; forming a bottle preform by drawing, redrawing, ironing, and doming the cup; placing the preform into a mold cavity; applying an axial load to the preform; and injecting an inert gas into the interior of the preform with sufficient pressure until the preform expands to fill the mold cavity. Optionally, the sheet has a thickness in the range of about 0.381 mm (0.0150 in) to about 0.635 mm (0.0250 in). Optionally, the disk has a diameter in the range of about 152.4 mm (6.0 in) to about 241.3 mm (9.5 in).
- In some examples, the preform is heated to a forming temperature prior to injecting the inert gas. In some cases, the forming temperature is about 200 °C to about 300 °C. In some cases, the forming temperature is about 250 °C to about 255 °C, or nominally 250 °C. When the process includes heating the preform to a forming temperature, the heating may be carried out while the preform is under the axial load. That is, the heating may be carried out while the axial load is applied. The axial load prevents the preform from expanding in the axial direction, but the axial load does not compress (i.e., reduce the length of) the preform.
- The inert gas is injected after a preset axial load is reached. In some examples, the preset axial load is in the range of about 488.243 to 1220.61 kg/m2 (100 to 250 lb/ft2). As the preform expands, the axial load decreases, so the injected gas applies pressure to the preform at a controlled rate.
- In some examples, the preform may be annealed before it is placed in a mold cavity. In some cases, the annealing temperature is from about 100 °C to about 400 °C. In some cases, the annealing temperature is from about 300 °C to about 400 °C.
- Also included within the scope of this disclosure are aluminium bottles made by any method disclosed herein.
- The flexibility of the methods disclosed herein allows for production of elaborate designs in the aluminium bottle market, which would be difficult with other aluminium forming methods, for example mechanical shaping.
-
-
Figure 1 is an illustration of a mold cavity according to the methods described herein. -
Figure 2 is a schematic of a blow forming process according to the methods described herein. -
Figure 3 is a graph of the forming parameters of a D&I preform upon expansion to fill a mold during a high-speed blow-forming process. - The methods described herein provide shaped aluminium bottles from conventional 3xxx can body stock alloys with up to 100% recycled content. In some cases, the methods include manufacturing a preform having a wall, a closed end, and an open end by a D&I process and expanding the preform into a shaped container by high-speed blow forming.
- By way of example, but not limitation, a disk is blanked out of an aluminium sheet. The blank may be formed by any method known in the art, such as by punching or cutting. In one embodiment an outer cutting tool cuts a 3xxx series aluminium sheet having a thickness ranging from about 0.381 mm (0.0150 in) to about 0.635 mm (0.0250 in) (e.g., 0.381 mm (0.0150 in) to 0.508 mm (0.0200 in), 0.4572 mm (0.0180 in) to 0.508 mm (0.0200 in), 0.4572 mm (0.0180 in) to 0.635 mm (0.0250 in), or 0.508 to 0.635 mm (0.0200 to 0.0250 in)), into a disk, and the disk is immediately drawn into a cup. The disk may be drawn into a cup with an inner cup forming tool. The cutting and drawing is carried out by a double action press, where the first action performs disk cutting and the second action performs cup forming in a continuous motion. To provide sufficient material for aluminium bottles, including large format aluminium bottles, the cut-out disk may have a diameter ranging from about 152.4 mm (6.0 in) to about 254.0 mm (10.0 in) (e.g., 152.4 mm (6.0 in), 157.48 mm (6.2 in), 165.1 mm (6.5 in), 170.18 mm (6.7 in), 177.8 mm (7.0 in), 182.88 mm (7.2 in), 190.5 mm (7.5 in), 195.58 mm (7.7 in), 203.2 mm (8.0 in), 208.28 mm (8.2 in), 215.9 mm (8.5 in), 220.98 mm (8.7 in), 228.6 mm (9.0 in), 233.68 mm (9.2 in), 241.3 mm (9.5 in), 246.38 mm (9.7 in), or 254.0 mm (10.0 in).)
- The formed cup has a fairly large diameter that requires further operation to reduce its size to a smaller diameter to facilitate subsequent operations. This is accomplished by a redraw process. A suitable redraw process for the methods described herein includes, for example, the direct redraw process wherein the cup is drawn from inside of the cup base by using similar cup forming tools to reduce its diameter and displace the material to form a taller cup wall. Another suitable redraw process for use in the methods described herein is the reverse redraw process wherein the cup is drawn from the bottom of the cup and metal is folded in an opposite direction to form the taller cup wall. The methods disclosed herein may include either of these preform redraw processes, but are not limited to these redraw processes. Depending on machine requirements, limitations, and process requirements, there may be multiple redraw processes or combinations of redraw processes.
- Once the cup is drawn to a final bottle preform diameter, an ironing tool will stretch and thin the cup wall to achieve the final preform wall thickness and length. At the end of the D&I process, a doming operation is performed wherein the bottom of the preform, i.e., the dome profile, is formed. For use in the blow forming process described herein, the final preform may have a diameter ranging from about 50.8 mm (2.0 in) to about 88.9 mm (3.5 in) (e.g., 50.8 mm (2.0 in) to 76.2 mm (3.0 in), or 63.5 mm (2.5 in) to 88.9 mm (3.5 in)) and may be as tall as about 254.0 mm (10.0 in) to about 317.5 mm (12.5 in) (e.g., 254.0 mm (10.0 in), 266.7 mm (10.5 in), 279.4 mm (11.0 in), 292.1 mm (11.5 in), 304.8 mm (12.0 in), or 317.5 mm (12.5 in)). The preform wall has a thickness ranging from about 0.1524 mm (0.006 in) to about 0.508 mm (0.020 in) (e.g., 0.1524 mm (0.006 in), 0.1778 mm (0.007 in), 0.2032 mm (0.008 in), 0.2286 mm (0.009 in), 0.254 mm (0.010 in), 0.3048 mm (0.012 in), 0.3556 mm (0.014 in), 0.4064 mm (0.016 in), 0.4572 mm (0.018 in), or 0.508 mm (0.020 in)). In some cases, the preform may have a constant wall thickness of about 0.254 mm (0.010 in) to about 0.508 mm (0.020 in) (e.g., 0.3048 mm (0.012 in), 0.3556 mm (0.014 in), 0.4064 mm (0.016 in), or 0.4572 mm (0.018 in)). In other cases, the bottle preform may have a variable wall thickness with a thicker portion at the top of about 0.254 mm (0.010 in) to about 0.508 mm (0.020 in) (e.g., 0.254 mm (0.010 in), 0.3048 mm (0.012 in), 0.3556 mm (0.014 in), 0.4064 mm (0.016 in), 0.4572 mm (0.018 in), or 0.508 mm (0.020 in)) and a thinner portion in the middle of about 0.1524 mm (0.006 in) to about 0.3048 mm (0.012 in) (e.g., 0.1524 mm (0.006 in), 0.1778 mm (0.007 in), 0.2032 mm (0.008 in), 0.2286 mm (0.009 in), 0.254 mm (0.010 in), or 0.3048 mm (0.012 in)). The preform dome has a depth from about 10.16 mm (0.400 in) to about 25.4 mm (1.00 in) (e.g., 10.16 mm (0.400 in), 12.7 mm (0.500 in), 15.24 mm (0.600 in), 17.78 mm (0.700 in), 20.32 mm (0.800 in), 22.86 mm (0.900 in), or 25.4 mm (1.00 in)).
- During the preform forming process, the preform may be subjected to an optional annealing operation with a temperature ranging from about 100 °C to about 400 °C (e.g., 100 °C - 300 °C, 100 °C - 200 °C, 200 °C - 400 °C, 200 °C - 300 °C, or 300 °C - 400 °C for a duration ranging from about 1 minute to about 3 hours (e.g., 1 minute - 1 hour, 1 minute - 30 minutes, 5 minutes - 20 minutes, 1 hour - 3 hours, 2 hours - 3 hours, or 1 hour - 2 hours). The annealing process may be performed to improve metal formability. In certain cases, the annealing process may have a duration ranging from about 1 hour to about 3 hours. In other cases, the annealing process may range from about 1 minute up to about 30 minutes. The annealing operation may be added during aluminium sheet production or during one or more preform production steps. The annealing process may be applied locally to a specific portion of the preform. For example, the annealing process may be applied to the neck portion of the bottle, to the body portion of the bottle, to the base portion of the bottle, or any combination thereof. The annealing process may also be applied to selective portions of the aluminium sheet before it is processed into a preform. Consequently, a gradient of mechanical properties is induced along the height of the sidewall of the preforms. Alternatively, the annealing step may be applied as an intermediate step in the necking and shaping progression operations.
- In some examples, the methods provide high-speed blow forming processes for shaping D&I preforms of conventional 3xxx can body stock alloys with high recycled content. The recycled content may be present in an amount of up to 100 wt. % of the alloy. In some cases, the recycled content may be present from 50 wt. % to 100 wt. % of the alloy (e.g., 50 wt. %, 55 wt. %, 60 wt. %, 65 wt. %, 70 wt. %, 75 wt. %, 80 wt. %, 85 wt. %, 90 wt. %, 95 wt. %, or 100 wt. %).
- In one example, standard AA3104 can body stock alloys are used. Other non-limiting alloys that may be used in the methods disclosed herein are AA3003, AA3004, AA3105, and AA3204.
- In one non-limiting example, a preform optionally is annealed in a box furnace prior to blow-forming. After optional annealing, the preform is placed in a mold cavity for blow forming. The mold cavity typically has a long axis. The preform also has a long axis and is disposed substantially coaxially within the mold cavity. Optionally, the mold cavity is part of a split mold, i.e., a mold made up of two or more mating segments around the periphery of the mold cavity, separable for removal of the formed container. With a split mold, the defined shape may be asymmetric about the long axis of the cavity.
- In one example, a high-speed blow forming process uses an ambient or heated mold cavity. In the case of the heated mold cavity, a controlled temperature gradient may be used, such that the temperature of the mold cavity varies about 5 °C to 10 °C (e.g., 5 °C, 6 °C, 7 °C, 8 °C, 9 °C, or 10 °C) from the top to the bottom of the perform. In practice, the top and bottom of the mold cavity are heated to temperatures from about 200 °C to 300 °C (e.g., 200 °C, 220 °C, 240 °C, 260 °C, 280 °C, or 300 °C), with the bottom being 5 °C to 10 °C higher than the top. In some examples, a mold apparatus includes a split mold having two halves (left and right), a backing ram (bottom), and a preform seal (top). In addition to the mold cavity being heated, the backing ram and preform seal may also be heated. When the backing ram and seal are heated, the backing ram is generally heated to a temperature from about 215 °C to about 335 °C (215 °C, 225 °C, 235 °C, 245 °C, 255 °C, 265 °C, 275 °C, 285 °C, 295 °C, 305 °C, 315 °C, 325 °C, or 335 °C), and the preform seal is generally heated to a temperature similar to the upper portion of the mold cavity, for example, to about 180 °C to 320 °C (e.g., 180 °C, 200 °C, 220 °C, 240 °C, 260 °C, 280 °C, 300 °C, or 320 °C).
Figure 1 is a schematic of a mold cavity showing one half of asplit mold 110 and abacking ram 120. -
Figure 2 is a schematic of a blow-forming process. During a blow-forming process, amold cavity 210, abacking ram 220, and apreform seal 230 enclose apreform 240 as shown inFig. 2 , panel A. Thebacking ram 220 places an axial load indicated byarrow 250 on thepreform 240 while thepreform 240 is heated to its forming temperature, as shown inFig. 2 , panel B. The axial load typically is in the range of 488.243 kg/m2 (100 lb/ft2) to 1220.61 kg/m2 (250 lb/ft2) (e.g., 488.243 kg/m2 (100 lb/ft2), 610.303 kg/m2 (125 lb/ft2), 732.364 kg/m2 (150 lb/ft2), 854.425 kg/m2 (175 lb/ft2), 976.486 kg/m2 (200 lb/ft2), 1098.55 kg/m2 (225 lb/ft2), or 1220.61 kg/m2 (250 lb/ft2)). Although thebacking ram 220 exerts a load on thepreform 240, there is no significant compression, or reduction in length, of the preform. The displacement of thebacking ram 220 is about 0 mm (0 in) to about 1.27 mm (0.050 in) (e.g., 0.635 mm (0.025 in) - 1.27 mm (0.05 in)). Thebacking ram 220 is essentially stationary once in place in contact with the preform dome and during the molding process. - Once the forming temperature is reached, the
preform 240 is pressurized with aninert gas 260, such as nitrogen, until thepreform 240 expands to completely fill themold cavity 210, as shown inFig. 2 , panels C and D. The blowing pressure is applied to the preform at a controlled rate. As thepreform 240 expands, the axial load decreases. - In one non-limiting example, for a preform nominal temperature of 250 °C, the upper portion of the mold cavity is heated to 250 °C and the bottom portion of the mold cavity is heated to 255 °C. The seal is heated to 250 °C and the backing ram is heated to 275 °C. During the forming process, the four parts (i.e., the two halves of the mold, the backing ram, and the seal) enclose the preform. An axial load of about 297.683 kg/m (200 lb/foot) is placed on the preform while the preform is heated to its forming temperature. Once the forming temperature is reached, the preform is pressurized with nitrogen until the mold cavity is filled.
- Optionally, a blow forming method may be carried out at ambient temperatures, i.e., without heating the mold apparatus. When forming under ambient temperature conditions, for example 23 °C, the preform is immediately pressurized with an inert gas once the preset axial load is reached. The pressurization rate is approximately 1 second and the pressure is held until the blow formed preform completely fills the mold cavity.
- The split mold expansions increase in diameter up to 40% larger than the original diameter (e.g., 15 %, 20%, 25%, 30%, 35%, or 40%). The forming temperature ranges from ambient temperature, for example about 23 °C, to about 300 °C (e.g., 23 °C - 100 °C, 23 °C - 200 °C, 100 °C - 300 °C, or 200 °C - 300 °C).
-
Figure 3 is a graph showing change in forming parameters over time as a D&I preform was expanded to a straight wall mold in a high-speed blow forming process. The fully formed bottle had a 40% expansion (to 2.933 in final diameter). This bottle was formed at a nominal temperature of 250 °C with a 5 °C temperature gradient from the top to the bottom of the preform, i.e., the temperature at the top of the preform was 250 °C and the temperature at the bottom of the preform was 255 °C. As shown inFigure 3 , the entire forming process for making the straight wall container took approximately 5 seconds. - The shaped aluminium containers described herein may be used for beverages including, but not limited to, soft drinks, water, beer, wine, energy drinks, and other beverages.
Claims (13)
- A process for shaping aluminium containers comprising the sequential steps of:blanking out a disk from a sheet of a 3xxx series aluminium alloy;forming a bottle preform (240) by drawing, redrawing, ironing, and doming the disk;placing the bottle preform (240) into a mold cavity (110; 210);applying an axial load (250) to the bottle preform (240) using a backing ram (120; 220), wherein application of the axial load (250) does not reduce the length of the preform (240), and wherein the backing ram (120; 220) is held essentially stationary while applying the axial load (250), undergoing a displacement of between about 0 mm (0 inches) and about 1.27 mm (0.05 inches); andinjecting an inert gas (260) into an interior of the bottle preform (240) with pressure until the bottle preform (240) expands to fill the mold cavity (110; 210).
- The process of claim 1, wherein the sheet has a thickness ranging from about 0.381 mm (0.0150 in) to about 0.635 mm (0.0250 in), preferably from about 0.4572 mm (0.0180 in) to about 0.635 mm (0.025 in), more preferably from about 0.508 mm (0.0200 in) to about 0.635 mm (0.025 in).
- The process of claim 1 or claim 2, wherein the disk has a diameter ranging from about 152.4 mm (6.0 in) to about 254.0 mm (10.00 in), preferably from about 152.4 mm (6.0 in) to about 177.8 mm (7.0 in) or from about 203.2 mm (8.0 in) to about 241.3 mm (9.50 in).
- The process of any of claims 1-3, further comprising heating the bottle preform (240) to a forming temperature prior to injecting the inert gas (260).
- The process of claim 4, wherein the forming temperature is from about 200 °C to about 300 °C, preferably from about 250 °C to about 255 °C.
- The process of claim 4, wherein the bottle preform (240) has a top and a bottom, wherein the forming temperature comprises a temperature gradient from the top to the bottom of the preform (240), and wherein the forming temperature at the bottom of the preform (240) is from 5 °C to 10 °C higher than the forming temperature at the top of the preform (240).
- The process of any of claims 4-6, wherein the heating is carried out while the axial load (250) is applied.
- The process of any of claims 1-7, wherein the inert gas (260) is injected after a preset axial load (250) is reached.
- The process of any of claims 1-8, wherein the 3xxx alloy is selected from the group consisting of AA3104, AA3003, AA3004, and AA3105.
- The process of any of claims 1-9, wherein the 3xxx alloy includes at least 50 wt. % recycled material.
- The process of any of claims 1-10, further comprising fully or partially annealing the bottle preform (240) prior to placing the bottle preform (240) in the mold cavity (110; 210).
- The process of claim 11, wherein the annealing temperature is from about 100 °C to about 400 °C, preferably from about 300 °C to about 400 °C.
- The process of any of claims 1-12, wherein the bottle preform (240) has:a diameter of about 63.5 mm (2.5 in) to about 76.2 mm (3.0 in);a height of about 254.0 mm (10.0 in) to about 317.5 mm (12.5 in);a wall thickness of about 0.1524 mm (0.006 in) to about 0.508 mm (0.020 in); anda depth of dome from about 10.16 mm (0.400 in) to about 25.4 mm (1.00 in).
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US201562166212P | 2015-05-26 | 2015-05-26 | |
| PCT/US2016/034214 WO2016191513A1 (en) | 2015-05-26 | 2016-05-26 | High speed blow forming process to shape aluminum containers using 3xxx alloys with high recycle content |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP3302846A1 EP3302846A1 (en) | 2018-04-11 |
| EP3302846B1 true EP3302846B1 (en) | 2020-02-12 |
Family
ID=56116573
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP16728186.4A Revoked EP3302846B1 (en) | 2015-05-26 | 2016-05-26 | High speed blow forming process to shape aluminum containers using 3xxx alloys with high recycle content |
Country Status (10)
| Country | Link |
|---|---|
| US (1) | US20180126440A1 (en) |
| EP (1) | EP3302846B1 (en) |
| JP (1) | JP6534494B2 (en) |
| KR (1) | KR102028816B1 (en) |
| AU (1) | AU2016267097B2 (en) |
| BR (1) | BR112017023293A2 (en) |
| CA (1) | CA2985088C (en) |
| ES (1) | ES2777611T3 (en) |
| MX (1) | MX2017014373A (en) |
| WO (1) | WO2016191513A1 (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| PL3601626T3 (en) | 2017-03-23 | 2022-07-18 | Novelis, Inc. | Casting recycled aluminum scrap |
| CN109317554A (en) * | 2018-10-24 | 2019-02-12 | 佛山市顺德区金帝实业有限公司 | A kind of heating and pressure forming device for special-shaped metal container and forming method thereof |
| KR20220105167A (en) * | 2020-01-23 | 2022-07-26 | 노벨리스 인크. | Engineered can body material and can end material and methods of making and using the same |
| CN111843397A (en) * | 2020-08-06 | 2020-10-30 | 温州深拉防爆设备有限公司 | Natural gas cylinder liner formed by stretching process |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3896648A (en) | 1973-10-02 | 1975-07-29 | Alter Licensing Ets | Blow molding process for container of superplastic alloy |
| US5832766A (en) | 1996-07-15 | 1998-11-10 | Crown Cork & Seal Technologies Corporation | Systems and methods for making decorative shaped metal cans |
| WO2002087802A1 (en) | 2001-05-01 | 2002-11-07 | Alcan International Limited | Method of pressure-ram-forming metal containers and the like |
| US6499329B1 (en) | 1999-08-30 | 2002-12-31 | Daiwa Can Company | Production method for bottle type can and form-working tool |
| US20130167607A1 (en) | 2011-12-30 | 2013-07-04 | The Coca-Cola Company | System and method for forming a metal beverage container using pressure molding |
| US8683837B2 (en) | 2010-01-12 | 2014-04-01 | Novelis Inc. | Methods of pressure forming metal containers and the like from preforms having wall thickness gradient |
| US20140298641A1 (en) | 2013-04-09 | 2014-10-09 | Ball Corporation | Aluminum impact extruded bottle with threaded neck made from recycled aluminum and enhanced alloys |
| WO2015054284A2 (en) | 2013-10-08 | 2015-04-16 | The Coca-Cola Company | Shaped metal container, microstructure, a method for making a shaped metal container |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6253597B1 (en) * | 1988-02-19 | 2001-07-03 | Corus Staal B.V. | Body-necking a wall-ironed can |
| FR2683750B1 (en) * | 1991-11-19 | 1995-09-01 | Cmb Packaging Sa | METHOD FOR CONFORMING A METAL BOX BODY AND INSTALLATION FOR CONFORMING SUCH A BOX BODY. |
| JPH08168828A (en) * | 1994-12-15 | 1996-07-02 | Furukawa Electric Co Ltd:The | DI can molding method |
| JP3604835B2 (en) * | 1996-09-11 | 2004-12-22 | 大和製罐株式会社 | Method for manufacturing aluminum DI can having irregular pattern on body |
| JPH11130611A (en) * | 1997-10-24 | 1999-05-18 | Yamaichi Kinzoku Kk | Production of antimicrobial article utilizing waste pigment |
| US7191032B2 (en) * | 2004-05-14 | 2007-03-13 | Novelis Inc. | Methods of and apparatus for forming hollow metal articles |
-
2016
- 2016-05-26 KR KR1020177033749A patent/KR102028816B1/en not_active Expired - Fee Related
- 2016-05-26 EP EP16728186.4A patent/EP3302846B1/en not_active Revoked
- 2016-05-26 CA CA2985088A patent/CA2985088C/en not_active Expired - Fee Related
- 2016-05-26 JP JP2018511368A patent/JP6534494B2/en not_active Expired - Fee Related
- 2016-05-26 AU AU2016267097A patent/AU2016267097B2/en not_active Ceased
- 2016-05-26 BR BR112017023293A patent/BR112017023293A2/en not_active Application Discontinuation
- 2016-05-26 US US15/574,371 patent/US20180126440A1/en not_active Abandoned
- 2016-05-26 ES ES16728186T patent/ES2777611T3/en active Active
- 2016-05-26 MX MX2017014373A patent/MX2017014373A/en unknown
- 2016-05-26 WO PCT/US2016/034214 patent/WO2016191513A1/en not_active Ceased
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3896648A (en) | 1973-10-02 | 1975-07-29 | Alter Licensing Ets | Blow molding process for container of superplastic alloy |
| US5832766A (en) | 1996-07-15 | 1998-11-10 | Crown Cork & Seal Technologies Corporation | Systems and methods for making decorative shaped metal cans |
| US6499329B1 (en) | 1999-08-30 | 2002-12-31 | Daiwa Can Company | Production method for bottle type can and form-working tool |
| WO2002087802A1 (en) | 2001-05-01 | 2002-11-07 | Alcan International Limited | Method of pressure-ram-forming metal containers and the like |
| US8683837B2 (en) | 2010-01-12 | 2014-04-01 | Novelis Inc. | Methods of pressure forming metal containers and the like from preforms having wall thickness gradient |
| US20130167607A1 (en) | 2011-12-30 | 2013-07-04 | The Coca-Cola Company | System and method for forming a metal beverage container using pressure molding |
| US20140298641A1 (en) | 2013-04-09 | 2014-10-09 | Ball Corporation | Aluminum impact extruded bottle with threaded neck made from recycled aluminum and enhanced alloys |
| WO2015054284A2 (en) | 2013-10-08 | 2015-04-16 | The Coca-Cola Company | Shaped metal container, microstructure, a method for making a shaped metal container |
Non-Patent Citations (1)
| Title |
|---|
| "IUPAC - Compendium of Chemical Terminology GOLD BOOK", IUPAC - COMPENDIUM OF CHEMICAL TERMINOLOGY, 24 February 2014 (2014-02-24), pages 729 - 1622, XP055754857 |
Also Published As
| Publication number | Publication date |
|---|---|
| CA2985088C (en) | 2020-07-28 |
| ES2777611T3 (en) | 2020-08-05 |
| BR112017023293A2 (en) | 2018-08-14 |
| KR20170139619A (en) | 2017-12-19 |
| CA2985088A1 (en) | 2016-12-01 |
| WO2016191513A1 (en) | 2016-12-01 |
| AU2016267097A1 (en) | 2017-11-16 |
| JP2018517569A (en) | 2018-07-05 |
| JP6534494B2 (en) | 2019-06-26 |
| AU2016267097B2 (en) | 2019-02-21 |
| MX2017014373A (en) | 2018-03-02 |
| EP3302846A1 (en) | 2018-04-11 |
| KR102028816B1 (en) | 2019-10-04 |
| US20180126440A1 (en) | 2018-05-10 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US11738382B2 (en) | Shaped metal container, microstructure, a method for making a shaped metal container | |
| US8683837B2 (en) | Methods of pressure forming metal containers and the like from preforms having wall thickness gradient | |
| CN101479057B (en) | Bulging die and method for forming containers | |
| US9849500B2 (en) | Can manufacture | |
| US20170008656A1 (en) | Process to manufacture large format aluminum bottles | |
| CA2985088C (en) | High-speed blow forming process to shape aluminum containers using 3xxx alloys with high recycled content | |
| RU2003134535A (en) | METHOD OF PLUNGING FORMING UNDER PRESSURE OF METAL CONTAINERS AND SIMILAR PRODUCTS | |
| EP3007838B1 (en) | Multi blow molded metallic container | |
| EP3052258B1 (en) | Multiple blow molded metallic container sidewalls | |
| JP6676949B2 (en) | Manufacturing method of metal container | |
| JP2001087832A (en) | Method and device for forming pot shaped metal product having necked part and intermediate formed body using the forming method | |
| KR20040022214A (en) | Method of pressure-ram-forming metal containers and the like | |
| KR100284057B1 (en) | Method of manufacturing a 3 piece can for a self-cooling container |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE |
|
| PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE |
|
| 17P | Request for examination filed |
Effective date: 20171205 |
|
| AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
| AX | Request for extension of the european patent |
Extension state: BA ME |
|
| DAV | Request for validation of the european patent (deleted) | ||
| DAX | Request for extension of the european patent (deleted) | ||
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: EXAMINATION IS IN PROGRESS |
|
| 17Q | First examination report despatched |
Effective date: 20190408 |
|
| GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: GRANT OF PATENT IS INTENDED |
|
| INTG | Intention to grant announced |
Effective date: 20190918 |
|
| GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
| GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE PATENT HAS BEEN GRANTED |
|
| AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
| REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D |
|
| REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
| REG | Reference to a national code |
Ref country code: AT Ref legal event code: REF Ref document number: 1231419 Country of ref document: AT Kind code of ref document: T Effective date: 20200215 |
|
| REG | Reference to a national code |
Ref country code: CH Ref legal event code: NV Representative=s name: BOVARD AG PATENT- UND MARKENANWAELTE, CH |
|
| REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D |
|
| REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 602016029536 Country of ref document: DE |
|
| REG | Reference to a national code |
Ref country code: NO Ref legal event code: T2 Effective date: 20200212 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: RS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200212 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200212 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: NO Payment date: 20200424 Year of fee payment: 5 Ref country code: FR Payment date: 20200422 Year of fee payment: 5 Ref country code: DE Payment date: 20200421 Year of fee payment: 5 Ref country code: ES Payment date: 20200602 Year of fee payment: 5 Ref country code: CH Payment date: 20200422 Year of fee payment: 5 |
|
| REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2777611 Country of ref document: ES Kind code of ref document: T3 Effective date: 20200805 |
|
| REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG4D |
|
| REG | Reference to a national code |
Ref country code: NL Ref legal event code: MP Effective date: 20200212 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200212 Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200512 Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200612 Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200513 Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200212 Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200212 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20200423 Year of fee payment: 5 Ref country code: IT Payment date: 20200421 Year of fee payment: 5 Ref country code: BE Payment date: 20200423 Year of fee payment: 5 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200212 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200212 Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200212 Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200212 Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200212 Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200212 Ref country code: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200212 Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200705 Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200212 |
|
| REG | Reference to a national code |
Ref country code: DE Ref legal event code: R026 Ref document number: 602016029536 Country of ref document: DE |
|
| PLBI | Opposition filed |
Free format text: ORIGINAL CODE: 0009260 |
|
| PLAX | Notice of opposition and request to file observation + time limit sent |
Free format text: ORIGINAL CODE: EPIDOSNOBS2 |
|
| 26 | Opposition filed |
Opponent name: ARDAGH PACKAGING INTERNATIONAL SERVICES LIMITED Effective date: 20201112 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200212 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200212 Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200212 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20200526 |
|
| REG | Reference to a national code |
Ref country code: AT Ref legal event code: UEP Ref document number: 1231419 Country of ref document: AT Kind code of ref document: T Effective date: 20200212 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20200526 |
|
| REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 602016029536 Country of ref document: DE |
|
| REG | Reference to a national code |
Ref country code: NO Ref legal event code: MMEP |
|
| REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
| RDAF | Communication despatched that patent is revoked |
Free format text: ORIGINAL CODE: EPIDOSNREV1 |
|
| GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20210526 |
|
| REG | Reference to a national code |
Ref country code: DE Ref legal event code: R103 Ref document number: 602016029536 Country of ref document: DE Ref country code: DE Ref legal event code: R064 Ref document number: 602016029536 Country of ref document: DE |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210531 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210531 Ref country code: NO Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210531 |
|
| REG | Reference to a national code |
Ref country code: BE Ref legal event code: MM Effective date: 20210531 |
|
| PLAB | Opposition data, opponent's data or that of the opponent's representative modified |
Free format text: ORIGINAL CODE: 0009299OPPO |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210526 Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20211201 |
|
| RDAG | Patent revoked |
Free format text: ORIGINAL CODE: 0009271 |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: PATENT REVOKED |
|
| R26 | Opposition filed (corrected) |
Opponent name: ARDAGH PACKAGING INTERNATIONAL SERVICES LIMITED Effective date: 20201112 |
|
| REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
| REG | Reference to a national code |
Ref country code: FI Ref legal event code: MGE |
|
| 27W | Patent revoked |
Effective date: 20220128 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: TR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200212 Ref country code: MT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200212 Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210531 Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200212 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200212 Ref country code: AL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200212 |
|
| REG | Reference to a national code |
Ref country code: AT Ref legal event code: MA03 Ref document number: 1231419 Country of ref document: AT Kind code of ref document: T Effective date: 20220128 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20200526 |
|
| P01 | Opt-out of the competence of the unified patent court (upc) registered |
Effective date: 20230518 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: ES Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210527 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: ES Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210527 Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210531 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AT Free format text: LAPSE BECAUSE OF THE APPLICANT RENOUNCES Effective date: 20220128 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AT Free format text: LAPSE BECAUSE OF THE APPLICANT RENOUNCES Effective date: 20220128 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210526 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: AT Payment date: 20260410 Year of fee payment: 5 |