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Publication numberUSRE41557 E1
Publication typeGrant
Application numberUS 12/263,054
Publication dateAug 24, 2010
Filing dateOct 31, 2008
Priority dateApr 17, 1995
Also published asUS5626786, USRE40651, USRE41558
Publication number12263054, 263054, US RE41557 E1, US RE41557E1, US-E1-RE41557, USRE41557 E1, USRE41557E1
InventorsJohn H. Huntington, Peter D. Haaland
Original AssigneeEclipse Aerospace, Inc.
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Environmentally friendly; release bromine atoms such as phosphorous tribromide (PBr3), thionyl bromide (SOBr2), boron tribromide (BBr3), and the like are very efficient at extinguishing fires; hydrolyze or oxidize rapidly in troposphere and consequently they have no stratospheric ozone depletion; airbags
US RE41557 E1
Abstract
A class of fire suppressant compounds which have labile bromine atoms bound to atoms other than carbon have been discovered to be more effective at suppressing fires than Halon 1211 and Halon 1301. Moreover, this class of fire suppressant compounds hydrolyze or oxidize rapidly in the troposphere and as a consequence thereof, they have minimal ozone depletion potential.
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Claims(48)
1. A fire suppressant composition consisting essentially of at least one brominated, non-carbon compound selected from the group consisting of PBr3, POBr3, SOBr2, BrF3, BrF5, PBr5, TiBr4, SiBr4, IBr, CuBr, NOBr, BrF, and BBr3, which is combined with a propellant such that the ozone depletion potential of the composition is less than 0.1.
2. The fire suppressant composition of claim 1 wherein ozone depletion potential is defined on a scale where the ozone depletion caused by CFCl3 is 1.0.
3. A fire suppressant composition consisting of at least one labile brominated compound selected from the group consisting of PBr3, POBr3, SOBr2, BrF3, BrF5, TiBr4, SiBr4, IBr, CuBr, NOBr, BrF, BBr3, and BrCl, which is combined with a propellant selected from the group consisting of CO2, N2, compressed air, and HCFC-123 (CF3CCl2H).
4. The fire suppressant composition of claim 3 wherein ozone depletion potential of the propellant equals 0.016.
5. A fire suppressant composition consisting essentially of: at least one brominated, non-carbon compound in a liquid state selected from the group consisting of CuBr, IBr, and BrCl; and a propellant combined with the compound for propelling the composition such that sufficient bromine atoms are liberated from the composition to suppress a fire, wherein the composition has no ozone depletion potential.
6. The composition of claim 5, wherein the propellant is selected from the group consisting of CO2 , N 2 , and compressed air.
7. The composition of claim 5 wherein said brominated compound is CuBr.
8. The composition of claim 5 wherein said brominated compound is IBr.
9. The composition of claim 5 wherein said brominated compound is BrCl.
10. The composition of claim 5 wherein said brominated compound is CuBr and the propellant is nonflammable.
11. The composition of claim 5 wherein said brominated compound is IBr and the propellant is nonflammable.
12. The composition of claim 5 wherein said brominated compound is BrCl and the propellant is nonflammable.
13. The composition of claim 7 wherein said brominated compound is not stable in, and said sufficient bromine atoms are liberated in, the presence of oxygen.
14. The composition of claim 13 wherein said liberated bromine atoms are sufficient to catalytically suppress the fire.
15. The composition of claim 7 wherein said brominated compound is not stable in, and said sufficient bromine atoms are liberated in, the presence of heat.
16. The composition of claim 15 wherein said liberated bromine atoms are sufficient to catalytically suppress the fire.
17. The composition of claim 7 wherein said brominated compound is not stable in, and said sufficient bromine atoms are liberated in, the presence of water.
18. The composition of claim 17 wherein said wherein said liberated bromine atoms are sufficient to catalytically suppress the fire.
19. The composition of claim 8 wherein said brominated compound is not stable in, and said sufficient bromine atoms are liberated in, the presence of oxygen.
20. The composition of claim 19 wherein said liberated bromine atoms are sufficient to catalytically suppress the fire.
21. The composition of claim 8 wherein said brominated compound is not stable in, and said sufficient bromine atoms are liberated in, the presence of heat.
22. The composition of claim 21 wherein said liberated bromine atoms are sufficient to catalytically suppress the fire.
23. The composition of claim 8 wherein said brominated compound is not stable in, and said sufficient bromine atoms are liberated in, the presence of water.
24. The composition of claim 23 wherein said wherein said liberated bromine atoms are sufficient to catalytically suppress the fire.
25. The composition of claim 9 wherein said brominated compound is not stable in, and said sufficient bromine atoms are liberated in, the presence of oxygen.
26. The composition of claim 25 wherein said liberated bromine atoms are sufficient to catalytically suppress the fire.
27. The composition of claim 9 wherein said brominated compound is not stable in, and said sufficient bromine atoms are liberated in, the presence of heat.
28. The composition of claim 27 wherein said liberated bromine atoms are sufficient to catalytically suppress the fire.
29. The composition of claim 9 wherein said brominated compound is not stable in, and said sufficient bromine atoms are liberated in, the presence of water.
30. The composition of claim 29 wherein said wherein said liberated bromine atoms are sufficient to catalytically suppress the fire.
31. The composition of claim 7 wherein the propellant is selected from the group consisting of a non-flammable, pressurized gas; a deflagrating, solid, gas-generating cartridge; and a pressurized liquid.
32. The composition of claim 8 wherein the propellant is selected from the group consisting of a non-flammable, pressurized gas; a deflagrating, solid, gas-generating cartridge; and a pressurized liquid.
33. The composition of claim 9 wherein the propellant is selected from the group consisting of a non-flammable, pressurized gas; a deflagrating, solid, gas-generating cartridge; and a pressurized liquid.
34. A fire suppressant composition consisting essentially of CuBr in a liquid state and a propellant combined with the CuBr for propelling the composition to catalytically suppress a fire, wherein the composition has no ozone depletion potential.
35. The composition of claim 34, wherein the propellant is selected from the group consisting of CO2 , N 2 , and compressed air.
36. The composition of claim 34 wherein the propellant is nonflammable.
37. The composition of claim 34 wherein the CuBr is not stable in the presence of at least one of oxygen, heat, and water.
38. The composition of claim 34 wherein the propellant is selected from the group consisting of a non-flammable, pressurized gas; a deflagrating, solid, gas-generating cartridge; and a pressurized liquid.
39. A fire suppressant composition consisting essentially of IBr in a liquid stage and a propellant combined with the IBr for propelling the composition to catalytically suppress a fire, wherein the composition has no ozone depletion potential.
40. The composition of claim 39, wherein the propellant is selected from the group consisting of CO2 , N 2 , and compressed air.
41. The composition of claim 39 wherein the propellant is nonflammable.
42. The composition of claim 39 wherein the CuBr is not stable in the presence of at least one of oxygen, heat, and water.
43. The composition of claim 39 wherein the propellant is selected from the group consisting of a non-flammable, pressurized gas; a deflagrating, solid, gas-generating cartridge; and a pressurized liquid.
44. A fire suppressant composition consisting essentially of BrCl in a liquid state and a propellant combined with the BrCl for propelling the composition to catalytically suppress a fire, wherein the composition has no ozone depletion potential.
45. The composition of claim 44, wherein the propellant is selected from the group consisting of CO2 , N 2 , and compressed air.
46. The composition of claim 44 wherein the propellant is nonflammable.
47. The composition of claim 44 wherein the CuBr is not stable in the presence of at least one of oxygen, heat, and water.
48. The composition of claim 44 wherein the propellant is selected from the group consisting of a non-flammable, pressurized gas; a deflagrating, solid, gas-generating cartridge; and a pressurized liquid.
Description

More than one divisional reissue application has been filed for the reissue of U.S. Pat. No. 5,626,786. The reissue applications are application Ser. No. 10/893,705 now RE40,651 E, application Ser. No. 12/263,122 pending, and the present application Ser. No. 12/263,054.

GOVERNMENT RIGHTS

This invention was made with support by the U.S. Government. The Government may have certain rights in this invention.

BACKGROUND OF THE INVENTION

1. Field of the Invention

The present invention generally relates to prevention and extinguishment of fires of combustible materials by utilizing a composition of matter group which is highly efficient and environmentally friendly. More particularly, the invention relates to prevention and extinguishment of fires of combustible materials by using a group of fire suppressants having labile bonds between bromine atoms and atoms other than carbon.

2. Description of the Prior Art

Fire suppression by halogenated alkanes is well-established in both the scientific literature and commercial practice as taught, for example, in R. G. Gann ed., Halogenated Fire Suppressants, ACS Symposium Series 16 (American Chemical Society, Washington, D.C.) 1975. The two most widely used halogenated suppressants are Halon 1301 (CF3Br) and Halon 1211 (CF2ClBr). These compounds are very stable, so they survive long enough in the troposphere to be gradually transported to the stratosphere, where they are photolyzed by solar ultraviolet radiation to produce free radicals that catalyze ozone depletion as taught, for example, in J. G. Anderson, D. W. Toohey, and W. F. Brune, Science, 251, 39 (1991). Production of these materials has therefore been internationally prohibited after January, 1994 by the Montreal Protocol on Substances that Deplete the Ozone Layer. The problem is therefore to find fire suppression materials and methods which are at least as effective as Halon 1301 and Halon 1211 but which do not deplete the ozone layer.

Representative of the prior art directed to the use of fluorocarbons which have no chlorine or bromine is U.S. Pat. No. 5,236,611 (Shiflet). These fluorocarbons are slowly transported into the stratosphere, but the catalytic efficiency of fluorine is very much smaller than that of chlorine, bromine, or iodine.

Representative of the prior art directed to the use of hydrogenated halocarbons, which are less stable than Halon 1301 or Halon 1211 in the troposphere, are U.S. Pat. Nos. 5,084,190 (Fernandez), 5,135,054 (Nimitz et al.); 5,093,013 (Sprague); and 5,080,177 (Robin et al.). It is well known that Halons containing chlorine or bromine will suppress fires in smaller quantities than those which contain only fluorine. However, it is understood by people practiced in the art of combustion that the principal source of heat release in hydrocarbon combustion is oxidation of hydrogen atoms to form water vapor. Thus hydrogenated halocarbons are expected to act chemically both as fuels and as fire suppressants.

SUMMARY OF THE INVENTION

In accordance with the teachings of the present invention compositions of matter having labile bromine atoms bound to atoms other than carbon have been discovered to have improved fire suppressant properties and to be environmentally friendly. Compounds which release bromine atoms and are commonly used as brominating agents in organic synthesis such as phosphorous tribromide (PBr3), thionyl bromide (SOBr2), boron tribromide (BBr3), and the like are very efficient at extinguishing fires. Moreover, they hydrolyze or oxidize rapidly in the troposphere and consequently they have no stratospheric ozone depletion potential.

Additionally included in this class of fire suppressant compounds of labile bromine atoms bound to atoms other than carbon are silicon tetrabromide (SiBr4), titanium tetrabromide (TiBr4), iodine bromide (IBr), phosphorous oxybromide (POBr3), bromine trifluoride (BrF3), bromine pentafluoride (BrF5), N-bromosuccinimide (C4H4O2NBr) {the bromine is bound to nitrogen, not carbon}, nitrosyl bromide (NOBr), chlorine bromide (ClBr), and cuprous bromide (CuBr). These compounds are used as brominating agents in chemical synthesis as taught, for example, in the Merck Index, ninth edition, (Merck & Co., Rahway, N.J., 1976) or suffer thermal decomposition with liberation of bromine at temperatures less than 200 degrees centigrade.

Examples of non-labile bromine compositions are found in such high-melting, ionically bound salts as lithium bromide (LiBr, m.p. 547° C.), calcium bromide (CaBr2, m.p. 730° C.), or chromous bromide (CrBr2, m.p. 842° C.), and other bromine-containing compositions that are thermally and oxidatively stable according to criteria familiar to people practiced in the art of synthetic chemistry.

In order to extinguish fires with a composition having one or more compounds of the aforesaid class of fire suppressants, equipment for delivering the composition incorporates such factors as specific geometry, gas flow, and flame conditions. A method of delivery of a composition having one or more liquid compounds of the aforesaid class of fires suppressants may employ a nonflammable, pressurized gas to propel the composition through a nozzle to the flame. Another method of delivery of liquid compositions may employ a deflagrating solid, gas-generating cartridge, such as is found in automotive airbags, to propel a mist of liquid to the flame. A third method for delivery of liquid compositions may employ a pressurized liquid propellant such as liquid carbon dioxide or liquid argon to atomize and direct a mist of suppressant onto the flame. Other methods for propelling powders or slurries of solid materials of the aforesaid class may employ a deflagrating solid gas generating cartridge and a wider nozzle such as would be used for an ordinary shotgun cartridge. Other methods for propelling gaseous materials of the aforesaid class may employ mixtures with pressurized inert propellants to aid transport of suppressant to the flame.

The primary advantage of the use of the class of fire suppressants of this discovery is to extinguish fires more efficiently with smaller volumes and masses of extinguishant than existing fire suppressants, without depleting the stratospheric ozone layer. PBr3, POBr3, SOBr2, BBr3, and the like react rapidly with water vapor or liquid to produce mild acids which precipitate with normal rain and are ultimately neutralized in soils. The short lifetimes of these materials also reduce toxicity of the suppressants since their simple acid decomposition products pose no chronic risk to pH buffered, living organisms.

These and other advantages and attainments of the present invention will become apparent to those skilled in the art upon a reading of the detailed description wherein there are described several embodiments of the invention.

DESCRIPTION OF THE PREFERRED EMBODIMENTS

In accordance with the teachings of the present invention a class of fire suppressants which have labile bromine atoms bound to atoms other than carbon are shown in Table I. These compounds are more effective at suppressing fire than Halon 1301 or Halon 1211 and have no ozone depletion potential.

The effectiveness of the class of suppressants described herein is a result of the relative ease with which bromine atoms are liberated in a flame environment. Halons 1301 and 1211 also liberate bromine atoms in a flame; however, the strength of the C—Br bond in these materials requires higher temperatures or longer interaction times than the compositions of matter described herein. The stability of the Halons against oxidation or hydrolysis in the troposphere is one indication of the stability of the C—Br bond. The compositions of matter described herein are not stable in the presence of water, oxygen, or heat, liberating bromine atoms under these conditions and thereby providing a catalyst for flame suppression.

Another indication of the stability of the C—Br bond is the measurement of its bond dissociation energy of 68 kilocalories per mole as taught by A. H. Sehon and M. Szwarc (Proceedings of the Royal Society (London), page 110, [1951]). This energy is larger than the bond energy of typical P—Br bonds (63 kcal/mole), I—Br bonds (43 kcal/mole), or S—Br bonds (52 kcal/mole) as taught by Streitweiser and Heathcock, Introduction to Organic Chemistry, (Macmillan:NY), 1976 and Cotton and Wilkinson, Advanced Inorganic Chemistry, (3rd ed. Wiley:NY), 1972. As is known to people practiced in the art of chemistry the interpretation of bond dissociation energies involves approximations based on the nature of the full molecular fragments (XYn) from which bromine is liberated according to the reaction:
YnX—Br→YnX+Br.
Thus lower average bond energies indicate the possibility of labile bonds in a group of materials, but further experimentation with specific materials is required to establish the lability of the bond compared with Halons.

TABLE I
Composition Phase % Br Comments
PBr3 liquid 88 brominating agent
POBr3 liquid 83 brominating agent
SOBr2 liquid 77 brominating agent
BrF3 liquid 58 reactive solvent
BrF5 liquid 46 reactive solvent
PBr5 solid 91 brominating agent
TiBr4 solid 87 reacts with water
SiBr4 liquid 92 reacts with water
IBr solid 39 decomposes at 116° C.
CuBr solid 29 brominating agent
NOBr gas 73 brominating agent
B2F gas 81 boils at −20° C.
C6H4O2NBr solid 44.9 decomposes at 170° C.
BBr3 liquid 96 boils at 90° C.
BrCl gas 70 decomposes at 10° C.

In one embodiment of the invention liquid SOBr2 is introduced as an air-pressurized mist into a 500,000 Btu/hr fire resulting from kerosene flowing at a rate of 4 grams per second through a nozzle with cross-flowing compressed air to atomize the liquid into a fine mist. The fire is contained in a flame holder whose volume is approximately 8 liters and is further blown by an atmospheric cross-wind of 40 miles per hour. The fire is reproducibly and irreversibly extinguished with less than one gram of SOBr2 in less than 0.2 seconds as confirmed by videotape records of the experiments. The same fire is not reproducibly suppressed with aliquots of 25 grams of CF3Br added to the same location.

In another embodiment of the invention 0.2 cubic centimeters of PBr3 is mixed with 0.7 cubic centimeters of liquid carbon dioxide. The liquid CO2 propels the PBr3 through a valve and into the flame zone, generated as herein above described, as it is opened, irreversibly and completely extinguishing the flame in the presence of flowing fuel, air, and hot surfaces.

Extinguishment of a similar fire, with a hydrocarbon fuel burn rate of 12 grams per second, by Halon 1301 is taught by Alvarez in chapter 3 of Gann (ibid.) to require between 90 and 130 grams per second of CF3Br for suppression. Another example of a gasoline fire with similar heat output is taught by Ford in chapter 1 of Gann (ibid.) to require between 500 and 1500 grams of Halon 1301 for suppression. Another fire, in which 10 grams per second of jet fuel are burned in fast-flowing air at the Air Force Flight Dynamics Laboratory Engine Nacelle test facility (Wright-Patterson AFB, OH) requires between one and three kilograms of Halon 1301 for reproducible suppression. In each of these examples the quantity of Halon 1301 required to suppress a similar fire is between 100 and 1000 times greater than that required of the compositions of matter described herein above, of which SOBr2 and PBr3 are specific embodiments.

The labile bromine atoms and high proportion of bromine in the composition of matter listed in Table I provide a more efficient fire suppression formulation than the Halons, which typically have less bromine by weight (Halon 1301 and 1211 are 54% and 48% Br, respectively) and lesser proclivity for liberating bromine atoms when thermally or chemically activated in a combustion environment.

Methods for dispersing gas, liquid, or solid suppressants require designs based upon such factors as specific geometry of the locus of the fire, flow properties of the fire suppressants, and flame conditions of the fire. For example, fine mists of liquid are transported by fluid-dynamical drag forces along flow streamlines in the nacelle of an aircraft engine. The mists vaporize in hot zones, liberating bromine atoms by pyrolysis in precisely the regions where the heat released by combustion is most intense. Inasmuch as the drag coefficient is inversely proportional to the droplet diameter, as is known to people practiced in the art of fluid dynamics, there is a range of aerosol size distributions which most effectively deliver specific suppressants to specific fires. Another such factor for a gaseous composition is the mixing of suppressant flow with turbulent flames in a well-ventilated fire, which is affected by the delivery pressure, the nozzle contour and orientation, the mass-flow rate of the suppressant, and the fluid dynamical properties of the fire. Dispersing methods designed for suppressing fire in the nacelle of a jet engine differ from dispersing methods designed for suppressing fire in the engine compartment of a motor vehicle, the flu of a chimney, or the gas-handling manifold of a semiconductor processing clean-room.

Methods for preventing and extinguishing fires of jet fuel using a composition of matter class which is highly efficient and environmentally friendly is also disclosed by the present inventors in Final Technical Report FR-4021 (US Air Force Phase I SBIR Contract F33615-94-C-5005, November 1994).

Although preferred embodiments of the invention have been described, it will be understood that within the scope of this invention various changes may be made in the amount of fire suppressant, the composition of a fire suppressant mixture, and the method for dispersing fire suppressants which is generally stated consist of a class of fire suppressants and methods of dispersing such fire suppressants capable of carrying out the objects set forth as disclosed in the appended claims.

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US955316 *Jul 26, 1907Apr 19, 1910Minimax Cons LtdProcess of extinguishing burning benzin, &c.
US2732410 *Jan 12, 1955Jan 24, 1956 Process for preparing tetrafluoro
US2791490 *Apr 29, 1952May 7, 1957Du PontMethod and means for commingling and reacting fluid substances
US2918125 *May 9, 1955Dec 22, 1959Sweetman William GChemical cutting method and apparatus
US3076507 *May 16, 1958Feb 5, 1963Sweetman William GChemical cutting method and apparatus for use in wells
US3266674 *Aug 24, 1964Aug 16, 1966Richard L SmithThermo-shave dispensing and reusable unit
US3372208 *Mar 20, 1964Mar 5, 1968Dow Chemical CoFlame resistant epoxy resins containing phosphorus and a halogen
US3479286 *Sep 19, 1966Nov 18, 1969Montedison SpaFlame-extinguishing compositions
US3637022 *Oct 30, 1969Jan 25, 1972Jack L HummelUse of high water content oil-external micellar solutions for extinguishing fires
US3657030 *Jul 31, 1970Apr 18, 1972Bell Telephone Labor IncTechnique for masking silicon nitride during phosphoric acid etching
US3663283 *Oct 2, 1969May 16, 1972Moynihan Daniel JProcess and apparatus for the production of finely-divided metal oxides
US3812239 *Aug 24, 1970May 21, 1974Ppg Industries IncPreparation of submicron titanium carbide
US3903037 *Aug 31, 1972Sep 2, 1975Monsanto CoLow melt viscosity self-extinguishing polymeric polyblend
US3959741 *Jun 9, 1975May 25, 1976United Technologies CorporationInterhalogen based combustion-driven laser which provides continuous wave output lasing from dual species
US3985689 *May 20, 1974Oct 12, 1976Minnesota Mining And Manufacturing CompanySorbent foam material
US4022872 *Nov 12, 1975May 10, 1977Ppg Industries, Inc.Process for preparing finely-divided refractory powders
US4043950 *May 3, 1976Aug 23, 1977Wilmsen HansProcess for the manufacture of plastic foams and flame-proofing foams characterized by the use of a carrier foam
US4048290 *Jan 28, 1976Sep 13, 1977Cabot CorporationProcess for the production of finely-divided metal and metalloid oxides
US4125161 *Sep 6, 1977Nov 14, 1978Weatherford/Dmc, Inc.Chemical cutting apparatus and method for use in wells
US4129513 *Jan 21, 1977Dec 12, 1978The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern IrelandElectric field responsive fluids
US4241042 *Jun 19, 1978Dec 23, 1980Montedison S.P.A.Spherical titanium dioxide particles and process of manufacture
US4250960 *Dec 19, 1979Feb 17, 1981Weatherford/Dmc, Inc.Chemical cutting apparatus
US4292290 *Apr 16, 1980Sep 29, 1981Cabot CorporationProcess for the production of finely-divided metal and metalloid oxides
US4397977 *May 11, 1981Aug 9, 1983Pennwalt CorporationTetrahalophthalates as flame retardant plasticizers for halogenated resins
US4406797 *Nov 3, 1981Sep 27, 1983The United States Of America As Represented By The Administrator Of The National Aeronautics And Space AdministrationFire extinguishant materials
US4415029 *Jul 23, 1981Nov 15, 1983Gearhart Industries, Inc.Downhole well tool and anchoring assembly
US4428430 *Jan 13, 1981Jan 31, 1984Gearhart Industries, Inc.Method for increasing fluid flow circulation
US4481119 *Mar 11, 1983Nov 6, 1984The United States Of America As Represented By The Secretary Of The NavyCompositions for extinguishing titanium fires
US4494601 *Sep 14, 1981Jan 22, 1985Gearhart Industries, Inc.Downhole chemical cutting tool
US4619318 *Sep 27, 1984Oct 28, 1986Gearhart Industries, Inc.Chemical cutting method and apparatus
US4819728 *Sep 1, 1987Apr 11, 1987Lafitte Louis DCutting an object within an earth bore
US4822513 *Nov 12, 1985Apr 18, 1989Diversey CorporationMixture of interhalogen and mineral acid
US4889187 *Apr 25, 1988Dec 26, 1989Jamie Bryant TerrellMulti-run chemical cutter and method
US4949789 *Apr 10, 1989Aug 21, 1990Leon A. RobichauxPressure relief system for down hole chemical cutters
US4971146 *Nov 23, 1988Nov 20, 1990Terrell Jamie BDownhole chemical cutting tool
US5017525 *Mar 17, 1988May 21, 1991Imperial Chemical Industries PlcOrganometallic or other polymer
US5055208 *Jan 2, 1991Oct 8, 1991Powsus, Inc.Fire extinguishing compositions
US5080177 *Jul 26, 1990Jan 14, 1992Great Lakes Chemical CorporationSafe for ozone layer
US5082575 *Mar 22, 1990Jan 21, 1992Shin-Etsu Handotai Company, Ltd.Method for fire-extinguishment on hardly extinguishable burning materials
US5084190 *Nov 14, 1989Jan 28, 1992E. I. Du Pont De Nemours And CompanyFlluoro substituted propanes for extinguishing fires without e ffecting the ozone layer
US5093013 *Dec 11, 1989Mar 3, 1992Halocarbon Products CorporationBromotetrafluoroethane, nitrogen, carbon dioxide and carbon tetrafluoride as propellant
US5120689 *Nov 13, 1990Jun 9, 1992Imperial Chemical Industries PlcMetallic or non-metallic oxide in matrix of carbon
US5135054 *Oct 5, 1990Aug 4, 1992University Of New MexicoFire extinguishing agents for flooding applications
US5165916 *Oct 2, 1989Nov 24, 1992Phillips Petroleum CompanyMethod for producing carbide products
US5192714 *Feb 13, 1991Mar 9, 1993Kabushiki Kaisha ToshibaSemiconducotrs
US5219474 *Aug 8, 1990Jun 15, 1993Korea Institute Of Science And TechnologyHalogenated alkane and aorganophosphorus compound
US5235000 *Dec 10, 1990Aug 10, 1993Ethyl CorporationMaintaining an inert atmosphere containing a low carbon monoxide concentration over the bromine chloride to prevent formation of carbonyl halide
US5236611 *Oct 28, 1991Aug 17, 1993E. I. Du Pont De Nemours And CompanyConstant boiling; ozone layer preservation and air pollution control
US5287920 *Jun 16, 1992Feb 22, 1994Terrell Donna KLarge head downhole chemical cutting tool
US5320174 *Jun 16, 1992Jun 14, 1994Terrell Donna KDownhole chemical cutting tool and process
US5444102 *Jun 30, 1994Aug 22, 1995Ikon CorporationUsing a foam blowing agent
US5491028 *Apr 18, 1995Feb 13, 1996Trustees Of Boston UniversityFormed from oxygen and acetylene in a combustion flame in the presence of a deposition promoter
US5520826 *May 16, 1994May 28, 1996The United States Of America As Represented By The Secretary Of The NavyFlame extinguishing pyrotechnic and explosive composition
US5562764 *Jun 23, 1995Oct 8, 1996E. I. Du Pont De Nemours And CompanyProcess for preparing improved TIO2 by silicon halide addition
US5573744 *Feb 17, 1995Nov 12, 1996Kerr-Mcgee CorporationMethod for enhancing production of titanium dioxide
US20060273223 *Jan 12, 2006Dec 7, 2006Haaland Peter DFire suppression systems
US20070119602 *Jun 29, 2006May 31, 2007Eclipse Aviation Corp.Fire suppression systems
US20070119603 *Jul 10, 2006May 31, 2007Eclipse Aviation Corp.Fire suppression systems
US20080115950 *Oct 30, 2007May 22, 2008Eclipse Aviation CorporationFire suppression systems
USRE40651 *Jul 16, 2004Mar 10, 2009Eclipse Aviation CorporationEnvironmentally friendly; release bromine atoms such as phosphorous tribromide (PBr3), thionyl bromide (SOBr2), boron tribromide (BBr3), and the like are very efficient at extinguishing fires; hydrolyze or oxidize rapidly in troposphere and consequently they have no stratospheric ozone depletion, airbag
JPS569230A * Title not available
SU981338A1 * Title not available
WO1993015794A1 *Jan 22, 1993Aug 19, 1993Bejaro Product AbGas-liquid mixture as well as unit and method for the use thereof
Non-Patent Citations
Reference
1 *A.N. Baratov, A Review of Investigations on the Chemical Inhibition of Flames, Problems in Combustion and Extinguishment, 1968, 29-51, TsNIIPO MOOP, Moscow.
2 *Chemical Abstracts No. 117:134014, "Preparation of a Fire Extinguishing Composition", Valukonis et al. (1991).
3 *Chemical Abstracts No. 98:129086. "Combustion inhibitor for hydrocarbon-air Mixture", Petrova et al. (1982).
4 *CRC Handbook of Chemistry and Physics, 63rd Edition. pp. B-84, B-97, B-106, B-125, B-127, B-143, B-157, B-159 and C-525, (1982).
5 *D.R. Miller, et al., Effects of Various Inhibitors on Hydrogen-Air Flame Speeds, Combustion and Flame, Mar. 1963, 137-142, vol. 7, Butterworths, London.
6 *D.R. Miller, et al., Effects of Various Inhibitors on Hydrogen—Air Flame Speeds, Combustion and Flame, Mar. 1963, 137-142, vol. 7, Butterworths, London.
7 *Final Technical Report FR-4021 Halogen Replacement for Aviation Systems, Peter D. Haaland & John H Huntington, May 1994-Nov. 1994.
8 *G. Lask & H. GG. Wagner, Influence of Additives on the Velocity of Laminar Flames, 8th Symposium (International) on Combustion, 1962, 432-438, Williams & Wilkens Co.,Baltimore.
9 *Hawley's Condensed Chemical Dictionary, 11u~ Edition, pp. 164, 169, 170, 173,329,642,913, and 1040, Van Nostrand Reinhold Company, N.Y. (1987).
10 *Hawley's Condensed Chemical Dictionary, 11u˜ Edition, pp. 164, 169, 170, 173,329,642,913, and 1040, Van Nostrand Reinhold Company, N.Y. (1987).
11 *Letter dated Aug. 15, 2006, from T. Howard to J. Sawtelle.
12 *Letter dated Aug. 18, 2006, from J. Sawtelle to T. Howard.
13 *The Montreal Protocol on Substances that Deplete the Ozone Layer, 2000, 1-47, UNEP Ozone Secretariat UN Environment Programme, Kenya.
14 *W.A. Rosser, et al., The Effect of Metal Salts on Premixed Hydrocarbon-Air Flames, Combustion and Flame, Mar. 1963, 107-119, vol. 7, Butterworths, London.
15 *W.A. Rosser, et al., The Effect of Metal Salts on Premixed Hydrocarbon—Air Flames, Combustion and Flame, Mar. 1963, 107-119, vol. 7, Butterworths, London.
16 *W.A. Rosser, et al., The Quenching of Premixed Flames by Volatile Inhibitors, ICombustion and Flame, Mar. 1966, 287-294, vol. 10, Butterworths, London.
Classifications
U.S. Classification252/2, 252/8, 252/4, 252/3, 169/46, 169/47, 252/5
International ClassificationA62D1/00, A62D1/08
Cooperative ClassificationA62D1/0028, A62D1/0092, A62D1/0014
European ClassificationA62D1/00C, A62D1/00B2, A62D1/00G