EP1637511A3 - Pyrotechnical actuator with a charge comprising an oxidizer and a dissociated reducing agent - Google Patents

Pyrotechnical actuator with a charge comprising an oxidizer and a dissociated reducing agent Download PDF

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Publication number
EP1637511A3
EP1637511A3 EP05291744A EP05291744A EP1637511A3 EP 1637511 A3 EP1637511 A3 EP 1637511A3 EP 05291744 A EP05291744 A EP 05291744A EP 05291744 A EP05291744 A EP 05291744A EP 1637511 A3 EP1637511 A3 EP 1637511A3
Authority
EP
European Patent Office
Prior art keywords
dissociated
charge
oxidizer
reducing agent
actuator
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.)
Granted
Application number
EP05291744A
Other languages
German (de)
French (fr)
Other versions
EP1637511B1 (en
EP1637511A2 (en
Inventor
Christian Perut
Pierre Humbert
Michael Mamou
Antoine Roussy
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.)
Pyroalliance SA
Original Assignee
Pyroalliance SA
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Filing date
Publication date
Application filed by Pyroalliance SA filed Critical Pyroalliance SA
Publication of EP1637511A2 publication Critical patent/EP1637511A2/en
Publication of EP1637511A3 publication Critical patent/EP1637511A3/en
Application granted granted Critical
Publication of EP1637511B1 publication Critical patent/EP1637511B1/en
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • C06D5/10Generation of pressure gas, e.g. for blasting cartridges, starting cartridges, rockets by reaction of solids with liquids
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B45/00Compositions or products which are defined by structure or arrangement of component of product
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B15/00Fluid-actuated devices for displacing a member from one position to another; Gearing associated therewith
    • F15B15/19Pyrotechnical actuators

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Combustion & Propulsion (AREA)
  • Analytical Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Actuator (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Air Bags (AREA)
  • Feeding, Discharge, Calcimining, Fusing, And Gas-Generation Devices (AREA)

Abstract

Le domaine technique de l'invention est celui des actionneurs pyrotechniques ayant pour fonction essentielle soit de gonfler une structure, soit de déplacer une pièce par l'intermédiaire d'un vérin.The technical field of the invention is that of pyrotechnic actuators whose essential function is either to inflate a structure, or to move a part by means of a jack.

L'objet de l'invention porte plus spécifiquement sur un actionneur (1,100) à génération de gaz comprenant un système d'allumage (3,103) et une charge énergétique.The object of the invention relates more specifically to a gas generation actuator (1,100) comprising an ignition system (3,103) and an energy load.

La principale caractéristique de l'actionneur (1,100) est que la charge est constituée par un matériau réducteur (4,104) et un fluide oxydant (2,102) dissociés.

Figure imgaf001
The main characteristic of the actuator (1,100) is that the charge is constituted by a dissociated reducing material (4,104) and a oxidizing fluid (2,102).
Figure imgaf001

EP05291744.0A 2004-09-14 2005-08-18 Pyrotechnical actuator with a charge comprising an oxidizer and a dissociated reducing agent Not-in-force EP1637511B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0409721A FR2875293B1 (en) 2004-09-14 2004-09-14 HYBRID ACTUATOR WITH CHARGE COMPRISING A DISSOCATED OXIDANT AND REDUCER

Publications (3)

Publication Number Publication Date
EP1637511A2 EP1637511A2 (en) 2006-03-22
EP1637511A3 true EP1637511A3 (en) 2012-12-05
EP1637511B1 EP1637511B1 (en) 2018-05-16

Family

ID=34952800

Family Applications (1)

Application Number Title Priority Date Filing Date
EP05291744.0A Not-in-force EP1637511B1 (en) 2004-09-14 2005-08-18 Pyrotechnical actuator with a charge comprising an oxidizer and a dissociated reducing agent

Country Status (5)

Country Link
US (1) US20060065337A1 (en)
EP (1) EP1637511B1 (en)
JP (2) JP4213698B2 (en)
ES (1) ES2670926T3 (en)
FR (1) FR2875293B1 (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE531342C2 (en) * 2007-07-06 2009-03-03 Bae Systems Bofors Ab Method and apparatus for mixing and initiating a pyrotechnic kit
SE532521C2 (en) * 2008-06-11 2010-02-16 Bae Systems Bofors Ab Mechanism of action for graded blasting action and method
FR2984307B1 (en) 2011-12-20 2014-01-10 Sme PROCESS FOR GENERATING COMBUSTION GAS FROM SOLID OXYGEN PRECURSOR MATERIAL AND DISSOCATED SOLID REDUCER MATERIAL AND DEVICE THEREOF
CN110749251B (en) * 2019-11-07 2020-09-04 北京理工大学 Charging sequence of combustion-driven high-temperature-resistant fire separation device for deep space probe
US11912221B2 (en) * 2019-12-05 2024-02-27 Autoliv Asp, Inc. Actuator devices and assemblies for automotive safety devices
JP7431441B2 (en) * 2020-03-17 2024-02-15 学校法人 中央大学 Fluid pressure actuator drive system and fluid pressure actuator drive method
CN111174654A (en) * 2020-03-25 2020-05-19 田永和 Safe and environment-friendly gas mixed heat energy expansion device and construction method

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3813007A (en) * 1970-12-11 1974-05-28 Poudres Et Exyslosifs Soc Nat Gas generator with coolant expulsion means
US4527389A (en) * 1982-06-21 1985-07-09 Thiokol Corporation Highly soluble, non-hazardous hydroxylammonium salt solutions for use in hybrid rocket motors
US5509981A (en) * 1994-02-18 1996-04-23 Mcdonnell Douglas Corporation Hybrid rocket fuel
US5533331A (en) * 1994-05-25 1996-07-09 Kaiser Marquardt, Inc. Safe propulsion system for missile divert thrusters and attitude control thrusters and method for use of same
US5847311A (en) * 1996-10-22 1998-12-08 Trw Vehicle Safety Systems Inc. Hybrid inflator with crystalline and amorphous block copolymer
US6068290A (en) * 1997-12-23 2000-05-30 Trw Vehicle Safety System Inc. Inflator structure
US6125763A (en) * 1998-08-14 2000-10-03 Environmental Aeroscience Corp. Integral solid booster and hybrid thrust sustaining system and projectile incorporating the same
US6250072B1 (en) * 1999-07-02 2001-06-26 Quoin, Inc. Multi-ignition controllable solid-propellant gas generator
US6481357B1 (en) * 1998-11-26 2002-11-19 Trw Airbag Systems Gmbh & Co. Kg Gas generator for a safety system
WO2003027045A2 (en) * 2001-09-27 2003-04-03 Vanderbilt University Monopropellant/hypergolic powered proportional actuator

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3726088A (en) * 1971-08-20 1973-04-10 Us Navy On-demand variable flow closed loop gas generator system with a variable area injector
US4619111A (en) * 1984-09-07 1986-10-28 Hydril Company Oilfield closing device operating system
DE3621186A1 (en) * 1986-06-25 1988-01-07 Bbc Brown Boveri & Cie METHOD AND DEVICE FOR DRIVING A LINEAR MOVABLE COMPONENT, IN PARTICULAR THE MOVABLE SWITCHING CONTACT OF AN ELECTRICAL HIGH VOLTAGE CIRCUIT BREAKER
FR2685741A1 (en) 1991-12-31 1993-07-02 Thomson Brandt Armements PYROTECHNIC CYLINDER WITH AMORTIZED RUN.
US5579636A (en) * 1995-03-21 1996-12-03 Aerotech, Inc. Pyrotechnic valve, igniter and combustion preheater for hybrid rocket motors
US6007022A (en) * 1996-11-08 1999-12-28 Newport News Shipbuilding Internal combustion catapult
CA2338213A1 (en) * 1998-07-22 2000-02-03 M. Arif Karabeyoglu High regression rate hybrid rocket propellants
US6684624B2 (en) * 1998-07-22 2004-02-03 The Board Of Trustees Of The Leland Stanford Junior University High regression rate hybrid rocket propellants
FR2824875B1 (en) 2001-05-21 2004-01-02 Pyroalliance PYROTECHNIC ACTUATOR PROVIDED WITH A RETAINING WASHER
JP2003089590A (en) * 2001-09-11 2003-03-28 Hosoya Fireworks Co Ltd Solid fuel and hybrid propellant
US6679049B2 (en) * 2002-01-22 2004-01-20 Hy Pat Corporation Hybrid rocket motor having a precombustion chamber

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3813007A (en) * 1970-12-11 1974-05-28 Poudres Et Exyslosifs Soc Nat Gas generator with coolant expulsion means
US4527389A (en) * 1982-06-21 1985-07-09 Thiokol Corporation Highly soluble, non-hazardous hydroxylammonium salt solutions for use in hybrid rocket motors
US5509981A (en) * 1994-02-18 1996-04-23 Mcdonnell Douglas Corporation Hybrid rocket fuel
US5533331A (en) * 1994-05-25 1996-07-09 Kaiser Marquardt, Inc. Safe propulsion system for missile divert thrusters and attitude control thrusters and method for use of same
US5847311A (en) * 1996-10-22 1998-12-08 Trw Vehicle Safety Systems Inc. Hybrid inflator with crystalline and amorphous block copolymer
US6068290A (en) * 1997-12-23 2000-05-30 Trw Vehicle Safety System Inc. Inflator structure
US6125763A (en) * 1998-08-14 2000-10-03 Environmental Aeroscience Corp. Integral solid booster and hybrid thrust sustaining system and projectile incorporating the same
US6481357B1 (en) * 1998-11-26 2002-11-19 Trw Airbag Systems Gmbh & Co. Kg Gas generator for a safety system
US6250072B1 (en) * 1999-07-02 2001-06-26 Quoin, Inc. Multi-ignition controllable solid-propellant gas generator
WO2003027045A2 (en) * 2001-09-27 2003-04-03 Vanderbilt University Monopropellant/hypergolic powered proportional actuator

Also Published As

Publication number Publication date
FR2875293A1 (en) 2006-03-17
EP1637511B1 (en) 2018-05-16
JP4988670B2 (en) 2012-08-01
US20060065337A1 (en) 2006-03-30
JP2006084030A (en) 2006-03-30
ES2670926T3 (en) 2018-06-04
JP4213698B2 (en) 2009-01-21
FR2875293B1 (en) 2009-01-16
EP1637511A2 (en) 2006-03-22
JP2008281210A (en) 2008-11-20

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