CLOSURE ASSEMBLY WITH A CAP HAVING CORRUGATED WINGS

Abstract

A closure assembly for a container, comprises a spout (1, 3) and a rotational cap (2) injection moulded of plastic material. The cap comprises a top wall (2a) and a downward depending skirt (2b). The cap has two wings (5), which are integrally moulded of plastic material and extend vertically and outward in a lateral direction over a wing length in substantially opposite directions from an inner end to a tip. The wings each have a base portion, a center portion, a top portion, and opposite front and back sides. At least the center portion of each wing is connected to the skirt of the cap. The base portion and the top portion of each wing are substantially flat. The center portion of each wing comprise at least one corrugation (12, 12, 12) that extends along a part of the length of the wing and forms a groove on both sides of the wing, which grooves of the corrugation, as seen from a sideways view of the wing, together form an alternating waveform, e.g. a sinusoidal shape.

Claims

1. A closure assembly for a container, comprising: a spout having a spout body that is injection moulded of plastic material, said spout body having, above an attachment portion thereof configured to be sealed or sealed to a container, a tubular neck, wherein a product passage extends through the attachment portion and the neck of the spout, said tubular neck having a vertical main axis and forming a mouth at a top end of said product passage allowing to dispense a product from the container, said neck having an exterior side; a rotational cap that is injection moulded of plastic material and that is secured on or is to be secured on said neck of the spout in a closed position of the cap on said neck such that the cap seals the product passage, and the capfor removal of the cap from the neck of the spout by a user to open the product passagebeing adapted to be manually rotated from the closed position in an opening direction; wherein the cap comprises a top wall and a downward depending skirt, said skirt having an interior side, an exterior side, and a lower edge remote from the top wall, wherein the cap has two wings, which are integrally moulded of plastic material and extend vertically and outward in a lateral direction over a wing length in substantially opposite directions from an inner end to a tip, wherein the wings each have a base portion, a center portion, a top portion, and opposite front and back sides, wherein the base portion is located below the center portion and the top portion is located above the center portion, wherein at least the center portion of each wing is connected to the skirt of the cap, wherein the base portion and the top portion of each wing are substantially flat, and wherein the center portion of each wing comprises at least one corrugation that extends along a part of the length of the wing and forms a groove on both sides of the wing, which grooves of the corrugation, as seen from a sideways view of the wing, together form an alternating waveform.

2. Closure assembly according to claim 1, wherein, seen in a view from above, the at least one corrugation in the center portion of the wing tapers off towards the tip of the wing.

3. Closure assembly according to claim 1, wherein the at least one corrugation is substantially parallel to the lateral extending direction of the wings.

4. Closure assembly according to claim 1, wherein the one or more corrugations are perpendicular to the vertical main axis of the tubular neck at least in a closed configuration of the closure assembly.

5. Closure assembly according to claim 1, wherein the one at least one corrugation extends at an angle of less than 60 degrees with respect to the lateral extending direction of the wings.

6. Closure assembly according to claim 1, wherein the at least one corrugation extends at an angle of less than 45 degrees with respect to the lateral extending direction of the wings.

7. Closure assembly according to claim 1, wherein the at least one corrugation tapers off towards the tip of the wing along the length of the wing.

8. Closure assembly according to claim 7, wherein the tapering of the corrugation towards the tip of the wing along the length of the wing is such that the tip of the wing is substantially flat.

9. Closure assembly according to claim 1, wherein the largest height of the one or more corrugations is less than 80% of the largest height of the wing.

10. Closure assembly according to claim 1, wherein the one or more corrugations span the length of the center portion of the wing.

11. Closure assembly according to claim 1, wherein the depth and/or height of the one or more corrugations is largest at the inner part of the wing.

12. Closure assembly according to claim 1, wherein the largest depth and/or height of the one or more corrugations is around 2 to 5 mm.

13. Closure assembly according to claim 1, wherein the center portion of the wings is larger than the top portion and/or the base portion.

14. Closure assembly according to claim 1, wherein the center part of the wing comprises at least two corrugations.

15. Closure assembly according to claim 1, wherein the center part of the wing comprises corrugations formed in opposite directions, wherein the corrugations are offset from a main surface of the wing such that one of the two sides of the wing does not have any protrusions past its surface as a result of the corrugations.

16. Closure assembly according to claim 1, wherein the one or more corrugations as seen from the side of the wing have a sinusoidal shape.

17. Closure assembly according to claim 1, wherein the corrugations as seen from the side of the wing have a shape similar to a square wave.

18. A container provided with a closure assembly according to claim 1.

19. Closure assembly according to claim 2, the at least one corrugation in the center portion of the wing merging with the substantially flat base portion and substantially flat top portion of the wing.

Description

[0038] In the drawings:

[0039] FIG. 1 shows a schematic of a closure assembly with a winged cap,

[0040] FIG. 2 shows a schematic of a closure assembly with an illustrated corrugation in the wings,

[0041] FIGS. 3a, 3b and 3c show a schematic cross-sectional sideview of a wing of a closure assembly,

[0042] FIG. 3d shows a schematic view of a wing without tapering of the corrugation towards the tip of the wing,

[0043] FIGS. 3e and 3f show a schematic view of a wing with illustrated tapering of the corrugation,

[0044] FIG. 4a shows a schematic cross-sectional sideview of a wing with multiple corrugations,

[0045] FIG. 4b, shows a schematic view of a wing with multiple corrugations,

[0046] FIGS. 5a, 5b and 5c show schematic cross-sectional side views of wings of a closure assembly,

[0047] FIGS. 6a and 6b show schematic cross-sectional side views of wings of a closure assembly comprising corrugations with variable heights,

[0048] FIGS. 7a, 7b, 7c, 7d, 7e, 7f and 7g show several schematic cross-sectional side views of wings illustrating various corrugation forms,

[0049] FIG. 8, shows a first practical embodiment of a closure assembly comprising corrugated wings,

[0050] FIG. 9, shows a second practical embodiment of a closure assembly comprising corrugated wings,

[0051] FIG. 10, shows a third practical embodiment of a closure assembly comprising corrugated wings.

[0052] FIG. 1 shows a schematic figure of a closure assembly with a winged cap 2.

[0053] The closure assembly comprises a spout 1 (mostly hidden by the cap 2). The spout 1 has spout body that is injection moulded of plastic material.

[0054] The figure shows an attachment portion 3 of the spout body that is sealed to a container 4.

[0055] Not visible is the tubular neck above the portion 3 as it is hidden under the cap. As known in the art, a product passage extends through the attachment portion and the neck of the spout. The tubular neck has a vertical main axis and forms a mouth at a top end of the product passage allowing to dispense a product from the container 4. The neck has an exterior side.

[0056] The cap 2 is a rotational cap that is injection moulded of plastic material and that illustrated in a position secured on the neck of the spout in a closed position of the cap 2 on the neck such that the cap seals the product passage. The cap 2, for removal of the cap from the neck of the spout by a user to open the product passage, is adapted to be manually rotated from the closed position in an opening direction.

[0057] Generally, the plastic cap 2 comprises a top wall 2a and a downward depending skirt 2b. The skirt has an interior side, an exterior side, and a lower edge remote from the top wall 2a. For example, a tamper-evident structure is provided at the lower edge of the skirt.

[0058] The cap 2 has two wings 5, so a single pair of wings 5. It is illustrated, as preferred, thatin view from abovethe two wings 5 of the cap 2 are generally aligned with a top edge of the pouch 4 when the cap is closed, e.g. before first time opening of the closure.

[0059] The wings 5 are integrally moulded of plastic material with the rest of the cap 2. The wings 5 extend generally vertically and outward in a lateral direction over a wing length in substantially opposite directions from an inner end to a tip of the wing that is remote from the skirt.

[0060] In FIG. 2 the same schematic figure of a closure assembly is shown with the addition of a schematic illustration of a single corrugation 6 according to the invention in a center portion of the wing. The wings 5 are shown to each further include a flat top portion 10a and a flat base portion 10b, respectively above and below the center portion with the corrugation.

[0061] In FIG. 2, the flat top portion 10a and a flat base portion 10b extend in a common vertical plane.

[0062] The point where the wing 5 connects with the skirt cap is referred to as the inner end or junction 7 of the wing.

[0063] The end of the wing furthest away from the skirt 2b cap is referred to as the tip 8 of the wing 5. It is illustrated that the wing tip is a flat wing tip 11 that adjoins the ends of the portion 10a, 10b to form a flat contour along the top, tip, and bottom delineation of the corrugated center portion.

[0064] Furthermore a cross sectional indication line X is shown illustrating a cross section location used for further clarification of the corrugation.

[0065] FIGS. 3a, 3b and 3c show side views of three different embodiments of a wing of the closure assembly, seen in direction of arrow III in FIG. 2.

[0066] The side view 3a illustrates a corrugation 12 in the wing 5 of the closure assembly with an alternating waveform, here a sinusoidal shape, wherein the corrugation 12 does not taper to the edges and the tip of the wing 5. So, both the depth d and the height h of the grooves 12a, 12b associated with the single corrugation 12 are constant over the length of the corrugation.

[0067] In FIG. 3a the flat top portion 10a, and flat bottom portion 10b extend in a common vertical plane.

[0068] In FIG. 3a, the corrugation 12 extends in sinusoidal form relative to a vertical plane.

[0069] FIG. 3b shows a corrugation 12 that tapers off towards the tip 11 of the wing 5. This tapering can be recognized by several cross sections X1, X2 and X3 shown in FIG. 3b, which correspond to various positions along the length of the wing 5 such that a reduced amplitude of the sinusoidal shape at each cross section towards the tip of the wing becomes apparent. As preferred, the greatest depth of the grooves 12a,b is where the center portion adjoins the skirt 2b of the cap.

[0070] In FIG. 3c a corrugation 12 is illustrated that not only tapers towards the tip 11 of the wing 5 but simultaneously tapers towards a lengthwise axis of the wing 5. In the illustrated embodiment, this tapering occurs towards an axis along the middle of the wing in lengthwise direction but an axis under an angle or an axis translated over the width of the wing can be envisioned as alternative embodiments. It is illustrated in the cross-sections X4, X5, X6 that both the depth and the height of the grooves associated with the corrugation reduces from the inner end of the wing 5 towards the tip of the wing.

[0071] FIGS. 3d, 3e and 3f each show a schematic 3-dimensional representation of an embodiment of a corrugated wing according to the invention.

[0072] FIG. 3d matches with FIG. 3a, wherein the sinusoidal shape of the corrugation 12 does not taper off towards the tip of the wing 5.

[0073] FIG. 3e matches with FIG. 3b, wherein the sinusoidal shape of the corrugation 12 can be seen to taper off towards the tip of the wing 5 by a diminishing amplitude of the sinusoidal shape towards the tip of the wing.

[0074] FIG. 3f matches with FIG. 3c, wherein the sinusoidal shape of the corrugation can be seen to taper off towards the tip of the wing as well as towards an axis M along the length of the wing.

[0075] From the schematic 3-dimensional representations of the wing embodiments in FIGS. 3d, 3e and 3f it can also be seen that the wing 5 comprises, in addition to the corrugation 12 or 12, the flat portions 10a, 10b above and below the center portion with the corrugation 12 or 12.

[0076] A tip zone 11 located at the tip of the wing which can, but not necessarily is, substantially flat.

[0077] The corrugations in the wings of FIGS. 2 and 3a, 3b, 3c, 3d, 3e have a single peak and a single valley in the cross-sectional sinusoidal shape of the corrugation 12 and 12.

[0078] The one or more corrugations of the wing center portion comprise a minimum of a one peak and one valley, e.g. in sinusoidal form.

[0079] A corrugated wing can comprise more than a single corrugation, e.g. as is shown in FIGS. 4a and 4b.

[0080] Depending on the direction from which one sees the embodiment of the wing in FIG. 4a either two valleys and one peak or two peaks and one valley is shown thus giving 1.5 (one and a half) corrugation 12 in the wing of FIG. 4a. Three grooves 12a, 12b, and 12c are present.

[0081] FIG. 4b is a 3-dimensional schematic representation of a corrugated wing embodiment similar to the sideways cross-sectional view of 4a with a few notable differences.

[0082] The first notable difference is the axis C1 along the sinusoidal shape in FIG. 4a which coincides with the substantially flat portions 20a, b such that the peaks and valleys of the corrugations are on one side of the axis C1. This as opposed to the axis C2 in FIG. 4b which cuts the corrugation such that the single valley lies below the axis C2 while the two peaks lie above the axis C2 when seen from the direction II along the length of the wing as shown in FIG. 4b.

[0083] From peak to valley and vice versa the corrugations in FIG. 4b transition through the axis C2 whereas the corrugations of FIG. 4a do not.

[0084] The substantially flat portions 24a, b from FIG. 4b still coincide with the axis C2 as is the case with the corrugations of FIG. 4a.

[0085] This illustrates that the corrugations can in principle be lifted out of or sunk into the plane defined by the wing 5. This lifting or sinking of the corrugations can in embodiments be beneficial for production purposes, ease of use, stiffness, storage etc.

[0086] Secondly, another observable difference between the corrugations of FIGS. 4a and 4b are the smooth transitions 26 from the corrugation center portion to the substantially flat base and top portions 20a, b of the wing. These smooth transitions can in embodiments be omitted or introduced. The introduction or omission of which would serve aesthetics, production purposes, or ease of use.

[0087] FIGS. 5a and 5b again show these differences more clearly by setting the cross sectional view of a single corrugation in FIG. 5b alternating through a centerline next to a cross sectional view of 1,5x corrugations lifted out of the plane such that the corrugations do not cross the line coinciding with the edge zones.

[0088] Both corrugations in FIGS. 5a and 5b illustrate the smooth transitions from the corrugations to the edge zones.

[0089] In yet another embodiment similar to the corrugations of FIG. 5a are the 1,5x corrugations seen in FIG. 5c wherein the wing has been curved along the curve 31 such that the edge zones 30 of the wing now smoothly transition into the corrugations without a curvature and help form the peaks of the corrugations.

[0090] FIG. 5c also illustrates that the valley (or peak depending on the viewing direction) does not need to reach or cross the axis C3.

[0091] FIGS. 6a and 6b show that the sinusoidal shape of the corrugations are not required to have equal amplitude and as such can, in embodiments, be varied.

[0092] FIGS. 7a, 7b, 7c, 7d, 7e, 7f and 7g show several schematic cross-sectional side views of wings illustrating various corrugation forms.

[0093] FIG. 7a is included as reference again since it is similar to the right side of FIG. 6a wherein the cross section comprises 1.5 corrugations and wherein the amplitude of at least one the peaks (or valleys depending on viewing direction) is different from the others.

[0094] In FIG. 7b a more discretized sinusoidal waveform is shown, wherein the peaks and valleys of the corrugations are now made with straight lines and angles instead of continuous curves as is the case in FIG. 7a. The valley in between the two peaks of FIG. 7b also crosses the axis that coincides with the two substantially flat edge zones, but in embodiments this valley can coincide or stay on one side of this axis.

[0095] It is then understood that in light of the invention, a sinusoidal waveform is meant to include all types of waveforms such as square waves. More specifically, the term sinusoidal waveform is, in light of the invention, used to describe alternating waveforms.

[0096] FIG. 7c shows a similar discretized sinusoidal waveform as in FIG. 7b although here a single corrugation has been used. The corrugation of FIG. 7c also crosses the axis that coincides with the two substantially flat edge zones as it transitions from a valley to a peak and vice versa.

[0097] In FIG. 7d a combination between the discretized and a normal sinusoidal waveform is introduced and furthermore it is shown that the edge zones are intentionally placed on different heights and no longer share a common coinciding axis.

[0098] It is not necessary to combine these two characteristics into the same embodiment, e.g. discretized vs. normal and non-coinciding edge zones axis. These characteristics are shown in the same embodiment to illustrate various options.

[0099] In FIG. 7e another such characteristic is introduced wherein the period of the waveform (i.e. the length of the wave or how far the wave has been stretched) changes within the waveform such that the peak and the valley of the corrugation are of different widths.

[0100] We also see from FIG. 7e that the discretized waveform has been squished more together resulting in a shape more resembling a square wave. Forming this waveform which more resembles a square wave has an added benefit of increasing the angle of attack of the transitioning line 45 between the valley and the peak of the waveform. Changing the angle of attack of the transitioning line does not require a waveform resembling a square wave but can also be achieved by using the regular sinusoidal waveforms.

[0101] By increasing the angle of attack of the transitioning line 45 created by the transition between the valley and the peak of a corrugation the stiffness in the direction perpendicular to the surface of the wing can be influenced.

[0102] Furthermore the discretized waveform resembling a square wave of FIG. 7e has been provided with smooth transitions instead of sharp edges, although this too is optional and can be omitted in alternative embodiments.

[0103] These characteristics have in FIG. 7e been combined with different amplitudes of the peak and valley and edge zones without a common coinciding axis.

[0104] FIG. 7f shows a combination of a rounded regular sinusoidal waveform with a waveform resembling a square wave of different periods with an optional edge zone coinciding axis illustrated by the dotted line.

[0105] FIG. 7g shows yet another alternating waveform having a triangular or sawtooth shape. Here the waveform comprises 1.5 corrugations wherein the peaks and valleys of the waveform comprise different amplitudes.

[0106] For all waveforms, e.g. like the ones described above, more than 1.5 corrugations can be envisioned to be implemented in alternative embodiments. For example, (1+n0.5) corrugations for n0.

[0107] FIG. 8 shows a first practical embodiment of a cap 2 of the closure assembly wherein the top and bottom portions 10a, 10b along the lengthwise edge of the wings are formed such that the overall wings create a leaflike resemblance.

[0108] One the wings of the closure assembly with its leaflike resemblance can here be seen to comprise an integrally formed strap 40 following a part of the contour of the wing.

[0109] This strap, and several other embodiments of it, has been previously disclosed in WO2020/221801 and is not a necessary or required part of this invention. It is here nonetheless described for the sake of clarity.

[0110] The strap 40 is here integral with the wing at or near the top portion 10a at a first attachment point 43.

[0111] Starting from the first attachment point 43 at or near the top portion 10a of the wing there is provided a cut-out or slot between the strap 40 and the wing 5 along the contour of the tip of the wing and the bottom portion 10b of the wing.

[0112] The strap further comprises a tamper-evident strap part 41 bridging the cut-out towards the wing.

[0113] The strap is integrated with a base part 45 of the cap 2 at a second attachment point 44. The base part 45 of the cap 2 is configured to be mounted on the attachment portion 3 of the closure assembly. The base part 45 also comprising tamper evident cap parts 46 connecting the base part 45 of the cap with the skirt of the cap 2b.

[0114] The tip of the wing with regards to the implementation of the corrugation on the strapped wing is here considered to be located before the strap.

[0115] A part of the tip zone on the strapped wing is here missing as a result of the cut-out 42.

[0116] The (single) corrugation tapers off towards the tip as was illustrated schematically in FIG. 3d.

[0117] The tip zone of the wing here is not flat but still contains the trailing edges of the tapering corrugation.

[0118] FIG. 9 shows a second practical embodiment of a cap 2 of the closure assembly wherein the top portion 10a of the wing overlaps more with the cap of the closure assembly. This can add stiffness and may also serve aesthetic purposes.

[0119] The bottom portions 10b of the wings in FIG. 9 are, in this embodiment, purely there for aesthetic purposes since they do not add stiffness to the wing when no bridging connection is made with the cap body.

[0120] Here one of the wings again comprises a strap 40 following the contour of the second embodiment of the wing. The strapped wing here also comprising a tamper-evident strap part 41, a cut-out 42, a first attachment point 43 and a second attachment point 44.

[0121] The cap 2 comprises a base part 45 and tamper-evident cap parts 46.

[0122] FIG. 10 shows a third practical embodiment of a cap 2 of the closure assembly wherein the wings have been provided with discretized corrugations similar to as was illustrated schematically in FIG. 7b.

[0123] In the practical embodiment of FIG. 10 however the corrugations taper off under an angle from the cap to the tip of the wings, similar to that which was described in the text corresponding to FIG. 3c.

[0124] Just as in the previous two embodiments one of the wings comprises a strap 40. Here following the contour of the third embodiment of the wing. The strapped wing here also comprising a tamper-evident part 41, a cut-out 42, a first attachment point 43 and a second attachment point 44. The cap 2 comprises a base part 45 and tamper-evident cap parts 46.