EP4651742A2 - Procédés et ensembles pour le traitement d'une feuille continue d'un matériau - Google Patents

Procédés et ensembles pour le traitement d'une feuille continue d'un matériau

Info

Publication number
EP4651742A2
EP4651742A2 EP24702584.4A EP24702584A EP4651742A2 EP 4651742 A2 EP4651742 A2 EP 4651742A2 EP 24702584 A EP24702584 A EP 24702584A EP 4651742 A2 EP4651742 A2 EP 4651742A2
Authority
EP
European Patent Office
Prior art keywords
component
sheet material
sheet
consumable
mandrel
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.)
Pending
Application number
EP24702584.4A
Other languages
German (de)
English (en)
Inventor
Andrei GRISHCHENKO
Gilbert AYINA
Louise ADAMS
Junior KABIRAT
Rosa GALATI
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nicoventures Trading Ltd
Original Assignee
Nicoventures Trading Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Nicoventures Trading Ltd filed Critical Nicoventures Trading Ltd
Publication of EP4651742A2 publication Critical patent/EP4651742A2/fr
Pending legal-status Critical Current

Links

Classifications

    • AHUMAN NECESSITIES
    • A24TOBACCO; CIGARS; CIGARETTES; SIMULATED SMOKING DEVICES; SMOKERS' REQUISITES
    • A24DCIGARS; CIGARETTES; TOBACCO SMOKE FILTERS; MOUTHPIECES OF CIGARS OR CIGARETTES; MANUFACTURE OF TOBACCO SMOKE FILTERS OR MOUTHPIECES
    • A24D3/00Tobacco smoke filters, e.g. filter tips or filtering inserts; Filters specially adapted for simulated smoking devices; Mouthpieces of cigars or cigarettes
    • A24D3/02Manufacture of tobacco smoke filters
    • A24D3/0204Preliminary operations before the filter rod forming process, e.g. crimping, blooming
    • AHUMAN NECESSITIES
    • A24TOBACCO; CIGARS; CIGARETTES; SIMULATED SMOKING DEVICES; SMOKERS' REQUISITES
    • A24DCIGARS; CIGARETTES; TOBACCO SMOKE FILTERS; MOUTHPIECES OF CIGARS OR CIGARETTES; MANUFACTURE OF TOBACCO SMOKE FILTERS OR MOUTHPIECES
    • A24D3/00Tobacco smoke filters, e.g. filter tips or filtering inserts; Filters specially adapted for simulated smoking devices; Mouthpieces of cigars or cigarettes
    • A24D3/04Tobacco smoke filters characterised by their shape or structure
    • AHUMAN NECESSITIES
    • A24TOBACCO; CIGARS; CIGARETTES; SIMULATED SMOKING DEVICES; SMOKERS' REQUISITES
    • A24DCIGARS; CIGARETTES; TOBACCO SMOKE FILTERS; MOUTHPIECES OF CIGARS OR CIGARETTES; MANUFACTURE OF TOBACCO SMOKE FILTERS OR MOUTHPIECES
    • A24D3/00Tobacco smoke filters, e.g. filter tips or filtering inserts; Filters specially adapted for simulated smoking devices; Mouthpieces of cigars or cigarettes
    • A24D3/17Filters specially adapted for simulated smoking devices

Definitions

  • the present invention relates to a method of processing a continuous sheet material in the manufacture of a component of a consumable for use in or with an aerosol provision system and an assembly for doing the same.
  • the present invention also relates to a component formed using the assembly and associated method.
  • Aerosol provision systems include traditional systems such as cigarettes, as well as more recent systems such electronic aerosol generating devices and their associated consumables. These systems are complex and have many components, many of which can consist of non-biodegradable materials. There is therefore a drive to design new components with the same or better functionality and performance, but that have improved biodegradability for reduced environmental impact.
  • a method of processing a continuous sheet material in the manufacture of a component of a consumable for use in or with an aerosol provision system comprising: drawing the sheet material through a groove of a pre-folding unit such that the sheet material at least partially adopts the profile of the groove, wherein the groove extends along a helical path.
  • the groove maybe part of a series of grooves.
  • the grooves maybe formed in a convex side of a curved wall of the pre-folding unit.
  • the grooves may be formed in a concave side of a curved wall of the pre-folding unit.
  • the helical path may form at least one complete turn of a helix.
  • An upstream end of the curved wall may comprise a first radius and a downstream end a second radius, wherein the first radius is greater than the second radius.
  • the pitch of at least one groove at the downstream end may be between 3mm and
  • the sheet of material may comprise paper.
  • the sheet material may comprise a nonwoven material.
  • the method may comprise applying a crimping pattern to the sheet material prior to drawings said sheet material over said edge.
  • the crimping pattern may comprise a crimp amplitude of between about o.imm and 0.2mm.
  • the method may further comprise feeding the sheet material into a channel of a transport jet comprising a funnel and a mandrel.
  • the method may further comprise applying a bonding agent to the material.
  • the bonding agent may comprises about 6wt% Pectin.
  • the mandrel may be disposed within the funnel so that an outer surface of the mandrel is spaced from an inner surface of the funnel to define the channel therebetween, wherein the mandrel may comprise an internal conduit, and wherein apertures in a wall of the mandrel may communicate the conduit with the channel; and wherein applying a bonding agent to the material may comprise applying the bonding agent through the apertures of the mandrel.
  • the method may further comprise splitting the sheet material into individual strands of sheet material upstream of the pre-folding unit.
  • an assembly comprising a pre-folding unit for processing a continuous sheet of material in the manufacture of a component of a consumable for use in or with an aerosol provision system, the prefolding unit comprising at least one groove in a surface of the pre-folding unit, the at least one groove extending along a helical path.
  • the grooves may be formed in a convex side of the curved wall.
  • the grooves maybe formed in a concave side of the curved wall.
  • the helical path may form at least one complete turn of a helix.
  • An upstream end of the curved wall may comprise a first radius and a downstream end a second radius, wherein the first radius is greater than the second radius.
  • the pitch of at least one groove of the series of grooves at the downstream end may be between 3mm and 20mm.
  • a component of a consumable for use in or with an aerosol provision system comprising a hollow tube formed of a gathered sheet of material, wherein the gathered sheet of material extends along a helical path about a longitudinal axis of the component.
  • a component of a consumable for use in or with an aerosol provision system may comprise a sheet of material processed as described above.
  • the gathered sheet of material may comprises individual strands of sheet material that each extend along a helical path.
  • the gathered sheet of material may comprise a gathered sheet of crimped material.
  • the component may comprise an axial length between 4mm and 12mm and, optionally, an internal diameter of between 2.5mm and 5.5mm and, optionally, a wall thickness of between imm and 1.5mm.
  • the helical path of the or each strand may have a pitch of between 50mm and 550mm.
  • the helical path may comprise 0.7 degrees angle of twist per cm of axial length of the component.
  • the sheet of material may comprises any one of paper, lyocell, viscose, silk, cotton, linen, jute or tobacco paper.
  • the sheet material may comprises an aerosol generating material.
  • a consumable configured to generate an aerosol when used with an electronic aerosol generating device, the consumable comprising the component as described above.
  • the component may form part of a filter assembly, an aerosol generating section or any other section of the consumable through which aerosol is drawn in use.
  • an aerosol provision system comprising the component as described above.
  • Fig. 1 illustrates a consumable in cross-section
  • Fig. 2 schematically illustrates part of a manufacturing line for a component of the consumable
  • Fig. 3 illustrates a section of sheet material following transit through a crimping station
  • Fig. 4 illustrates the section of sheet material following transit through a pre-folding unit
  • Fig. 5 illustrates a crimping pattern impressed into the sheet material by the crimping station
  • Fig. 6 illustrates a first example of the pre-folding unit
  • Fig. 7 illustrates a second example of the pre-folding unit
  • Fig. 8 illustrates a transport jet in cross section
  • Fig. 9a schematically illustrates a tapered portion of a mandrel of the transport jet
  • Fig. 9b schematically illustrates a converging section of a funnel of the transport jet
  • Fig. 10 is a flow chart of a method of manufacturing the component of the consumable
  • Fig. 11 is a flow chart of a method of processing the sheet material in the manufacture of the component of the consumable.
  • Fig. 12 illustrates a component formed in accordance with methods and apparatus described herein.
  • a “combustible” aerosol provision system is one where a constituent aerosol-generating material of the aerosol provision system (or component thereof) is combusted or burned during use in order to facilitate delivery of at least one substance to a user.
  • the delivery system is a combustible aerosol provision system, such as a system selected from the group consisting of a cigarette, a cigarillo and a cigar.
  • the disclosure relates to a component for use in a combustible aerosol provision system, such as a filter, a filter rod, a filter segment, a tobacco rod, a spill, an aerosol-modifying agent release component such as a capsule, a thread, or a bead, or a paper such as a plug wrap, a tipping paper or a cigarette paper.
  • a component for use in a combustible aerosol provision system such as a filter, a filter rod, a filter segment, a tobacco rod, a spill, an aerosol-modifying agent release component such as a capsule, a thread, or a bead, or a paper such as a plug wrap, a tipping paper or a cigarette paper.
  • a “non-combustible” aerosol provision system is one where a constituent aerosol-generating material of the aerosol provision system (or component thereof) is not combusted or burned in order to facilitate delivery of at least one substance to a user.
  • the delivery system is a non-combustible aerosol provision system, such as a powered non-combustible aerosol provision system.
  • the non-combustible aerosol provision system is an electronic cigarette, also known as a vaping device or electronic nicotine delivery system (END), although it is noted that the presence of nicotine in the aerosol-generating material is not a requirement.
  • END electronic nicotine delivery system
  • the non-combustible aerosol provision system is an aerosolgenerating material heating system, also known as a heat-not-burn system.
  • a heat-not-burn system An example of such a system is a tobacco heating system.
  • the non-combustible aerosol provision system is a hybrid system to generate aerosol using a combination of aerosol-generating materials, one or a plurality of which may be heated.
  • Each of the aerosol-generating materials may be, for example, in the form of a solid, liquid or gel and may or may not contain nicotine.
  • the hybrid system comprises a liquid or gel aerosol-generating material and a solid aerosol-generating material.
  • the solid aerosol-generating material may comprise, for example, tobacco or a non-tobacco product.
  • the non-combustible aerosol provision system may comprise a noncombustible aerosol provision device and a consumable for use with the noncombustible aerosol provision device.
  • the disclosure relates to consumables comprising aerosolgenerating material and configured to be used with non-combustible aerosol provision devices. These consumables are sometimes referred to as articles throughout the disclosure.
  • the non-combustible aerosol provision system such as a non-combustible aerosol provision device, may comprise a power source and a controller.
  • the power source may, for example, be an electric power source or an exothermic power source.
  • the exothermic power source comprises a carbon substrate which may be energised so as to distribute power in the form of heat to an aerosol-generating material or to a heat transfer material in proximity to the exothermic power source.
  • the non-combustible aerosol provision system may comprise an area for receiving the consumable, an aerosol generator, an aerosol generation area, a housing, a mouthpiece, a filter and/or an aerosol-modifying agent.
  • the consumable for use with the non-combustible aerosol provision device may comprise aerosol-generating material, an aerosol-generating material storage area, an aerosol-generating material transfer component, an aerosol generator, an aerosol generation area, a housing, a wrapper, a filter, a mouthpiece, and/or an aerosol-modifying agent.
  • Fig. 1 shows an aerosol provision system 10 in the form of a rod-shaped consumable 10 for use with an electronic aerosol generating device.
  • Fig. 1 is presented as a section taken along the system’s longitudinal axis.
  • the system comprises a hollow component 11.
  • the hollow component 11 is a tube 11 formed of a sheet of crimped paper gathered into the tube according to the method outlined herein.
  • Other components of the system may vary according to the particular application of the system, but are readily selected by the skilled person and can include an aerosol generating section, a filter and other additive or active laden sections as required.
  • the tube 11 itself may be provided with aerosol generating material.
  • the hollow component 11 is attached to a rod-shaped aerosol generating section 13 by an overlapping wrapping material 14 that circumscribes both.
  • the wrapping paper 14 may be a tipping paper, a cigarette paper, a plug wrap or any other suitable combining overwrap that will be available to the skilled person.
  • Fig. 2 schematically illustrates part of a manufacturing line 20 for the component 11.
  • the line 20 comprises a supply 21 of continuous sheet material 22 at an upstream end
  • the manufacturing line 20 further comprises a crimping station 23, an optional cutting station 24, a pre-folding unit 25, a transport jet 26, a pressure chamber 28 and a drying chamber 29.
  • the continuous sheet material 22 is processed to form a continuous hollow rod 30, which is output from the transport jet 26.
  • the endless garniture belt 27 conveys the continuous hollow rod 30 before being cut into individual components for conveyance to further assembly stations for forming a consumable.
  • the supply of continuous sheet material 21 comprises a reel 211 about which is wound the continuous sheet material 22 (also referred to herein as simply ‘sheet material 22’ for brevity).
  • sheet material 22 is unwound from the reel 211 and conveyed in the machine direction.
  • the sheet material may comprise a non-woven material.
  • the sheet material 22 is preferably a paper of cellulose fibres having paper weight of 30 gsm to 70 gsm, however other biodegradable materials having any suitable thickness maybe used.
  • the sheet material 22 can be any of paper, lyocell, viscose, silk, cotton, linen (1.0 - 5.0 denier), jute or a tobacco paper.
  • the sheet material 22 may also comprise an aerosol generating material.
  • the width of the sheet material 22 is preferably between 70mm and 160mm and, in a particular example, is 90mm.
  • the thickness of the sheet material 22 may be between 6op and loop and, in a particular example, is 8s .
  • the crimping station 23 comprises a pair of crimping rollers 231, 231’.
  • Each roller 231, 231’ is a cylinder arranged to rotate about its axis.
  • the rollers 231, 231’ are arranged with their axes parallel and their circumferential surfaces closely spaced such that, in use, the rollers 231, 231’ rotate to grip the sheet material 22 in between.
  • the crimping rollers 231, 231’ maybe driven to assist in drawing the sheet material from the reel 21, or they may be passive and rotate as a result of the sheet material 22 being drawn therebetween.
  • the sheet material may be drawn in the machine direction solely by the endless garniture belt 27 at the downstream end of the line 20.
  • One or both of the rollers 231, 231’ comprises an embossing pattern on its circumferential surface to impress the pattern into the sheet material 22 as it passes in between.
  • the pattern comprises a series of ridges and grooves as shown in Figs. 3 and 5 and is referred to herein as the ‘crimp pattern’ or ‘crimping pattern’.
  • Fig. 3 illustrates a section of the sheet material 22 as it emerges from the crimping station 23.
  • the grooves impressed into the sheet material extend in a longitudinal direction LD of the sheet material 22, that is to say, in the machine direction MD.
  • Fig. 5 illustrates the crimping pattern in more detail.
  • the crimping pattern comprises a crimp amplitude A (also known as “crimping factor”), which refers to the depth of the grooves the crimping pattern forms in the sheet material 22. That is, crimping the sheet material 22 produces a plurality of peaks 221 and troughs 222 in the sheet material 22, where the crimp amplitude ‘A’ is the depth of the troughs 222, measured from their peak 221.
  • the crimping factor has an influence on the hardness and roundness of the component 11 being produced. That is, increasing the crimping factor has been found to increase the hardness and roundness of the component 11, with associated benefits in terms of component integrity and quality.
  • the crimping may form a ‘Zig-Zag’ formation or another shape. Adjacent grooves of the crimped sheet material are spaced by a distance, or have a pitch ‘P’.
  • the pitch is preferably in the range of too pm to 1000
  • the crimp amplitude is preferably between 50 pm and 250 pm, or more preferably in the range of too pm and 200 pm.
  • the crimped sheet material comprises a pitch of 300 pm and a crimp amplitude of 150 pm.
  • the sheet material may optionally pass to the cutting station 24 where the sheet material 22 is slit into individual strands 22’, 22”, 22”’ of sheet material 22, as shown in Fig. 2. If the cutting station 24 is omitted, the sheet material 22 is instead advanced directly to the pre-folding unit 25 without being divided into strands and remains intact.
  • slitting the sheet material 22 into individual strands 22’, 22”, 22”’ results in a more uniform distribution of the sheet material 22 when it is gathered into the shape of the component 11 in the transport jet 25. This is explained further below.
  • the cutting station 24 comprises an arrangement of blades 241 which extend into the path of the sheet material 22 to slice the sheet material 22 into the individual strands 22’, 22”, 22”’ as the sheet material 22 is drawn across the blades 241.
  • the blades 241 may comprise a straight edge or, alternatively, the blades 241 may be discs that cut the sheet material against an anvil roller or other cutting surface. Where the cutting station 24 is employed, the sheet material 22 may be cut into two, three, four or five strands, as desired.
  • the pre-folding unit 25 comprises a series of grooves 251 that extend along a helical path.
  • Fig. 6 shows a first example pre-folding unit 25 in which the grooves 251 are formed in a convex side of a curved wall 252 of the pre-folding unit 25.
  • the curved wall 252 is the curved outer surface 252 of a solid frusto-conical, single piece component 25’.
  • the component 25’ comprises an upstream end U which is configured to face the direction of incoming sheet material 22 and a downstream end D, opposite the upstream end.
  • the upstream end is the larger diameter end of the frustum-cone.
  • the component 25’ comprises five grooves 251 that each follow a helical path about the outer surface 252 of the component 25’, though any number of grooves may be adopted as required.
  • sheet material 22 is drawn over the upstream end U the component 25’ and into the transport jet 26.
  • An inlet to the transport jet 26 has a diameter equal to or less than the diameter of the downstream end D of the pre-component 25’ so that the sheet material 22 is drawn tightly over its curved surface 252 and into the grooves 251, causing the sheet material 22 to adopt the profile of the grooves 251. In this way the sheet material 22 is pre folded as the sheet material 22 remains in the shape imparted by the grooves 251 as it leaves the component 25’.
  • a second example pre-folding unit 25 is shown in Fig. 7 in which like features retain the same reference numbers.
  • the grooves 251 are formed in a concave side 253 of a curved wall 254 of the pre-folding unit 25.
  • the curved wall 254 forms a hollow frusto-conical, single piece component 25” with the grooves 251 provided in an inner surface 253 of the hollow component 25” in a manner similar to rifling.
  • the hollow component 25” comprises an upstream end U which is configured to face the direction of incoming sheet material 22 and a downstream end D, opposite the upstream end, with the upstream end being the larger diameter end of the frustum-cone.
  • the component 25 comprises eight grooves 251 that each follow a helical path about the inner surface 253 of the component 25”, though any number of grooves 251 may be adopted as required.
  • sheet material is drawn into the upstream end and leaves through the downstream end before passing into the transport jet 26. Due to the decreasing diameter of the inner surface 253 between the upstream and downstream ends, the sheet material 22 closely follows the inner surface 253 of the component 25” and adopts the profile of the grooves 251. In this way, the sheet material is pre folded in the same manner as with the solid component 25’.
  • Fig. 4 shows a section of sheet material that has left the pre-folding unit 25.
  • the sheet material 22 comprises a macro and micro fold pattern.
  • the macro fold pattern refers to the shape imparted by the grooves 251 of the pre-folding unit 25 and comprises a series of ridges and grooves that are sinusoidal in appearance.
  • the micro fold pattern refers to the much finer series of peaks 221 and troughs 222 imparted by the crimping rollers 23 as described above.
  • the continuous sheet material 22 itself begins to adopt a helical path as it passes from the pre-folding unit 25 into the transport jet 26.
  • each individual strand is caused to adopt a helical path as it is passed into the transport jet 26.
  • the sheet material 22 is gathered within the transport jet 26 to form a continuous hollow rod 30, with each strand of the gathered sheet material 22 following a helical path about the axis of the continuous hollow rod 30.
  • An advantage of this is that the continuous hollow rod 30 is provided with more uniform distribution of gathered sheet material 22 along the length of the continuous hollow rod 30 than if the individual strands were not caused to adopt a helical shaped path.
  • the grooves 251 of the pre-folding units 25 described herein may have a pitch at the downstream end D of the pre-folding unit 25 of between 50mm and 550mm, such as between 200mm and 400mm.
  • pitch it is meant the axial distance over which the helical path takes to complete one turn (i.e. to turn through 360 degrees).
  • pitch at the downstream end D it is meant the pitch of the of the helical path at the diameter of the downstream end D of the pre-folding unit 25.
  • the pitch at the downstream end will be substantially equal to the pitch of the individual strands of the sheet material 22 as they enter the transport jet 26. It will be appreciated that the pitch need not be constant across the length of the pre-folding unit 25.
  • the grooves 251 may have a pitch at the downstream end D of the pre-folding unit 25 that is less than the pitch at the upstream end U of the pre-folding unit 25. In this way, the helical path described by the grooves 251 may gradually tighten between the upstream and downstream ends U, D. In one example, the helical path may describe a conic helix.
  • the illustrated pre-folding units 25 are machined from aluminium, steel or any other suitable material - a detailed description of which will be omitted for falling within the purview of the skilled person. They may be mounted to a bed of the manufacturing line 20 by bracket (not shown) or any other suitable way. What is important is that the axis X-X of the pre-folding unit 25 is parallel to the machine direction MD with the upstream end U facing the direction of incoming sheet material 22.
  • the pre-folding units 25 should be positioned within the path of the sheet of material 22 such that the sheet material follows the grooves 251 of the pre-folding unit 25 in the way described.
  • the grooves 251 of the illustrated pre-folding units 25 may have a width of between 3mm and 20mm. The narrower the width of each groove 251, the more tightly the sheet material 22 is pre folded.
  • Fig. 8 illustrates the transport jet 26 in a section taken along its longitudinal axis.
  • the transport jet 26 comprises a funnel 261 and a mandrel 262.
  • the mandrel 262 is an elongate rod positioned within the funnel 261 so that an outer surface 263 of the mandrel 262 is spaced from an inner surface 264 of the funnel 261, forming an annular channel 265.
  • the mandrel 262 comprises a tapered portion 266 and a uniform portion 267.
  • tapered it is meant that an overall diameter of the mandrel 262 decreases between an upstream end 2610 of the mandrel 262 and the uniform portion 267.
  • uniform it is meant that an overall diameter of the uniform portion 267 is constant along its length to a downstream end 2611 of the mandrel 262.
  • the funnel 261 comprises a converging section 268 and a uniform section 269, downstream of the converging section 268.
  • An internal diameter of the funnel 261 in the converging section 268 decreases between an upstream end 2612 of the funnel and the uniform section 269, whereupon the internal diameter is constant for the length of the uniform section 269 to a downstream end 2613 of the funnel 261.
  • the mandrel 262 is positioned within the funnel 261 so that the tapered portion 266 of the mandrel 262 sits within the converging portion 268 of the funnel 261 and the uniform portion 267 of the mandrel 262 within the uniform section 269 of the funnel 261.
  • a taper angle of the tapered portion 266 of the mandrel 262 is less than a convergence angle of the converging section 268 of the funnel 261.
  • the channel 265 comprises a section 2614 (herein referred to as an ‘upstream section 2614’) in which the outer surface 263 of the mandrel 262 and the inner surface 264 of the funnel 261 converge.
  • the cross-sectional area of the upstream section 2614 of the channel 265 decreases between an inlet 2616 of the channel 265 and an intermediate-point 2617 of the channel 265.
  • the intermediate-point 2617 of the channel 265 is a position along the length of the channel 265 where the upstream section 2614 meets a downstream section 2615 and is represented graphically in Fig.
  • the downstream section 2615 is defined as a portion of the channel in which the cross-section area of the channel 265 is constant. In other words, it is the section of the channel 265 defined between the uniform portion 267 of the mandrel 262 and the uniform section 269 of the funnel 261. In the illustrated example, the downstream section 2615 extends from the intermediate-point 2617 to an outlet 2618 of the channel 265.
  • the taper angle AT of the mandrel is given by the formula:
  • AT is the taper angle
  • DSM is the smaller diameter end of the tapered portion of the mandrel
  • DLM is the larger diameter end of the tapered portion of the mandrel; and L M is the length of the tapered portion of the mandrel.
  • DSF is the smaller diameter end of the upstream section of the funnel
  • DLF is the larger diameter end of the upstream section of the funnel.
  • LF is the length of the upstream section of the funnel.
  • Fig. 9b shows the converging section 268 of the funnel 261 schematically.
  • DSF, DLF of the funnel 261 are internal diameters of the funnel 261.
  • ctional area at the intermediate point (CIP) is given by:
  • a T ⁇ Ac such that CIN > Cip. This ensures a smooth and gradual gathering of the sheet material 22 as it travels through the upstream section of the funnel.
  • the mandrel 262 comprises an internal conduit 2619 and apertures 2620 that communicate the internal conduit 2619 with the channel 265.
  • the internal conduit 2619 and apertures 2620 that communicate the internal conduit 2619 with the channel 265.
  • the 2619 is connected to a supply of bonding agent 210 which is pumped through the internal conduit 2619, out of the apertures 2620 and into the channel 265 during operation of the transport jet 26.
  • the internal conduit 2619 and apertures 2620 are provided in the tapered portion 266 of the mandrel 262 such that the apertures 2620 communicate with the upstream section 2614 of the channel 265. Therefore, bonding agent is introduced into the upstream section 2614 of the channel 265 as the sheet material 22 is gathered around the mandrel 262.
  • the apertures 2620 are regularly spaced along the length of the tapered portion 266 of the mandrel 262 so that bonding agent is evenly distributed into the sheet material 22 in the upstream section 2614 of the channel 265.
  • aperture 2620 spacing Another advantage of regular aperture 2620 spacing is that it is possible to continually apply the bonding agent as the sheet material 22 moves over the apertures 2620. For a viscous agent, such as the intended bonding agents described below, this is necessary to provide the required amount of bonding agent to the sheet material 22.
  • the apertures 2620 may become more closely spaced with proximity to the intermediate point 2617 of the channel 265.
  • the apertures maybe provided in groups of apertures 2620 that extend radially from the conduit 2619 at a position along the length of the tapered portion 266 of the mandrel 262. In this way, the bonding agent is even distributed about the circumference of the mandrel 262.
  • apertures may be grouped into spirals that extend along the length of the tapered portion 266 mandrel 262.
  • a spiral of apertures 2620 is a group of apertures
  • each spiral of apertures 2620 maybe arranged to align with the helical direction taken by individual strands of sheet material 22 as they leave the pre-folding unit 25.
  • the downstream section 2615 of the channel 265 has a cross sectional area equal in size and shape to the cross section of the finished component 11. Therefore, following gathering of the sheet material 22 in the upstream section 2614 of the channel 265, the gathered sheet material 22 takes on the dimensions of the channel 265 in the downstream section 2615, emerging from the outlet 2618 as the continuous hollow rod 30 for cutting into individual components 11.
  • the downstream section 2615 of the mandrel 262 may be heated. This may be achieved by either heating the outer surface 263 of the mandrel 262 or by heating the inner surface 264 of the funnel 261.
  • the funnel 261 and/or mandrel 262 maybe heated in any suitable way. For example, electrical filaments (not shown) may be embedded in the surface 263, 264 to be heated.
  • the filaments are heated by electrical resistance so that applying a voltage to the filaments causes them to generate heat.
  • the surface in which the filaments are embedded - i.e. the outer surface 263 of the mandrel 262 or the inner surface 264 of the funnel 261 - maybe made of a heat conductive material, such as a metal.
  • the mandrel 262 and funnel 261 are machined from a machine grade aluminium or stainless steel. Tracks (not shown) may be machined into the outer surface 263 of the mandrel 262 or the inner surface 264 of the funnel 261 into which the filaments maybe laid. When the filaments are heated, the heat is conducted into the funnel 261 or mandrel 262 to heat the gathered sheet material 22 passing through the channel 265.
  • the inner surface 264 of the funnel 261 and/or the outer surface of the mandrel 262 are heated to a temperature of between 150 Celsius and 250 Celsius, or greater than about 200 Celsius.
  • a pressurisation mechanism 2621 may be provided in the upstream section 2614 of the channel 265.
  • the pressurisation mechanism 2621 comprises a nozzle 2622 configured to direct a stream of air toward the inlet 2616 of the channel 265 and thereby increase the static pressure at the inlet 2616.
  • the pressurisation mechanism may be configured to increase the static pressure at the inlet 2616 to between 4 bar and 8 bar.
  • the pressurisation mechanism is configured to increase the static pressure at the inlet 2616 to 6 bar.
  • a pressure chamber 28 and drying chamber 29 may be employed downstream of the transport jet 26. These chambers 28, 29 are enclosures having openings to allow the continuous hollow rod 30 to pass therethrough.
  • the pressure within the pressure chamber 28 is greater than ambient and assists in setting the bonding agent and causing a hardening of the continuous hollow rod 30.
  • the temperature within the drying chamber 29 is greater than ambient and further assists in setting the bonding agent and causing a hardening of the continuous hollow rod 30.
  • the transport jet 26 maybe mounted to the bed of the manufacturing line 20 by a bracket (not shown) or in any other suitable way.
  • the bracket may attach an outer surface of the funnel 261 to the bed.
  • the mandrel 262 may be supported within the funnel 261 by a bracket of its own that either attaches the mandrel 262 to the inner surface 264 of the funnel 261 or, alternatively, to the bed of the manufacturing line 20.
  • the tapered portion 266 of the mandrel 262 protrudes from the inlet 2616 beyond the funnel 261 and a bracket (not illustrated) secures the protruding part of the tapered portion 266 to the bed of the manufacturing line 20.
  • the bracket needs to be configured for minimal obstruction of the inlet 2616.
  • the bracket maybe a fin shaped support that extends radially from the mandrel 262 to the bed. In this way, the bracket does not obstruct the helical path of the sheet material 22 as it travels through the channel 265.
  • the bracket may include a line for the supply of bonding agent to the conduit 2619 of the mandrel 262.
  • a method 40 of manufacturing the hollow component 11 of the consumable 10 will now be described with reference to Fig. 10.
  • the method 40 comprises using 41 the transport jet 26 to gather continuous sheet material 20 into the shape of the hollow component
  • use 41 of the transport jet 26 comprises supplying 42 the sheet material 20 into the channel 265 of the transport jet 26, gathering 43 the sheet material 20 within the channel 265 and applying 44 a bonding agent to the gathered sheet material 20 through the apertures 2620 of the mandrel 262.
  • supplying 42 the material 20 comprises supplying a fibrous material.
  • the fibrous material is a continuous sheet of paper.
  • the continuous sheet of paper is a continuous sheet of crimped paper.
  • the crimped paper comprises a crimp amplitude of between about 0.1mm and 0.2mm.
  • applying 44 the bonding agent comprises applying a bonding agent comprising about 6wt% of food grade pectin. In one example, the bonding agent maybe 4wt% of food grade pectin.
  • a bonding agent other than pectin may be used such as a starch based bonding agent, a clay based bonding agent, BioWax, cellulose acetate (in one example 5% of cellulose acetate dissolved in triacetin) and a tree resin based bonding agent.
  • the method may further comprise setting 45 the bonding agent by heating a surface of the transport jet 26 to a temperature of between 150 Celsius and 250 Celsius, or greater than about 200 Celsius.
  • gathering 43 the sheet material may further comprise pressurising 46 the transport jet 26 to increase the static pressure within the channel 265 of the transport jet 26 to 6 bar.
  • the method 50 comprises drawing 51 the sheet material 20 through a groove 251 of the prefolding unit 25 such that the sheet material 20 at least partially adopts the profile of the groove 251.
  • the method of processing the sheet material may further comprise splitting 52 the sheet material into individual strands 22, 22”, 22”’ of sheet material 22 upstream of the pre-folding unit 25.
  • Fig. 12 illustrates an example hollow component 11 formed using examples of the method and apparatus outlined above and, in particular, example apparatus using the pre-folding unit 25 illustrated by Figs. 6 and 7.
  • the gathered sheet material of the component of Fig. 12 comprises individual strands 22’, 22”, 22”’ that each extend along a helical path about a longitudinal axis of the component.
  • the component could alternatively comprise any number of strands, including a single strand.
  • the helical path of the or each strand has an angle of twist of between 5 degrees and 45 degrees for an example component having an axial length of 7cm.
  • angle of twist it is meant the angle a radii will travel through tracing the helical path as it advances along the longitudinal axis by a given distance (7cm in this example).
  • the angle of twist per cm of axial length of the component 11 is between 0.7 degrees and 6.5 degrees. This equates to a pitch of between 50mm and 550mm. Therefore, the pitch of the helical path of the or each strand of the gathered sheet material 22 falls within a similar range to the pitch of the helical path of the grooves 251 of the pre-folding unit 25, though they may not be exactly the same in any given example.
  • the component comprises an axial length between 4mm and 12mm and, optionally, an internal diameter of between 2.5mm and 5.5mm and, optionally, a wall thickness of between imm and 1.5mm.
  • the component 11 may be used as part of a filter assembly, an aerosol generating section or any other section of a consumable 10 through which a user will draw an aerosol in use of the consumable 10.

Landscapes

  • Cigarettes, Filters, And Manufacturing Of Filters (AREA)
  • Folding Of Thin Sheet-Like Materials, Special Discharging Devices, And Others (AREA)
  • Manufacturing Of Cigar And Cigarette Tobacco (AREA)

Abstract

Procédé de traitement d'un matériau en feuille continue dans la fabrication d'un composant d'un consommable destiné à être utilisé dans ou avec un système de fourniture d'aérosol. Le procédé consiste à étirer le matériau en feuille à travers une rainure d'une unité de prépliage de telle sorte que le matériau en feuille adopte au moins partiellement le profil de la rainure, la rainure s'étendant le long d'un trajet hélicoïdal. Un ensemble comprenant une unité de prépliage pour traiter une feuille continue de matériau dans la fabrication d'un composant d'un consommable destiné à être utilisé dans ou avec un système de fourniture d'aérosol est également divulgué. L'unité de prépliage comprend au moins une rainure dans une surface de l'unité de prépliage, ladite au moins une rainure s'étendant le long d'un trajet hélicoïdal. Un composant d'un consommable destiné à être utilisé dans ou avec un système de fourniture d'aérosol est également divulgué. Le composant comprend un tube creux formé d'une feuille froncée de matériau, la feuille froncée de matériau s'étendant le long d'un trajet hélicoïdal autour d'un axe longitudinal du composant.
EP24702584.4A 2023-01-19 2024-01-19 Procédés et ensembles pour le traitement d'une feuille continue d'un matériau Pending EP4651742A2 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB2300835.2A GB202300835D0 (en) 2023-01-19 2023-01-19 Methods and assemblies for the processing of a continuous sheet of material
PCT/GB2024/050143 WO2024153943A2 (fr) 2023-01-19 2024-01-19 Procédés et ensembles pour le traitement d'une feuille continue d'un matériau

Publications (1)

Publication Number Publication Date
EP4651742A2 true EP4651742A2 (fr) 2025-11-26

Family

ID=85383208

Family Applications (1)

Application Number Title Priority Date Filing Date
EP24702584.4A Pending EP4651742A2 (fr) 2023-01-19 2024-01-19 Procédés et ensembles pour le traitement d'une feuille continue d'un matériau

Country Status (6)

Country Link
EP (1) EP4651742A2 (fr)
JP (1) JP2026508075A (fr)
KR (1) KR20250138187A (fr)
GB (1) GB202300835D0 (fr)
TW (1) TW202430064A (fr)
WO (1) WO2024153943A2 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20260035225A (ko) * 2023-07-07 2026-03-12 필립모리스 프로덕츠 에스.에이. 개선된 상류 요소

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2001709A (en) * 1932-02-27 1935-05-21 Davidson Glenn Cigarette mouthpiece or the like
DE4340029A1 (de) * 1993-11-24 1995-06-01 Hauni Werke Koerber & Co Kg Anordnung zum Aufbereiten eines Streifens aus Filtermaterial
US7305739B2 (en) * 2004-09-15 2007-12-11 Celanese Acetate, Llc Apparatus for tow opening
JP5877570B2 (ja) * 2012-11-26 2016-03-08 日本たばこ産業株式会社 フィルタシガレット製造方法並びにフィルタ及びフィルタシガレット
GB201812492D0 (en) * 2018-07-31 2018-09-12 Nicoventures Trading Ltd Consumable for use with apparatus for heating aerosolisable material

Also Published As

Publication number Publication date
TW202430064A (zh) 2024-08-01
WO2024153943A3 (fr) 2024-10-10
WO2024153943A2 (fr) 2024-07-25
KR20250138187A (ko) 2025-09-19
JP2026508075A (ja) 2026-03-10
GB202300835D0 (en) 2023-03-08

Similar Documents

Publication Publication Date Title
JP7620044B2 (ja) 喫煙物品に使用するロッド
JP7641256B2 (ja) エアロゾル生成材料ロッドセグメント
EP3469923B1 (fr) Machine de fabrication d'articles de tabac en forme de tige
RU2634858C1 (ru) Ароматизированные стержни для использования в аэрозоль-генерирующих изделиях
EP2893820A1 (fr) Procédé de fabrication d'une cigarette à filtre, filtre, et cigarette à filtre
CN108813721A (zh) 用在气溶胶生成物品中的导热杆
JP6878519B2 (ja) 風味付け部材、風味付け部材の製造装置および風味付け部材の製造方法
WO2016079468A1 (fr) Filtre, et appareil et procédé pour la fabrication de filtres
CN112804891A (zh) 吸烟物品的制造方法
EP4651742A2 (fr) Procédés et ensembles pour le traitement d'une feuille continue d'un matériau
EP4651741A1 (fr) Procédés et ensembles pour la fabrication d'un composant creux destiné à être utilisé dans ou avec un système de fourniture d'aérosol
AU7695587A (en) Fiber separator
CN111542235A (zh) 吸烟制品烟嘴
WO2020141301A1 (fr) Appareil et procédé de production d'une tige de matériau de génération d'aérosol
CN221980049U (zh) 用于气雾产生制品或吸烟制品的元件以及多段式产品
EP4565081A2 (fr) Appareil de fabrication d'un composant destiné à être utilisé dans un système de distribution
WO2026022050A1 (fr) Embout buccal ou élément filtre pour un article de génération d'aérosol
WO1985000092A1 (fr) Filtre a tabac ameliore
AU1822683A (en) Improved tobacco filter

Legal Events

Date Code Title Description
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: UNKNOWN

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: 20250627

AK Designated contracting states

Kind code of ref document: A2

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 ME MK MT NL NO PL PT RO RS SE SI SK SM TR