WO1997045294A2 - Autoignition composition - Google Patents
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- WO1997045294A2 WO1997045294A2 PCT/US1997/007933 US9707933W WO9745294A2 WO 1997045294 A2 WO1997045294 A2 WO 1997045294A2 US 9707933 W US9707933 W US 9707933W WO 9745294 A2 WO9745294 A2 WO 9745294A2
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- nitrate
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- autoignition
- alkali metal
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- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B33/00—Compositions containing particulate metal, alloy, boron, silicon, selenium or tellurium with at least one oxygen supplying material which is either a metal oxide or a salt, organic or inorganic, capable of yielding a metal oxide
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- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06C—DETONATING OR PRIMING DEVICES; FUSES; CHEMICAL LIGHTERS; PYROPHORIC COMPOSITIONS
- C06C9/00—Chemical contact igniters; Chemical lighters
Definitions
- the invention relates to gas generating compositions, such as those used in "air bag” passive restraint systems, and, in particular, to autoignition compositions that provide a means for initiating combustion of a main pyrotechnic charge in a gas generator or pyrotechnic device exposed to temperatures significantly above the temperatures at which the unit is designed to operate.
- One method commonly used for inflating air bags in vehicle passive restraint systems involves the use of an ignitable gas generator that generates an inflating gas by an exothermic reaction of the components of the gas generator composition. Because of the nature of passive restraint systems, the gas must be generated, and the air bag deployed in a matter of milliseconds. For example, under representative conditions, only about 60 milliseconds elapse between primary and secondary collisions in a motor vehicle accident, i.e., between the collision of the vehicle with another object and the collision of the driver or passenger with either the air bag or a portion of the vehicle interior.
- the inflation gas must meet several stringent reguirements.
- the gas must be non-toxic, non-noxious, must have a generation temperature that is low enough to avoid burning the passenger and the air bag, and it must be chemically inert so that it is not detrimental to the mechanical strength or integrity of the bag.
- the stability and reliability of the gas generator composition over the life of the vehicle are also extremely important.
- the gas generator composition must be stable over a wide range of temperature and humidity conditions, and must be resistant to shock, so that it is virtually impossible for the gas generator to be set off except when the passive restraint system is activated by a collision.
- the inflation gas is nitrogen, which is produced by the decomposition reaction of a gas generator composition containing a metal azide.
- a gas generator composition containing a metal azide.
- the solid reactants of the composition include an alkali metal azide and a metal oxide, and are formulated to ignite at an ignition temperature of over about 315°C.
- the gas generator composition is typically stored in a metal inflator unit mounted in the steering wheel or dashboard of the vehicle.
- Several representative inflator units are disclosed in U.S. Patent Nos. 4,923,212, 4,907,819, and 4,865,635.
- inflator units are often formed from light weight materials, such as aluminum, that can lose strength and mechanical integrity at temperatures significantly above the normal operating temperature of the unit. Although the temperature required for the unit to lose strength and mechanical integrity is much higher than will be encountered in normal vehicle use, these temperatures are readily reached in, for example, a vehicle fire.
- a gas generator composition at its autoignition temperature will produce an operating pressure that is too high for a pressure vessel that was designed for minimum weight.
- the melting point of many non-azide gas generator compositions is low enough for the gas generator composition to be molten at the autoignition temperature of the composition, which can result in a loss of ballistic control and excessive operating pressures. Therefore, in a vehicle fire, the ignition of the gas generator composition can result in an explosion in which fragments of the inflation unit are propelled at dangerous and potentially lethal velocities.
- an autoignition composition that will autoignite and initiate the combustion of the main gas generating pyrotechnic charge at a temperature below that at which the shell or housing begins to soften and lose structural integrity.
- the number of autoignition compositions available in the prior art is limited, and includes nitrocellulose and mixtures of potassium chlorate and a sugar. However, nitrocellulose decomposes with age, so that the amount of energy released upon autoignition decreases, and may become insufficient to properly ignite the main gas generator charge.
- prior art autoignition compositions have autoignition temperatures that are too high for some applications, e.g., non-azide auto air bag main charge generants.
- a need exists for a stable autoignition composition that is capable of igniting the gas generator composition at a temperature that is sufficiently low that the inflator unit maintains mechanical integrity at the autoignition temperature, but which is significantly higher than the temperatures reached under normal vehicle operating conditions.
- the present invention relates to an autoignition composition for safely initiating combustion in a main pyrotechnic charge in a gas generator or pyrotechnic device exposed to flame or a high temperature environment.
- the autoignition compositions of the invention comprise a mixture of an oxidizer composition and a powdered metal fuel, wherein the oxidizer composition comprises- at least one of an alkali metal or an alkaline earth metal nitrate, a complex salt nitrate, such as Ce(NH 4 ) 2 (N0 3 ) 6 or ZrO(N0 3 ) 2 , a dried, hydrated nitrate, such as Ca(N0 3 ) 2 « 4H 2 0 or Cu(N0 3 ) 2 «2.5 H 2 0, silver nitrate, an alkali or alkaline earth metal chlorate or perchlorate, ammonium perchlorate, a nitrite of sodium, potassium, or silver, or a solid organic nitrate, nitrite, or amine,
- the autoignition temperature the temperature at which the autoignition compositions of the invention spontaneously ignite or autoignite, is between about 80°C and about 250°C.
- the autoignition compositions of the invention may further comprise an alkali or alkaline earth chloride, fluoride, or bromide comelted with a nitrate, nitrite, chlorate, or perchlorate, such that the autoignition composition has a eutectic or peritectic in the range of about 80 ⁇ C to about 250°C.
- an output augmenting composition which comprises an energetic oxidizer of ammonium perchlorate or an alkali metal chlorate, perchlorate or nitrate, in combination with a metal, may be added to the composition.
- Preferred autoignition compositions include oxidizers of a comelt of silver nitrate and alkali metal or alkaline metal nitrates, nitrites, chlorates or perchlorates, or a nitrite of sodium, potassium, or silver, and mixtures of silver nitrate and solid organic nitrates, nitrites, or amines.
- the powdered metals useful as fuel in the present invention include molybdenum, magnesium, calcium, strontium, barium, titanium, zirconium, vanadium, niobium, tantalum, chromium, tungsten, manganese, iron, cobalt, nickel, copper, zinc, cadmium, tin, antimony, bismuth, aluminum, and silicon. It should be noted that molybdenum appears to be unique in its reactivity with the oxidizers described above, and is therefore the preferred metal fuel.
- the most preferred inorganic autoignition compositions include comelts of silver nitrate and potassium nitrate, mixed with powdered molybdenum metal.
- the comelt is ground to a particle size of about 10 to about 30 microns, and the molybdenum powder has a particle size of less than about 2 microns.
- the mole fraction of silver nitrate in the comelt is typically about 0.4 to about 0.6, the mole fraction of potassium nitrate in the comelt is about 0.6 to 0.4, and the comelt is mixed with at least a stoichiometric amount of molybdenum powder.
- the most preferred organic autoignition compositions include a mixture of silver nitrate, guanidine nitrate, and molybdenum.
- the amount of molybdenum may be varied to adjust the autoignition temperature. If the amount of molybdenum is greater than the stoichiometric amount, the autoignition temperature of the autoignition composition will decrease as the amount of molybdenum is increased.
- the present invention also relates to a method for safely initiating combustion of a gas generator or pyrotechnic composition in a gas generator or pyrotechnic device having a housing when the gas generator or pyrotechnic device is exposed to flame or a high temperature environment.
- the method of the invention comprises forming an autoignition composition, as described above, and placing the autoignition composition in thermal contact with the gas generator or pyrotechnic composition within the gas generator or pyrotechnic device, such that the autoignition composition autoignites and initiates combustion of the gas generator or pyrotechnic composition when the gas generator or pyrotechnic device is exposed to flame or a high temperature environment.
- the method of the invention may also include the step of mixing the autoignition composition with an output augmenting composition, as described above, such that the autoignition composition autoignites and initiates combustion of the output augmenting composition, which, in turn, initiates combustion of the gas generator or «pyrotechnic composition when the gas generator or pyrotechnic device is exposed to flame or a high temperature environment.
- the autoignition compositions of the invention are suitable for use with a variety of gas generating and pyrotechnic devices, in particular, vehicle restraint system air bag inflators.
- the autoignition compositions ensure that the gas generating or pyrotechnic device functions properly and safely when exposed to a high temperature environment, i.e., that combustion of the main pyrotechnic charge is initiated at a temperature below the temperature at which the material used to form the shell or housing begins to weaken or soften. If the autoignition composition is not utilized, the device may not function properly or safely if exposed to high heat or flame, because the operating pressure of standard pyrotechnics increases with increasing temperature. Therefore, a gas generator composition at its autoignition temperature can produce an operating pressure that is too high for a pressure vessel that was designed for minimum weight.
- the melting point of many non-azide gas generator compositions is low enough for the gas generator composition to be molten at the autoignition temperature of the composition, which can result in a loss of ballistic control and excessive operating pressures.
- the components of the gas generator or pyrotechnic composition within the device can decompose, melt, or sublime, and burn at an accelerated rate, resulting in an explosion that would destroy the device, and could possibly propel harmful or lethal fragments.
- the autoignition compositions of the invention provide an effective means for preventing such a catastrophic occurrence.
- the pyrotechnic autoignition compositions of the invention provide several advantages over typical autoignition materials currently in use, such as nitrocellulose, including a lower autoignition temperature and better thermal stability.
- The.preferred compositions autoignite over a narrow temperature range, and provide extremely repeatable performance.
- the complete series of compositions described and claimed herein have a wide range of autoignition temperatures that can be tailored for particular applications.
- the autoignition compositions also may have low to moderate hazard sensitivities, i.e., DOT 1.3c or lower.
- the autoignition compositions of the invention comprise a mixture of a powdered metal fuel and an oxidizer of one or more alkali metal or alkaline earth metal nitrates, silver nitrate, alkali or alkaline earth metal chlorates or perchlorates, ammonium perchlorate, nitrites of sodium, potassium, or silver, or a complex salt nitrate, such as eerie ammonium nitrate, Ce(NH 4 ) 2 (N0 3 ) 6 , or zirconium oxide dinitrate, ZrO(N0 3 ) 2 .
- the term "powdered metal” encompasses metal powders, particles, prills, flakes, and any other form of the metal that is of the appropriate size and/or surface area for use in the present invention, i.e., typically, with a dimension of less than about 100 microns.
- oxidizer eutectics and/or peritectics in the range of about 80° to 250° C.
- Solid organic nitrates R-(ON0 2 ) x , nitrites, R- (N0 2 ) x , and amines R-(NH 2 ) X , can also be used as the oxidizer component, either alone or in combination with one or more other solid organic nitrate, nitrite, or amine, or with one or more of the inorganic nitrates, nitrites, chlorates or perchlorates listed above, but preferably only as mechanical mixes because in some cases comelts of these solid organic materials with inorganic/organic oxidizers may produce unstable combinations.
- the solid organic nitrates, nitrites and amines that are useful in forming the autoignition compositions of the invention have melting points between about 80°C and about 250°C.
- mixtures should preferably produce eutectics and peritectics in the range of about 80°C to about 250°C.
- These mixtures may be combined with one or more of the metals disclosed herein, and can be used in a powdered, granular or pelletized form.
- hygroscopic, low melting point metal nitrates can be dehydrated and stabilized relative to moisture absorption by comelting with anhydrous metal nitrates, such as those described above.
- Autoignition compositions of this type may require an output augmenting material or charge to initiate combustion of the enhancer and main pyrotechnic charge.
- the ignition train for such a composition is initiated when the autoignition composition is heated to the autoignition temperature and ignites.
- the heat generated by the combustion of the autoignition device ignites the output augmenting material, which, in turn, ignites the enhancer and main pyrotechnic charge of the gas generator.
- the augmentation material can be a charge which is separate from the autoignition material, or is mixed in with the autoignition composition to boost its output.
- an output augmenting composition comprises an energetic oxidizer, such as ammonium perchlorate or alkali metal chlorate, perchlorate or nitrate, and a metal such as Mg, Ti, or Zr or a nonmetal such as boron.
- an energetic oxidizer such as ammonium perchlorate or alkali metal chlorate, perchlorate or nitrate
- a metal such as Mg, Ti, or Zr or a nonmetal such as boron.
- the presence of certain metal oxides in a nitrate, nitrite, chlorate or perchlorate oxidizer mix or comelt of the invention can have a catalytic effect in lowering the autoignition temperature for the reaction of the oxidizer and the metal, which is equivalent to lowering the energy of activation.
- Metal oxides useful in the invention for this purpose include, but are not limited to A1 2 0 3 , Si0 2 , Ce0 2 , and transition metal oxides, which include, but are not limited to V 2 0 s , Cr0 3 , Cr 2 0 3 , Mn0 2 , F ⁇ 2 ⁇ 3 , Co 3 0 4 , NiO, CuO, ZnO, zr ⁇ 2 , Nb j Oi, Mo0 3 , and Ag 2 0.
- transition metal oxides include, but are not limited to V 2 0 s , Cr0 3 , Cr 2 0 3 , Mn0 2 , F ⁇ 2 ⁇ 3 , Co 3 0 4 , NiO, CuO, ZnO, zr ⁇ 2 , Nb j Oi, Mo0 3 , and Ag 2 0.
- the nitrate, nitrite, chlorate or perchlorate component or components function as an oxidizer, and the metal serves as a fuel.
- the reaction of a composition comprising a comelt of metal nitrates and a metal proceeds according to the general equation
- oxidizer systems containing silver nitrate and/or silver nitrite will generally yield very efficient autoignition materials with respect to ease, rate, and intensity of reaction when compounded with metals which are high in the activity or electromotive series.
- Mg, Al, Mn, Zn, Cr, Fe, Cd, Co, Ni and Mo are all well above Ag in the series.
- a typical reaction is represented by equations II to V.
- DSC Differential Scanning Calorimeter
- Calibrated Tube Furnace autoignition test results for inorganic, organic and mixed inorganic/organic nitrate, nitrite, chlorate and perchlorate oxidizer systems with selected metals, demonstrates that at least two different autoignition mechanisms may be involved.
- purely inorganic systems e.g. , KN ⁇ 3 /AgN ⁇ 3 /Mo, generally autoignite in the vicinity of a thermal event clearly visible on a DSC scan, such as a crystalline phase transition, a melting point, or a eutectic or peritectic point.
- the amount of the nitrate, nitrite, chlorate or perchlorate used in an autoignition composition can vary significantly.
- the mole percent or molar ratio of the nitrate, nitrite, chlorate or perchlorate oxidizer components in binary and ternary mixes and comelts should be stoichiometrically balanced with the metal or metals in the final autoignition composition, i.e., the molar amounts of the oxidizer and metal fuel are substantially proportional to the molar amounts given in the balanced chemical equation for the reaction of the oxidizer with the fuel.
- the autoignition temperature for organic/inorganic compositions comprising molybdenum metal can be tailored by adjusting the molybdenum metal content from stoichiometrically balanced to extremely metal (fuel) rich. As the molybdenum metal content is increased the autoignition temperature decreases. It is believed that this holds true for the other metal fuels described above.
- each oxidizer component in a mixture or comelt depends on the molar amounts of the oxidizers at or near the eutectic point for the specific oxidizer mixture or comelt composition.
- the nitrate, nitrite, chlorate or perchlorate oxidizer component or components will be the major component in some autoignition compositions of the invention, and the powdered metal fuel will be the major component in others.
- Those skilled in the art will be able to determine the required amount of each component from the stoichiometry of the autoignition reaction or by routine experimentation.
- the preferred compositions comprise a comelt of silver nitrate, AgN0 3 , and a nitrate of an alkali metal or an alkaline earth metal, preferably, lithium nitrate, LiN0 3 , sodium nitrate, NaN0 3 , potassium nitrate, KN0 3 , rubidium nitrate, RbN0 3 , cesium nitrate, CsN0 3 , magnesium nitrate, Mg(N0 3 ) 2 , calcium nitrate, Ca(N0 3 ) 2 , strontium nitrate, Sr(N0 3 ) 2 , or barium nitrate, Ba(N0 3 ) 2 , a nitrite of sodium, NaN0 2 , potassium, KN0 2 , and silver, AgN0 2 , a chlorate of an alkali metal or an alkaline earth metal, preferably lithium chlorate, LiC10 3 , sodium chlorate, NaC10 3 ,
- Preferred compositions also include mixtures of AgN0 3 and the solid organic nitrate guanidine nitrate, CHgN ⁇ .
- the preferred metals are molybdenum, Mo, magnesium, Mg, calcium, Ca, strontium, Sr, barium, Ba, titanium, Ti, zirconium, Zr, vanadium, V, niobium, Nb, tantalum, Ta, chromium, Cr, tungsten, W, manganese, Mn, iron, Fe, cobalt, Co, nickel, Ni, copper, Cu, zinc, Zn, cadmium, Cd, tin, Sn, antimony, Sb, bismuth, Bi, aluminum, Al, and silicon, Si. These metals may be used alone or in combination.
- molybdenum appears to be unique in its reactivity with nitrate, nitrite, chlorate and perchlorate salts, mixes and comelts. Molybdenum metal has reacted and autoignited with every oxidizer and oxidizer system of nitrates, nitrites, chlorates and perchlorates tested. Although the mechanism is not fully understood, there appears to be a sensitizing or catalytic interaction between molybdenum and nitrates, nitrites, chlorates and perchlorates.
- the binary and ternary oxidizer systems can be mixed by physical or mechanical means, or can be comelted to produce a higher level of ingredient intimacy in the mix.
- the oxidizers in mechanical mixes should each be ground to an average particle size (APS) of about 100 microns or less prior to mixing, preferably about 5 to about 20 microns. Comelts of oxidizers should also be ground to less than about 100 microns APS, again, with a preferred APS of about 5 to about 20 microns. Average particle size of the metals used in the autoignition compositions should be about 35 microns or less with the preferred APS being less than about 10 microns.
- the reaction or burning rate and ease of autoignition increases as mix intimacy and homogeneity increases, and as the average particle size of the oxidizers and metals decreases. In other words, reaction rate and ease of autoignition are proportional to mix intimacy and homogeneity and inversely proportional to the average particle size of the oxidizer and metal components.
- the most preferred purely inorganic composition is a comelt of silver nitrate and potassium nitrate, ground to a particle size of about 20 microns, mixed with powdered molybdenum having a particle size of less than about 2 microns.
- the mole fraction of silver nitrate in the comelt is from about 0.4 to about 0.6, and the mole fraction of potassium nitrate is from about 0.6 to about 0.4.
- the composition further comprises an essentially stoichiometric amount of molybdenum.
- the autoignition temperature can be adjusted and tailored for specific uses by varying the amounts and types of the metal nitrates in the comelt and the specific metal used.
- compositions of AgN0 3 /KN0 3 /Mo have an autoignition temperature between 130° and 135°C.
- autoignition appears to occur very near a phase change.
- binary and ternary comelt systems autoignition occurs near a eutectic or peritectic point.
- the oxidizer softens or melts producing a kinetically favorable environment for reaction with the metal.
- Each system of comelted oxidizers is unique.
- a simple binary system can have a single eutectic point, as described by the phase diagram of the system, that results in a single autoignition temperature for a specific metal/comelt composition.
- a binary comelt of LiN0 3 /KN0 3 with molybdenum will autoignite at 230°C.
- the autoignition temperature of the composition is dependent on the molar ratio of the oxidizers in the comelt.
- a binary comelt of AgN0 3 /KN0 3 with molybdenum has an autoignition temperature near the peritectic point of 135°C for comelts with less than 58 mole percent AgN0 3 , based on the weight of the comelt, but has an autoignition temperature near the eutectic point of 118°C for comelts with 58 mole percent AgN0 3 or higher.
- the eutectic and peritectic melting points of a binary system tends to set the upper limit for any ternary system containing the specific binary combination of oxidizers. In other words, the melting point or eutectic of a ternary system cannot be higher than the lowest melting point of a binary combination within it.
- certain non-energetic salts such as alkali and alkaline earth chlorides, fluorides and bromides can be comelted with selected nitrates, nitrites, chlorates and perchlorates, preferably AgN0 3 and AgN0 2 , to produce eutectics or peritectics preferably in the range of about 80°C to about 250°C. These comelts will be combined with any one or more of the listed metals to produce the autoignition reaction. Selected nitrates, chlorates, or perchlorates may also be added to augment ignition and output.
- the autoignition composition of the invention is preferably placed within a gas generating or pyrotechnic device, e.g., within an inflator housing, where, when the inflator is exposed to flame or a high temperature environment, they operate in a manner that allows the autoignition composition to ignite and initiate combustion of the pyrotechnic charge of the device at a device temperature that is lower than the temperature at which the device loses mechanical integrity.
- a gas generator composition at its autoignition temperature will produce an operating pressure that is too high for a pressure vessel that was designed for minimum weight.
- the melting point of many non-azide gas generator compositions is low enough for the gas generator composition to be molten at the autoignition temperature of the composition, which can result in a loss of ballistic control and excessive operating pressures. Therefore, in a vehicle fire, the ignition of the gas generator composition can result in an explosion in which fragments of the inflation unit are propelled at dangerous and potentially lethal velocities.
- the autoignition compositions of the present invention the combustion of the main pyrotechnic charge is initiated at a temperature below the temperature at which the material used to form the shell or housing begins to weaken or soften, and the uncontrolled combustion of the gas generator or pyrotechnic composition at higher temperatures is prevented, which could otherwise result in an explosion of the device.
- Preferred locations within the gas generating or pyrotechnic device include a cup or recessed area at the bottom of the housing of the device, a coating or pellet affixed to the inner surface of the housing, or inclusion as part of the squib used to ignite the gas generator or pyrotechnic composition during normal operation.
- a number of the autoignition compositions display mass effects that can affect the autoignition temperature. For example, a 6 mg sample of LiCl0 4 /Mo will autoignite at 146°C on the DSC (l°C/min scan rate) . This autoignition occurs just after a crystalline phase transition. On the other hand, a 2 mg sample does not autoignite until 237°C, which is just before the melting point of LiC10 4 (248°C) . To address these mass effects on a larger scale and also to test application size samples, typically about 50 to about 250 grams, a tightly temperature controlled tube furnace is used. This also provides a practical means of determining time to autoignition at a selected temperature for various sample sizes ranging from about 50 to about 250 grams.
- An autoignition composition was prepared by mixing a comelt of equimolar amounts of silver nitrate (AgN0 3 ) and potassium nitrate (KN0 3 ) with a stoichiometric amount of a molybdenum (Mo) metal according to equation VI, i.e., 39.4% by weight AgN0 3 , 23.5% by weight KN0 3 , and 37.1% by weight Mo.
- An autoignition temperature of 135 ⁇ l ⁇ C was determined for the composition using differential scanning calorimetry (DSC) with 2 to 8 mg samples. However, when a 200 mg sample was tested in a tube furnace, the autoignition temperature was 13012°C, demonstrating the existence of a mass effect.
- a composition with a weight percent of AgN0 3 greater than 44.6% of the autoignition composition melts and autoignites at the eutectic at 118 ⁇ 2*C. However, with a weight percent of AgN0 3 of less than 44.6%, the composition melts and autoignites at the peritectic at 135 ⁇ 2°C.
- a comelt of equimolar amounts of AgN0 2 and AgN0 3 was mixed with a stoichiometric amount of Mo metal in accordance with equation VIII, i.e., 34.1% by weight AgN0 2 , 37.6% by weight AgN0 3 , and 28.3% by weight Mo.
- An autoignition temperature of 131 ⁇ 2°C was determined for the composition using DSC.
- Example 4
- Lithium perchlorate LiC10 4
- Mo a stoichiometric amount of Mo in accordance with equation IX, i.e., 45.4% by weight LiCl0 4 and 54.6% by weight Mo.
- An autoignition temperature of 147 ⁇ 2°C was determined for the composition using DSC.
- AgN0 3 was mixed with a stoichiometric amount of magnesium, Mg, metal in accordance with equation X, i.e., 73.7% by weight AgN0 3 and 26.3% by weight Mg.
- An autoignition temperature of 157 ⁇ 2°C was determined for the composition using DSC.
- AgN0 3 was mixed with a stoichiometric amount of potassium perchlorate, KC10 4 , and Mg in accordance with equation XI, i.e., 19.9% by weight KC10 4 , 48.7% by weight AgN0 3 and 31.4% by weight Mg.
- An autoignition temperature of 154 ⁇ 2°C was determined for the composition using DSC. It may be noted that the composition of example 5,
- AgN0 3 /Mg has about the same autoignition temperature, 157° vs 154°C, as the composition of example 6, AgN0 3 /KC10 4 /Mg. Accordingly, it might be concluded that the AgN ⁇ 3 /Mg reaction is the driving force in both cases. However, the AgN0 3 /KC10 4 /Mg composition reacts with much greater energy than the AgN0 3 /Mg composition. In general, perchlorates produce greater energy than nitrates in this type of reaction, and, thus, this example demonstrates output augmentation by KC10 4 .
- a comelt of equimolar amounts of lithium nitrate, LiN0 3 , and AgN ⁇ 3 was mixed with a stoichiometric amount of Mo metal, in accordance with equation XII, i.e., 17.3% by weight LiN0 3 , 42.6% by weight AgN ⁇ 3 and 40.1% by weight Mo.
- An autoignition temperature of 175 ⁇ 2°C was determined for the composition using DSC.
- the Ca(N0 3 ) 2 was received as Ca(N0 3 ) 2 «4H 2 0 and was dried to remove the H 2 0 before comelting.
- AgN0 3 was mixed with a stoichiometric amount of Mo in accordance with equation XIV, i.e., 68.0% by weight AgN0 3 and 32.0% by weight Mo. This composition autoignited at 199 ⁇ 2°C by DSC analysis.
- Example 10 This composition autoignited at 199 ⁇ 2°C by DSC analysis.
- KC10 4 and Mo in accordance with equation XV, i.e., 18.1% by weight KC10 4 , 44.3% by weight AgN0 3 and 37.6% by weight Mo.
- the composition autoignited at 192 ⁇ 2°C as determined by DSC analysis.
- AgN0 3 /Mg and KC10 4 /AgN0 3 /Mg described above, AgN0 3 /Mo autoignites at nearly the same temperature, 199°C vs 192°C, as the KC10 4 /AgN0 3 /Mo.
- the KC10 4 /AgN0 3 /Mo system autoignites with greater energy than the AgN0 3 /Mo, and is another example of output augmentation by KC10 4 .
- the composition autoignited at 217 ⁇ 2°C by DSC analysis.
- Guanidine nitrate, CH ⁇ N 4 0 3 was mixed with a stoichiometric amount of Mo in accordance with equation XVII, i.e., 60.4% by weight CH 6 N 4 0 3 and 39.6% by weight Mo.
- the composition autoignited at 230 ⁇ 2 ⁇ C by DSC analysis.
- a 1:2 ratio of guanidine nitrate to AgN0 3 was mixed with a stoichiometric amount of Mo in accordance with equation XIX, i.e., 21.9% by weight CH 6 N 4 0 3 , 60.9% AgN0 3 and 17.2% by weight Mo.
- the composition autoignited at 172 ⁇ 2°C (by DSC) .
- This composition is also an example of organic nitrates in autoignition reactions. However, this composition is fully oxidized, and, therefore, requires no external source of oxygen.
- Tetramethyl ammonium nitrate, N(CH 3 ) 4 N0 3 was mixed with 5-aminotetraz ⁇ le, CN 5 H 3 , potassium chlorate, KC10 3 , and molybdenum, Mo, in accordance with equation XXV, i.e., 11.8% by weight N(CH 3 ) 4 N0 3 , 8.2% by weight CN 5 H 3 , 56.7% by weight KC10 3 , and 23.3% by weight Mo.
- Tetramethyl ammonium nitrate, N(CH 3 ) 4 N0 3 was mixed with 5-aminotetrazole, CN S H 3 , potassium perchlorate, KC10 4 , and molybdenum, Mo, in accordance with equation XXVI, i.e., 13.1% by weight N(CH 3 ) 4 N0 3 , 9.1% by weight CN S H 3 , 52.1% by weight KC10 4 , and 25.7% by weight Mo.
- An autoignition temperature of 170 + 3°C was determined for this composition by DSC analysis.
- the 5-aminotetrazole used should be anhydrous.
- the invention has also been successfully tested in timed autoignition tests at various temperatures, and in bonfire tests in prototype automobile air bag inflators.
Abstract
Description
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Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BR9711087-6A BR9711087A (en) | 1996-05-14 | 1997-05-12 | Auto-ignition composition to safely initiate combustion of a main pyrotechnic charge and process to safely initiate combustion of a gas generator or pyrotechnic composition to a gas generator or pyrotechnic device |
CA002254903A CA2254903A1 (en) | 1996-05-14 | 1997-05-12 | Autoignition composition |
EP97924657A EP0902773A4 (en) | 1996-05-14 | 1997-05-12 | Autoignition composition |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/645,945 US5959242A (en) | 1996-05-14 | 1996-05-14 | Autoignition composition |
US08/645,945 | 1996-05-14 |
Publications (2)
Publication Number | Publication Date |
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WO1997045294A2 true WO1997045294A2 (en) | 1997-12-04 |
WO1997045294A3 WO1997045294A3 (en) | 1998-10-08 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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PCT/US1997/007933 WO1997045294A2 (en) | 1996-05-14 | 1997-05-12 | Autoignition composition |
Country Status (6)
Country | Link |
---|---|
US (3) | US5959242A (en) |
EP (1) | EP0902773A4 (en) |
BR (1) | BR9711087A (en) |
CA (1) | CA2254903A1 (en) |
TW (1) | TW344738B (en) |
WO (1) | WO1997045294A2 (en) |
Families Citing this family (72)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19581542T1 (en) | 1994-12-21 | 1999-04-01 | Daicel Chem | Gas generating composition |
US6235132B1 (en) * | 1995-03-10 | 2001-05-22 | Talley Defense Systems, Inc. | Gas generating compositions |
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US6214138B1 (en) | 1997-08-18 | 2001-04-10 | Breed Automotive Technology, Inc. | Ignition enhancer composition for an airbag inflator |
US6019861A (en) * | 1997-10-07 | 2000-02-01 | Breed Automotive Technology, Inc. | Gas generating compositions containing phase stabilized ammonium nitrate |
US5985060A (en) * | 1998-07-25 | 1999-11-16 | Breed Automotive Technology, Inc. | Gas generant compositions containing guanidines |
US6123359A (en) * | 1998-07-25 | 2000-09-26 | Breed Automotive Technology, Inc. | Inflator for use with gas generant compositions containing guanidines |
US6156230A (en) * | 1998-08-07 | 2000-12-05 | Atrantic Research Corporation | Metal oxide containing gas generating composition |
DE29821541U1 (en) * | 1998-12-02 | 1999-02-18 | Trw Airbag Sys Gmbh & Co Kg | Azide-free, gas generating composition |
US6086693A (en) * | 1999-02-02 | 2000-07-11 | Autoliv Asp, Inc. | Low particulate igniter composition for a gas generant |
US6165296A (en) * | 1999-02-02 | 2000-12-26 | Autoliv Development As | Gas generant igniter composition and method |
US6077372A (en) * | 1999-02-02 | 2000-06-20 | Autoliv Development Ab | Ignition enhanced gas generant and method |
US6183569B1 (en) * | 1999-03-15 | 2001-02-06 | Spectre Enterprises, Inc. | Cutting torch and associated methods |
US6277221B1 (en) * | 1999-04-13 | 2001-08-21 | Atlantic Research Corporation | Propellant compositions with salts and complexes of lanthanide and rare earth elements |
JP4131486B2 (en) * | 1999-07-09 | 2008-08-13 | 日本化薬株式会社 | Auto-igniting enhancer composition |
US6143101A (en) * | 1999-07-23 | 2000-11-07 | Atlantic Research Corporation | Chlorate-free autoignition compositions and methods |
US6298784B1 (en) * | 1999-10-27 | 2001-10-09 | Talley Defense Systems, Inc. | Heat transfer delay |
US6430920B1 (en) | 1999-11-23 | 2002-08-13 | Technanogy, Llc | Nozzleless rocket motor |
US6503350B2 (en) | 1999-11-23 | 2003-01-07 | Technanogy, Llc | Variable burn-rate propellant |
US6454886B1 (en) | 1999-11-23 | 2002-09-24 | Technanogy, Llc | Composition and method for preparing oxidizer matrix containing dispersed metal particles |
US6485588B1 (en) * | 2000-01-20 | 2002-11-26 | Trw Inc. | Autoignition material additive |
DE60128455T2 (en) * | 2000-03-15 | 2007-09-13 | Daicel Chemical Industries, Ltd., Sakai | Gas generator with automatic ignition |
DE20010154U1 (en) | 2000-06-07 | 2000-09-07 | Trw Airbag Sys Gmbh & Co Kg | Ignition mixture for use in gas generators |
US6605167B1 (en) | 2000-09-01 | 2003-08-12 | Trw Inc. | Autoignition material for a vehicle occupant protection apparatus |
US6673172B2 (en) | 2001-05-07 | 2004-01-06 | Atlantic Research Corporation | Gas generant compositions exhibiting low autoignition temperatures and methods of generating gases therefrom |
US6530382B2 (en) | 2001-06-06 | 2003-03-11 | Basf Corporation | Gel purge formulations and methods of cleaning extruders by using the same |
DE20111410U1 (en) * | 2001-07-10 | 2001-08-30 | Trw Airbag Sys Gmbh & Co Kg | Nitrocellulose free gas generating composition |
US6645326B2 (en) | 2002-03-25 | 2003-11-11 | Breed Automotive Technology, Inc. | Low temperature autoignition material |
WO2004024503A2 (en) * | 2002-09-13 | 2004-03-25 | Automotive Systems Laboratory, Inc. | Inflator |
US6878221B1 (en) * | 2003-01-30 | 2005-04-12 | Olin Corporation | Lead-free nontoxic explosive mix |
US20060054257A1 (en) * | 2003-04-11 | 2006-03-16 | Mendenhall Ivan V | Gas generant materials |
WO2004104491A2 (en) | 2003-05-21 | 2004-12-02 | Alexza Pharmaceuticals, Inc. | Percussively ignited or electrically ignited self-contained heating unit and drug-supply unit employing same |
US20050016646A1 (en) * | 2003-07-25 | 2005-01-27 | Barnes Michael W. | Chlorine-containing gas generant compositions including a copper-containing chlorine scavenger |
US20060289096A1 (en) * | 2003-07-25 | 2006-12-28 | Mendenhall Ivan V | Extrudable gas generant |
US8101033B2 (en) * | 2004-07-26 | 2012-01-24 | Autoliv Asp, Inc. | Alkali metal perchlorate-containing gas generants |
US7337856B2 (en) * | 2003-12-02 | 2008-03-04 | Alliant Techsystems Inc. | Method and apparatus for suppression of fires |
US20050115721A1 (en) | 2003-12-02 | 2005-06-02 | Blau Reed J. | Man-rated fire suppression system |
FR2870234B1 (en) * | 2004-05-13 | 2007-02-09 | Snpe Materiaux Energetiques Sa | DOSABLE PYROTECHNIC COMPOSITION USED AS A THERMAL FUSE IN A GAS GENERATOR AND A GAS GENERATOR INCLUDING A COMPOUND HAVING THE SAME |
WO2005123631A1 (en) * | 2004-06-17 | 2005-12-29 | Nof Corporation | Firing agent for gas generating device |
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FR2883868B1 (en) * | 2005-03-30 | 2007-08-03 | Davey Bickford Snc | SELF-INITIATING COMPOSITIONS, ELECTRIC INITIATORS USING SUCH COMPOSITIONS AND GAS GENERATORS COMPRISING SUCH INITIATORS |
US20060220363A1 (en) * | 2005-03-31 | 2006-10-05 | Blackburn Jeffery S | Gas generating system with autoignition device |
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US20110110833A1 (en) * | 2009-11-12 | 2011-05-12 | Chevron U.S.A. Inc. | Method and apparatus for removing acid gases from a natural gas stream |
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WO2013074428A1 (en) | 2011-11-16 | 2013-05-23 | Eveready Battery Company, Inc. | Hydrogen generator for a fuel cell |
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US8877137B2 (en) | 2012-12-03 | 2014-11-04 | Intelligent Energy Inc. | Hydrogen generator |
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Citations (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3609115A (en) * | 1963-09-30 | 1971-09-28 | North American Rockwell | Propellant binder |
US3652349A (en) * | 1969-08-25 | 1972-03-28 | Susquehanna Corp | Thixotropic gas producing gel |
US3837938A (en) * | 1965-08-19 | 1974-09-24 | Rockwell International Corp | Solid propellant containing fuel-oxidizer component prepared from fused oxidizers |
US3862866A (en) * | 1971-08-02 | 1975-01-28 | Specialty Products Dev Corp | Gas generator composition and method |
US3890174A (en) * | 1972-02-18 | 1975-06-17 | Jr Horace H Helms | Pyrotechnic composition |
US4203786A (en) * | 1978-06-08 | 1980-05-20 | Allied Chemical Corporation | Polyethylene binder for pyrotechnic composition |
US4238253A (en) * | 1978-05-15 | 1980-12-09 | Allied Chemical Corporation | Starch as fuel in gas generating compositions |
US4248644A (en) * | 1978-04-11 | 1981-02-03 | Aeci Limited | Emulsion of a melt explosive composition |
US4274893A (en) * | 1979-03-26 | 1981-06-23 | Rocket Research Company | High temperature two component explosive |
US4402269A (en) * | 1981-06-29 | 1983-09-06 | The United States Of America As Represented By The Secretary Of The Navy | Electric delay detonator |
US4632714A (en) * | 1985-09-19 | 1986-12-30 | Megabar Corporation | Microcellular composite energetic materials and method for making same |
US5026442A (en) * | 1989-04-11 | 1991-06-25 | Ici Australia Operations Proprietary Limited | Melt-in-fuel emulsion explosive composition and method |
US5035756A (en) * | 1989-01-10 | 1991-07-30 | United States Of America As Represented By The Secretary Of The Navy | Bonding agents for thermite compositions |
US5084118A (en) * | 1990-10-23 | 1992-01-28 | Automotive Systems Laboratory, Inc. | Ignition composition for inflator gas generators |
US5380380A (en) * | 1994-02-09 | 1995-01-10 | Automotive Systems Laboratory, Inc. | Ignition compositions for inflator gas generators |
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 |
US5482579A (en) * | 1993-04-15 | 1996-01-09 | Nof Corporation | Gas generator compositions |
US5538567A (en) * | 1994-03-18 | 1996-07-23 | Olin Corporation | Gas generating propellant |
US5542688A (en) * | 1992-10-27 | 1996-08-06 | Atlantic Research Corporation | Two-part igniter for gas generating compositions |
US5551725A (en) * | 1995-03-10 | 1996-09-03 | Ludwig; Christopher P. | Vehicle airbag inflator and related method |
Family Cites Families (33)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2008366A (en) * | 1931-11-12 | 1935-07-16 | Hercules Powder Co Ltd | Igniter powder |
US1964077A (en) * | 1932-05-05 | 1934-06-26 | Hercules Powder Co Ltd | Flash composition |
US2316358A (en) * | 1940-08-02 | 1943-04-13 | Gen Electric | Flash powder and method of preparation |
US2981616A (en) * | 1956-10-01 | 1961-04-25 | North American Aviation Inc | Gas generator grain |
US3053710A (en) * | 1957-12-12 | 1962-09-11 | Dow Chemical Co | Magnesium hydride explosive compositions |
US3028229A (en) * | 1958-08-27 | 1962-04-03 | Universal Match Corp | Pyrotechnic compositions |
US3017301A (en) * | 1959-03-27 | 1962-01-16 | Du Pont | Propellant compositions containing a polycyano fuel component |
US3175979A (en) * | 1961-09-22 | 1965-03-30 | Foote Mineral Co | Controlling the decomposition rate of lithium perchlorate |
US3195302A (en) * | 1962-01-22 | 1965-07-20 | Atlantic Res Corp | Solid propellant grain of variable electron-emissive composition |
US3269879A (en) * | 1964-04-13 | 1966-08-30 | Aerojet General Co | Ammonium salt lattice with isomorphously substituted inorganic salts |
US3309250A (en) * | 1965-03-24 | 1967-03-14 | Charles W Falterman | Temperature resistant explosive containing titanium and alkali metal perchlorate |
US3370537A (en) * | 1965-07-22 | 1968-02-27 | Mine Safety Appliances Co | Castable pyrotechnic composition comprising metal nitrates or chlorates and finely divided metal |
US3418184A (en) * | 1968-01-16 | 1968-12-24 | Navy Usa | Smoke producing propellant |
US3490966A (en) * | 1969-01-28 | 1970-01-20 | Mine Safety Appliances Co | Cast flares for red,green and blue color |
US4406228A (en) * | 1969-04-22 | 1983-09-27 | The United States Of America As Represented By The Secretary Of The Navy | Device for burning pyrotechnic mixtures in a very low pressure environment |
US3729351A (en) * | 1969-10-01 | 1973-04-24 | Us Navy | Flare composition comprising dry blend of metal fuel and eutectic mixture of oxidizer salts |
US3726728A (en) * | 1970-04-20 | 1973-04-10 | Us Navy | Binderless cast photoflash compositions |
US3773351A (en) * | 1971-08-02 | 1973-11-20 | Timmerman H | Gas generator |
GB1391310A (en) * | 1972-07-24 | 1975-04-23 | Canadian Ind | Gas generating compositions |
US4179327A (en) * | 1978-07-13 | 1979-12-18 | Allied Chemical Corporation | Process for coating pyrotechnic materials |
DE3105060C1 (en) * | 1981-02-12 | 1982-09-30 | Diehl GmbH & Co, 8500 Nürnberg | Initiating explosive mixture without detonator and provision of the initiating explosive mixture in a missile |
US4438700A (en) * | 1982-07-19 | 1984-03-27 | The United States Of America As Represented By The Secretary Of The Army | White smoke spotting composition for training ammunition |
US4561675A (en) * | 1984-04-02 | 1985-12-31 | Morton Thiokol, Inc. | Auto ignition device |
IN171629B (en) * | 1986-07-07 | 1992-11-28 | Aeci Ltd | |
US4861397A (en) * | 1988-03-09 | 1989-08-29 | The United States Of America As Represented By The Secretary Of The Army | Fire-resistant explosives |
US5035757A (en) * | 1990-10-25 | 1991-07-30 | Automotive Systems Laboratory, Inc. | Azide-free gas generant composition with easily filterable combustion products |
US5858460A (en) * | 1991-07-01 | 1999-01-12 | The United States Of America As Represented By The Secretary Of The Navy | Metal matrices reinforced with silver coated boron carbide particles |
US5431103A (en) * | 1993-12-10 | 1995-07-11 | Morton International, Inc. | Gas generant compositions |
US5531473A (en) * | 1994-05-31 | 1996-07-02 | Morton International, Inc. | Fluid fuel-containing initiator device for an air bag inflator |
US5672843A (en) * | 1994-10-05 | 1997-09-30 | Ici Americas Inc. | Single charge pyrotechnic |
US5514230A (en) * | 1995-04-14 | 1996-05-07 | Automotive Systems Laboratory, Inc. | Nonazide gas generating compositions with a built-in catalyst |
US5959242A (en) * | 1996-05-14 | 1999-09-28 | Talley Defense Systems, Inc. | Autoignition composition |
US5847315A (en) * | 1996-11-29 | 1998-12-08 | Ecotech | Solid solution vehicle airbag clean gas generator propellant |
-
1996
- 1996-05-14 US US08/645,945 patent/US5959242A/en not_active Expired - Fee Related
-
1997
- 1997-01-30 US US08/791,176 patent/US5739460A/en not_active Expired - Lifetime
- 1997-05-12 EP EP97924657A patent/EP0902773A4/en not_active Withdrawn
- 1997-05-12 BR BR9711087-6A patent/BR9711087A/en not_active Application Discontinuation
- 1997-05-12 WO PCT/US1997/007933 patent/WO1997045294A2/en not_active Application Discontinuation
- 1997-05-12 CA CA002254903A patent/CA2254903A1/en not_active Abandoned
- 1997-05-14 TW TW086106430A patent/TW344738B/en active
-
1998
- 1998-01-22 US US09/010,822 patent/US6749702B1/en not_active Expired - Fee Related
Patent Citations (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3609115A (en) * | 1963-09-30 | 1971-09-28 | North American Rockwell | Propellant binder |
US3837938A (en) * | 1965-08-19 | 1974-09-24 | Rockwell International Corp | Solid propellant containing fuel-oxidizer component prepared from fused oxidizers |
US3652349A (en) * | 1969-08-25 | 1972-03-28 | Susquehanna Corp | Thixotropic gas producing gel |
US3862866A (en) * | 1971-08-02 | 1975-01-28 | Specialty Products Dev Corp | Gas generator composition and method |
US3890174A (en) * | 1972-02-18 | 1975-06-17 | Jr Horace H Helms | Pyrotechnic composition |
US4248644A (en) * | 1978-04-11 | 1981-02-03 | Aeci Limited | Emulsion of a melt explosive composition |
US4238253A (en) * | 1978-05-15 | 1980-12-09 | Allied Chemical Corporation | Starch as fuel in gas generating compositions |
US4203786A (en) * | 1978-06-08 | 1980-05-20 | Allied Chemical Corporation | Polyethylene binder for pyrotechnic composition |
US4274893A (en) * | 1979-03-26 | 1981-06-23 | Rocket Research Company | High temperature two component explosive |
US4402269A (en) * | 1981-06-29 | 1983-09-06 | The United States Of America As Represented By The Secretary Of The Navy | Electric delay detonator |
US4632714A (en) * | 1985-09-19 | 1986-12-30 | Megabar Corporation | Microcellular composite energetic materials and method for making same |
US5035756A (en) * | 1989-01-10 | 1991-07-30 | United States Of America As Represented By The Secretary Of The Navy | Bonding agents for thermite compositions |
US5026442A (en) * | 1989-04-11 | 1991-06-25 | Ici Australia Operations Proprietary Limited | Melt-in-fuel emulsion explosive composition and method |
US5084118A (en) * | 1990-10-23 | 1992-01-28 | Automotive Systems Laboratory, Inc. | Ignition composition for inflator gas generators |
US5542688A (en) * | 1992-10-27 | 1996-08-06 | Atlantic Research Corporation | Two-part igniter for gas generating compositions |
US5482579A (en) * | 1993-04-15 | 1996-01-09 | Nof Corporation | Gas generator compositions |
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 |
US5380380A (en) * | 1994-02-09 | 1995-01-10 | Automotive Systems Laboratory, Inc. | Ignition compositions for inflator gas generators |
US5538567A (en) * | 1994-03-18 | 1996-07-23 | Olin Corporation | Gas generating propellant |
US5551725A (en) * | 1995-03-10 | 1996-09-03 | Ludwig; Christopher P. | Vehicle airbag inflator and related method |
Non-Patent Citations (1)
Title |
---|
See also references of EP0902773A2 * |
Also Published As
Publication number | Publication date |
---|---|
CA2254903A1 (en) | 1997-12-04 |
WO1997045294A3 (en) | 1998-10-08 |
EP0902773A4 (en) | 2000-05-24 |
US6749702B1 (en) | 2004-06-15 |
BR9711087A (en) | 2000-07-11 |
US5959242A (en) | 1999-09-28 |
EP0902773A2 (en) | 1999-03-24 |
TW344738B (en) | 1998-11-11 |
US5739460A (en) | 1998-04-14 |
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