NAPPA MARIO JOSEPH (US)
SIEVERT ALLEN CAPRON (US)
SWEARINGEN EKATERINA N (US)
CREAZZO JOSEPH ANTHONY (US)
NAPPA MARIO JOSEPH (US)
SIEVERT ALLEN CAPRON (US)
SWEARINGEN EKATERINA N (US)
| WO2004037913A2 | 2004-05-06 | |||
| WO2005099718A1 | 2005-10-27 | |||
| WO2006101882A2 | 2006-09-28 |
| US20040256594A1 | 2004-12-23 | |||
| US3884828A | 1975-05-20 | |||
| US5900185A | 1999-05-04 | |||
| US6610250B1 | 2003-08-26 | |||
| US20050233934A1 | 2005-10-20 | |||
| DE2534315A1 | 1976-02-12 |
Claims
We Claim:
1. A propellant comprising at least one fluorocarbon or hydrofluorocarbon selected from the group consisting of:
(i) a hydrofluorocarbon having the formula E- or Z-R 1 CH=CHR 2 , wherein R 1 and R 2 are, independently, Ci to Cβ perfluoroalkyl groups; and
a fluorocarbon or hydrofluorocarbon selected from the group consisting of CF 3 CF=CHF, CF 3 CH=CF 2 , CHF 2 CF=CF 2 , CHF 2 CH=CHF, CF 3 CF=CH 2 , CF 3 CH=CHF, CH 2 FCF=CF 2 , CHF 2 CH=CF 2 , CHF 2 CF=CHF, CHF 2 CF=CH 2 , CF 3 CH=CH 2 , CH 3 CF=CF 2 , CH 2 FCHCF 2 , CH 2 FCF=CHF, CHF 2 CH=CHF, CF 3 CF=CFCF 3 , CF3CF 2 CF=CF 2 , CF 3 CF=CHCF 3 , CF 3 CF 2 CF=CH 2 , CF 3 CH=CHCF 3 , CF 3 CF 2 CH=CH 2 , CF 2 =CHCF 2 CF 3 , CF 2 =CFCHFCF 3 , CF 2 =CFCF 2 CHF 2 , CHF 2 CH=CHCF 3 , (CFs) 2 C=CHCF 3 , CF 3 CF=CHCF 2 CF 3 , CF 3 CH=CFCF 2 CF 3 , (CFs) 2 CFCH=CH 2 , CF 3 CF 2 CF 2 CH=CH 2 , CF 3 (CF 2 ) 3 CF=CF 2 , CF 3 CF 2 CF=CFCF 2 CF 3 , (CF 3 ) 2 C=C(CF 3 ) 2 , (CF S ) 2 CFCF=CHCF 3 , CF 2 =CFCF 2 CH 2 F, CF 2 =CFCHFCHF 2 , CH 2 =C(CFs) 2 , CH 2 CF 2 CF=CF 2 , CH 2 FCF=CFCHF 2 , CH 2 FCF 2 CF=CF 2 , CF 2 =C(CF 3 )(CH 3 ), CH 2 =C(CHF 2 )(CF 3 ), CH 2 =CHCF 2 CHF 2 , CF 2 =C(CHF 2 )(CH 3 ), CHF=C(CF 3 )(CHs), CH 2 =C(CHF 2 ) 2 , CF 3 CF=CFCHs, CH 3 CF=CHCF 3 , CF 2 =CFCF 2 CF 2 CF 31 CHF=CFCF 2 CF 2 CFS, CF 2 =CHCF 2 CF 2 CFS 1 CF 2 =CFCF 2 CF 2 CHF 2 , CHF 2 CF=CFCF 2 CF 31 CF S CF=CFCF 2 CHF 2 , CF 3 CF=CFCHFCFs, CHF=CFCF(CF 3 ) 2l CF 2 =CFCH(CF 3 ) 2 , CFsCH=C(CFs) 2 , CF 2 =CHCF(CFs) 2 , CH 2 =CFCF 2 CF 2 CFs, CHF=CFCF 2 CF 2 CHF 21 CH 2 =C(CF 3 )CF 2 CF 3 , CF 2 =CHCH(CFs) 2 , CHF=CHCF(CFs) 2 , CF 2 =C(CF 3 )CH 2 CF 3 ,
CH 2
=CFCF 2
CF 2
CHF 21
CF 2
=CHCF 2
CH 2
CF 31
CF 3
CF=C(CF 3
)(CH 3
), CH 2
=CFCH(CF 3
) 2
, CHF=CHCH(CF 3
) 2
, CH 2
FCH=C(CFs) 2
, CH 3
CF=C(CFs) 2
, CH 2
=CHCF 2
CHFCF 3
, CH 2
C(CF 3
)CH 2
CF 3
, (CFs) 2
C=CHC 2
F 5
, (CF3) 2
CFCF=CHCF 3
, CH 2
=CHC(CFS) 31
(CFS) 2
C=C(CH 3
)(CFS), CH 2
=CFCF 2
CH(CFS) 21
CF 3
CF=C(CH 3
)CF 2
CF 31
CF 3
CH=CHCH(CF 3
) 2
, CH 2
=CHCF 2
CF 2
CF 2
CHF 2)
(CFS) 2
C=CHCF 2
CH 31
CH 2
=C(CF 3
)CH 2
C 2
F 5
, CH 2
=CHCH 2
CF 2
C 2
F 51
CH 2
=CHCH 2
CF 2
C 2
F 5
,
CHF 2
CBr=CFC 2
F 5
, CF 2
=CBrCHFC 2
F 5
,
2. The propellant of claim 1 , wherein R 1 and R 2 are, independently, CF 3 , C 2 F 5 , CF 2 CF 2 CF 3 , CF(CF 3 ) 2 , CF 2 CF 2 CF 2 CF 3 , CF(CF 3 )CF 2 CF 3 , CF 2 CF(CFa) 2 , C(CF 3 ) 3 , CF 2 CF 2 CF 2 CF 2 CF 3 , CF 2 CF 2 CF(CF 3 ) 2 , C(CFs) 2 C 2 F 5 , CF 2 CF 2 CF 2 CF 2 CF 2 CF 3 , CF(CF 3 ) CF 2 CF 2 C 2 F 5 , or C(CFs) 2 CF 2 C 2 F 5 .
3. The propellant of claim 1 , wherein the hydrofluorocarbon is CF 3 CH=CHCF 3 , CF 3 CH=CHC 2 F 5 , CF 3 CH=CHCF 2 C 2 F 5 , CF 3 CH=CHCF(CF 3 ) 2 , C 2 F 5 CH=CHC 2 F 5 , CF 3 CH=CH(CF 2 ) 3 CF 3) CF 3 CH=CHCF 2 CF(CFS) 2 , CF 3 CH=CHCF(CF 3 )C 2 F 5 , CF 3 CH=CHC(CF 3 ) 3 , C 2 F 5 CH=CHCF 2 C 2 F 5 , C 2 F 5 CH=CHCF(CFs) 2 , CF 3 CH=CH(CF 2 ) 4 CFs, CF 3 CH=CHCF 2 CF 2 CF(CF 3 ) 2 , CF 3 CH=CHC(CFs) 2 C 2 F 5 , C 2 F 5 CH=CH(CF 2 ) 3 CF 3 , C 2 FSCH=CHCF 2 CF(CFS) 2 ,
C 2 F 5 CH=CHCF(CF 3 )C 2 F 5 , C 2 F 5 CH=CHC(CF 3 )S, C 2 F 5 CF 2 CH=CHCF 2 C 2 F 5 , (CF 3 ) 2 CFCH=CHCF(CF 3 ) 2 , C 2 F 5 CH=CHCF(CF 3 ) 2 , CF 3 CH=CH(CF 2 ) 5 CF 3 , CF 3 CH=CHCF(CF 3 )(CF 2 ) 2 C 2 F 5 , CF 3 CH=CHC(CFS) 2 CF 2 C 2 F 5 , C 2 F 5 CH=CH(CF 2 ) 4 CF 3( C 2 F 5 CH=CHCF 2 CF 2 CF(CFS) 2 , C 2 F 5 CH=CHC(CFS) 2 C 2 F 5 , C 2 F 5 CF 2 CH=CH(CF 2 ) 3 CFs, C 2 F 5 CF 2 CH=CHCF 2 CF(CFS) 21 C 2 F 5 CF 2 CH=CHCF(CF 3 )C 2 F 5 , C 2 F 5 CF 2 CH=CHC(CFs) 3 , (CF 3 ) 2 CFCH=CH(CF 2 ) 3 CFs, (CF 3 ) 2 CFCH=CHCF 2 CF(CF 3 ) 2 , (CF 3 ) 2 CFCH=CHCF(CF 3 )C 2 Fs, (CF 3 ) 2 CFCH=CHC(CF 3 ) 3 , C 2 F 5 CH=CH(CF 2 ) 5 CFs, C 2 F 5 CH=CHCF(CF 3 )(CF 2 ) 2 C 2 Fs, C 2 F 5 CH=CHC(CFs) 2 CF 2 C 2 F 5 , C 2 FsCF 2 CH=CH(CF 2 ) 4 CF 3 , C 2 F 5 CF 2 CH=CHCF 2 CF 2 CF(CF 3 ) 2 , C 2 F 5 CF 2 CH=CHC(CF 3 ) 2 C 2 F 5 , (CF 3 ) 2 CFCH=CH(CF 2 ) 44 CF 3 , (CF 3 ) 2 CFCH=CHCF 2 CF 2 CF(CF 3 ) 2 , (CFS) 2 CFCH=CHC(CFS) 2 C 2 F 5 ,
CF 3
(CF 2
)3CH=CH(CF 2
)3CF3, CF3(CF2)3CH=CHCF2CF(CF3) 2,
4. The propellant of claim 1 , wherein the propellant consists essentially of the fluorocarbon or hydrofluorocarbon.
5. The propellant of claim 4, wherein the propellant consists of the fluorocarbon or hydrofluorocarbon.
6. A sprayable composition comprising the propellant of claim 1.
7. The sprayable composition of claim 6, wherein the sprayable composition is an aerosol.
8. The sprayable composition of claim 7, wherein the aerosol has a vapor pressure in a range of from about 138 to 621 kPa at 21 0 C.
9. The sprayable composition of claim 6, wherein the sprayable composition is a cleaner, duster, personal care product, household product, automotive product, or medicament.
10. The sprayable composition of claim 9, wherein the personal care product is a deodorant, perfume, or hair spray.
11. The sprayable composition of claim 9, wherein the household product is a wax, polish, pan spray, room freshener, or household insecticide.
12. The sprayable composition of claim 9, wherein medicament is a metered dose inhaler.
13. The sprayable composition of claim 9, wherein the medicament further comprises a beta-agonist or a corticosteroid.
14. The sprayable composition of claim 9, wherein the automotive product is a cleaner or polisher.
15. An aerosol dispensing system comprising the propellant of claim 1.
16. A sealed container comprising the aerosol dispensing system of claim 15.
17. The sealed container of claim 16, further comprising an aerosol dispensing valve.
18. A process for producing aerosol products comprising the step of adding a composition of claim 1 to active ingredients in an aerosol container, wherein said composition functions as a propellant.
19. A process for producing aerosol products comprising the step of adding a composition of claim 3 to active ingredients in an aerosol container, wherein said composition functions as a propeiiant. |
TITLE
AEROSOL PROPELLANTS COMPRISING
UNSATURATED FLUOROCARBONS
CROSS REFERENCE TO RELATED APPLICATION(S) This application claims the benefit of priority to US Provisional Application No. 60/732,292, the complete disclosure of which is incorporated herein by reference.
FIELD OF THE INVENTION
Disclosed herein are aerosol propellant compositions comprising unsaturated fluorocarbons or unsaturated hydrofluorocarbons. Also disclosed is the use of these compositions in preparing aerosol products.
BACKGROUND OF THE INVENTION In the early 1970s, concern began to be expressed that the stratospheric ozone layer (which provides protection against penetration of the Earth's atmosphere by ultraviolet radiation) was being depleted by chlorine atoms introduced to the atmosphere from the release of chlorofluorocarbons. These chlorofluorocarbons were used as propellants in aerosols, as blowing agents for foams, as refrigerants and as cleaning/drying solvent systems. Because of the great chemical stability of fully halogenated chlorofluorocarbons, according to the ozone depletion theory, these compounds do not decompose in the Earth's troposphere but reach the stratosphere where they slowly degrade liberating chlorine atoms which in turn react with the ozone.
Concern reached such a level that in 1978 the U.S. Environmental Protection Agency (EPA) placed a ban on nonessential uses of fully halogenated chlorofluorocarbons (CFC) as aerosol propellants, and in 1995 banned nonessential uses of hydrochlorofluorocarbon (HCFC) propellants.
There is also a demand for aerosol propellents which have significantly less photochemical reactivity than hydrocarbons that contribute to the formation of ambient ozone and ground level smog. These compounds are typically referred to as low-VOC (volatile organic compound) or non-VOC.
The disclosure herein relates to the discovery of compositions, which include unsaturated fluorocarbons and hydrofluorocarbons. These compositions have zero ozone depletion potential (ODP), low global warming potential (GWP) and are lower VOC than hydrocarbons. These compositions are useful as pure components or in mixtures. These compositions are used as aerosol propellants.
SUMMARY OF THE INVENTION One aspect is for a propellant comprising at least one fluorocarbon or hydrofluorocarbon selected from the group consisting of:
(i) a hydrofluorocarbon having the formula E- or Z-R 1 CH=CHR 2 , wherein R 1 and R 2 are, independently, C^ to Ce perfluoroalkyl groups; or (ii) a fluorocarbon or hydrofluorocarbon selected from the group consisting of CF 3 CF=CHF, CF 3 CH=CF 2 , CHF 2 CF=CF 2 ,
CHF 2 CH=CHF, CF 3 CF=CH 2 , CF 3 CH=CHF, CH 2 FCF=CF 2 , CHF 2 CH=CF 2 , CHF 2 CF=CHF, CHF 2 CF=CH 2 , CF 3 CH=CH 2 , CH 3 CF=CF 2 , CH 2 FCHCF 2 , CH 2 FCF=CHF, CHF 2 CH=CHF, CF 3 CF=CFCF 3 , CF3CF 2 CF=CF 2 , CF 3 CF=CHCF 3 , CF 3 CF 2 CF=CH 2 , CF 3 CH=CHCF 3 , CF 3 CF 2 CH=CH 2 ,
CF 2 =CHCF 2 CF 3 , CF 2 =CFCHFCF 3 , CF 2 =CFCF 2 CHF 2 , CHF 2 CH=CHCF 3 , (CF 3 ) 2 C=CHCF 3 , CF 3 CF=CHCF 2 CF 3 , CF 3 CH=CFCF 2 CF 3 , (CF 3 ) 2 CFCH=CH 2 , CF 3 CF 2 CF 2 CH=CH 2 , CF 3 (CF 2 ) 3 CF=CF 2 , CF 3 CF 2 CF=CFCF 2 CF 3 , (CF 3 ) 2 C=C(CF 3 ) 2 , (CF 3 ) 2 CFCF=CHCF 3 , CF 2 =CFCF 2 CH 2 F, CF 2 =CFCHFCHF 2 ,
CH 2 =C(CFs) 2 , CH 2 CF 2 CF=CF 2 , CH 2 FCF=CFCHF 2 , CH 2 FCF 2 CF=CF 2 , CF 2 =C(CF 3 )(CH 3 ), CH 2 =C(CHF 2 )(CF 3 ), CH 2 =CHCF 2 CHF 21 CF 2 =C(CHF 2 )(CH 3 ), CHF=C(CF 3 )(CH 3 ),
CH 2 =C(CHF 2 )2, CF 3 CF=CFCH 3 , CH 3 CF=CHCF 3 , CF 2 =CFCF 2 CF 2 CF 31 CHF=CFCF 2 CF 2 CF 3 , CF 2 =CHCF 2 CF 2 CF 31 CF 2 =CFCF 2 CF 2 CHF 2 , CHF 2 CF=CFCF 2 CF 31 CF 3 CF=CFCF 2 CHF 2 ,
5 CF 3
CF=CFCHFCF 3
,
CF 3 CH=C(CFs) 2 , CF 2 =CHCF(CF 3 ) 2l CH 2 =CFCF 2 CF 2 CF 3 , CHF=CFCF 2 CF 2 CHF 21 CH 2 =C(CF 3 )CF 2 CF 31 CF 2 =CHCH(CFg) 2 , CHF=CHCF(CFs) 2 , CF 2 =C(CF 3 )CH 2 CF 3 , CH 2 =CFCF 2 CF 2 CHF 27 CF 2 =CHCF 2 CH 2 CF 3 ,
10 CF 3 CF=C(CF 3 )(CH 3 ), CH 2 =CFCH(CFs) 2 , CHF=CHCH(CF 3 ) 2 ,
CH 2
FCH=C(CFs) 2
, CH 3
CF=C(CFs) 2
, CH 2
=CHCF 2
CHFCF 3
, CH 2
C(CF 3
)CH 2
CF 3
, (CFs) 2
C=CHC 2
F 5
, (CF3) 2
CFCF=CHCF 3
, CH 2
=CHC(CF 3
)S 1
(CFS) 2
C=C(CH 3
)(CFS) 1
15 CF 3 CH=CHCH(CFS) 2 , CH 2 =CHCF 2 CF 2 CF 2 CHF 2 ,
(CFS) 2 C=CHCF 2 CH 31 CH 2 =C(CF 3 )CH 2 C 2 F 5 , CH 2 =CHCH 2 CF 2 C 2 Fs, CH 2 =CHCH 2 CF 2 C 2 Fs, CFsCF 2 CF=CFC 2 H 5 , CH 2 =CHCH 2 CF(CFS) 21 CF 3 CF=CHCH(CFs)(CH 3 ), (CF 3 ) 2 C=CFC 2 H5, cyclo-
20 CF 2 CF 2 CF 2 CH=CH-, cyclo-CF 2 CF 2 CH=CH-,
CF 3 CF 2 CF 2 C(CHS)=CH 2 , CF 3 CF 2 CF 2 CH=CHCH 3 , cyclo- CF 2 CF 2 CF=CF-, CyCIo-CF 2 CF=CFCF 2 CF 2 -, cyclo- CF 2 CF=CFCF 2 CF 2 CF 21 CF 3 CF 2 CF 2 CF 2 CH=CH 2 , CF 3 CH=CHCF 2 CF 31 CF 2 CF 2 CH=CHCF 2 CFS,
25 CF 3 CH=CHCF 2 CF 2 CF 3 , CF 3 CF=CFC 2 F 5 ,
CFSCF=CFCF 2 CF 2 C 2 F 5 , CF 3 CF 2 CF=CFCF 2 C 2 FS, CF 3 CH=CFCF 2 CF 2 C 2 FS 1 CF 3 CF=CHCF 2 CF 2 C 2 F 5 , CF 3 CF 2 CH=CFCF 2 C 2 F 51 CF 3 CF 2 CF=CHCF 2 C 2 F 5 , C 2 F 5 CF 2 CF=CHCH 3 , C 2 F 5 CF=CHCH 3 , (CF 3 ) 2 C=CHCH 3 ,
30 CF 3 C(CHs)=CHCF 3 , CHF=CFC 2 F 5 , CHF 2 CF=CFCFs 1
(CFs) 2 C=CHF, CH 2 FCF=CFCF 3 , CHF=CHCF 2 CF 3 , CHF 2 CH=CFCF 3 , CHF=CFCHFCF 3 , CF 3 CH=CFCHF 2 , CHF=CFCF 2 CHF 2 , CHF 2 CF=CFCHF 2 , CH 2 CF=CFCF 3 ,
CH 2 FCH=CFCF 3 , CH 2 =CFCHFCF 3 , CH 2 =CFCF 2 CHF 2 , CF 3 CH=CFCH 2 F, CHF=CFCH 2 CF 3 , CHF=CHCHFCF 3) CHF=CHCF 2 CHF 2 , CHF 2 CF=CHCHF 2 , CHF=CFCHFCHF 2 , CF 3 CF=CHCH 3 , CF 2 =CHCF 2 Br, CHF=CBrCHF 2 , CHBr=CHCF 3 , CF 3 CBr=CFCF 3 , CH 2 =CBrCF 2 CF 3 ,
CHBr=CHCF 2 CF 3 , CH 2 =CHCF 2 CF 2 Br, CH 2 =CHCBrFCF 3 , CH 3 CBr=CHCF 3 , CF 3 CBr=CHCH 3 , (CFs) 2 C=CHBr, CF 3 CF=CBrCF 2 CF 3 , E-CHF 2 CBr=CFC 2 F 5 , Z- CHF 2 CBr=CFC 2 F 5 , CF 2 =CBrCHFC 2 F 5 , (CF 3 ) 2 CFCBr=CH 2 , CHBr=CF(CF 2 ) 2 CHF 2l CH 2 =CBrCF 2 C 2 F 5 , CF 2 =C(CH 2 Br)CF 3 ,
CH 2 =C(CBrF 2 )CF 3 , (CF 3 ) 2 CHCH=CHBr, (CFs) 2 C=CHCH 2 Br, CH 2 =CHCF(CF 3 )CBrF 21 CF 2 =CHCF 2 CH 2 CBrF 2 , CFBr=CHCF 3 , CFBr=CFCF 3 , CF 3 CF 2 CF 2 CBr=CH 2 , and CF 3 (CF 2 ) 3 CBr=CH 2 . A further aspect is for a sprayable composition comprising the above-described propellant. Preferably, the sprayable composition is an aerosol.
Other objects and advantages will become apparent to those skilled in the art upon reference to the detailed description that hereinafter follows.
DETAILED DESCRIPTION OF THE INVENTION Applicants specifically incorporate the entire content of all cited references in this disclosure. Applicants also incorporate by reference the co-owned and concurrently filed applications entitled "Fire Extinguishing and Fire Suppression Compositions Comprising Unsaturated Fluorocarbons" (Attorney Docket # FL 1165 US PRV), "Solvent Compositions Comprising Unsaturated Fluorocarbons" (Attorney Docket # FL 1181 US PRV) 1 "Blowing Agents for Forming Foam Comprising Unsaturated Fluorocarbons" (Attorney Docket # FL 1184 US PRV), and "Compositions Comprising Fluoroolefins and Uses Thereof (Attorney docket * FL 1159).
Further, when an amount, concentration, or other value or parameter is given as either a range, preferred range, or a list of upper preferable values and lower preferable values, this is to be understood as specifically disclosing all ranges formed from any pair of any upper range limit or preferred value and any lower range limit or preferred value, regardless of whether ranges are separately disclosed. Where a range of numerical values is recited herein, unless otherwise stated, the range is intended to include the endpoints thereof, and all integers and fractions within the range. It is not intended that the scope of the invention be limited to the specific values recited when defining a range.
One aspect relates to compositions useful in aerosol; i.e., pressurized, dispensing systems. The disclosure herein relates in particular to the field of aerosol compositions which exhibit environmental responsibility while retaining desirable properties associated with aerosol dispensing systems.
There are numerous difficulties associated with formulating an environmentally responsible propellant for use with an aerosol dispensing system, including but not limited to achieving a single phase, soluble composition which will retain desirable spray characteristics and product performance characteristics of aerosols currently marketed. Flammability is also a consideration. Also problematic in the formulation of personal care products is obtaining a composition useful in dispensing active ingredient from an aerosol dispensing system absent toxic side effects. Aerosol products are generally preferred over products dispensed by pumps or other systems. Many advantages of aerosols stem from the fact that air is not drawn into the aerosol container to replace ingredients dispensed. Thus the product is not exposed to deteriorating or oxidizing effects of air and/or transient moisture, the product maintains its sterility, and preservatives need not be included in the product composition. Consumers prefer aerosols for their convenience, ease of use and cleanliness. Broadly speaking, the characteristics of the spray dispensed from aerosol systems are superior to those of other systems. The product composition is generally applied with a finer, more even spray than when
applied with pump sprays. Pump-type dispensers tend to over- concentrate the product in one spot because of inability to maintain uniformity of product dispersal throughout the target area. This is important, for example, in a hairspray product where it is desirable that the spray retain manageability and hold of the hair style yet not weigh the hair down, give an unnatural hold, or feel sticky to touch.
It is, therefore, desirable to develop a homogeneous, soluble and nontoxic composition with limited flammability, useful in an aerosol dispensing system for personal care as well as other products, which retains advantageous spray characteristics and other properties of an aerosol, while achieving environmental responsibility.
Accordingly, one aspect to provide a composition useful in an aerosol dispensing system which achieves the advantageous properties of an aerosol. A further object to provide a sealed container with an aerosol dispensing system and a composition which attains the objectives described herein.
The foregoing objectives are achieved with the unsaturated fluorocarbon and hydrofluorocarbon propellant compositions disclosed herein. The compositions may be formulated with active ingredient from about 1-15% by weight, or more. Total propellant may vary from 15-95%.
Also contemplated is an aerosol dispensing system comprising a sealed container equipped with an aerosol dispensing valve and containing therein the composition and active ingredient as above. An important physical property associated with the dispensing of aerosol products is the vapor pressure of the propellant. By "vapor pressure" is meant the pressure exerted when a liquefied propellant gas is in equilibrium with its vapor in a closed container, such as an aerosol can. Vapor pressure can be measured by connecting a pressure gauge to the valve on an aerosol can or gas cylinder containing the vapor/liquid mixture. A standard of measurement of vapor pressure in the U.S. aerosol industry is pounds per square inch gauge (psig) with the gas/liquefied mixture at constant temperature, most commonly at 70 0 F (21 0 C). The
vapor pressure of liquefied gases most widely employed as aerosol propellants will vary over the range of about 20 to 90 psig (138 to 621 kPa) at 70 0 F. (21 0 C). The propellant systems disclosed herein have vapor pressures in this range. One aspect encompasses non-toxic compositions useful in an aerosol dispensing system. The compositions comprise unsaturated fluorocarbons (FCs) and/or hydrofluorocarbons (HFCs) alone or in mixture with each other or other suitable propellants, including saturated HFCs, hydrocarbons (HCs), dimethylether, carbon dioxide, nitrous oxide, and nitrogen. Optional active ingredients and additives may be included in the formulation in order to prepare different forms of end products by numerous methods known to those skilled in the art.
One embodiment provides blowing agents having the formula E- or Z-R 1 CH=CHR 2 (Formula I), wherein R 1 and R 2 are, independently, Ci to Cβ perfluoroalkyl groups. Examples of R 1 and R 2 groups include, but are not limited to, CF 3 , C 2 F 5 , CF 2 CF 2 CF 3 , CF(CF 3 ) 2 , CF 2 CF 2 CF 2 CF 3 , CF(CF 3 )CF 2 CF 3 , CF 2 CF(CF 3 ) 2 , C(CFs) 3 , CF 2 CF 2 CF 2 CF 2 CF 3 , CF 2 CF 2 CF(CFs) 2 , C(CFs) 2 C 2 F 5 , CF 2 CF 2 CF 2 CF 2 CF 2 CF 3 , CF(CF 3 ) CF 2 CF 2 C 2 F 5 , and C(CF 3 ) 2 CF 2 C 2 F 5 . Exemplary, non-limiting Formula I compounds are presented in Table 1.
TABLE 1
Compounds of Formula I may be prepared by contacting a perfluoroalkyi iodide of the formula R 1 I with a perfluoroalkyltrihydroolefin of the formula R 2 CH=CH 2 to form a trihydroiodoperfluoroalkane of the formula R 1 CH 2 CHIR 2 . This trihydroiodoperfluoroalkane can then be dehydroiodinated to form R 1 CH=CHR 2 . Alternatively, the olefin
R 1 CH=CHR 2 may be prepared by dehydroiodination of a trihydroiodoperfluoroalkane of the formula R 1 CHICHaR 2 formed in turn by reacting a perfluoroalkyl iodide of the formula R 2 I with a perfluoroalkyltrihydroolefin of the formula R 1 CH=CH 2 . Said contacting of a perfluoroalkyl iodide with a perfluoroalkyltrihydroolefin may take place in batch mode by combining the reactants in a suitable reaction vessel capable of operating under the autogenous pressure of the reactants and products at reaction temperature. Suitable reaction vessels include fabricated from stainless steels, in particular of the austenitic type, and the well-known high nickel alloys such as Monel® nickel-copper alloys, Hastelloy® nickel based alloys and Inconel® nickel-chromium alloys.
Alternatively, the reaction may take be conducted in semi-batch mode in which the perfluoroalkyltrihydroolefin reactant is added to the perfluoroalkyl iodide reactant by means of a suitable addition apparatus such as a pump at the reaction temperature.
The ratio of perfluoroalkyl iodide to perfluoroalkyltrihydroolefin should be between about 1 :1 to about 4:1 , preferably from about 1.5:1 to 2.5:1. Ratios less than 1.5:1 tend to result in large amounts of the 2:1 adduct as reported by Jeanneaux, et al. in Journal of Fluorine Chemistry, Vol. 4, pages 261-270 (1974).
Preferred temperatures for contacting of said perfluoroalkyl iodide with said perfluoroalkyltrihydroolefin are preferably within the range of about 150°C to 300 0 C, preferably from about 170°C to about 250°C, and most preferably from about 180 0 C to about 230°C.
Suitable contact times for the reaction of the perfluoroalkyl iodide with the perfluoroalkyltrihydroolefin are from about 0.5 hour to 18 hoursi preferably from about 4 to about 12 hours.
The trihydroiodoperfluoroalkane prepared by reaction of the perfluoroalkyl iodide with the perfluoroalkyltrihydroolefin may be used directly in the dehydroiodination step or may preferably be recovered and purified by distilled prior to the dehydroiodination step.
The dehydroiodination step is carried out by contacting the trihydroiodoperfluoroalkane with a basic substance. Suitable basic substances include alkali metal hydroxides (e.g., sodium hydroxide or potassium hydroxide), alkali metal oxide (for example, sodium oxide), alkaline earth metal hydroxides (e.g., calcium hydroxide), alkaline earth metal oxides (e.g., calcium oxide), alkali metal alkoxides (e.g., sodium methoxide or sodium ethoxide), aqueous ammonia, sodium amide, or mixtures of basic substances such as soda lime. Preferred basic substances are sodium hydroxide and potassium hydroxide. Said contacting of the trihydroiodoperfluoroalkane with a basic substance may take place in the liquid phase preferably in the presence of a solvent capable of dissolving at least a portion of both reactants. Solvents suitable for the dehydroiodination step include one or more polar organic solvents such as alcohols (e.g., methanol, ethanol, n-propanol, isopropanol, n-butanol, isobutanol, and tertiary butanol), nitriles (e.g., acetonitrile, propionitrile, butyronitrile, benzonitrile, or adiponitrile), dimethyl sulfoxide, N,N-dimethylformamide, N,N-dimethylacetamide, or sulfolane. The choice of solvent may depend on the boiling point product and the ease of separation of traces of the solvent from the product during purification. Typically, ethanol or isopropanol are good solvents for the reaction.
Typically, the dehydroiodination reaction may be carried out by addition of one of the reactants (either the basic substance or the trihydroiodoperfluoroalkane) to the other reactant in a suitable reaction vessel. Said reaction may be fabricated from glass, ceramic, or metal and is preferably agitated with an impellor or stirring mechanism.
Temperatures suitable for the dehydroiodination reaction are from about 1O 0 C to about 100 0 C, preferably from about 20 0 C to about 70 0 C. The dehydroiodination reaction may be carried out at ambient pressure or at reduced or elevated pressure. Of note are dehydroiodination reactions in which the compound of Formula I is distilled out of the reaction vessel as it is formed.
Alternatively, the dehydroiodination reaction may be conducted by contacting an aqueous solution of said basic substance with a solution of the trihydroiodoperfluoroalkane in one or more organic solvents of lower polarity such as an alkane (e.g., hexane, heptane, or octane), aromatic hydrocarbon (e.g., toluene), halogenated hydrocarbon (e.g., methylene chloride, ethylene dichloride, chloroform, carbon tetrachloride, or perchloroethylene), or ether (e.g., diethyl ether, methyl tert-butyl ether, tetrahydrofuran, 2-methyl tetrahydrofuran, dioxane, dimethoxyethane, diglyme, or tetraglyme) by in the presence of a phase transfer catalyst. Suitable phase transfer catalysts include quaternary ammonium halides (e.g., tetrabutylammonium bromide, tetrabutylammonium hydrosulfate, triethylbenzylammonium chloride, dodecyltrimethylammonium chloride, and tricaprylylmethylammonium chloride), quaternary phosphonium halides (e.g., triphenylmethylphosphonium bromide and tetraphenylphosphonium chloride), cyclic ether compounds known in the art as crown ethers (e.g., 18-crown-6 and 15-crown-5).
Alternatively, the dehydroiodination reaction may be conducted in the absence of solvent by adding the trihydroiodoperfluoroalkane to a solid or liquid basic substances. Suitable reaction times for the dehydroiodination reactions are from about 15 minutes to about six hours or more depending on the solubility of the reactants. Typically the dehydroiodination reaction is rapid and requires about 30 minutes to about three hours for completion. The compound of formula I may be recovered from the dehydroiodination reaction mixture by phase separation after addition of water, by distillation, or by a combination thereof.
The compositions disclosed herein may comprise a single compound of Formula I 1 for example, one of the compounds in Table 1 , or may comprise a combination of compounds of Formula I. In addition to the inventive compounds described above, compounds presented in Table 2 can be used as aerosol propellants.
TABLE 2
The compounds listed in Table 2 are available commercially or may be prepared by processes known in the art.
In addition to the inventive compounds described above, the bromine-containing fluorocarbons or hydrofluorocarbons presented in Table 3 can be used as aerosol propellants.
TABLE 3
The compounds listed in Table 3 are available commercially or may be prepared by processes known in the art.
1-Bromo-3,3,4,4,4-pentafluoro-1-butene may be prepared by a three step sequence beginning with reaction of phosphorous tribromide with 3,3,4,4,4-pentafluoro-1 -butanol to give 4- bromo-1 ,1 ,1 ,2,2- pentafluorobutane. Thermal bromination of 4- bromo-1 , 1,1 , 2,2- pentafluorobutane at 350-400 0 C gives 4,4-dibromo-1,1,1,2,2- pentafluorobutane which may in turn be heated with powdered potassium hydroxide to give the desired bromobutene. 2-Bromo-3,4,4,4-tetrafluoro-3-(trifluoromethyl)-1-butene may be prepared by addition of bromine to 3,4,4-tetrafluoro-3-(trifluoromethyl)-1- butene followed by treatment of the resulting dibromide with ethanolic potassium hydroxide.
Many of the compounds of Formulas I, Table 1 , Table 2 and Table 3 exist as different configurational isomers or stereoisomers. When the specific isomer is not designated, the disclosure herein is intended to include all single configurational isomers, single stereoisomers, or any combination thereof. For instance, CF 3 CH=CHCFa is meant to represent the E-isomer, Z-isomer, or any combination or mixture of both isomers in any ratio. Another example is C 2 F 5 CF 2 CH=CH-CF 2 C 2 F 5 , by which is represented the E-isomer, Z-isomer, or any combination or mixture of both isomers in any ratio.
Aerosol propellants may comprise a single compound as listed, for example, in Table 2, or may comprise a combination of compounds from Table 2 or, alternatively, a combination of compounds from Table 1 , Table 2, Table 3, and/or Formula I.
The amount of the fluorocarbons (FCs) or HFCs contained in the present compositions (from, e.g., Formula I, Table 1 , or Table 2, or Table 3) can vary widely, depending the particular application, and compositions containing more than trace amounts and less than 100% of the compound are within broad the scope of the present disclosure. Preferably, the compositions have a Global Warming Potential (GWP) of not greater than 150, more preferably not greater than 100, and even more preferably not
greater than 75. As used herein, "GWP" is measured relative to that of carbon dioxide and over a 100-year time horizon, as defined in "The Scientific Assessment of Ozone Depletion, 2002, a report of the World Meteorological Association's Global Ozone Research and Monitoring Project," which is incorporated herein by reference.
The present compositions also preferably have an Ozone Depletion Potential (ODP) of not greater than 0.05, more preferably not greater than 0.02 and even more preferably about zero. As used herein, "ODP" is as defined in "The Scientific Assessment of Ozone Depletion, 2002, A report of the World Meteorological Association's Global Ozone Research and Monitoring Project," which is incorporated herein by reference.
The compositions may be prepared by any convenient method to combine the desired amounts of the individual components. A preferred method is to weigh the desired component amounts and thereafter combine the components in an appropriate vessel. Agitation may be used, if desired.
The propellants may comprise a single compound as listed, for example, in Table 1 , or may comprise a combination of compounds of Formula I, Table 1 , Table 2, and/or Table 3. Additionally, many of the compounds described herein may exist as different configurational isomers or stereoisomers. The disclosure herein is intended to include all single configurational isomers, single stereoisomers, or any combination thereof. For instance, F11 E is meant to represent the E-isomer, Z-isomer, or any combination or mixture of both isomers in any ratio. Another example is F33E, by which is represented the E-isomer, Z-isomer, or any combination or mixture of both isomers in any ratio.
Preferably, the propellants disclosed herein have a Global Warming Potential (GWP) of not greater than 150, more preferably not greater than 100, and even more preferably not greater than 75. As used herein, "GWP" is measured relative to that of carbon dioxide and over a 100-year time horizon, as defined in "The Scientific Assessment of Ozone Depletion, 2002, a report of the World Meteorological Association's Global
Ozone Research and Monitoring Project," which is incorporated herein by reference.
The present compositions also preferably have an Ozone Depletion Potential (ODP) of not greater than 0.05, more preferably not greater than 0.02 and even more preferably about zero. As used herein, "ODP" is as defined in "The Scientific Assessment of Ozone Depletion, 2002, A report of the World Meteorological Association's Global Ozone Research and Monitoring Project," which is incorporated herein by reference.
The compositions may be prepared by any convenient method to combine the desired amounts of the individual components. A preferred method is to weigh the desired component amounts and thereafter combine the components in an appropriate vessel. Agitation may be used, if desired.
The propellant composition comprises, more preferably consists essentially of, and, even more preferably, consists of compositions disclosed herein. The active ingredient to be sprayed together with inert ingredients, solvents, and other materials may also be present in the sprayable mixture. Preferably, the sprayable composition is an aerosol. Another embodiment of the present disclosure provides a process for producing aerosol products comprising the step of adding a composition as disclosed herein to active ingredients in an aerosol container, wherein said composition functions as a propellant.
The compositions are capable of providing nonflammable, liquefied gas propellant and aerosols that do not contribute substantially to global warming. The present compositions can be used to formulate a variety of industrial aerosols or other sprayable compositions such as contact cleaners, dusters, lubricant sprays, mold release sprays, and the like, and consumer aerosols such as personal care products (such as, e.g., hair sprays, deodorants, and perfumes), household products (such as, e.g., waxes, polishes, pan sprays, room fresheners, and household insecticides), and automotive products (such as, e.g., cleaners and polishers), as well as medicinal materials such as anti-asthma and anti- halitosis medications. Examples of this includes metered dose inhalers
(MDIs) for the treatment of asthma and other chronic obstructive pulmonary diseases and for delivery of medicaments to accessible mucous membranes or intranasally.
All such products utilize the pressure of a propellant gas or a mixture of propellant gases (i.e., a propellant gas system) to expel active ingredients from the container. For this purpose, most aerosols employ liquefied gases which vaporize and provide the pressure to propel the active ingredients when the valve on the aerosol container is pressed open. The medicinal aerosol and/or propellant and/or sprayable compositions in many applications include, in addition to a compound disclosed herein, a medicament such as a beta-agonist, a corticosteroid or other medicament, and, optionally, other ingredients, such as surfactants, solvents, other propellants, flavorants, and other excipients. The compositions disclosed herein, unlike many compositions previously used in these applications, have good environmental properties and are not considered to be potential contributors to global warming. The present compositions therefore provide in certain preferred embodiments substantially nonflammable, liquefied gas propellants having very low GWPs.
All of the compositions and methods disclosed and claimed herein can be made and executed without undue experimentation in light of the present disclosure. While the compositions and methods disclosed herein have been described in terms of preferred embodiments, it will be apparent to those of skill in the art that variations may be applied to the compositions and methods and in the steps or in the sequence of steps of the method described herein without departing from the concept, spirit, and scope of the present disclosure. More specifically, it will be apparent that certain agents which are chemically related may be substituted for the agents described herein while the same or similar results would be achieved. All such similar substitutes and modifications apparent to those skilled in the art are deemed to be within the spirit, scope, and concept of the present disclosure as defined by the appended claims.
EXAMPLES
The present disclosure is further defined in the following Examples. It should be understood that these Examples, while indicating preferred embodiments, are given by way of illustration only. From the above discussion and these Examples, one skilled in the art can ascertain the preferred features, and without departing from the spirit and scope thereof, can make various changes and modifications to adapt it to various uses and conditions.
Example 1 55% VOC Hair Spray
A 55% VOC (volatile organic compound) hairspray was formulated as follows:
Wt %
Octylacrylamide/acrylates/butylaminoethyl methylacrylate copolymer (National Starch Amphomer LV-71) 5.0 AMP (2-amino-2-methyl-1-propanol) 1.0
Water 3.5
Ethanol 55.0
Propellant 35.0
Vapor Pressure © 70DF 40 psig
The formulation was one phase indicating complete miscibility and showed good spray patterns and delivery.
Example 2
Air Freshener An air freshener was formulated as follows:
Wt %
Fragrance (Dragoco 0/716873 mixed flowers scent) 1.0 Water 4.0
Ethanol 30.0
Propellant 65.0
Vapor Pressure @ 70DF 48 psig
The formulation was one phase indicating complete miscibility and showed good spray patterns and delivery.
Example 3 Fragrance A fragrance was formulated as follows:
Wt % Perfume (Dragoco 0/716873 mixed flowers scent) 3.0
Water 15.0
Ethanol 70.0
Propellant 12.0
Vapor Pressure @ 70DF 17 psig
The formulation was one phase indicating complete miscibility and showed good spray patterns and delivery.
Example 4 Aerosol Antioerspirant An aerosol antiperspirant was formulated as follows:
Wt % Aluminum chlorohydrate (Reheis Activated ACH
Modified R277-265A) 10.0 lsopropyl myristate 6.0
Silicone fluid DC-344 6.0
Quaternium-18 hectorite (Rheox Bentone 38) 0.5
Ethanol 2.0
Propellant 75.0
Propellant 12.0
Vapor Pressure @ 70DF 48 psig
The formulation provided good suspendability for the antiperspirant active, showed good spray patterns and delivery, and did not plug the valve.
Similar formulations can also be developed for household disinfectants, insect foggers, and spray paints using the compositions of the present disclosure.