US3912561A - Pyrotechnic compositions for gas generation - Google Patents
Pyrotechnic compositions for gas generation Download PDFInfo
- Publication number
- US3912561A US3912561A US404762A US40476273A US3912561A US 3912561 A US3912561 A US 3912561A US 404762 A US404762 A US 404762A US 40476273 A US40476273 A US 40476273A US 3912561 A US3912561 A US 3912561A
- Authority
- US
- United States
- Prior art keywords
- composition
- aminotetrazole
- parts
- azide
- group
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 239000000203 mixture Substances 0.000 title claims abstract description 84
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims abstract description 40
- -1 ALKALI METAL AZIDES Chemical class 0.000 claims abstract description 30
- ULRPISSMEBPJLN-UHFFFAOYSA-N 2h-tetrazol-5-amine Chemical compound NC1=NN=NN1 ULRPISSMEBPJLN-UHFFFAOYSA-N 0.000 claims abstract description 20
- 239000000377 silicon dioxide Substances 0.000 claims abstract description 20
- JVSMPWHQUPKRNV-UHFFFAOYSA-N 2h-tetrazol-5-amine;hydrate Chemical compound O.NC=1N=NNN=1 JVSMPWHQUPKRNV-UHFFFAOYSA-N 0.000 claims abstract description 16
- 229910052783 alkali metal Inorganic materials 0.000 claims abstract description 14
- 150000001340 alkali metals Chemical class 0.000 claims abstract description 9
- 239000007800 oxidant agent Substances 0.000 claims abstract description 9
- 230000001590 oxidative effect Effects 0.000 claims abstract description 9
- JGZAFSFVZSXXCJ-ONEGZZNKSA-N (E)-bis(2H-tetrazol-5-yl)diazene Chemical compound N(=N\C1=NN=NN1)/C1=NN=NN1 JGZAFSFVZSXXCJ-ONEGZZNKSA-N 0.000 claims abstract description 6
- 229910052784 alkaline earth metal Inorganic materials 0.000 claims abstract description 6
- 239000004156 Azodicarbonamide Substances 0.000 claims abstract description 5
- 229910001485 alkali metal perchlorate Inorganic materials 0.000 claims abstract description 5
- XOZUGNYVDXMRKW-AATRIKPKSA-N azodicarbonamide Chemical compound NC(=O)\N=N\C(N)=O XOZUGNYVDXMRKW-AATRIKPKSA-N 0.000 claims abstract description 5
- 235000019399 azodicarbonamide Nutrition 0.000 claims abstract description 5
- 239000000446 fuel Substances 0.000 claims abstract description 5
- 150000001875 compounds Chemical class 0.000 claims abstract 2
- PXIPVTKHYLBLMZ-UHFFFAOYSA-N Sodium azide Chemical compound [Na+].[N-]=[N+]=[N-] PXIPVTKHYLBLMZ-UHFFFAOYSA-N 0.000 claims description 40
- 150000001540 azides Chemical class 0.000 claims description 22
- AXZAYXJCENRGIM-UHFFFAOYSA-J dipotassium;tetrabromoplatinum(2-) Chemical compound [K+].[K+].[Br-].[Br-].[Br-].[Br-].[Pt+2] AXZAYXJCENRGIM-UHFFFAOYSA-J 0.000 claims description 15
- 229910001487 potassium perchlorate Inorganic materials 0.000 claims description 15
- 239000008188 pellet Substances 0.000 claims description 9
- VLTRZXGMWDSKGL-UHFFFAOYSA-N perchloric acid Chemical compound OCl(=O)(=O)=O VLTRZXGMWDSKGL-UHFFFAOYSA-N 0.000 claims description 7
- VLTRZXGMWDSKGL-UHFFFAOYSA-M perchlorate Inorganic materials [O-]Cl(=O)(=O)=O VLTRZXGMWDSKGL-UHFFFAOYSA-M 0.000 claims description 6
- IOLCXVTUBQKXJR-UHFFFAOYSA-M potassium bromide Chemical compound [K+].[Br-] IOLCXVTUBQKXJR-UHFFFAOYSA-M 0.000 claims description 6
- CEGOLXSVJUTHNZ-UHFFFAOYSA-K aluminium tristearate Chemical compound [Al+3].CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O CEGOLXSVJUTHNZ-UHFFFAOYSA-K 0.000 claims description 5
- 239000011230 binding agent Substances 0.000 claims description 5
- 229920001343 polytetrafluoroethylene Polymers 0.000 claims description 3
- 239000004810 polytetrafluoroethylene Substances 0.000 claims description 3
- 238000010586 diagram Methods 0.000 claims description 2
- 238000002485 combustion reaction Methods 0.000 abstract description 18
- 239000007787 solid Substances 0.000 abstract description 6
- 239000000654 additive Substances 0.000 abstract description 3
- 230000000996 additive effect Effects 0.000 abstract description 3
- MWUXSHHQAYIFBG-UHFFFAOYSA-N nitrogen oxide Inorganic materials O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 description 21
- 239000000567 combustion gas Substances 0.000 description 14
- 239000007789 gas Substances 0.000 description 14
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 8
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 4
- 229910002091 carbon monoxide Inorganic materials 0.000 description 4
- 239000000470 constituent Substances 0.000 description 4
- 229910052757 nitrogen Inorganic materials 0.000 description 4
- 229940063655 aluminum stearate Drugs 0.000 description 3
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 3
- 231100000252 nontoxic Toxicity 0.000 description 3
- 230000003000 nontoxic effect Effects 0.000 description 3
- 239000001301 oxygen Substances 0.000 description 3
- 229910052760 oxygen Inorganic materials 0.000 description 3
- 239000002245 particle Substances 0.000 description 3
- KKCBUQHMOMHUOY-UHFFFAOYSA-N sodium oxide Chemical compound [O-2].[Na+].[Na+] KKCBUQHMOMHUOY-UHFFFAOYSA-N 0.000 description 3
- 229910001948 sodium oxide Inorganic materials 0.000 description 3
- 230000007423 decrease Effects 0.000 description 2
- 238000009472 formulation Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- QJGQUHMNIGDVPM-UHFFFAOYSA-N nitrogen group Chemical group [N] QJGQUHMNIGDVPM-UHFFFAOYSA-N 0.000 description 2
- 239000003380 propellant Substances 0.000 description 2
- 230000001629 suppression Effects 0.000 description 2
- 231100000331 toxic Toxicity 0.000 description 2
- 230000002588 toxic effect Effects 0.000 description 2
- 239000002341 toxic gas Substances 0.000 description 2
- 231100000419 toxicity Toxicity 0.000 description 2
- 230000001988 toxicity Effects 0.000 description 2
- 235000015842 Hesperis Nutrition 0.000 description 1
- 235000012633 Iberis amara Nutrition 0.000 description 1
- 239000003513 alkali Substances 0.000 description 1
- 229910000272 alkali metal oxide Inorganic materials 0.000 description 1
- 229910000287 alkaline earth metal oxide Inorganic materials 0.000 description 1
- 239000003054 catalyst Substances 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 231100000171 higher toxicity Toxicity 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 125000004435 hydrogen atom Chemical class [H]* 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 231100001231 less toxic Toxicity 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- QIQXTHQIDYTFRH-UHFFFAOYSA-N octadecanoic acid Chemical compound CCCCCCCCCCCCCCCCCC(O)=O QIQXTHQIDYTFRH-UHFFFAOYSA-N 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 150000004760 silicates 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
- C06B43/00—Compositions characterised by explosive or thermic constituents not provided for in groups C06B25/00 - C06B41/00
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B35/00—Compositions containing a metal azide
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06D—MEANS FOR GENERATING SMOKE OR MIST; GAS-ATTACK COMPOSITIONS; GENERATION OF GAS FOR BLASTING OR PROPULSION (CHEMICAL PART)
- C06D5/00—Generation of pressure gas, e.g. for blasting cartridges, starting cartridges, rockets
- C06D5/06—Generation of pressure gas, e.g. for blasting cartridges, starting cartridges, rockets by reaction of two or more solids
Definitions
- a fuel selected from the group consisting of alkali metal azides and alkaline earth metal azides,
- an alkali metal oxidant selected from the group consisting of alkali metal perchlorates and bichromates,
- a nitrogenous compound selected from the group consisting of aminotetrazole, aminotetrazole hydrate, azodicarbonamide and azotetrazole, and
- silica as an additive for reacting with the solid combustion residues of the composition.
- compositions are particularly intended for the deployment of inflatable safety devices for driver and passenger protection in automobiles and other fast vehicles.
- the present invention is concerned with pyrotechnic compositions which generate combustion gases which are substantially non-toxic and which can be used, in particular, for the deployment of inflatable safety devices designed to protect the drivers and passengers of motor vehicles and other fast vehicles.
- Propellant compositions containing, as an combustion catalyst, are also known. However, these compositions have only a limited yield of gas unless the mixture is so formulated as to provide a substantially stoichiometric quantity of oxygen which, in turn, leads to the production of toxic nitrogen oxides in the combustion gases.
- These propellant compositions are, however; primarily intended for the propulsion of rockets, for which purpose the production of such nitrogen oxides is not disadvantageous.
- Gas-generating compositions have also been proposed which enable a large volume of non-toxic gas to be obtained in a very short period.
- These compositions comprise an inorganic oxidant and a plastics'binder and produce combustion gases containing a relatively high proportion of oxygen.
- the latter characteristic could be a disadvantage when such compositions are used for the deployment of inflatable safety devices in case of accidents in view of the risk of fire.
- a gasgenerating pyrotechnic composition which comprises:
- a fuel consisting of an alkali metal azide or alkaline earth metal azide
- an alkali metal oxidant selected from alkali meta perchlorates and bichromates
- a nitrogenous compound selected from aminotetrazole, aminotetrazole hydrate, azocarbonamide and azotetrazole, and
- silica as an additive for reacting with
- the weight ratio of azide: alkali metal oxidant ' is greater than 1 and the weight ratio nitrogenous compound:
- azide is less than 48%.
- the composition preferably comprises, by weight: a. 50 to parts of sodium azide, 1 b. 50 to 20 parts of potassium perchlorate, for a total of parts of azide and perchlorate,
- the solid combustion residues of the composition according to the invention comprise alkali metal or alkaline earth metal oxides, most of which have an irritating physiological action and can cause burns, particularly when the constituents (a) and (b) are sodium azide and potassium perchlorate, respectively.
- the incorporation of silica in the composition enables these oxides to be suppressed by converting them into silicates which have no physiological action on the organism.
- the total suppression of sodium oxide in the combustion residues is obtained by using 9.3% of silica with respect to the quantity of sodium azide; in practice, an amount of silica greater than 6% enables a partial, but satisfactory, suppression of sodium oxide to be obtained.
- compositions according to the invention have a shorter ignition time, of the order of several milliseconds, while retaining a sufficiently high selfignition temperature for the composition to be completely safe in use;
- combustion gases obtained from the compositions according to the invention contain some carbon monoxide, the proportion of the latter can be kept below the critical toxic value and the combustion gases contain substantially less toxic nitrogen oxides than the gases obtained from known gasgenerating pyrotechnic compositions. Since the combustion gases obtained from the composition according to the invention are particularly intended for the deployment of inflatable safety devices, for which purpose the gases should be at only a moderate temperature, it is of particular importance to obtain:
- compositions comprising sodium azide, potassium perchlorate, and aminotetrazole hydrate
- the ratio NaNn should be 6 less than i.e. less than 8.5%
- composition diagram When a composition diagram is constructed in which the ordinates represent the weight ratio NaN /KCl and the abscissae the weight ratio aminotetrazole/- NaN the curve passing through the three points, a, b and c, defined as follows:
- the region representing the most preferred compositions is that lying between the curve defined by the three points a, b and c, the ordinate axis, and the straight line parallel to the abscissae axis for which the ordinate value 1, corresponding to equal amounts of potassium perchlorate and sodium azide.
- compositions A, B and C were equal to: 1330 cal/g, 1270 cal/g and 1220 cal/g for compositions A, B and C respectively.
- the self-ignition temperature of the three compsitions was 415C.
- the gas yield was from 0.248 l/g and 0.356 l/g (the gases being at normal pressure and temperature) and the combustion gases contained from 96% to 99.5% of nitrogen mass of the combustion gases.
- the elimination of sodium oxide in the solid combustion residues was satisfactory due to the presence of powdered silica in the indicated quantities.
- compositions A. B, C show the importance of using large amounts of azide. since, on the one hand, the combustion temperature, which is related to the potential of the composition, decreases and, on the other hand, the yield of gases increases. but concommitantly the formation of nitrogen oxides also increases and, for example, in the range of proportions comprised between the compositions of the prior art type have a higher toxicity due to the excessive formation of nitrogen oxides.
- the potentials and combustion rates of these compositions were lower than those of compositions A, B and C having the same NaN /KC10 ratio.
- the potentials obtained were about the order of 1000 cal/g and the gaseous yields were about 0.45 l/g (at normal pressure and temperature).
- Combustion rate 350 mm/s at bars.
- Composition K (in the form of pellets) NaN 70 parts KClO, 30 parts aminotetrazole 6.5 parts SiO (average particle size 30y) 6.5 parts
- the combustion characteristics obtained with this composition were as follows:
- the preparation of the pyrotechnic compositions according to the invention is effected in a conventional manner by mixing of the constituents.
- Shaped charges can be formed by incorporating a suitable binder and subjecting the composition to a conventional pelleting or extrusion operation.
- Various shapes can be used according to the firing characteristics required.
- compositions containing from 1 to 2 parts by weight of a metal stearate and in the form of pellets of 9.5 mm diameter and 3 mm thickness are suitable.
- the constituents are preferably physically treated to select a particular particle size fraction and/or to eliminate moisture.
- potassium perchlorate is preferably dried at 80C for 12 hours and sodium azide is preferably crushed by rollers to pass through a 295 p. screen.
- the mixing should be carried out to obtain a mixture which is powdery and apparently homogeneous. Simultaneous introduction of the constituents into a mixer, such as a V mixer (Moritz), and mixing for 1 hour is suitable in most cases.
- pelletising of the powder mixture is preferably effected under the following working conditions in, for example a pelletiser of the Stokes type:
- a gas-generating pyrotechnic composition which comprises:
- a fuel selected from the group consisting of alkali metal azides and alkaline earth metal azides,
- an alkali metal oxidant selected from the group consisting of alkali metal perchlorates and bichromates,
- a nitrogenous compound selected from the group consisting of aminotetrazole, aminotetrazole hydrate, azodicarbonamide and azotetrazole.
- composition according to claim 1 additionally comprising silica.
- a nitrogenous compound selected from the group consisting of aminotetrazole and aminotetrazole hydrate, and
- composition as set forth in claim 6, which comprises, by weight, about 9.3% of silica with respect to the azide.
- composition as set forth in claim 5 in which- NaN;, 50 aminotetrazole 24 ii. the straight line parallel to the abscissae axis for which the ordinate value 1, and
Landscapes
- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Air Bags (AREA)
- Emergency Lowering Means (AREA)
- Feeding, Discharge, Calcimining, Fusing, And Gas-Generation Devices (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7236738A FR2228043B1 (enrdf_load_stackoverflow) | 1972-10-17 | 1972-10-17 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3912561A true US3912561A (en) | 1975-10-14 |
Family
ID=9105769
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US404762A Expired - Lifetime US3912561A (en) | 1972-10-17 | 1973-10-09 | Pyrotechnic compositions for gas generation |
Country Status (19)
Cited By (43)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4021275A (en) * | 1975-04-23 | 1977-05-03 | Daicel, Ltd. | Gas-generating agent for air bag |
US4214438A (en) * | 1978-02-03 | 1980-07-29 | Allied Chemical Corporation | Pyrotechnic composition and method of inflating an inflatable device |
EP0055547A1 (en) * | 1980-12-31 | 1982-07-07 | Morton Thiokol, Inc. | Solid compositions for generating nitrogen, the generation of nitrogen therefrom and inflation of gas bags therewith |
EP0055904A1 (en) * | 1980-12-31 | 1982-07-14 | Morton Thiokol, Inc. | Azide-free compositions for generating nitrogen, the generation of nitrogen therefrom and inflation of gas bags therewith |
US4601344A (en) * | 1983-09-29 | 1986-07-22 | The United States Of America As Represented By The Secretary Of The Navy | Pyrotechnic fire extinguishing method |
US4604151A (en) * | 1985-01-30 | 1986-08-05 | Talley Defense Systems, Inc. | Method and compositions for generating nitrogen gas |
US4734141A (en) * | 1987-03-27 | 1988-03-29 | Hercules Incorporated | Crash bag propellant compositions for generating high quality nitrogen gas |
US4758287A (en) * | 1987-06-15 | 1988-07-19 | Talley Industries, Inc. | Porous propellant grain and method of making same |
US4920743A (en) * | 1988-07-25 | 1990-05-01 | Hercules Incorporated | Crash bag propellant composition and method for generating nitrogen gas |
US4929290A (en) * | 1988-07-25 | 1990-05-29 | Hercules Incorporated | Crash bag propellant composition and method for generating nitrogen gas |
JPH02225159A (ja) * | 1988-12-02 | 1990-09-07 | Automot Syst Lab Inc | 安全防護袋を膨らませる方法 |
US5160386A (en) * | 1991-11-04 | 1992-11-03 | Morton International, Inc. | Gas generant formulations containing poly(nitrito) metal complexes as oxidants and method |
US5198046A (en) * | 1991-03-14 | 1993-03-30 | Fraunhofer-Gesellschaft Zur Forderung Der Angewandten Forschund E.V. | Stable, nitrogen-rich composition |
US5197758A (en) * | 1991-10-09 | 1993-03-30 | Morton International, Inc. | Non-azide gas generant formulation, method, and apparatus |
WO1995004015A1 (en) * | 1993-08-02 | 1995-02-09 | Thiokol Corporation | Bitetrazoleamine gas generant compositions and methods of use |
WO1995004016A1 (en) * | 1993-08-02 | 1995-02-09 | Thiokol Corporation | Anhydrous tetrazole gas generant compositions and methods of preparation |
WO1995004014A1 (en) * | 1993-08-02 | 1995-02-09 | Thiokol Corporation | Method for preparing anhydrous tetrazole gas generant compositions |
US5401340A (en) * | 1993-08-10 | 1995-03-28 | Thiokol Corporation | Borohydride fuels in gas generant compositions |
US5403035A (en) * | 1992-06-01 | 1995-04-04 | Oea, Inc. | Preparing air bag vehicle restraint device having cellulose containing sheet propellant |
US5429691A (en) * | 1993-08-10 | 1995-07-04 | Thiokol Corporation | Thermite compositions for use as gas generants comprising basic metal carbonates and/or basic metal nitrates |
US5439537A (en) * | 1993-08-10 | 1995-08-08 | Thiokol Corporation | Thermite compositions for use as gas generants |
US5460668A (en) * | 1994-07-11 | 1995-10-24 | Automotive Systems Laboratory, Inc. | Nonazide gas generating compositions with reduced toxicity upon combustion |
US5514230A (en) * | 1995-04-14 | 1996-05-07 | Automotive Systems Laboratory, Inc. | Nonazide gas generating compositions with a built-in catalyst |
US5557062A (en) * | 1994-12-13 | 1996-09-17 | United Technologies Corporation | Breathable gas generators |
US5592812A (en) * | 1994-01-19 | 1997-01-14 | Thiokol Corporation | Metal complexes for use as gas generants |
US5629494A (en) * | 1996-02-29 | 1997-05-13 | Morton International, Inc. | Hydrogen-less, non-azide gas generants |
US5661261A (en) * | 1996-02-23 | 1997-08-26 | Breed Automotive Technology, Inc. | Gas generating composition |
US5725699A (en) * | 1994-01-19 | 1998-03-10 | Thiokol Corporation | Metal complexes for use as gas generants |
US5844164A (en) * | 1996-02-23 | 1998-12-01 | Breed Automotive Technologies, Inc. | Gas generating device with specific composition |
US5883330A (en) * | 1994-02-15 | 1999-03-16 | Nippon Koki Co., Ltd. | Azodicarbonamide containing gas generating composition |
US5898126A (en) * | 1992-07-13 | 1999-04-27 | Daicel Chemical Industries, Ltd. | Air bag gas generating composition |
US6074502A (en) * | 1996-11-08 | 2000-06-13 | Automotive Systems Laboratory, Inc. | Smokeless gas generant compositions |
EP1065192A1 (en) | 1999-06-29 | 2001-01-03 | Uop Llc | Process and apparatus for inflating airbags and remediating toxic waste gases |
US6726788B2 (en) * | 1994-01-19 | 2004-04-27 | Universal Propulsion Company, Inc. | Preparation of strengthened ammonium nitrate propellants |
US20040226639A1 (en) * | 1991-06-21 | 2004-11-18 | Klaus Redecker | Propellant for gas generators |
US20050257866A1 (en) * | 2004-03-29 | 2005-11-24 | Williams Graylon K | Gas generant and manufacturing method thereof |
US6969435B1 (en) | 1994-01-19 | 2005-11-29 | Alliant Techsystems Inc. | Metal complexes for use as gas generants |
FR2926545A1 (fr) * | 2008-01-21 | 2009-07-24 | Snpe Materiaux Energetiques Sa | Composition generatrice de gaz azote, comprenant de l'azodicarbonamide et procede de generation de gaz azote par decomposition de ladite composition |
US20090255611A1 (en) * | 2008-04-10 | 2009-10-15 | Autoliv Asp, Inc. | High peformance gas generating compositions |
US20100084060A1 (en) * | 1994-01-19 | 2010-04-08 | Alliant Techsystems Inc. | Metal complexes for use as gas generants |
US20100116384A1 (en) * | 2008-11-12 | 2010-05-13 | Autoliv Asp, Inc. | Gas generating compositions having glass fibers |
US20100230945A1 (en) * | 2006-06-21 | 2010-09-16 | Autoliv Asp, Inc. | Monolithic gas generant grains |
US9051223B2 (en) | 2013-03-15 | 2015-06-09 | Autoliv Asp, Inc. | Generant grain assembly formed of multiple symmetric pieces |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4948439A (en) * | 1988-12-02 | 1990-08-14 | Automotive Systems Laboratory, Inc. | Composition and process for inflating a safety crash bag |
GB2280946B (en) * | 1993-06-05 | 1997-12-10 | British Aerospace | Method of and apparatus for propelling a spacecraft in space |
DE19505568A1 (de) * | 1995-02-18 | 1996-08-22 | Dynamit Nobel Ag | Gaserzeugende Mischungen |
RU2379274C1 (ru) * | 2008-07-08 | 2010-01-20 | Государственное образовательное учреждение высшего профессионального образования "Алтайский государственный технический университет им. И.И. Ползунова" (АлтГТУ) | Твердый пиротехнический газогенерирующий элемент |
PT3164375T (pt) * | 2014-07-03 | 2019-12-02 | Ruag Ammotec Gmbh | Dispositivo de ignição pirotécnico |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3785674A (en) * | 1971-06-14 | 1974-01-15 | Rocket Research Corp | Crash restraint nitrogen generating inflation system |
US3797854A (en) * | 1971-06-14 | 1974-03-19 | Rocket Research Corp | Crash restraint air generating inflation system |
-
1972
- 1972-10-17 FR FR7236738A patent/FR2228043B1/fr not_active Expired
-
1973
- 1973-09-25 IE IE1714/73A patent/IE38282B1/xx unknown
- 1973-09-26 GB GB4516573A patent/GB1406002A/en not_active Expired
- 1973-09-26 CH CH1379973A patent/CH584669A5/xx not_active IP Right Cessation
- 1973-09-26 ZA ZA737600*A patent/ZA737600B/xx unknown
- 1973-10-09 US US404762A patent/US3912561A/en not_active Expired - Lifetime
- 1973-10-11 AU AU61304/73A patent/AU476753B2/en not_active Expired
- 1973-10-11 AR AR250495A patent/AR200284A1/es active
- 1973-10-15 ES ES419629A patent/ES419629A1/es not_active Expired
- 1973-10-15 NL NL7314143.A patent/NL161424C/xx active
- 1973-10-15 LU LU68613A patent/LU68613A1/xx unknown
- 1973-10-16 JP JP11536973A patent/JPS572677B2/ja not_active Expired
- 1973-10-16 SU SU1976301A patent/SU559638A3/ru active
- 1973-10-16 SE SE7314045A patent/SE399063B/xx unknown
- 1973-10-16 IT IT70060/73A patent/IT999653B/it active
- 1973-10-16 BR BR8071/73A patent/BR7308071D0/pt unknown
- 1973-10-17 CA CA183,564A patent/CA1020357A/en not_active Expired
- 1973-10-17 CS CS737154A patent/CS190412B2/cs unknown
- 1973-10-17 BE BE136804A patent/BE806209A/xx unknown
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
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US3785674A (en) * | 1971-06-14 | 1974-01-15 | Rocket Research Corp | Crash restraint nitrogen generating inflation system |
US3797854A (en) * | 1971-06-14 | 1974-03-19 | Rocket Research Corp | Crash restraint air generating inflation system |
Cited By (61)
Publication number | Priority date | Publication date | Assignee | Title |
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Also Published As
Publication number | Publication date |
---|---|
SE399063B (sv) | 1978-01-30 |
DE2351401A1 (de) | 1974-05-09 |
JPS4987583A (enrdf_load_stackoverflow) | 1974-08-21 |
BR7308071D0 (pt) | 1974-07-18 |
SU559638A3 (ru) | 1977-05-25 |
ZA737600B (en) | 1974-08-28 |
CH584669A5 (enrdf_load_stackoverflow) | 1977-02-15 |
IT999653B (it) | 1976-03-10 |
CS190412B2 (en) | 1979-05-31 |
AU6130473A (en) | 1975-04-17 |
AR200284A1 (es) | 1974-10-31 |
IE38282B1 (en) | 1978-02-01 |
ES419629A1 (es) | 1976-06-16 |
AU476753B2 (en) | 1976-09-30 |
FR2228043B1 (enrdf_load_stackoverflow) | 1977-03-04 |
CA1020357A (en) | 1977-11-08 |
NL161424B (nl) | 1979-09-17 |
FR2228043A1 (enrdf_load_stackoverflow) | 1974-11-29 |
DE2351401B2 (de) | 1976-05-20 |
NL161424C (nl) | 1980-02-15 |
JPS572677B2 (enrdf_load_stackoverflow) | 1982-01-18 |
GB1406002A (en) | 1975-09-10 |
LU68613A1 (enrdf_load_stackoverflow) | 1975-06-16 |
BE806209A (fr) | 1974-04-17 |
IE38282L (en) | 1974-04-17 |
NL7314143A (enrdf_load_stackoverflow) | 1974-04-19 |
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