SG11201600999XA - Method of manufacturing multi-layered propellant grains - Google Patents

Method of manufacturing multi-layered propellant grains

Info

Publication number
SG11201600999XA
SG11201600999XA SG11201600999XA SG11201600999XA SG11201600999XA SG 11201600999X A SG11201600999X A SG 11201600999XA SG 11201600999X A SG11201600999X A SG 11201600999XA SG 11201600999X A SG11201600999X A SG 11201600999XA SG 11201600999X A SG11201600999X A SG 11201600999XA
Authority
SG
Singapore
Prior art keywords
manufacturing multi
propellant grains
layered propellant
layered
grains
Prior art date
Application number
SG11201600999XA
Inventor
Simon Durand
Pierre-Yves Paradis
Daniel Lepage
Original Assignee
Gen Dynamics Ordnance & Tactic
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 Gen Dynamics Ordnance & Tactic filed Critical Gen Dynamics Ordnance & Tactic
Publication of SG11201600999XA publication Critical patent/SG11201600999XA/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/03—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor characterised by the shape of the extruded material at extrusion
    • B29C48/09—Articles with cross-sections having partially or fully enclosed cavities, e.g. pipes or channels
    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B21/00—Apparatus or methods for working-up explosives, e.g. forming, cutting, drying
    • C06B21/0033—Shaping the mixture
    • C06B21/0075—Shaping the mixture by extrusion
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/16—Articles comprising two or more components, e.g. co-extruded layers
    • B29C48/18—Articles comprising two or more components, e.g. co-extruded layers the components being layers
    • B29C48/21—Articles comprising two or more components, e.g. co-extruded layers the components being layers the layers being joined at their surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25—Component parts, details or accessories; Auxiliary operations
    • B29C48/36—Means for plasticising or homogenising the moulding material or forcing it through the nozzle or die
    • B29C48/395—Means for plasticising or homogenising the moulding material or forcing it through the nozzle or die using screws surrounded by a cooperating barrel, e.g. single screw extruders
    • B29C48/40—Means for plasticising or homogenising the moulding material or forcing it through the nozzle or die using screws surrounded by a cooperating barrel, e.g. single screw extruders using two or more parallel screws or at least two parallel non-intermeshing screws, e.g. twin screw extruders
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25—Component parts, details or accessories; Auxiliary operations
    • B29C48/36—Means for plasticising or homogenising the moulding material or forcing it through the nozzle or die
    • B29C48/475—Means for plasticising or homogenising the moulding material or forcing it through the nozzle or die using pistons, accumulators or press rams
    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B25/00—Compositions containing a nitrated organic compound
    • C06B25/18—Compositions containing a nitrated organic compound the compound being nitrocellulose present as 10% or more by weight of the total composition
    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B45/00—Compositions or products which are defined by structure or arrangement of component of product
    • C06B45/04—Compositions or products which are defined by structure or arrangement of component of product comprising solid particles dispersed in solid solution or matrix not used for explosives where the matrix consists essentially of nitrated carbohydrates or a low molecular organic explosive
    • C06B45/06—Compositions or products which are defined by structure or arrangement of component of product comprising solid particles dispersed in solid solution or matrix not used for explosives where the matrix consists essentially of nitrated carbohydrates or a low molecular organic explosive the solid solution or matrix containing an organic component
    • C06B45/10—Compositions or products which are defined by structure or arrangement of component of product comprising solid particles dispersed in solid solution or matrix not used for explosives where the matrix consists essentially of nitrated carbohydrates or a low molecular organic explosive the solid solution or matrix containing an organic component the organic component containing a resin
    • C06B45/105—The resin being a polymer bearing energetic groups or containing a soluble organic explosive
    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B45/00—Compositions or products which are defined by structure or arrangement of component of product
    • C06B45/12—Compositions or products which are defined by structure or arrangement of component of product having contiguous layers or zones
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B33/00—Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02—Cartridges, i.e. cases with charge and missile
    • F42B5/16—Cartridges, i.e. cases with charge and missile characterised by composition or physical dimensions or form of propellant charge, with or without projectile, or powder
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/03—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor characterised by the shape of the extruded material at extrusion
    • B29C48/09—Articles with cross-sections having partially or fully enclosed cavities, e.g. pipes or channels
    • B29C48/11—Articles with cross-sections having partially or fully enclosed cavities, e.g. pipes or channels comprising two or more partially or fully enclosed cavities, e.g. honeycomb-shaped

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Organic Chemistry (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Health & Medical Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Dispersion Chemistry (AREA)
  • Molecular Biology (AREA)
  • Extrusion Moulding Of Plastics Or The Like (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)
SG11201600999XA 2013-08-16 2014-08-08 Method of manufacturing multi-layered propellant grains SG11201600999XA (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201361866748P 2013-08-16 2013-08-16
US14/166,622 US10843979B2 (en) 2013-08-16 2014-01-28 Method of manufacturing multi-layered propellant grains
PCT/CA2014/050755 WO2015021545A1 (en) 2013-08-16 2014-08-08 Method of manufacturing multi-layered propellant grains

Publications (1)

Publication Number Publication Date
SG11201600999XA true SG11201600999XA (en) 2016-03-30

Family

ID=52467881

Family Applications (1)

Application Number Title Priority Date Filing Date
SG11201600999XA SG11201600999XA (en) 2013-08-16 2014-08-08 Method of manufacturing multi-layered propellant grains

Country Status (11)

Country Link
US (1) US10843979B2 (en)
EP (1) EP3033585B1 (en)
JP (1) JP6524083B2 (en)
KR (1) KR102219278B1 (en)
AU (1) AU2014306330B2 (en)
BR (1) BR112016003232B1 (en)
CA (1) CA2920690C (en)
ES (1) ES2792274T3 (en)
IL (1) IL244125B (en)
SG (1) SG11201600999XA (en)
WO (1) WO2015021545A1 (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10843979B2 (en) 2013-08-16 2020-11-24 General Dynamics Ordnance and Tactical Systems—Canada Valleyfield Inc. Method of manufacturing multi-layered propellant grains
US10731604B2 (en) * 2015-08-13 2020-08-04 Aerojet Rocketdyne, Inc. Rocket motor with concentric propellant structures for shock mitigation
EP3222961A1 (en) * 2016-03-22 2017-09-27 Nederlandse Organisatie voor toegepast- natuurwetenschappelijk onderzoek TNO Propellant charge or grain
US10252954B1 (en) 2016-05-17 2019-04-09 The United States Of America As Represented By The Secretary Of The Army Multi-layered stable propellant composition
CN107162864B (en) * 2017-04-25 2018-10-16 西北工业大学 A kind of hybrid motor fuel powder column and ignition charge one process of preparing
EP3444234A1 (en) * 2017-08-18 2019-02-20 Nederlandse Organisatie voor toegepast- natuurwetenschappelijk onderzoek TNO Co-layered propellant charge
EP3705465A1 (en) 2019-03-08 2020-09-09 Nederlandse Organisatie voor toegepast- natuurwetenschappelijk Onderzoek TNO Improved printing of energetic materials
JP2022003249A (en) * 2020-06-23 2022-01-11 三菱重工業株式会社 Method and apparatus for manufacturing propellant
US20230107457A1 (en) * 2021-09-27 2023-04-06 General Dynamics Ordnance and Tactical System - Canada of Valleyfield Inc. Combustible containers manufactured using reactive injection molding of azido polymers

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3194851A (en) 1955-06-20 1965-07-13 Charles W Sauer Process for forming propellant grains having a composite structure
US3002459A (en) 1955-11-09 1961-10-03 Ici Ltd Propellant charges
US3951706A (en) * 1962-07-03 1976-04-20 Eldridge Judson B Solid propellant mixtures and process of preparation
US3867214A (en) 1967-09-18 1975-02-18 Us Army Nitrocellulose doublebase propellant containing ternary mixture of nitrate esters
US3599573A (en) * 1968-05-31 1971-08-17 Whittaker Corp Composite preformed penetrators
US3706278A (en) 1971-02-25 1972-12-19 Us Army Distributed propulsion for guns
US4369688A (en) * 1977-10-17 1983-01-25 E. I. Du Pont De Nemours And Company Method and apparatus for producing a detonating cord
US5129304A (en) * 1988-08-29 1992-07-14 Apv Chemical Machinery Inc. Method and apparatus for processing potentially explosive and sensitive materials for forming longitudinally perforated extrudate strands
GB2384207B (en) * 1989-04-18 2003-10-29 Royal Ordnance Plc Production of energetic materials
ZA926028B (en) 1991-08-15 1993-03-10 Ireco Inc Co-extruded shock tube.
US5316600A (en) 1992-09-18 1994-05-31 The United States Of America As Represented By The Secretary Of The Navy Energetic binder explosive
US5690868A (en) 1993-01-19 1997-11-25 The United States Of America As Represented By The Secretary Of The Army Multi-layer high energy propellants
US6562276B1 (en) * 1998-08-20 2003-05-13 Eastman Chemical Company Process for forming a multilayer, coinjected article
JP2000185317A (en) 1998-12-22 2000-07-04 Ube Ind Ltd Twin screw-type waste extrusion molding machine and method for molding two-layer structure molding of waste using this machine
DK1031547T3 (en) * 1999-02-23 2005-10-10 Gen Dynamics Ordnance & Tactic Perforated propellant and process for making this
US7063810B1 (en) * 2002-11-27 2006-06-20 The United States Of America As Represented By The Secretary Of The Navy Co-extrusion of energetic materials using multiple twin screw extruders
US20050092166A1 (en) * 2003-10-31 2005-05-05 Alliant Techsystems Inc. Propellant extrusion die
US7869989B1 (en) 2005-01-28 2011-01-11 Artificial Cognition Inc. Methods and apparatus for understanding machine vocabulary
JP4642520B2 (en) * 2005-03-28 2011-03-02 住化カラー株式会社 DIE DEVICE AND METHOD FOR PRODUCING MULTILAYER EXTRUSION PRODUCT USING THE SAME
US20120305083A1 (en) * 2011-06-04 2012-12-06 Wlp Holding Corporation Co-extruded oxidation-resistant polyethylene pipe and method of manufacture
US10843979B2 (en) 2013-08-16 2020-11-24 General Dynamics Ordnance and Tactical Systems—Canada Valleyfield Inc. Method of manufacturing multi-layered propellant grains

Also Published As

Publication number Publication date
US10843979B2 (en) 2020-11-24
EP3033585A4 (en) 2017-04-19
CA2920690C (en) 2021-12-07
KR102219278B1 (en) 2021-02-24
AU2014306330A1 (en) 2016-02-11
EP3033585A1 (en) 2016-06-22
IL244125A0 (en) 2016-04-21
BR112016003232A2 (en) 2020-07-07
IL244125B (en) 2020-10-29
AU2014306330B2 (en) 2017-09-28
JP6524083B2 (en) 2019-06-05
JP2016534313A (en) 2016-11-04
KR20160051787A (en) 2016-05-11
WO2015021545A1 (en) 2015-02-19
CA2920690A1 (en) 2015-02-19
BR112016003232B1 (en) 2021-02-17
EP3033585B1 (en) 2020-04-15
US20150284301A1 (en) 2015-10-08
ES2792274T3 (en) 2020-11-10

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