METHOD OF MAKING AN AEROSOL CONTAINER
20190152683 ยท 2019-05-23
Assignee
Inventors
- Tapan Y. Patel, JR. (Nashua, NH, US)
- Thomas E. Nahill (Amherst, NH, US)
- Stephen R. Guerin (Milford, NH, US)
Cpc classification
B29C49/4205
PERFORMING OPERATIONS; TRANSPORTING
B65D1/0246
PERFORMING OPERATIONS; TRANSPORTING
B29C49/56
PERFORMING OPERATIONS; TRANSPORTING
B29C49/00
PERFORMING OPERATIONS; TRANSPORTING
B29C49/20
PERFORMING OPERATIONS; TRANSPORTING
Y10T29/4998
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B65D41/0471
PERFORMING OPERATIONS; TRANSPORTING
International classification
B65D41/04
PERFORMING OPERATIONS; TRANSPORTING
B29C49/20
PERFORMING OPERATIONS; TRANSPORTING
B65D1/02
PERFORMING OPERATIONS; TRANSPORTING
B29C49/56
PERFORMING OPERATIONS; TRANSPORTING
B29C49/42
PERFORMING OPERATIONS; TRANSPORTING
Abstract
An aerosol container includes a main body portion that is constructed and arranged to withstand aerosol pressurization within a range that is about 90-180 prig and a threaded finish portion that is unitary with the main body portion. The threaded finish portion has at least one helical thread, a support ledge beneath the helical thread and a secondary flange that is positioned beneath the support ledge. The secondary flange has an outer circumference that is noncircular in at least one location, whereby it may be engaged during a capping operation to prevent rotation of the container during capping. A method of making an aerosol container in which a preform is capped before the blow molding process is also disclosed.
Claims
1. A method of assembling an aerosol container, comprising: providing a container having a threaded finish portion having at least one helical thread, a support ledge positioned beneath the threaded finish portion, the support ledge having at least one position-registering recess defined therein, and a secondary flange positioned beneath the support ledge, the secondary flange having an outer circumference that is noncircular in at least one location; preventing rotation of the container by engaging the noncircular portion of the secondary flange; screwing at least a portion of an aerosol dispensing closure assembly onto the threaded finish portion at a torque that is within a range of about 15 in-lbs to about 50 in-lbs; and pressurizing the container with an aerosol mixture having an aerosol propellant.
2. The method according to claim 1, wherein the support ledge has a first maximum outer diameter and the secondary flange has a second maximum outer diameter, and wherein the second maximum outer diameter is substantially the same as the first maximum outer diameter.
3. The method according to claim 1, wherein the support ledge has a first maximum outer diameter and the secondary flange is a second maximum outer diameter, and wherein the second maximum outer diameter is not substantially greater than the first maximum outer diameter.
4. The method according to claim 1, wherein the secondary flange has at least one substantially flat portion defined thereon.
5. The method according to claim 1, further comprising securing the aerosol dispensing closure against rotation with respect to the container by applying a securement means.
6. The method according to claim 1, wherein the threaded finish portion and the main body portion are fabricated from a material comprising polyethylene terephthalate.
7. The method according to claim 1, wherein a space is defined between the support ledge and the secondary flange, and the space has a minimum vertical dimension that is at least about 1 mm.
8. The method according to claim 7, wherein the minimum vertical dimension is at least about 1.5 mm.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT(S)
[0025] Referring now to the drawings, wherein like reference numerals designate corresponding structure throughout the views, and referring in particular to
[0026] Plastic aerosol container 10 is preferably fabricated from a plastic material such as polyethylene terephthalate (PET), polyethylene naphthalate (PEN), acrilonitrile (AN), polycarbonate (PC), polyamide (Nylon), or a blend containing some combination of the same from a plastic preform using a conventional blow molding process such as the reheat stretch blow molding process. In the preferred embodiment, container 10 is fabricated from a high intrinsic viscosity polyethylene terephthalate material, which most preferably has an intrinsic viscosity that is substantially within a range of about 0.76 to about 0.95.
[0027] Container 10 preferably has an average wall thickness in the main body portion 12 that is substantially within a range of about 0.018 inch to about 0.022 inch, permitting it to withstand aerosol pressures.
[0028] The aerosol container 10 further includes a threaded finish portion 14 that is unitary with the main body portion 12 and that has at least one helical thread 16 defined thereon for receiving an aerosol dispensing closure. Finish portion 14 further includes a support ledge 18 beneath the helical thread 16, which is used to help convey the container 10 during manufacture and filling. The support ledge 18 has a first maximum outer diameter D.sub.L, as is best shown in
[0029] The support ledge 18 is preferably constructed so that it has a substantially circular circumference as viewed in top plan. In the preferred embodiment, the outer circumference of the support ledge 18 includes a pair of small recesses 24, which are used for registering the position of the container 10 during the capping process, in which an aerosol dispensing closure is applied to the finish portion 14.
[0030] The threaded finish portion 14 further includes at least one secondary flange 20, which is positioned beneath the support ledge 18. The secondary flange 20 is preferably constructed so that it has an outer circumference that is noncircular in at least one location, so that it may be engaged during a capping operation to prevent rotation of the container 10 during capping.
[0031] The secondary flange 20 in the preferred embodiment is fabricated using an injection molding process together with the rest of a plastic preform 50, shown in
[0032] In an alternative embodiment of the invention, shown in
[0033] In another alternative embodiment of the invention, anti-rotation features could be incorporated into the support ledge of the finish portion without the provision of a secondary flange. For example, the support ledge could be provided with two or more flat surfaces, grooves or notches on the underside of the support ledge or one or more lugs or notches on the top surface of the support ledge.
[0034] The secondary flange 20 is preferably constructed so as to have a second maximum outer diameter D.sub.S, which is not substantially greater than the first maximum outer diameter D.sub.L of the support ledge 18. Preferably, the second maximum outer diameter D.sub.S of the secondary flange 20 is substantially the same as the first maximum outer diameter D.sub.1 of the support ledge 18.
[0035] Preferably, the secondary flange 20 has at least one substantially flat portion defined thereon that may be engaged by a capping machine in order to prevent relative rotation of the container 10 with respect to the capping machine during the capping process. As is best shown in
[0036] An annular space 28 is defined between the support ledge 18 and the secondary flange 20. Annular space 28 has a minimum vertical dimension H.sub.S that is preferably at least about 1 mm, and that is more preferably at least about 1.5 mm.
[0037] The aerosol container assembly further includes an aerosol dispensing closure assembly 40, which is diagrammatically shown in
[0038] The aerosol dispensing closure assembly 40 also preferably includes a metallic insert 44 mounted on the collar 42 having a central opening in which an aerosol dispensing valve 46 is positioned.
[0039] A method of assembling an aerosol container assembly according to the preferred embodiment of the invention is diagrammatically shown in
The collar 42 of the aerosol dispensing closure assembly 40 is then screwed onto the threaded finish portion 14 using a commercial capping machine. During the capping process, the container 10 is secured against rotation relative to the capping machine by engagement of a portion of the capping machine with the noncircular portion of the secondary flange 20. The collar 42 of the aerosol dispensing closure 40 is preferably screwed onto the threaded finish portion at a torque that is substantially within a range of about 15 in-lbs to about 50 in-lbs. The container 10 is then filled with product, after which the metallic insert 44 of the aerosol dispensing closure assembly 40 is applied to the collar and the container is pressurized with an aerosol mixture at a range of pressurization that is substantially between about 50 psig to about 300 psig, and more preferably substantially within a range of about 90 psig to about 180 psig using known aerosol pressurization processes and equipment.
[0040] The aerosol mixture preferably includes a propellant, which could be a liquefied gas propellant or a compressed or soluble gas propellant. Liquefied gas propellants that could be used include hydrocarbon propellants such as propane, isobutene, normal butane, isopentane, normal pentane and dimethyl ether, and hydrofluorocarbon propellants such as difluoroethane (HFC-152a) and tetrafluoroethane (HFC-134a). Compressed and soluble gas propellants that could be used include carbon dioxide (C02), nitrous oxide (N20), nitrogen (N2) and compressed air.
[0041] In an alternative embodiment that is depicted in
[0042] During this preform capping process, the preform 50 is secured against rotation relative to the capping machine by engagement of a portion of the capping machine with the noncircular portion of the secondary flange 20, shown in
[0043] The container 10 is then blow molded and filled with product, including the aerosol mixture. The container 10 is subsequently pressurized.
[0044] It is to be understood, however, that even though numerous characteristics and advantages of the present invention have been set forth in the foregoing description, together with details of the structure and function of the invention, the disclosure is illustrative only, and changes may be made in detail, especially in matters of shape, size and arrangement of parts within the principles of the invention to the full extent indicated by the broad general meaning of the terms in which the appended claims are expressed.