NO993826D0 - Beholder til brennbare materialer og fremgangsmåter for fremstilling og anvendelse herav - Google Patents

Beholder til brennbare materialer og fremgangsmåter for fremstilling og anvendelse herav

Info

Publication number
NO993826D0
NO993826D0 NO993826A NO993826A NO993826D0 NO 993826 D0 NO993826 D0 NO 993826D0 NO 993826 A NO993826 A NO 993826A NO 993826 A NO993826 A NO 993826A NO 993826 D0 NO993826 D0 NO 993826D0
Authority
NO
Norway
Prior art keywords
container
processes
preparation
combustible materials
combustible
Prior art date
Application number
NO993826A
Other languages
English (en)
Other versions
NO993826L (no
Inventor
Donald E Olander
James Campbell
Original Assignee
Universal Propulsion Co Inc
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 Universal Propulsion Co Inc filed Critical Universal Propulsion Co Inc
Publication of NO993826D0 publication Critical patent/NO993826D0/no
Publication of NO993826L publication Critical patent/NO993826L/no

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02Cartridges, i.e. cases with charge and missile
    • F42B5/18Caseless ammunition; Cartridges having combustible cases
    • F42B5/188Manufacturing processes therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32Constructional parts; Details not otherwise provided for
    • F02K9/34Casings; Combustion chambers; Liners thereof
    • F02K9/346Liners, e.g. inhibitors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B39/00Packaging or storage of ammunition or explosive charges; Safety features thereof; Cartridge belts or bags
    • F42B39/20Packages or ammunition having valves for pressure-equalising; Packages or ammunition having plugs for pressure release, e.g. meltable ; Blow-out panels; Venting arrangements
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60RVEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
    • B60R21/00Arrangements or fittings on vehicles for protecting or preventing injuries to occupants or pedestrians in case of accidents or other traffic risks
    • B60R21/02Occupant safety arrangements or fittings, e.g. crash pads
    • B60R21/16Inflatable occupant restraints or confinements designed to inflate upon impact or impending impact, e.g. air bags
    • B60R21/26Inflatable occupant restraints or confinements designed to inflate upon impact or impending impact, e.g. air bags characterised by the inflation fluid source or means to control inflation fluid flow
    • B60R21/264Inflatable occupant restraints or confinements designed to inflate upon impact or impending impact, e.g. air bags characterised by the inflation fluid source or means to control inflation fluid flow using instantaneous generation of gas, e.g. pyrotechnic
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60RVEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
    • B60R21/00Arrangements or fittings on vehicles for protecting or preventing injuries to occupants or pedestrians in case of accidents or other traffic risks
    • B60R21/02Occupant safety arrangements or fittings, e.g. crash pads
    • B60R21/16Inflatable occupant restraints or confinements designed to inflate upon impact or impending impact, e.g. air bags
    • B60R21/26Inflatable occupant restraints or confinements designed to inflate upon impact or impending impact, e.g. air bags characterised by the inflation fluid source or means to control inflation fluid flow
    • B60R21/264Inflatable occupant restraints or confinements designed to inflate upon impact or impending impact, e.g. air bags characterised by the inflation fluid source or means to control inflation fluid flow using instantaneous generation of gas, e.g. pyrotechnic
    • B60R21/2644Inflatable occupant restraints or confinements designed to inflate upon impact or impending impact, e.g. air bags characterised by the inflation fluid source or means to control inflation fluid flow using instantaneous generation of gas, e.g. pyrotechnic using only solid reacting substances, e.g. pellets, powder

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Laminated Bodies (AREA)
  • Air Bags (AREA)
  • Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
  • Moulding By Coating Moulds (AREA)
  • Feeding, Discharge, Calcimining, Fusing, And Gas-Generation Devices (AREA)
NO993826A 1997-02-10 1999-08-09 Beholder til brennbare materialer og fremgangsmaater for fremstilling og anvendelse herav NO993826L (no)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/798,456 US5976293A (en) 1997-02-10 1997-02-10 Method for making a case for combustible materials
PCT/US1998/002504 WO1998036975A2 (en) 1997-02-10 1998-02-09 Case for combustible materials and methods for making and using the same

Publications (2)

Publication Number Publication Date
NO993826D0 true NO993826D0 (no) 1999-08-09
NO993826L NO993826L (no) 1999-10-07

Family

ID=25173450

Family Applications (1)

Application Number Title Priority Date Filing Date
NO993826A NO993826L (no) 1997-02-10 1999-08-09 Beholder til brennbare materialer og fremgangsmaater for fremstilling og anvendelse herav

Country Status (8)

Country Link
US (1) US5976293A (no)
EP (1) EP0960317B1 (no)
JP (1) JP2001521602A (no)
AU (1) AU6322598A (no)
DE (1) DE69814593D1 (no)
IL (1) IL131323A (no)
NO (1) NO993826L (no)
WO (1) WO1998036975A2 (no)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6523477B1 (en) * 1999-03-30 2003-02-25 Lockheed Martin Corporation Enhanced performance insensitive penetrator warhead
US6386110B1 (en) * 2000-12-11 2002-05-14 The United States Of America As Represented By The Secretary Of The Navy Deforming charge assembly and method of making same
CA2831630C (en) * 2004-02-06 2018-08-21 Jeffrey P. Reistroffer Ignition method for controlled burning
ITTO20040620A1 (it) * 2004-09-14 2004-12-14 Avio Spa Involucro di un motore a propellente solido e motore a propellente solido provvisto di tale involucro
IL186966A (en) * 2007-10-28 2013-08-29 Israel Military Ind Shell for insensitive ammunition and manufacturing process
DE202009005902U1 (de) * 2009-04-21 2009-07-02 Heumüller, Jürgen Anzündhilfe
KR101419787B1 (ko) * 2009-08-04 2014-07-15 니트로케미에 아샤우 게엠베하 추진제 파우더를 수용하는 슬리브
KR101097787B1 (ko) * 2009-08-20 2011-12-23 국방과학연구소 추진제용 압력용기, 그 폭발 방지 방법 및 제조 방법
DE102011113539B4 (de) * 2011-09-15 2015-10-01 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Thermalisolation für Raketentriebwerke
KR101428575B1 (ko) 2013-08-23 2014-08-11 국방과학연구소 일체 성형식 분리형 돔을 가진 복합재 연소관 및 그 제조방법
DE102014016023B3 (de) * 2014-10-29 2016-03-24 Daimler Ag Druckgasbehälter
DE102015112636A1 (de) * 2015-07-31 2017-02-02 Deutsches Zentrum für Luft- und Raumfahrt e.V. Mantel einer Festbrennstoffrakete, Verfahren zu dessen Herstellung, Festbrennstoffrakete und Vorrichtung
CN108226213A (zh) * 2018-01-12 2018-06-29 北京理工大学 基于机电系统和危险品的快烤烤燃温度测试平台及其方法
JP6987691B2 (ja) * 2018-04-19 2022-01-05 株式会社Ihiエアロスペース 分割型モータケースの製造方法

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2995011A (en) * 1959-09-17 1961-08-08 Phillips Petroleum Co Solid propellant rocket motor
US3316842A (en) * 1963-03-19 1967-05-02 Union Carbide Corp Propulsion product
US3745927A (en) * 1969-05-19 1973-07-17 Celanese Corp Casing and propellant of nitrocellulose filaments and nitrocellulose fibers
US3872205A (en) * 1971-06-02 1975-03-18 United Kingdom Government Molding process for bonding insula in rachet motor casing
US3943208A (en) * 1971-06-02 1976-03-09 Her Majesty The Queen In Right Of Canada As Represented By The Minister Of National Defense Method for binding solid propellant to rocket motor case
US3879243A (en) * 1973-01-05 1975-04-22 Jonas Medney Porous filament wound pipe and method for making same
US4470860A (en) * 1982-01-07 1984-09-11 Hercules Incorporated Fabricating large, thick wall, tubular structures
US4822832A (en) * 1985-02-19 1989-04-18 Hercules Incorporated Thermosetting epoxy resin compositions and thermosets therefrom
US4892764A (en) * 1985-11-26 1990-01-09 Loctite Corporation Fiber/resin composites, and method of making the same
AU621576B2 (en) * 1987-12-29 1992-03-19 Alliant Techsystems Inc. Filament winding of case onto solid propellant
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
US5060470A (en) * 1990-05-22 1991-10-29 Thiokol Corporation Gas generator ventable at a high temperature for hazard reduction
US5369955A (en) * 1990-07-25 1994-12-06 Thiokol Corporation Gas generator and method for making same for hazard reducing venting in case of fire
USH1144H (en) * 1990-10-04 1993-03-02 Hercules Incorporated Solid propellant rocket motor with fusible end closure holder
US5311820A (en) * 1991-01-17 1994-05-17 Thiokol Corporation Method and apparatus for providing an insensitive munition
US5170007A (en) * 1991-10-15 1992-12-08 Atlantic Research Corporation Tailorable roll-bonded insensitive munitions case
US5228285A (en) * 1992-03-02 1993-07-20 Thiokol Corporation Solid propellant rocket motor case for insensitive munitions requirements
US5341638A (en) * 1992-03-09 1994-08-30 Thiokol Corporation Low cost segmented structure for pressure vessels, rocket motors, piping
US5388399A (en) * 1992-03-11 1995-02-14 Atlantic Research Corporation Rocket motor having unitary case, insulation and propellant
US5398498A (en) * 1994-05-06 1995-03-21 Bei Electronics, Inc. Joint construction between components of military projectile and releasable by melting of fusible eutectic helical member
US5763027A (en) * 1994-06-30 1998-06-09 Thiokol Corporation Insensitive munitions composite pressure vessels

Also Published As

Publication number Publication date
WO1998036975A2 (en) 1998-08-27
AU6322598A (en) 1998-09-09
IL131323A (en) 2002-07-25
EP0960317B1 (en) 2003-05-14
IL131323A0 (en) 2001-01-28
EP0960317A2 (en) 1999-12-01
NO993826L (no) 1999-10-07
WO1998036975A3 (en) 1998-12-10
US5976293A (en) 1999-11-02
JP2001521602A (ja) 2001-11-06
DE69814593D1 (de) 2003-06-18
EP0960317A4 (en) 2000-03-29

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Legal Events

Date Code Title Description
FC2A Withdrawal, rejection or dismissal of laid open patent application