EP0666248B1 - Gas generating mixture - Google Patents

Gas generating mixture Download PDF

Info

Publication number
EP0666248B1
EP0666248B1 EP94119383A EP94119383A EP0666248B1 EP 0666248 B1 EP0666248 B1 EP 0666248B1 EP 94119383 A EP94119383 A EP 94119383A EP 94119383 A EP94119383 A EP 94119383A EP 0666248 B1 EP0666248 B1 EP 0666248B1
Authority
EP
European Patent Office
Prior art keywords
catalyst
mixture according
mixture
carrier
metal
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
Application number
EP94119383A
Other languages
German (de)
French (fr)
Other versions
EP0666248A1 (en
Inventor
Klaus Martin Dr. Bucerius
Helmut Schmid
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Fraunhofer Gesellschaft zur Forderung der Angewandten Forschung eV
Original Assignee
Fraunhofer Gesellschaft zur Forderung der Angewandten Forschung eV
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Fraunhofer Gesellschaft zur Forderung der Angewandten Forschung eV filed Critical Fraunhofer Gesellschaft zur Forderung der Angewandten Forschung eV
Publication of EP0666248A1 publication Critical patent/EP0666248A1/en
Application granted granted Critical
Publication of EP0666248B1 publication Critical patent/EP0666248B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B23/00Compositions characterised by non-explosive or non-thermic constituents
    • C06B23/007Ballistic modifiers, burning rate catalysts, burning rate depressing agents, e.g. for gas generating
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06DMEANS FOR GENERATING SMOKE OR MIST; GAS-ATTACK COMPOSITIONS; GENERATION OF GAS FOR BLASTING OR PROPULSION (CHEMICAL PART)
    • C06D5/00Generation of pressure gas, e.g. for blasting cartridges, starting cartridges, rockets
    • C06D5/06Generation of pressure gas, e.g. for blasting cartridges, starting cartridges, rockets by reaction of two or more solids

Definitions

  • the invention relates to a gas-generating mixture of a fuel, an oxidizer and a catalyst.
  • Gas-generating mixtures of the aforementioned type - also called gas generator sets - are characterized in that they enable a high gas yield (> 14 mol / kg) during combustion. They are used for rocket and barrel weapon drives as well as for inflatable restraint (airbag) and rescue systems. In the civil sector in particular, thermal-mechanical insensitivity and non-toxicity of the starting mixtures, but also a lack of toxicity in the resulting gases are required. Many systems in use do not meet these requirements, or meet them only very inadequately.
  • the invention has for its object to lower the combustion temperature and increase the rate of combustion in a mixture of the structure mentioned in the introduction.
  • the oxidizer is Cu (NO 3 ) 2 * 3Cu (OH) 2 and the catalyst consists of a metal or a metal alloy on a support.
  • the oxidizer provided according to the invention results in sustained and rapid combustion.
  • the maximum pressure is reached within milliseconds, with the gas temperature remaining below harmful limits.
  • Hitherto necessary slag formers, which in known systems for binding pollutants, e.g. Alkali oxides, required, can be omitted in the mixture according to the invention, so that a higher gas yield can be achieved.
  • the catalyst which is also used according to the invention is primarily used to reduce harmful gas (CO and NO), the term "catalyst" in the broader sense here denoting an active reaction component which can be implemented itself and has a reaction-guiding and / or reaction-accelerating effect.
  • the carrier serves to present the main component with a large specific surface and a defined grain size distribution. Another property of the carrier is to develop a cooling effect through physical and / or chemical processes - in a special phase of the reaction, that goes beyond a pure capacitive cooling effect.
  • the carrier can also act as a promoter of the main component. Not only the metal catalyst, but also the oxidizer are thermally and mechanically stable and in particular also not hygroscopic.
  • the catalyst is preferably a pyrophoric metal or such a metal alloy on a support which remains as a solid after the combustion.
  • This can be a silicate, preferably a layered or framework silicate.
  • N-rich and C-poor fuels include the well-known fuels TAGN (triaminoguanidine nitrate), NIGU (nitroguanidine), NTO (3-nitro-1,2,3-triazol-5-one) and the GZT (diguanidinium-5,5 '), which is characterized by a particularly high nitrogen content. -azotetrazolate) (DE 4 108 225).
  • TAGN, NIGU, NTO, but in particular GZT are preferably used in the mixture according to the invention when used for rescue and restraint systems.
  • a preferred mixture consists of GZT and Cu (NO 3 ) 2 * 3Cu (OH) 2 with a balanced oxygen balance and up to 30% by mass of the catalyst.
  • the mixture can contain Fe 2 O 3 as the coolant, the oxidative properties of which can additionally be used in the reaction mixture (DE 41 33 655, EP 0 536 525).
  • a mixture consisting of GZT, pyrophoric Ag on a layer or framework silicate support as catalyst and Cu (NO 3 ) 2 * 3Cu (OH) 2 as oxidizer in a ratio of 22.05: 20.0: 57.95 mass% manufactured.
  • This formulation is investigated experimentally in the ballistic bomb with regard to its ignition and combustion behavior.
  • a pressure curve diagram according to the system is obtained. The diagram shows that the mixture has good ignition and combustion properties.
  • the combustion temperature can be determined very precisely by thermodynamic calculation. It is 2345 K. With the same GZT fuel and a balanced oxygen balance, other oxidizers deliver higher combustion temperatures. For example, they are 2501 K for KNO 3 , 2850 K for NH 4 NO 3 and 3248 K for K Cl O 3 .

Landscapes

  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Catalysts (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)

Description

Die Erfindung betrifft eine gaserzeugende Mischung aus einem Brennstoff, einem Oxidator und einem Katalysator.The invention relates to a gas-generating mixture of a fuel, an oxidizer and a catalyst.

Gaserzeugende Mischungen der vorgenannten Art - auch Gasgeneratorsätze genannt - zeichnen sich dadurch aus, daß sie bei Verbrennung eine hohe Gasausbeute (> 14 mol/kg) ermöglichen. Sie werden für Raketen- und Rohrwaffenantriebe sowie für aufblasbare Rückhalte- (Airbag) und Rettungssysteme verwendet. Besonders im zivilen Bereich werden thermisch-mechanische Unempfindlichkeit und Ungiftigkeit der Ausgangsmischungen, aber auch fehlende Toxizität bei den entstehenden Gasen gefordert. Viele im Einsatz befindlichen Systeme erfüllen diese Forderungen nicht oder nur sehr unzulänglich.Gas-generating mixtures of the aforementioned type - also called gas generator sets - are characterized in that they enable a high gas yield (> 14 mol / kg) during combustion. They are used for rocket and barrel weapon drives as well as for inflatable restraint (airbag) and rescue systems. In the civil sector in particular, thermal-mechanical insensitivity and non-toxicity of the starting mixtures, but also a lack of toxicity in the resulting gases are required. Many systems in use do not meet these requirements, or meet them only very inadequately.

Die Reaktion dieser Brennstoffe mit den bisher eingesetzten Katalysatoren und Oxidatoren zeigen eine unbefriedigende Gaszusammensetzung und/oder ein ungenügendes Abbrandverhalten. Hinzu kommt, daß viele Reaktionsmischungen eine so hohe Verbrennungstemperatur besitzen, daß - bei Airbag-Anwendungen - die thermisch empfindlichen Sackmaterialien geschädigt werden.The reaction of these fuels with the previously used catalysts and oxidizers shows an unsatisfactory gas composition and / or inadequate combustion behavior. Add to that many Reaction mixtures have such a high combustion temperature that - in airbag applications - the thermally sensitive sack materials are damaged.

Der Erfindung liegt die Aufgabe zugrunde, bei einer Mischung des eingangs genannten Aufbaus, die Verbrennungstemperatur abzusenken und die Abbrandgeschwindigkeit zu erhöhen.The invention has for its object to lower the combustion temperature and increase the rate of combustion in a mixture of the structure mentioned in the introduction.

Diese an sich konträren Anforderungen werden erfindungsgemäß dadurch erfüllt, daß der Oxidator Cu(NO3)2*3Cu(OH)2 ist und der Katalysator aus einem Metall oder einer Metallegierung auf einem Träger besteht .According to the invention, these contradictory requirements are met in that the oxidizer is Cu (NO 3 ) 2 * 3Cu (OH) 2 and the catalyst consists of a metal or a metal alloy on a support.

Durch den erfindungsgemäß vorgesehenen Oxidator ergibt sich eine halte und schnelle Verbrennung. Der Maximaldruck wird innerhalb Millisekunden erreicht, wobei die Gastemperatur unterhalb schädlicher Grenzen bleibt. Bisher notwendige Schlackenbildner, die bei bekannten Systemen zur Bindung von Schadstoffen, z.B. Alkalioxiden, benötigt werden, können bei der erfindungsgemäßen Mischung entfallen, so daß eine höhere Gasausbeute erzielbar ist.The oxidizer provided according to the invention results in sustained and rapid combustion. The maximum pressure is reached within milliseconds, with the gas temperature remaining below harmful limits. Hitherto necessary slag formers, which in known systems for binding pollutants, e.g. Alkali oxides, required, can be omitted in the mixture according to the invention, so that a higher gas yield can be achieved.

Der weiterhin erfindungsgemäß eingesetzte Katalysator dient vornehmlich der Schadgasreduzierung (CO und NO), wobei hier der Begriff "Katalysator" im erweiterten Sinn einen aktiven Reaktionsbestandteil bezeichnet, der selbst umgesetzt werden kann und reaktionslenkend und/oder reaktionsbeschleunigend wirkt. Der Träger dient dazu, die Hauptkomponente mit einer großen spezifischen Oberfläche und einer definierten Korngrößenverteilung vorzulegen. Eine weitere Eigenschaft des Trägers besteht darin, durch physikalische und/oder chemische Prozesse - in einer speziellen Phase der Reaktion - eine Kühlwirkung zu entfalten, die über eine reine kapazitive Kühlwirkung hinausgeht. Der Träger kann ferner als Promotor der Hauptkomponente wirken. Nicht nur der Metallkatalysator, sondern auch der Oxidator sind thermisch und mechanisch stabil und insbesondere auch nicht hygroskopisch.The catalyst which is also used according to the invention is primarily used to reduce harmful gas (CO and NO), the term "catalyst" in the broader sense here denoting an active reaction component which can be implemented itself and has a reaction-guiding and / or reaction-accelerating effect. The carrier serves to present the main component with a large specific surface and a defined grain size distribution. Another property of the carrier is to develop a cooling effect through physical and / or chemical processes - in a special phase of the reaction, that goes beyond a pure capacitive cooling effect. The carrier can also act as a promoter of the main component. Not only the metal catalyst, but also the oxidizer are thermally and mechanically stable and in particular also not hygroscopic.

Der Katalysator ist vorzugsweise ein pyrophores Metall oder eine solche Metallegierung auf einem Träger, der nach dem Abbrand als Feststoff verbleibt. Es kann sich hierbei um ein Silikat, vorzugsweise ein Schicht- oder Gerüstsilikat, handeln.The catalyst is preferably a pyrophoric metal or such a metal alloy on a support which remains as a solid after the combustion. This can be a silicate, preferably a layered or framework silicate.

Als Metall hat sich insbesondere Ag hervorragend bewährt. Bei insbesondere zivilen Anwendungen werden ungiftige Ausgangsverbindungen und ungiftige Reaktionsprodukte gefordert. Diese Forderungen werden von N-reichen und C-armen Brennstoffen erfüllt. Hierzu zählen die bekannten Brennstoffe TAGN (Triaminoguanidinnitrat), NIGU (Nitroguanidin), NTO (3-Nitro-1,2,3-triazol-5-on) und das sich durch einen besonders hohen Stickstoffgehalt auszeichnende GZT (Diguanidinium-5,5'-azotetrazolat) (DE 4 108 225). Es werden deshalb im Rahmen der erfindungsgemäßen Mischung bei Verwendung für Rettungs- und Rückhaltsysteme vorzugsweise TAGN, NIGU, NTO, insbesondere aber GZT eingesetzt.Ag, in particular, has proven to be an excellent metal. In civil applications in particular, non-toxic starting compounds and non-toxic reaction products are required. These requirements are met by N-rich and C-poor fuels. These include the well-known fuels TAGN (triaminoguanidine nitrate), NIGU (nitroguanidine), NTO (3-nitro-1,2,3-triazol-5-one) and the GZT (diguanidinium-5,5 '), which is characterized by a particularly high nitrogen content. -azotetrazolate) (DE 4 108 225). For this reason, TAGN, NIGU, NTO, but in particular GZT, are preferably used in the mixture according to the invention when used for rescue and restraint systems.

Eine bevorzugte Mischung besteht aus GZT und Cu(NO3)2*3Cu(OH)2 mit ausgeglichener Sauerstoffbilanz und bis zu 30 Mass.-% des Katalysators.A preferred mixture consists of GZT and Cu (NO 3 ) 2 * 3Cu (OH) 2 with a balanced oxygen balance and up to 30% by mass of the catalyst.

Die Mischung kann als Kühlmittel Fe2O3 enthalten, dessen oxidative Eigenschaften in der Reaktionsmischung zusätzlich genutzt werden können (DE 41 33 655, EP 0 536 525).The mixture can contain Fe 2 O 3 as the coolant, the oxidative properties of which can additionally be used in the reaction mixture (DE 41 33 655, EP 0 536 525).

Beispielexample

Es wird eine Mischung bestehend aus GZT, pyrophorem Ag auf einem Schicht- oder Gerüstsilikatträger als Katalysator und Cu(NO3)2*3Cu(OH)2 als Oxidator im Verhältnis 22,05 : 20,0 : 57,95 Mass.-% hergestellt. Diese Formulierung wird bezüglich ihres Anzünd- und Verbrennungsverhaltens experimentell in der ballistischen Bombe untersucht. Dabei wird ein Druckverlaufsdiagramm gemäß Anlage erhalten. Das Diagramm zeigt, daß die Mischung gute Anzünd- und Verbrennungseigenschaften besitzt. Bei einer Ladedichte von 0,1 g/cm3 liegt der maximale Druck im Bereich von 250 bar (25MPa), der nach etwa 21 ms erreicht wird (t(pmax) = 21 ms). Die Druckanstiegszeit zwischen 30 bis 80 % des Maximaldrucks beträgt t30-80 = 4,35 ms.A mixture consisting of GZT, pyrophoric Ag on a layer or framework silicate support as catalyst and Cu (NO 3 ) 2 * 3Cu (OH) 2 as oxidizer in a ratio of 22.05: 20.0: 57.95 mass% manufactured. This formulation is investigated experimentally in the ballistic bomb with regard to its ignition and combustion behavior. A pressure curve diagram according to the system is obtained. The diagram shows that the mixture has good ignition and combustion properties. With a loading density of 0.1 g / cm 3 , the maximum pressure is in the range of 250 bar (25MPa), which is reached after about 21 ms (t (pmax) = 21 ms). The pressure rise time between 30 to 80% of the maximum pressure is t 30-80 = 4.35 ms.

Die Verbrennungstemperatur läßt sich sehr exakt durch thermodynamische Berechnung ermitteln. Sie liegt bei 2345 K. Bei gleichem Brennstoff GZT und ausgeglichener Sauerstoffbilanz liefern andere Oxidatoren höhere Verbrennungstemperaturen. Beispielsweise liegen sie bei KNO3 bei 2501 K, bei N H4 NO3 bei 2850 K und bei K Cl O3 bei 3248 K.The combustion temperature can be determined very precisely by thermodynamic calculation. It is 2345 K. With the same GZT fuel and a balanced oxygen balance, other oxidizers deliver higher combustion temperatures. For example, they are 2501 K for KNO 3 , 2850 K for NH 4 NO 3 and 3248 K for K Cl O 3 .

Claims (8)

  1. A gas generating mixture of a fuel, an oxidant and a catalyst, characterized in that the oxidant is Cu(NO3)2*3Cu(OH)2 and the catalyst consists of a metal or a metal alloy on a carrier.
  2. A mixture according to claim 1, characterized in that the catalyst is a pyrophoric metal or a pyrophoric metal alloy on a carrier.
  3. A mixture according to claim 1 or 2, characterized in that a silicate, especially a layer or skeleton silicate serves as the carrier for the metal catalyst.
  4. A mixture according to claim 3, characterized in that pyrophoric Ag on a layer or skeleton silicate carrier serves as the catalyst.
  5. A mixture according to any of claims 1 to 4, characterized in that TAGN (triaminoguanidine nitrate), NIGU (nitroguanidine), NTO (3-nitro-1,2,3-triazol-5-one) or GZT (diguanidinium-5,5'-azotetrazolate) serves as the fuel.
  6. A mixture according to any of claims 1 to 5, consisting of a mixture of GZT and Cu(NO3)2*3Cu(OH)2 with equalised oxygen balance and up to 30% by mass of the catalyst.
  7. A mixture according to any of claims 1 to 6, characterized in that the catalyst has a mean grain size < 10 µm.
  8. A mixture according to any of claims 1 to 7, characterized in that it includes Fe2O3 as a coolant.
EP94119383A 1994-01-18 1994-12-08 Gas generating mixture Expired - Lifetime EP0666248B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE4401214 1994-01-18
DE4401214A DE4401214C1 (en) 1994-01-18 1994-01-18 Gas-generating mixture

Publications (2)

Publication Number Publication Date
EP0666248A1 EP0666248A1 (en) 1995-08-09
EP0666248B1 true EP0666248B1 (en) 1996-10-23

Family

ID=6508092

Family Applications (1)

Application Number Title Priority Date Filing Date
EP94119383A Expired - Lifetime EP0666248B1 (en) 1994-01-18 1994-12-08 Gas generating mixture

Country Status (3)

Country Link
US (1) US5542999A (en)
EP (1) EP0666248B1 (en)
DE (2) DE4401214C1 (en)

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4442170C1 (en) * 1994-11-26 1995-12-21 Fraunhofer Ges Forschung Non-toxic gas-generating mixt. with thermal-mechanical stability
DE4442169C1 (en) * 1994-11-26 1995-12-21 Fraunhofer Ges Forschung Non-toxic gas-generating mixt. with thermal-mechanical stability
JPH08231291A (en) * 1994-12-27 1996-09-10 Daicel Chem Ind Ltd Gas generating agent composition
DE19531288A1 (en) * 1995-08-25 1997-02-27 Temic Bayern Chem Airbag Gmbh Airbag propellant gas generator
US5608183A (en) * 1996-03-15 1997-03-04 Morton International, Inc. Gas generant compositions containing amine nitrates plus basic copper (II) nitrate and/or cobalt(III) triammine trinitrate
DE59711752D1 (en) 1996-07-20 2004-08-05 Dynamit Nobel Ag THERMAL FUSE
US6527886B1 (en) 1996-07-22 2003-03-04 Daicel Chemical Industries, Ltd. Gas generant for air bag
US6497774B2 (en) 1996-07-22 2002-12-24 Daicel Chemical Industries, Ltd. Gas generant for air bag
US6306232B1 (en) 1996-07-29 2001-10-23 Automotive Systems Laboratory, Inc. Thermally stable nonazide automotive airbag propellants
WO1998039275A1 (en) * 1997-03-05 1998-09-11 Automotive Systems Laboratory, Inc. Gas generants comprising carbonato metal ammine complexes
DE19812372C2 (en) * 1998-03-20 2001-10-04 Nigu Chemie Gmbh Gas generator fuels
US6132538A (en) * 1998-07-30 2000-10-17 Autoliv Development Ab High gas yield generant compositions
US6143102A (en) * 1999-05-06 2000-11-07 Autoliv Asp, Inc. Burn rate-enhanced basic copper nitrate-containing gas generant compositions and methods
JP4800469B2 (en) * 1999-10-08 2011-10-26 ダイセル化学工業株式会社 Gas generant composition
KR20020048419A (en) * 1999-09-27 2002-06-22 고지마 아끼로, 오가와 다이스께 Basic metal nitrate, method for producing the same and gas-generating agent composition
US6224697B1 (en) 1999-12-03 2001-05-01 Autoliv Development Ab Gas generant manufacture
US6372191B1 (en) 1999-12-03 2002-04-16 Autoliv Asp, Inc. Phase stabilized ammonium nitrate and method of making the same
JP4500399B2 (en) * 2000-02-04 2010-07-14 ダイセル化学工業株式会社 Gas generant composition containing triazine derivative
US6436211B1 (en) 2000-07-18 2002-08-20 Autoliv Asp, Inc. Gas generant manufacture
US6589375B2 (en) 2001-03-02 2003-07-08 Talley Defense Systems, Inc. Low solids gas generant having a low flame temperature
EP1386899B1 (en) * 2001-05-10 2011-07-13 Nippon Kayaku Kabushiki Kaisha Igniting agent composition, and igniter using the igniting agent composition
US6854395B2 (en) 2001-08-10 2005-02-15 Daicel Chemical Industries, Ltd. Inflator for an air bag
US6875295B2 (en) 2001-12-27 2005-04-05 Trw Inc. Cool burning gas generating material for a vehicle occupant protection apparatus
US20040154710A1 (en) * 2002-07-25 2004-08-12 Mamoru Watabiki Gas generating composition
US20050263224A1 (en) * 2002-08-05 2005-12-01 Jianzhou Wu Gas generating composition for inflator containing melamine cyanurate
US6964716B2 (en) * 2002-09-12 2005-11-15 Daicel Chemical Industries, Ltd. Gas generating composition
US7618506B2 (en) * 2002-10-31 2009-11-17 Daicel Chemical Industries, Ltd. Gas generating composition
US6872265B2 (en) 2003-01-30 2005-03-29 Autoliv Asp, Inc. Phase-stabilized ammonium nitrate
US20050127324A1 (en) * 2003-10-22 2005-06-16 Jianzhou Wu Gas generating composition
US20050257866A1 (en) * 2004-03-29 2005-11-24 Williams Graylon K Gas generant and manufacturing method thereof
JP4610266B2 (en) 2004-09-09 2011-01-12 ダイセル化学工業株式会社 Gas generant composition
US8137771B2 (en) * 2004-09-09 2012-03-20 Daicel Chemical Industries, Ltd. Gas generating composition
US20060191614A1 (en) * 2005-02-10 2006-08-31 Daicel Chemical Industries, Ltd. Gas generating composition

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2604391A (en) * 1946-11-08 1952-07-22 Ici Ltd Gas-producing nondetonating composition
GB658643A (en) * 1949-01-12 1951-10-10 Alexander Cantlay Hutchison Improvements in or relating to solid gas generating charges
US3664898A (en) * 1969-08-04 1972-05-23 Us Navy Pyrotechnic composition
US3936330A (en) * 1973-08-08 1976-02-03 The Dow Chemical Company Composition and method for inflation of passive restraint systems
US4336085A (en) * 1975-09-04 1982-06-22 Walker Franklin E Explosive composition with group VIII metal nitroso halide getter
US4632714A (en) * 1985-09-19 1986-12-30 Megabar Corporation Microcellular composite energetic materials and method for making same
US4931112A (en) * 1989-11-20 1990-06-05 Morton International, Inc. Gas generating compositions containing nitrotriazalone
US4994123A (en) * 1990-05-29 1991-02-19 The United States Of America As Represented By The Secretary Of The Air Force Polymeric intermolecular emulsion explosive
US5145535A (en) * 1991-02-25 1992-09-08 United States Of America As Represented By The Secretary Of The Air Force Method for intermolecular explosive with viscosity modifier
DE4108225C1 (en) * 1991-03-14 1992-04-09 Fraunhofer-Gesellschaft Zur Foerderung Der Angewandten Forschung Ev, 8000 Muenchen, De
DE4218531C1 (en) * 1991-10-11 1993-07-15 Bayern-Chemie Gesellschaft Fuer Flugchemische Antriebe Mbh, 8261 Aschau, De

Also Published As

Publication number Publication date
EP0666248A1 (en) 1995-08-09
DE4401214C1 (en) 1995-03-02
DE59400902D1 (en) 1996-11-28
US5542999A (en) 1996-08-06

Similar Documents

Publication Publication Date Title
EP0666248B1 (en) Gas generating mixture
EP0665201B1 (en) Gas generating mixture
DE3602731C2 (en) Composition for the production of nitrogen gas
DE4412871C2 (en) Gas generator compositions
DE69730202T2 (en) AZIDFREE, GAS-CREATING COMPOSITIONS
EP0716058B1 (en) Gas generating mixture
EP0705809B1 (en) Propelland based on phase-stabilized ammonium nitrate
EP0503341B1 (en) Stable nitrogen-rich compound
EP0691317B1 (en) Non-azide gas generant formulations
EP0905108B1 (en) Particle-free gas generating mixture
EP0519485A1 (en) Propellant for gas generators
DE2439771A1 (en) PYROTECHNICAL MIXTURE
EP0716059B1 (en) Gas generating mixture
DE10034287C2 (en) Gas generating composition comprising guanyl urea dinitramide and its use
DE4446976B4 (en) Solid pyrotechnic compositions with thermoplastic binder and softener based on silylferrocene polybutadiene
EP1162183B1 (en) Ignition mixture for use in gas generators
DE19840993B4 (en) Use of a gas-generating mixture as ignition mixture in a gas generator
EP0914306A1 (en) Pyrotechnic mixture as propellant or a gas charge with carbon monoxide-reduced vapors
WO1998017607A1 (en) Azide-free, gas-generating solid mixture
EP0716060B1 (en) Gas generating mixture
WO2000048967A1 (en) Gas-generating substances
DE60012933T2 (en) COMPOSITE, GAS-PRODUCING MATERIAL FOR GAS-OPERATED VEHICLE SAFETY DEVICES
WO2006039892A2 (en) Substance mixture as a thermally initiatable ignition mixture
EP1051373B1 (en) Acid-free, gas-generating composition
DE102011100113A1 (en) Gas generator fuel composition on the basis of guanyl urea dinitramide, useful e.g. for hydraulic systems, comprises fuel- and/or explosive material and additional fuel- and/or explosive material, polymer binder, and combustion modifier

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): DE FR GB IT NL SE

17P Request for examination filed

Effective date: 19950819

17Q First examination report despatched

Effective date: 19951016

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE FR GB IT NL SE

GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)

Effective date: 19961001

ET Fr: translation filed
REF Corresponds to:

Ref document number: 59400902

Country of ref document: DE

Date of ref document: 19961128

ITF It: translation for a ep patent filed

Owner name: UFFICIO BREVETTI RICCARDI & C.

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
REG Reference to a national code

Ref country code: GB

Ref legal event code: IF02

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20061215

Year of fee payment: 13

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: NL

Payment date: 20061218

Year of fee payment: 13

Ref country code: GB

Payment date: 20061218

Year of fee payment: 13

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: SE

Payment date: 20061227

Year of fee payment: 13

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20061231

Year of fee payment: 13

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20070221

Year of fee payment: 13

EUG Se: european patent has lapsed
GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20071208

NLV4 Nl: lapsed or anulled due to non-payment of the annual fee

Effective date: 20080701

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20080701

Ref country code: SE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20071209

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20081020

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20080701

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20071208

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20071231

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20071208