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Title: Aerosol ointment compositions for topical use
United States Patent: 6,214,318
Inventors: Osipow; Lloyd I. (Boynton Beach, FL); Marra;
Dorothea C. (Summit, NJ); Spitzer; J. George (Palm Beach, FL)
Assignee: OMS Holdings LLC (New York, NY)
Appl. No.: 281162
Filed: March 30, 1999
Abstract
Aerosol compositions are provided that enhance the therapeutic action
of ointments by producing, upon topical application thereof, a sustained
cooling effect that provides fast relief form pain and itching as well as
a tendency to shrink swollen, inflamed tissue. The compositions contain
oils, thickening agents for the oils, and propellant. Aqueous solutions,
therapeutic ingredients and various adjuvants may also be present. The
specific propellant and the proportion used are selected to provide a
deposit with a temperature of about -5oC. to about +5oC.
In this temperature range, the deposit is cold enough for the required
therapeutic effect, but not so cold as to cause pain or tissue damage. The
choice and proportion of thickening agents used are selected to provide a
deposit that does not flow or spread. Were the deposit to spread, it would
present a large surface area from which propellant present in the deposit
would evaporate rapidly. By avoiding spreading, the propellant evaporates
more slowly and the cooling effect is more sustained.
SUMMARY OF THE INVENTION
The present invention relates to an aerosol composition
consisting essentially of the ingredients of an ointment-liquefied
propellant composition which when expelled from an aerosol container onto
damaged tissue provides a cold ointment which exerts a therapeutic effect
on said tissue in contact therewith.
The cooling effect provided by the expelled composition of this invention
is controlled so as to provide relief of pain for a desirable period of
time but not too cold to cause discomfort or tissue damage.
Thus, an object of this invention is to provide a therapeutic ointment
composition which when expelled from an aerosol container is cold enough
to provide a cooling effect for pain relief but not too cold as to cause
discomfort to damaged tissue to which the ointment is applied, said
ointment also exerting a therapeutic effect on damaged tissue in contact
therewith.
A further object is an ointment that can deliver appropriate medication as
well as a cooling effect where it is applied.
Another object of the invention is to provide a cold ointment for the
temporary relief of hemorrhoids which when applied to the swollen inflamed
tissue provides a cooling effect and quickly relieving pain and itching as
well as effecting shrinking of swollen inflamed tissue.
A still further object of the invention is an ointment for the treatment
of sunburn.
Another object of the invention is a cold anti-itch ointment as well as
one that provides relief from arthritic pain.
Another object of the invention is an antifungal ointment.
An object of this invention is an antibacterial ointment.
An additional object of the invention is to provide a cold ointment that
is initially unctious, but dries to leave a deposit that is neither greasy
nor oily.
More particularly, the present invention relates to novel aerosol
compositions that enhance the therapeutic action of an ointment by
instantly producing, upon topical application thereof, a sustained cooling
effect which provides fast relief from pain and itching as well as a
tendency to shrink swollen, inflamed tissue in advance of the slower
action of any medication present in the ointment, said aerosol composition
consisting essentially of from about 10 to about 60 percent by weight of
ointment ingredients and from about 40 to about 90 percent by weight of
liquefied propellant that is predominantly a non-polar propellant, i.e.,
at least about 80% by weight of the non-polar propellant and where the sum
of the ointment ingredients and the propellant equals 100 percent by
weight of the composition.
In another embodiment, applicants' invention is directed to a therapeutic
aerosol composition for topical use consisting of (a) from about 10 to
about 60 percent by weight of the ingredients of an ointment and (b) from
about 40 to about 90 percent by weight of liquefied propellant, where at
least about 80 percent by weight of the liquefied propellant is a
non-polar propellant or mixture of non-polar propellants selected from the
group consisting of a hydrocarbon propellant and a fluorocarbon propellant
and the sum of ingredients from (a) and (b) equals 100 percent by weight
of the composition, the composition when expelled from an aerosol device
containing the composition depositing as an ointment having a solid or
semi-solid consistency and a temperature between about -5oC.
and +5oC.
Preferably, the ointment ingredients constitute from 35 to 100 percent by
weight of an oil phase and from 0 to about 65 percent by weight of an
aqueous phase based on the weight of the ointment ingredients and the oil
phase of the ointment does not flow below about 35oC. The oil
phase includes ingredients selected from the group consisting of oils, and
oil soluble ingredients, the oil soluble ingredients including adjuvants,
topical therapeutic agents, oil soluble emulsifiers, and thickening agents
for the oils and oil soluble ingredients, where the oils and oil-soluble
ingredients are soluble in the propellant. The aqueous phase includes
water, water-soluble emulsifying agents and may also include topical
therapeutic agents, humectants and alcohols.
Also, the present invention relates to a novel method for enhancing the
therapeutic effect of a solid or semi-solid ointment which consists of
dissolving and/or dispersing:
(a) from about 10 to about 60 percent by weight of an ointment that
contains an oil phase and may contain an aqueous phase in the form of an
emulsion, where the oil phase of the ointment does not flow below about 35oC.,
in
(b) about 40 to about 90 percent by weight of a liquefied propellant that
is at least 80 percent non-polar propellant in an aerosol container,
whereby a solid or semi-solid deposit is formed when a portion of the
composition is expelled and this deposit placed in contact with injured
tissue it provides instant relief from pain and itching as the result of
its sustained cold, thereby enhancing the performance of the ointment with
its slower action medications.
The compositions used in the practice of this invention consist
essentially of an ointment, i.e., a solid or semisolid component,
dissolved and/or dispersed in a liquefied propellant in a suitable aerosol
container. The product is expelled from the aerosol container either as a
deposit confined to a small area or as a spray covering a wider area,
depending on the application. Thus, to relieve hemorrhoids the deposit
should be confined to a small area, while to relieve sunburn a wider area
is likely to be more convenient.
The expelled therapeutic composition for this invention will feel cold due
to the evaporation of the propellant. A substantial portion of the
propellant that is expelled should initially be part of the deposit, so
that there is a continuing cooling action as the propellant gradually
evaporates. It is also important that the deposit have a comparatively
high density and that it be applied thickly.
The temperature of the expelled deposit should be initially in the range
of about -5oC. to about +5oC. In this range the
deposit can have the therapeutic effects that are the objects of this
invention while not being so cold as to cause pain or tissue damage.
Suitable liquefied nonpolar propellants that can be used in aerosol
compositions of this invention to obtain a deposit falling within this
temperature range include the hydrocarbon propellants, e.g., n-butane,
isobutane and propane; the fluorocarbon propellants, e.g.,
1,1-difluoroethane; and mixtures of these liquefied nonpolar propellants.
It has now been found that n-butane is the preferred propellant for use in
the compositions of this invention. n-Butane has a vapor pressure of 17
p.s.i.g. and a boiling point of -0.5oC. and will tend to
maintain the deposit at about that temperature. If the deposit gets much
cooler, further cooling by evaporation will slow substantially. The
deposit will remain in the required temperature range until the proportion
of n-butane in the deposit has become quite low. If a significant amount
of liquefied propellant remains with the deposit when it reaches the
substrate, the temperature of the deposit will approximate the boiling
point of the propellant. Once it reaches that temperature, the rate of
evaporation will slow and absorption of heat from the substrate will
prevent it from falling much lower. One reason for preferring n-butane is
that a deposit containing it is not likely to become objectionally cold.
In contrast, isobutane with a boiling point of -11.7oC. is
likely to be unpleasantly cold, if the deposit contains a significant
amount of liquefied isobutane.
A related reason for preferring n-butane is that it has a lower vapor
pressure than the more widely used liquefied propellants: isobutane and
propane. The lower vapor pressure assures that less propellant will be
lost through evaporation as the exudate travels from the aerosol valve to
the substrate upon which it is to be deposited.
However, for those products that are likely to be used at lower ambient
temperatures, where n-butane does not provide sufficient pressure to expel
the composition properly, it is advantageous to combine n-butane with a
lesser amount of a higher vapor pressure propellant, e.g., isobutane,
propane, 1,1-difluorethane or dimethyl ether.
However, higher vapor pressure (lower boiling point) propellants can be
used under conditions when little if any liquefied propellant remains with
the deposit when it reaches the substrate so that the temperature of the
deposit is in the required range of -5oC. to +5oC.
This can be done by reducing the percent propellant in the composition. A
beneficial feature is that the higher the vapor pressure (lower the
boiling point) of the propellant, the greater the tendency to flash off
before reaching the substrate. Nonetheless, in general, the higher vapor
pressure propellants are not as effective as n-butane, the preferred
propellant.
The distance of the spray path as well as the characteristics of the
package play a role in determining how much propellant will be lost as the
exudate travels to the substrate upon which it will be deposited. It is
evident that the longer the spray path, the more propellant will be lost
by evaporation before reaching the substrate and the less propellant will
be available for sustained cooling. It has also been found that
restrictions in the delivery system also promote early evaporation of
propellant by reducing the flow rate of the exudate.
However, with some compositions a restricted delivery system is
beneficial, since it results in a heavier-bodied deposit. Also, where
layering of the composition occurs within the container, it is
advantageous to employ a capillary dip tube, i.e., a dip tube with an
inside diameter of 1 mm., to minimize the amount of separated material
that is released after first shaking the container. Shaking is not
effective in mixing material that is in the dip tube.
The dynamic physical characteristics of the composition play an important
role in determining the amount of propellant in the deposit and the amount
of time it will remain in the deposit to provide sustained cooling. The
aerosol compositions of this invention consist of the ingredients of an
ointment that generally contains a thickening agent in a solution of an
oil, and often one or more medicinal ingredients, dispersed and/or
dissolved in an appropriate propellant so that the expelled deposit is
initially in the range of about -5oC. to about +5oC.
As product is expelled there is some loss of propellant accompanied by
cooling of the exudate. If the deposit had been a liquid rather than an
ointment, it would have spread rapidly whereby expiration of the
propellant would occur too quickly and one would not obtain the desired
sustained cooling effect. The compositions of this invention deposit as
solids or semi-solids. The thickness of the deposit helps to provide
sustained therapeutic cooling.
It has been found that the oil phase of the ointment should have a flow
temperature that is at least about 35oC.; otherwise, the
deposit will liquefy readily and not provide sufficient cooling. It is
advantageous that the flow temperature of the oil phase of the ointment
not exceed about 60oC., otherwise manufacture becomes more
difficult.
The preferred compositions contained in an appropriate aerosol container
in accordance with this invention contain from about 10 to about 60
percent by weight of the ingredients of an ointment and from about 40 to
about 90 percent by weight of a propellant that is at least 80% by weight
n-butane. Also preferred are aerosol compositions of this invention that
consist essentially of from about 50% to about 75% by weight of a
non-polar propellant or mixture of non-polar propellants and 25% to 50% by
weight of ingredients of an ointment.
Claim 1 of 29 Claims
We claim:
1. A therapeutic aerosol composition for topical use consisting of:
(a) from about 10 to about 60 percent by weight of the following
ingredients:
oils selected from the group consisting of mineral oils, vegetable oils,
silicone oils and synthetic oils;
thickening agents for the oils in an amount sufficient to thicken the oils
to a non-flowable state below about 35oC., said thickening
agents being selected from the group consisting of mineral waxes, animal
and vegetable waxes, synthetic waxes, polymers and metallic soaps; and
optionally ingredients selected from the group consisting of an aqueous
solution, adjuvants, topical therapeutic agents and emulsifiers, and
(b) from about 40 to about 90 percent by weight of liquefied propellant,
where at least about 80 percent by weight of the liquefied propellant is a
non-polar propellant or mixture of non-polar propellants selected from the
group consisting of hydrocarbon and fluorocarbon propellants, and the sum
of (a) and (b) equals 100 percent by weight of the composition, the
composition when expelled from an aerosol device depositing as an ointment
having a solid or semi-solid consistency containing a substantial
proportion of said propellant, whose evaporation is restrained by the
solid or semi-solid nature of the deposit, thereby upon topical
application producing a sustained cooling effect at a temperature between
about -5oC. and +5oC.
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