US3126304A - Ammonium nitrate gas generator - Google Patents
Ammonium nitrate gas generator Download PDFInfo
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- US3126304A US3126304A US3126304DA US3126304A US 3126304 A US3126304 A US 3126304A US 3126304D A US3126304D A US 3126304DA US 3126304 A US3126304 A US 3126304A
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- US
- United States
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- ammonium nitrate
- carbon
- gas
- gas generator
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- PAWQVTBBRAZDMG-UHFFFAOYSA-N 2-(3-bromo-2-fluorophenyl)acetic acid Chemical compound OC(=O)CC1=CC=CC(Br)=C1F PAWQVTBBRAZDMG-UHFFFAOYSA-N 0.000 title claims description 20
- 239000000203 mixture Substances 0.000 claims description 32
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 21
- 229920002301 cellulose acetate Polymers 0.000 claims description 11
- 239000003054 catalyst Substances 0.000 claims description 10
- -1 AROMATIC HYDROCARBON AMINE Chemical class 0.000 claims description 9
- YIWOOPQOYHKISC-UHFFFAOYSA-N [O-][N+](=O)CC(O)([N+]([O-])=O)OC1=CC=CC=C1 Chemical compound [O-][N+](=O)CC(O)([N+]([O-])=O)OC1=CC=CC=C1 YIWOOPQOYHKISC-UHFFFAOYSA-N 0.000 claims description 8
- VBIXEXWLHSRNKB-UHFFFAOYSA-N ammonium oxalate Chemical compound [NH4+].[NH4+].[O-]C(=O)C([O-])=O VBIXEXWLHSRNKB-UHFFFAOYSA-N 0.000 claims description 8
- WEAPVABOECTMGR-UHFFFAOYSA-N triethyl 2-acetyloxypropane-1,2,3-tricarboxylate Chemical compound CCOC(=O)CC(C(=O)OCC)(OC(C)=O)CC(=O)OCC WEAPVABOECTMGR-UHFFFAOYSA-N 0.000 claims description 8
- FHQRDEDZJIFJAL-UHFFFAOYSA-N 4-phenylmorpholine Chemical compound C1COCCN1C1=CC=CC=C1 FHQRDEDZJIFJAL-UHFFFAOYSA-N 0.000 claims description 7
- 229910052799 carbon Inorganic materials 0.000 claims description 7
- 239000003112 inhibitor Substances 0.000 claims description 7
- 229910052783 alkali metal Inorganic materials 0.000 claims description 6
- 150000001340 alkali metals Chemical class 0.000 claims description 3
- 229940125717 barbiturate Drugs 0.000 claims description 3
- 239000008247 solid mixture Substances 0.000 claims description 3
- HNYOPLTXPVRDBG-UHFFFAOYSA-N barbituric acid Chemical compound O=C1CC(=O)NC(=O)N1 HNYOPLTXPVRDBG-UHFFFAOYSA-N 0.000 claims description 2
- 239000007789 gas Substances 0.000 description 23
- 239000000463 material Substances 0.000 description 12
- 239000006229 carbon black Substances 0.000 description 10
- 235000019241 carbon black Nutrition 0.000 description 10
- 239000003380 propellant Substances 0.000 description 8
- 239000011324 bead Substances 0.000 description 7
- 239000011230 binding agent Substances 0.000 description 7
- PAYRUJLWNCNPSJ-UHFFFAOYSA-N Aniline Chemical compound NC1=CC=CC=C1 PAYRUJLWNCNPSJ-UHFFFAOYSA-N 0.000 description 6
- 238000002485 combustion reaction Methods 0.000 description 6
- 239000002245 particle Substances 0.000 description 5
- MHQHHBYRYFICDV-UHFFFAOYSA-M sodium;pyrimidin-3-ide-2,4,6-trione Chemical compound [Na+].O=C1CC(=O)[N-]C(=O)N1 MHQHHBYRYFICDV-UHFFFAOYSA-M 0.000 description 5
- 150000001875 compounds Chemical class 0.000 description 4
- VOZKAJLKRJDJLL-UHFFFAOYSA-N 2,4-diaminotoluene Chemical compound CC1=CC=C(N)C=C1N VOZKAJLKRJDJLL-UHFFFAOYSA-N 0.000 description 3
- QTBSBXVTEAMEQO-UHFFFAOYSA-N Acetic acid Chemical compound CC(O)=O QTBSBXVTEAMEQO-UHFFFAOYSA-N 0.000 description 3
- AFBPFSWMIHJQDM-UHFFFAOYSA-N N-methylaniline Chemical compound CNC1=CC=CC=C1 AFBPFSWMIHJQDM-UHFFFAOYSA-N 0.000 description 3
- 230000000274 adsorptive effect Effects 0.000 description 3
- 239000001257 hydrogen Substances 0.000 description 3
- 229910052739 hydrogen Inorganic materials 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000002156 mixing Methods 0.000 description 3
- 239000003921 oil Substances 0.000 description 3
- 230000000717 retained effect Effects 0.000 description 3
- 238000003860 storage Methods 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- KRKNYBCHXYNGOX-UHFFFAOYSA-K Citrate Chemical compound [O-]C(=O)CC(O)(CC([O-])=O)C([O-])=O KRKNYBCHXYNGOX-UHFFFAOYSA-K 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 2
- CDBYLPFSWZWCQE-UHFFFAOYSA-L Sodium Carbonate Chemical compound [Na+].[Na+].[O-]C([O-])=O CDBYLPFSWZWCQE-UHFFFAOYSA-L 0.000 description 2
- 125000000217 alkyl group Chemical group 0.000 description 2
- 125000003118 aryl group Chemical group 0.000 description 2
- 125000004432 carbon atom Chemical group C* 0.000 description 2
- DMBHHRLKUKUOEG-UHFFFAOYSA-N diphenylamine Chemical compound C=1C=CC=CC=1NC1=CC=CC=C1 DMBHHRLKUKUOEG-UHFFFAOYSA-N 0.000 description 2
- 229910002804 graphite Inorganic materials 0.000 description 2
- 239000010439 graphite Substances 0.000 description 2
- 229930195733 hydrocarbon Natural products 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 239000002006 petroleum coke Substances 0.000 description 2
- FGIUAXJPYTZDNR-UHFFFAOYSA-N potassium nitrate Chemical compound [K+].[O-][N+]([O-])=O FGIUAXJPYTZDNR-UHFFFAOYSA-N 0.000 description 2
- VWDWKYIASSYTQR-UHFFFAOYSA-N sodium nitrate Chemical compound [Na+].[O-][N+]([O-])=O VWDWKYIASSYTQR-UHFFFAOYSA-N 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- CBSCOKJVHQZELD-UHFFFAOYSA-N 1-[1-(2,3-dinitrophenoxy)ethoxy]-2,3-dinitrobenzene Chemical compound [N+](=O)([O-])C=1C(=C(OC(C)OC2=C(C(=CC=C2)[N+](=O)[O-])[N+](=O)[O-])C=CC1)[N+](=O)[O-] CBSCOKJVHQZELD-UHFFFAOYSA-N 0.000 description 1
- CDULGHZNHURECF-UHFFFAOYSA-N 2,3-dimethylaniline 2,4-dimethylaniline 2,5-dimethylaniline 2,6-dimethylaniline 3,4-dimethylaniline 3,5-dimethylaniline Chemical group CC1=CC=C(N)C(C)=C1.CC1=CC=C(C)C(N)=C1.CC1=CC(C)=CC(N)=C1.CC1=CC=C(N)C=C1C.CC1=CC=CC(N)=C1C.CC1=CC=CC(C)=C1N CDULGHZNHURECF-UHFFFAOYSA-N 0.000 description 1
- SOANRMMGFPUDDF-UHFFFAOYSA-N 2-dodecylaniline Chemical compound CCCCCCCCCCCCC1=CC=CC=C1N SOANRMMGFPUDDF-UHFFFAOYSA-N 0.000 description 1
- JLTDJTHDQAWBAV-UHFFFAOYSA-N N,N-dimethylaniline Chemical compound CN(C)C1=CC=CC=C1 JLTDJTHDQAWBAV-UHFFFAOYSA-N 0.000 description 1
- XQVWYOYUZDUNRW-UHFFFAOYSA-N N-Phenyl-1-naphthylamine Chemical compound C=1C=CC2=CC=CC=C2C=1NC1=CC=CC=C1 XQVWYOYUZDUNRW-UHFFFAOYSA-N 0.000 description 1
- MUBZPKHOEPUJKR-UHFFFAOYSA-N Oxalic acid Chemical compound OC(=O)C(O)=O MUBZPKHOEPUJKR-UHFFFAOYSA-N 0.000 description 1
- 239000004264 Petrolatum Substances 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 125000000218 acetic acid group Chemical group C(C)(=O)* 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- HSFWRNGVRCDJHI-UHFFFAOYSA-N alpha-acetylene Natural products C#C HSFWRNGVRCDJHI-UHFFFAOYSA-N 0.000 description 1
- 150000001412 amines Chemical class 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 150000001721 carbon Chemical class 0.000 description 1
- 229920002678 cellulose Polymers 0.000 description 1
- 239000001913 cellulose Substances 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 239000000571 coke Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000001877 deodorizing effect Effects 0.000 description 1
- 238000010410 dusting Methods 0.000 description 1
- 125000002534 ethynyl group Chemical group [H]C#C* 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 238000005188 flotation Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 150000002430 hydrocarbons Chemical class 0.000 description 1
- 125000001183 hydrocarbyl group Chemical group 0.000 description 1
- 150000002431 hydrogen Chemical class 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 229910001959 inorganic nitrate Inorganic materials 0.000 description 1
- 238000002386 leaching Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- LAMTXWQPHWUMLX-UHFFFAOYSA-N n-butan-2-ylaniline Chemical compound CCC(C)NC1=CC=CC=C1 LAMTXWQPHWUMLX-UHFFFAOYSA-N 0.000 description 1
- 125000001624 naphthyl group Chemical group 0.000 description 1
- 150000005002 naphthylamines Chemical class 0.000 description 1
- 125000004957 naphthylene group Chemical group 0.000 description 1
- 239000003345 natural gas Substances 0.000 description 1
- 229910021382 natural graphite Inorganic materials 0.000 description 1
- 229930014626 natural product Natural products 0.000 description 1
- 150000002823 nitrates Chemical class 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 235000019645 odor Nutrition 0.000 description 1
- 239000011368 organic material Substances 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 229940066842 petrolatum Drugs 0.000 description 1
- 235000019271 petrolatum Nutrition 0.000 description 1
- 239000003208 petroleum Substances 0.000 description 1
- 125000001997 phenyl group Chemical group [H]C1=C([H])C([H])=C(*)C([H])=C1[H] 0.000 description 1
- MEGDIQXLXPPWGL-UHFFFAOYSA-N phenylmethanetriamine Chemical compound NC(N)(N)C1=CC=CC=C1 MEGDIQXLXPPWGL-UHFFFAOYSA-N 0.000 description 1
- 239000004014 plasticizer Substances 0.000 description 1
- 239000004323 potassium nitrate Substances 0.000 description 1
- 235000010333 potassium nitrate Nutrition 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 239000000779 smoke Substances 0.000 description 1
- 229910000029 sodium carbonate Inorganic materials 0.000 description 1
- 239000004317 sodium nitrate Substances 0.000 description 1
- 235000010344 sodium nitrate Nutrition 0.000 description 1
- 239000011343 solid material Substances 0.000 description 1
- 238000001179 sorption measurement Methods 0.000 description 1
- 239000011269 tar Substances 0.000 description 1
- 238000005979 thermal decomposition reaction Methods 0.000 description 1
- AXNUJYHFQHQZBE-UHFFFAOYSA-N toluenediamine group Chemical group C1(=C(C(=CC=C1)N)N)C AXNUJYHFQHQZBE-UHFFFAOYSA-N 0.000 description 1
- 150000004992 toluidines Chemical class 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B23/00—Compositions characterised by non-explosive or non-thermic constituents
- C06B23/007—Ballistic modifiers, burning rate catalysts, burning rate depressing agents, e.g. for gas generating
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B31/00—Compositions containing an inorganic nitrogen-oxygen salt
- C06B31/28—Compositions containing an inorganic nitrogen-oxygen salt the salt being ammonium nitrate
- C06B31/30—Compositions containing an inorganic nitrogen-oxygen salt the salt being ammonium nitrate with vegetable matter; with resin; with rubber
Definitions
- This invention relates to ammonium nitrate compositions suitable for use as gas generating materials having a relatively high burning rate, clean exhaust gases, and moderate flame temperature.
- Ammonium nitrate based propellant materials are used for gas generation purposes where the exhaust gas from the combustion of the propellant is used to drive the turbine prime mover.
- the temperature of the exhaust gases should be as low as possible [for the particular application in order to economize upon the type of metal used in the gas transfer lines or the amount of metal present to give a certain predetermined strength.
- the exhaust gases In order to keep the gas transfer lines and the turbine chamber as free from deposits as possible, it is desired that the exhaust gases be clean, i.e., have a minimum of solid material present theerin.
- Gas generating compositions need to be storage stable for long periods and over wide ranges of atmospheric temperatures; this is especially true in the case of compositions intended for military use.
- the gas generator composition of the invention contains about 6-7% of cellulose acetate, about 89.4% of acetyl trie'thyl citrate, about 7.18 .4% of essentially pure dinitrophenoxyethanol, about 0.8-1.5 of alkali metal barbiturate combustion catalyst, about 4.56.4% of finely divided carbon, about 02-03% of ammonium oxalate, about 0.5l.5% of aromatic hydrocarbon amine gassing inhibitor, about 02-05% of N- phenylmorpholine, and the remainder essentially ammonium nitrate.
- An especially suitable composition consists of about 6.5% of cellulose acetate, about 8.8% of acetyl triethyl citrate, about 7.7% of pure dinitrophenoxyethanol, about 1% of sodium barbiturate, about of carbon black, about 0.2% of diammonium oxalate, about 1% of toluene diamine, about 0.2% of N-phenylmorpholine, and the remainder ammonium nitrate. (It is to be understood that all percentages set out herein are weight percent.)
- ammonium nitrate as used in this specification and in the claims is intended to mean either C.P. grade or ordinary commercial grade ammonium nitrate or military grade.
- the particles may be coated with a small amount of moisture-resisting material such as petrolatum or parafiin. A minor amount of other inorganic nitrates such as sodium nitrate and/or potassium nitrate may be present. Finely ground ammonium nitrate is preferred.
- the combustion catalyst utilized in the composition of the invention is an alkali metal salt of barbituric acid.
- the sodium barbiturate is preferred.
- the catalyst is present in the low amount of about 0.8-1.5% and usually about 1.0%.
- composition of the invention includes, as a cooling material, an ammonium oxalate, preferably diammonium oxalate, dispersed intimately throughout the binder material.
- ammonium oxalate preferably diammonium oxalate
- the oxalate is present in the minor amount of about 02-03%.
- composition of the invention also includes N-phenylmorpholine, which may be the pure compound or commercial technical grade material, in an amount of about 02-05%.
- the composition of the invention includes finely divided carbon as a burning rate accelerator in an amount of about 4.5-6.4% and more commonly 4.8-5.5%.
- the carbon component of the propellant composition includes finely divided, highly adsorptive activated carbons. These are well known in the art of decolorizing sugar and adsorption of gases. Examples of these are Norit and Nuchar, the former being a highly-adsorptive activated carbon used to adsorb odors, and to decolorize water, gases, chemical solutions, oils and greases. Nuchar is an activated carbon made from a residual organic material obtained in the manufacture of cellulose and is characterized by high porosity resulting in high adsorptive capacity. Like Norit it is used as a decolorizing and deodorizing agent.
- carbon blacks Another general class of carbon useful for increasing the burning rate of the propellant composition are the carbon blacks. These are roughly classified as channel blacks prepared by the impingement of small natural gas flames, furnace combustion blacks producedf by the partial combustion of essentially gaseous hydrocarbons in closed retorts and furnace thermal blacks produced by thermal decomposition of hydrocarbons such as acetylene in preheated furnaces.
- the carbon blacks are characterized by low ash content by having extremely small particle size, that is, 50 to 5000 A., and contain adsorbed hydrogen and oxygen.
- Other carbon blacks which may be used in the propellant grains are lamp blacks produced by burning liquid fuels such as petroleum oils, tars and aromatic residues in specially designed pans, combustion taking place under restricted air supply conditions.
- the carbon blacks as indicated above are generally characterized by exceedingly small particle size, that is, well below #325 US. Standard sieve particle size. However, to avoid dusting and convenience in handling, some carbon blacks are formed to the so-called bead type carbon blacks which beads are generally of such dimensions as to pass through a #20 US. Standard sieve and are retained on a #200 US. Standard sieve. The beads are very soft and are physically unstable as beads and become disintegrated to smaller than #325 US. Standard sieve during the mixing and milling of the composited propellant components as described hereinbelow.
- the carbon blacks are of low ash content, and usually contain less than 0.5% ash. Examples of bead type carbon blacks are Micronex Beads (channel blacks) and Statex Beads (furnace blacks).
- Yet another type of carbon which is useful for improving the burning rate of our gas-producing propellant composition is graphite, flake and amorphous. If derived from a natural graphite, the ash content should be reduced below about 5% which can be accomplished by treating the natural product by air flotation or the ash content may be reduced by leaching with mineral acid or by other methods well known to the art. We prefer graphite of colloidal or semi-colloidal particle size.
- Still another type of carbon which has been found effective for increasing the burning rate of the gas-forming composition is finely ground petroleum coke, particularly petroleum coke obtained as a residue in the pipe-stilling of Mid-Continent heavy residuums.
- coke usually contains les than about 1% ash and is preferably pulverized to pass through a #325 U.S. Standard sive prior to incorporation in the gas-producing propellant composition.
- the composition of the invention includes a gassing inhibitor component.
- Aromatic hydrocarbon amines when introduced into the ammonium nitrate based grain have the very desirable characteristic of decreasing the amount of gassing in high temperature storage; frequently they eliminate gassing for prolonged periods of time.
- the gassing inhibitors used here are illustrated by diphenylamine, dinapht'nylamine, phenyl naphthylamine.
- the linkage between the naphthyl radical and the nitrogen may be either alpha or beta; and those amines represented by the empirical formula: RZ(NR'R") where Z is an aromatic nucleus selected from the class consisting of phenyl and naphthyl; R is selected from the class consisting of hydrogen and alkyl containing from 1 to 12 carbon atoms; R and R" are selected from the class consisting of hydrogen, and alkyl containing from 1 to 4 carbon atoms; and x is an integer from 1 to 3.
- monoamine compounds examples include: aniline (monophenylamine, monoamino benzene), l-naphthylamine, toluidine (methylaniline) xylidine (dimethylaniline), dodecyl aniline, N-methyl aniline, N,N-dimetl1y1 aniline, N-sec-butyl aniline.
- diamine compounds examples include diamino benzene (phenylene diamine), diamino toluene (toluene diamine), diamino naphthylene, methyl diamino naphthylene, dodecyl diamino naphthylene, i -secbutyl, diamino benzene, N,N-di-sec-butyl diamino benzene, and N-methyl diamino naphthylene.
- diamino benzene phenylene diamine
- diamino toluene toluene diamine
- diamino naphthylene methyl diamino naphthylene
- dodecyl diamino naphthylene i -secbutyl
- diamino benzene N,N-di-sec-butyl diamino benzene
- N-methyl diamino naphthylene examples
- triamine compounds are: triamino ben- Zeno, triamino naphthylene, triamino toluene, and triamino methyl naphthylene.
- the matrix former or binder material utilized in the instant composition consists of cellulose acetate, acetyl triethyl citrate and dinitrophenoxyethanol.
- the acetyl triethyl citrate is a well known plasticizer.
- the citrate may be the pure compound or commercial technical grade.
- the dinitrophenoxyethanol component is the pure or essentially pure material; i.e., contains 5% of the bis- (dinitrophenoxy)ethane. In all cases, the dinitrophenoxyethanol is the predominant member and usually will represent 70% or more of this component.
- U.S. Patent No. 2,988,571 sets out a method of preparation of dinitrophenoxyethanol suitable for use herein.
- the polymeric material present in the binder is cellulose acetate.
- Particularly suitable are the cellulose acetates which have combined acetic acid contents on the order of 50-58%.
- a preferred cellulose acetate is one made by Eastman Chemical Products, Inc, as Eastma 60.
- the binder materials are present, based on the whole composition, of about 67% of cellulose acetate, about 53-94% of acetyl triethyl citrate, and about 7.1-8.4% of dinitrophenoxyethancl. The relative proportions of these components will vary within these ranges as determined by the specification requirements of the composition.
- Illustration A generating composition was prepared by introducing the organic binder materials into a heated kettle provided with a mechanical stirrer; this composition is identified as Mark 4565.
- the binder materials were raised to a temperature Where they became a viscous homogeneous liquid.
- the catalyst and other additives were blended into the molten binder before the addition of the solid ammonium nitrate.
- the temperature of the mixing operation was held below 130 C.
- the ammonium nitrate was of a screen size: passing through a 14 number screen and retained by a 30 number screen; about 12% retained by a 80 number screen and passing through a 30 number screen; about 5% smaller than 80 number screen and the remainder larger than 14 number screen.
- composition Mark 4565 Ammonium nitrate 69.6 Cellulose acetate (Eastman-60) 6.5 Acetyl triethyl citrate 8.8 Dintrophenoxyethanol 7.7 Carbon black (Norite) 5.0 Sodium barbiturate 1.0 Toluene diamine 1.0 N phenylmorpholine 0.2 Diammonium oxalate 0.2
- a solid composition consisting of cellulose acetate, about 6-7%; acetyl triethyl citrate, about 89.4%; dinitrcphenoxyethanol, about 7.1-8.4%; alkali metal barbiturate catalyst, about 0.8-1.5%; finely divided carbon, about 4.5-6.4% ammonium oxalate, about 0.2-0.3%; aromatic hydrocarbon amine gassing inhibitor, about 0.5-1.5%; N-phenylmorpholine, about 0.2-0.5% and the remainder of said composition being essentially ammonium nitrate.
- composition of claim 1 wherein said gassing inhibitor is toluene diamine.
- composition of claim 1 wherein said catalyst is sodium barbiturate.
- a solid composition consisting of cellulose acetate, about 6.5%; acetyl triethyl citrate, about 8.8%; dinitrophenoxyethanol, about 7.7%; sodium barbiturate, about 1%; adsorptive activated carbon, about 5%; diammonium oxalate, about 0.2%; toluene diamine gassing inhibitor, about 1.0%; N-phenylmorpholine, about 0.2%; and the remainder of said composition being ammonium nitrate.
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- Organic Chemistry (AREA)
- Inorganic Chemistry (AREA)
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Description
United States Patent 3,126,304 AMMONIUM NITRATE GAS GENERATOR COMTOSITION Keith G. Penner and William G. Stanley, Seymour, Ind,
assignors to Standard Oil Company, Chicago, 111., a
corporation of Indiana No Drawing. Filed Aug. 27, 1962, Ser. No. 219,735
4 Claims. (1. 149-19) This invention relates to ammonium nitrate compositions suitable for use as gas generating materials having a relatively high burning rate, clean exhaust gases, and moderate flame temperature.
Ammonium nitrate based propellant materials are used for gas generation purposes where the exhaust gas from the combustion of the propellant is used to drive the turbine prime mover. The temperature of the exhaust gases (flame temperature) should be as low as possible [for the particular application in order to economize upon the type of metal used in the gas transfer lines or the amount of metal present to give a certain predetermined strength. In order to keep the gas transfer lines and the turbine chamber as free from deposits as possible, it is desired that the exhaust gases be clean, i.e., have a minimum of solid material present theerin. Gas generating compositions need to be storage stable for long periods and over wide ranges of atmospheric temperatures; this is especially true in the case of compositions intended for military use. It has been observed that even the alkali metal containing catalysts for the acceleration of the decomposition of ammonium nitrate produce some undesirable solid residues such as sodium carbonate and, therefore, it is desirable for many uses to have a low alkali metal containing catalyst content. On the other hand, many uses require a relatively high burning rate (inches per second at a given temperature and pressure) which burning rate is normally attained by using large amounts of such catalyst. It is the principal object of this invention to provide an ammonium nitrate composition particularly suitable for gas generator purposes which meets the above stringent requirements. Other objects of the invention will become apparent in the course of the detailed description thereof.
Broadly, the gas generator composition of the invention contains about 6-7% of cellulose acetate, about 89.4% of acetyl trie'thyl citrate, about 7.18 .4% of essentially pure dinitrophenoxyethanol, about 0.8-1.5 of alkali metal barbiturate combustion catalyst, about 4.56.4% of finely divided carbon, about 02-03% of ammonium oxalate, about 0.5l.5% of aromatic hydrocarbon amine gassing inhibitor, about 02-05% of N- phenylmorpholine, and the remainder essentially ammonium nitrate. An especially suitable composition consists of about 6.5% of cellulose acetate, about 8.8% of acetyl triethyl citrate, about 7.7% of pure dinitrophenoxyethanol, about 1% of sodium barbiturate, about of carbon black, about 0.2% of diammonium oxalate, about 1% of toluene diamine, about 0.2% of N-phenylmorpholine, and the remainder ammonium nitrate. (It is to be understood that all percentages set out herein are weight percent.)
The term ammonium nitrate as used in this specification and in the claims is intended to mean either C.P. grade or ordinary commercial grade ammonium nitrate or military grade. The particles may be coated with a small amount of moisture-resisting material such as petrolatum or parafiin. A minor amount of other inorganic nitrates such as sodium nitrate and/or potassium nitrate may be present. Finely ground ammonium nitrate is preferred.
The combustion catalyst utilized in the composition of the invention is an alkali metal salt of barbituric acid. The sodium barbiturate is preferred. The catalyst is present in the low amount of about 0.8-1.5% and usually about 1.0%.
The composition of the invention includes, as a cooling material, an ammonium oxalate, preferably diammonium oxalate, dispersed intimately throughout the binder material. The oxalate is present in the minor amount of about 02-03%.
The composition of the invention also includes N-phenylmorpholine, which may be the pure compound or commercial technical grade material, in an amount of about 02-05%.
The composition of the invention includes finely divided carbon as a burning rate accelerator in an amount of about 4.5-6.4% and more commonly 4.8-5.5%. The carbon component of the propellant composition includes finely divided, highly adsorptive activated carbons. These are well known in the art of decolorizing sugar and adsorption of gases. Examples of these are Norit and Nuchar, the former being a highly-adsorptive activated carbon used to adsorb odors, and to decolorize water, gases, chemical solutions, oils and greases. Nuchar is an activated carbon made from a residual organic material obtained in the manufacture of cellulose and is characterized by high porosity resulting in high adsorptive capacity. Like Norit it is used as a decolorizing and deodorizing agent.
Another general class of carbon useful for increasing the burning rate of the propellant composition are the carbon blacks. These are roughly classified as channel blacks prepared by the impingement of small natural gas flames, furnace combustion blacks producedf by the partial combustion of essentially gaseous hydrocarbons in closed retorts and furnace thermal blacks produced by thermal decomposition of hydrocarbons such as acetylene in preheated furnaces. The carbon blacks are characterized by low ash content by having extremely small particle size, that is, 50 to 5000 A., and contain adsorbed hydrogen and oxygen. Other carbon blacks which may be used in the propellant grains are lamp blacks produced by burning liquid fuels such as petroleum oils, tars and aromatic residues in specially designed pans, combustion taking place under restricted air supply conditions. The carbon blacks as indicated above are generally characterized by exceedingly small particle size, that is, well below #325 US. Standard sieve particle size. However, to avoid dusting and convenience in handling, some carbon blacks are formed to the so-called bead type carbon blacks which beads are generally of such dimensions as to pass through a #20 US. Standard sieve and are retained on a #200 US. Standard sieve. The beads are very soft and are physically unstable as beads and become disintegrated to smaller than #325 US. Standard sieve during the mixing and milling of the composited propellant components as described hereinbelow. The carbon blacks are of low ash content, and usually contain less than 0.5% ash. Examples of bead type carbon blacks are Micronex Beads (channel blacks) and Statex Beads (furnace blacks).
Yet another type of carbon which is useful for improving the burning rate of our gas-producing propellant composition is graphite, flake and amorphous. If derived from a natural graphite, the ash content should be reduced below about 5% which can be accomplished by treating the natural product by air flotation or the ash content may be reduced by leaching with mineral acid or by other methods well known to the art. We prefer graphite of colloidal or semi-colloidal particle size.
Still another type of carbon which has been found effective for increasing the burning rate of the gas-forming composition is finely ground petroleum coke, particularly petroleum coke obtained as a residue in the pipe-stilling of Mid-Continent heavy residuums. Such Patented Mar. 24-, 1964: v
coke usually contains les than about 1% ash and is preferably pulverized to pass through a #325 U.S. Standard sive prior to incorporation in the gas-producing propellant composition.
Ammonium nitrate compositions in general tend to develop gas in storage at elevated temperatures. The composition of the invention includes a gassing inhibitor component. Aromatic hydrocarbon amines when introduced into the ammonium nitrate based grain have the very desirable characteristic of decreasing the amount of gassing in high temperature storage; frequently they eliminate gassing for prolonged periods of time. The gassing inhibitors used here are illustrated by diphenylamine, dinapht'nylamine, phenyl naphthylamine. In the case of the naphthyl amines, the linkage between the naphthyl radical and the nitrogen may be either alpha or beta; and those amines represented by the empirical formula: RZ(NR'R") where Z is an aromatic nucleus selected from the class consisting of phenyl and naphthyl; R is selected from the class consisting of hydrogen and alkyl containing from 1 to 12 carbon atoms; R and R" are selected from the class consisting of hydrogen, and alkyl containing from 1 to 4 carbon atoms; and x is an integer from 1 to 3.
Examples of monoamine compounds are: aniline (monophenylamine, monoamino benzene), l-naphthylamine, toluidine (methylaniline) xylidine (dimethylaniline), dodecyl aniline, N-methyl aniline, N,N-dimetl1y1 aniline, N-sec-butyl aniline.
Examples of the diamine compounds are: diamino benzene (phenylene diamine), diamino toluene (toluene diamine), diamino naphthylene, methyl diamino naphthylene, dodecyl diamino naphthylene, i -secbutyl, diamino benzene, N,N-di-sec-butyl diamino benzene, and N-methyl diamino naphthylene.
Examples of triamine compounds are: triamino ben- Zeno, triamino naphthylene, triamino toluene, and triamino methyl naphthylene.
The matrix former or binder material utilized in the instant composition consists of cellulose acetate, acetyl triethyl citrate and dinitrophenoxyethanol.
The acetyl triethyl citrate is a well known plasticizer. The citrate may be the pure compound or commercial technical grade.
The dinitrophenoxyethanol component is the pure or essentially pure material; i.e., contains 5% of the bis- (dinitrophenoxy)ethane. In all cases, the dinitrophenoxyethanol is the predominant member and usually will represent 70% or more of this component. U.S. Patent No. 2,988,571 sets out a method of preparation of dinitrophenoxyethanol suitable for use herein.
The polymeric material present in the binder is cellulose acetate. Particularly suitable are the cellulose acetates which have combined acetic acid contents on the order of 50-58%. A preferred cellulose acetate is one made by Eastman Chemical Products, Inc, as Eastma 60.
The binder materials are present, based on the whole composition, of about 67% of cellulose acetate, about 53-94% of acetyl triethyl citrate, and about 7.1-8.4% of dinitrophenoxyethancl. The relative proportions of these components will vary within these ranges as determined by the specification requirements of the composition.
Illustration A generating composition was prepared by introducing the organic binder materials into a heated kettle provided with a mechanical stirrer; this composition is identified as Mark 4565. The binder materials were raised to a temperature Where they became a viscous homogeneous liquid. The catalyst and other additives were blended into the molten binder before the addition of the solid ammonium nitrate. During the blending of the ammonium nitrate, the temperature of the mixing operation was held below 130 C. In this instance, the ammonium nitrate was of a screen size: passing through a 14 number screen and retained by a 30 number screen; about 12% retained by a 80 number screen and passing through a 30 number screen; about 5% smaller than 80 number screen and the remainder larger than 14 number screen.
Data were obtained on burning rates at 70 F. and 1,000 p.s.i.a. by the Crawford Bomb Method. The approximate gas composition produced was obtained and the exhaust gas temperature calculated-attempts to measure exhaust gas temperature were subject to such lack of reproducibility as to be valueless for evaluation of dif ferences between compositions. The smokiness of the gas stream was noted. The composition here passed the military specification requirements.
Composition: Mark 4565 Ammonium nitrate 69.6 Cellulose acetate (Eastman-60) 6.5 Acetyl triethyl citrate 8.8 Dintrophenoxyethanol 7.7 Carbon black (Norite) 5.0 Sodium barbiturate 1.0 Toluene diamine 1.0 N phenylmorpholine 0.2 Diammonium oxalate 0.2
Exhaust gas temperature, F 2210 Burning rate, inches per second 0.130
Smoke None Specific impulse, seconds 184 Gas composition, mol percent:
CO 20.5 CO 9.5 H 22.3 H O 28.4 N 19.3
Thus having described the invention, what is claimed is:
1. A solid composition consisting of cellulose acetate, about 6-7%; acetyl triethyl citrate, about 89.4%; dinitrcphenoxyethanol, about 7.1-8.4%; alkali metal barbiturate catalyst, about 0.8-1.5%; finely divided carbon, about 4.5-6.4% ammonium oxalate, about 0.2-0.3%; aromatic hydrocarbon amine gassing inhibitor, about 0.5-1.5%; N-phenylmorpholine, about 0.2-0.5% and the remainder of said composition being essentially ammonium nitrate.
2. The composition of claim 1 wherein said gassing inhibitor is toluene diamine.
3. The composition of claim 1 wherein said catalyst is sodium barbiturate.
4. A solid composition consisting of cellulose acetate, about 6.5%; acetyl triethyl citrate, about 8.8%; dinitrophenoxyethanol, about 7.7%; sodium barbiturate, about 1%; adsorptive activated carbon, about 5%; diammonium oxalate, about 0.2%; toluene diamine gassing inhibitor, about 1.0%; N-phenylmorpholine, about 0.2%; and the remainder of said composition being ammonium nitrate.
No references cited.
Claims (1)
1. A SOLID COMPOSITION CONSISTING OF CELLULOSE ACETATE, ABOUT 6-7%; ACETYL TRIETHYL CITRATE, ABOUT 8-9.4%; DINITROPHENOXYETHANOL, ABOUT 7.1-8.4%; ALKALI METAL BARBITURATE CATALYST, ABOUT 0.8-1.5%; FINELY DIVIDED CARBON, ABOUT 4.5-6.4%; AMMONIUM OXALATE, ABOUT 0.2-0.3%; AROMATIC HYDROCARBON AMINE GASSING INHIBITOR, ABOUT 0.5-1.5%; N-PHENYLMORPHOLINE, ABOUT 0.2-0.5%; AND THE REMAINDER OF SAID COMPOSITION BEING ESSENTIALLY AMMONIUM NITRATE.
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US3126304A true US3126304A (en) | 1964-03-24 |
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US3126304D Expired - Lifetime US3126304A (en) | Ammonium nitrate gas generator |
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3839105A (en) * | 1972-03-10 | 1974-10-01 | Thiokol Chemical Corp | Oxalyl dihydrazide compositions and use as a coolant in gas generating process |
US3986908A (en) * | 1972-07-05 | 1976-10-19 | Societe Nationale Des Poudres Et Explosifs | Composite propellants with a cellulose acetate binder |
WO1997012847A1 (en) * | 1995-10-03 | 1997-04-10 | Atlantic Research Corporation | Extrudable gas-generating compositions |
-
0
- US US3126304D patent/US3126304A/en not_active Expired - Lifetime
Non-Patent Citations (1)
Title |
---|
None * |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3839105A (en) * | 1972-03-10 | 1974-10-01 | Thiokol Chemical Corp | Oxalyl dihydrazide compositions and use as a coolant in gas generating process |
US3986908A (en) * | 1972-07-05 | 1976-10-19 | Societe Nationale Des Poudres Et Explosifs | Composite propellants with a cellulose acetate binder |
WO1997012847A1 (en) * | 1995-10-03 | 1997-04-10 | Atlantic Research Corporation | Extrudable gas-generating compositions |
US5734123A (en) * | 1995-10-03 | 1998-03-31 | Atlantic Research Corporation | Extrudable gas-generating compositions |
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