1. Technical Field
Aspects of the present invention relate to a packaged product, and more particularly relate to a packaged product that includes a container with a consumer medium and a propellant medium stored therein.
2. Background Information
It is known to provide a packaged product that includes a container with a consumer medium and a propellant medium stored therein. In some instances, the container is a barrier type aerosol container, and when the consumer medium and the propellant medium are dispensed from the container, they at least partially mix to form a consumer mixture. The barrier type aerosol container can be advantageous in that it can permit the consumer mixture to have one or more desirable characteristics. The barrier type aerosol container can be problematic, however, in that it can be relatively more expensive and relatively more prone to mechanical failure than other known types of containers, such as non-barrier type aerosol containers. Aspects of the present invention are directed to these and other problems.
According to an aspect of the present invention, a packaged product is provided that includes a container with a consumer medium and a propellant medium stored therein. The container is a non-barrier type aerosol container. The propellant medium includes a hydrocarbon agent.
According to an additional or alternative aspect of the present invention, the container does not include a barrier that fluidly separates the consumer medium from the propellant medium.
According to an additional or alternative aspect of the present invention, the container includes a container reservoir and a container valve; the consumer medium and the propellant medium are stored within the container reservoir; the container valve is selectively actuatable between a closed position and an open position; the consumer medium and the propellant medium stored within the container reservoir cannot pass through the container valve when the container valve is in the closed position; and the consumer medium and the propellant medium stored within the container reservoir can pass through the container valve when the container valve is in the open position.
According to an additional or alternative aspect of the present invention, the volume of the reservoir is between approximately sixty (60) milliliters and three hundred fifty (350) milliliters.
According to an additional or alternative aspect of the present invention, the propellant medium provides a force that causes the consumer medium and the propellant medium to dispense from the container when the container valve is in the open position.
According to an additional or alternative aspect of the present invention, the consumer medium and the propellant medium are operable to mix with one another to form a consumer mixture as they dispense from the container.
According to an additional or alternative aspect of the present invention, the consumer medium is one of a shaving aid medium, a body wash medium, and a sunscreen medium.
According to an additional or alternative aspect of the present invention, the consumer medium is water-based.
According to an additional or alternative aspect of the present invention, the consumer medium is at least substantially free of solvents.
According to an additional or alternative aspect of the present invention, the hydrocarbon agent includes at least one of normal pentane, isopentane, normal butane, isobutane, and propane.
According to an additional or alternative aspect of the present invention, the propellant medium additionally include an organoflourine agent.
According to an additional or alternative aspect of the present invention, the organoflourine agent includes at least one of a difluoroethane compound, a trifluoropropene compound, a tetrafluoropropene compound, and a pentafluoropropane compound.
According to an additional or alternative aspect of the present invention, the propellant medium additionally includes carbon dioxide.
According to an additional or alternative aspect of the present invention, the propellant medium additionally includes air, and the carbon dioxide is provide in an amount that that is significantly greater than any amount of carbon dioxide already present in the air.
According to an additional or alternative aspect of the present invention, the propellant medium includes approximately twenty percent weight by volume of carbon dioxide.
According to an additional or alternative aspect of the present invention, a desired characteristic of the consumer mixture is achieved at least in part because the propellant medium has a particular vapor pressure at a particular temperature.
According to an additional or alternative aspect of the present invention, the propellant medium additionally includes carbon dioxide, and the desired characteristic of the consumer mixture is achieved at least in part because the carbon dioxide is included.
According to an additional or alternative aspect of the present invention, the desired characteristic is one of creaminess, cushion, lubricity, and hydration.
These and other aspects of the present invention will become apparent in light of the drawings and detailed description provided below.
Referring to
The container 12 is a non-barrier type aerosol container. The term “aerosol container” is used herein to mean a container that includes, and is designed to include, an internal pressure source (e.g., a propellant medium) that is operable to dispense a consumer medium from the container. The term “barrier type aerosol container” is used herein to mean an aerosol container that includes a barrier (e.g., a piston, a bag, etc.) that fluidly separates a consumer medium from at least a portion of the internal pressure source. The term “non-barrier type aerosol container” is used herein to mean an aerosol container that does not include a barrier that fluidly separates a consumer medium from an internal pressure source.
The structure of the container 12 can vary. In the embodiment illustrated in
The consumer medium 14 can be a personal care medium (e.g., a shaving aid medium, a body wash medium, a sunscreen medium, etc.), or any other type of medium that is capable of being stored within the container 12 with the propellant medium 16, and that is capable of being dispensed from the container 12. The consumer medium 14 can be in one or more fluidic forms (e.g., in the form of a liquid, in the form of a gel, etc.). In some embodiments, the packaged product 10 additionally includes one or more non-fluidic additives (e.g., beads, microcapsules) that are dispersed within the consumer medium 14. In some embodiments, the consumer medium 14 has foaming and/or post-foaming characteristics. In some embodiments, the consumer medium 14 can be water-based. In some embodiments, the consumer medium 14 can be at least substantially free of solvents. The ingredients of the consumer medium 14, and/or the relative amount of each ingredient can vary. In some embodiments, the ingredients and/or the relative amounts of the ingredients in the consumer medium 14 can be selected so that the consumer medium 14 and/or the consumer mixture 32 has one or more desired characteristics (e.g., creaminess, cushion, lubricity, hydration, etc.). In the embodiment illustrated in
In another embodiment, the consumer medium 14 is a shaving aid medium that includes the following ingredients:
In another embodiment, the consumer medium 14 is a shaving aid medium that includes the following ingredients:
Aloe Vera Powder
In another embodiment, the consumer medium 14 is a body wash medium that includes the following ingredients:
Aloe Vera Powder
The propellant medium 16 includes a hydrocarbon agent, and one or more of an organoflourine agent, air, and carbon dioxide.
The hydrocarbon agent included in the propellant medium 16 can have various ingredients and various relative amounts of each ingredient. In some embodiments, the hydrocarbon agent can include: normal pentane, isopentane, normal butane, isobutane, propane, and mixtures thereof.
In embodiments in which the propellant medium 16 includes an organoflourine agent, the organoflourine agent can have various ingredients and various relative amounts of each ingredient. In some embodiments, the organoflourine agent can include: one or more difluoroethane compounds, one or more trifluoropropene compounds, one or more tetrafluoropropene compounds, one or more pentafluoropropane compounds, and mixtures thereof. Examples of acceptable difluoroethane compounds include: 1,1 difluoroethane; and ethylidene fluoride. Examples of acceptable trifluoropropene compounds include: trans-1-chloro-3,3,3-trifluoropropene. Examples of acceptable tetrafluoropropene compounds include: 2,3,3,3, tetrafluoropropene; and 1,3,3,3 tetrafluoropropene. Examples of acceptable pentafluoropropane compounds include: 1,3-dichloro-1,1,2,2,3-petafluoropropane; 1,1,1,2,2 pentafluoropropane; and 1,1,1,3,3 Pentafluoropropane.
The term “air” is used herein to refer to the mixture of gases that form Earth's atmosphere. In embodiments in which the propellant medium 16 includes air, the air thus includes nitrogen, oxygen, and trace amounts of other gases.
In embodiments in which the propellant medium 16 includes air and carbon dioxide, the carbon dioxide is in addition to any trace amounts of carbon dioxide that may already be present in the air. That is, in embodiments of the propellant medium 16 described herein as including both air and carbon dioxide, the carbon dioxide is provided in addition to the air, and in an amount that that is significantly greater than any amount of carbon dioxide that may already be present in the air.
The ingredients and/or the relative amounts of the ingredients in the propellant medium 16 can vary. In some embodiments, the ingredients and/or the relative amounts of the ingredients in the propellant medium 16 can be selected so that the propellant medium 16 and/or the consumer mixture 32 has one or more desired characteristics (e.g., creaminess, cushion, lubricity, hydration, etc.). In the embodiment illustrated in
In another embodiment, the propellant medium 16 includes the following ingredients:
In another embodiment, the propellant medium 16 includes the following ingredients:
In another embodiment, the propellant medium 16 includes the following ingredients:
In some embodiments, the desired characteristic of the propellant medium 16 and/or the consumer mixture 32 is achieved at least in part because the propellant medium 16 has a particular vapor pressure at a particular temperature, before and/or after the consumer mixture 32 is dispensed from the container 12. In the propellant medium 16 embodiment described in Table 5, the propellant medium 16 has a vapor pressure of approximately seventeen and three tenths (17.3) psi gauge (i.e., approximately one hundred nineteen (119) KPa gauge) at approximately twenty one (21) degrees Celsius (i.e., approximately seventy (70) degrees Fahrenheit). In the propellant medium 16 embodiment described in Table 6, the propellant medium 16 has a vapor pressure of approximately sixteen (16) psi gauge (i.e., approximately one hundred ten and three tenths (110.3) KPa gauge) at approximately twenty one (21) degrees Celsius (i.e., approximately seventy (70) degrees Fahrenheit). In the propellant medium 16 embodiment described in Table 7, the propellant medium 16 has a vapor pressure of approximately twenty three (23) psi gauge (i.e., approximately one hundred fifty nine (159) KPa gauge) at approximately twenty one (21) degrees Celsius (i.e., approximately seventy (70) degrees Fahrenheit). In the propellant medium 16 embodiment described in Table 8, the propellant medium 16 has a vapor pressure of approximately sixteen (16) psi gauge (i.e., approximately one hundred ten and three tenths (110.3) KPa gauge) at approximately twenty one (21) degrees Celsius (i.e., approximately seventy (70) degrees Fahrenheit).
In some embodiments in which the propellant medium 16 includes carbon dioxide, the desired characteristic of the propellant medium 16 and/or the consumer mixture 32 is achieved at least in part because the carbon dioxide is included. In the propellant medium 16 embodiments described in Tables 6 and 8, for example, the inclusion of the carbon dioxide increases the vapor pressure of the propellant medium 16, which in turn increases the creaminess and cushion of the consumer mixture 32. If the propellant medium 16 embodiments described in Tables 6 and 8 excluded the carbon dioxide, the vapor pressure of the propellant medium 16 would be only eight and nine tenths (8.9) psi gauge (i.e., approximately sixty one and four tenths (61.4) KPa gauge) at approximately twenty one (21) degrees Celsius (i.e., approximately seventy (70) degrees Fahrenheit).
The relative amounts of the consumer medium 14 and the propellant medium 16 can vary. In some embodiments, the relative amounts of the consumer medium 14 and the propellant medium 16 can be selected so that the consumer mixture 32 has one or more desired characteristics (e.g., creaminess, cushion, lubricity, hydration, etc.). In the embodiment illustrated in
While several embodiments have been disclosed, it will be apparent to those of ordinary skill in the art that aspects of the present invention include many more embodiments and implementations. Accordingly, aspects of the present invention are not to be restricted except in light of the attached claims and their equivalents. It will also be apparent to those of ordinary skill in the art that variations and modifications can be made without departing from the true scope of the present disclosure. For example, in some instances, one or more features disclosed in connection with one embodiment can be used alone or in combination with one or more features of one or more other embodiments.
Filing Document | Filing Date | Country | Kind |
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PCT/US2014/045895 | 7/9/2014 | WO | 00 |
Number | Date | Country | |
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61844492 | Jul 2013 | US |