NO20030006L - Fremgangsmåte og anordning for å forhindre at innkapslede eksplosiver påvirkes til å eksplodere ved en ekstern brann - Google Patents

Fremgangsmåte og anordning for å forhindre at innkapslede eksplosiver påvirkes til å eksplodere ved en ekstern brann

Info

Publication number
NO20030006L
NO20030006L NO20030006A NO20030006A NO20030006L NO 20030006 L NO20030006 L NO 20030006L NO 20030006 A NO20030006 A NO 20030006A NO 20030006 A NO20030006 A NO 20030006A NO 20030006 L NO20030006 L NO 20030006L
Authority
NO
Norway
Prior art keywords
external fire
explosion
explosives
mounting components
explosive
Prior art date
Application number
NO20030006A
Other languages
English (en)
Other versions
NO20030006D0 (no
NO327421B1 (no
Inventor
Alf Prytz
Original Assignee
Saab Ab
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 Saab Ab filed Critical Saab Ab
Publication of NO20030006D0 publication Critical patent/NO20030006D0/no
Publication of NO20030006L publication Critical patent/NO20030006L/no
Publication of NO327421B1 publication Critical patent/NO327421B1/no

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B39/00—Packaging or storage of ammunition or explosive charges; Safety features thereof; Cartridge belts or bags
    • F42B39/20—Packages or ammunition having valves for pressure-equalising; Packages or ammunition having plugs for pressure release, e.g. meltable ; Blow-out panels; Venting arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/34—Casings; Combustion chambers; Liners thereof
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/26—Burning control
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/36—Propellant charge supports
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/38—Safety devices, e.g. to prevent accidental ignition

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Fire-Detection Mechanisms (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Drilling And Exploitation, And Mining Machines And Methods (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Air Bags (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Disintegrating Or Milling (AREA)
  • Diaphragms For Electromechanical Transducers (AREA)
  • Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
NO20030006A 2000-07-03 2003-01-02 Fremgangsmate og anordning for a forhindre at innkapslede eksplosiver pavirkes til a eksplodere ved en ekstern brann NO327421B1 (no)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SE0002504A SE519561C2 (sv) 2000-07-03 2000-07-03 Anordning vid raketmotorer för att förhindra att raketmotor bringas att explodera vid utvändig brand
PCT/SE2001/001370 WO2002003019A1 (en) 2000-07-03 2001-06-19 Method and arrangement for preventing encased explosives being caused to explode by an external fire

Publications (3)

Publication Number Publication Date
NO20030006D0 NO20030006D0 (no) 2003-01-02
NO20030006L true NO20030006L (no) 2003-02-28
NO327421B1 NO327421B1 (no) 2009-06-29

Family

ID=20280352

Family Applications (1)

Application Number Title Priority Date Filing Date
NO20030006A NO327421B1 (no) 2000-07-03 2003-01-02 Fremgangsmate og anordning for a forhindre at innkapslede eksplosiver pavirkes til a eksplodere ved en ekstern brann

Country Status (9)

Country Link
US (1) US7051511B2 (no)
EP (1) EP1297303B1 (no)
AT (1) ATE314622T1 (no)
AU (1) AU2001274759A1 (no)
DE (1) DE60116309T2 (no)
IL (2) IL153630A0 (no)
NO (1) NO327421B1 (no)
SE (1) SE519561C2 (no)
WO (1) WO2002003019A1 (no)

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US8082846B2 (en) * 2002-08-12 2011-12-27 Qinetiq Limited Temperature responsive safety devices for munitions
GB2391899A (en) * 2002-08-12 2004-02-18 Qinetiq Ltd Shape memory alloy connector and an overwound munition casing
SE0300834L (sv) * 2003-03-26 2004-07-20 Saab Ab Verkansdel
US7469538B2 (en) 2005-10-28 2008-12-30 Searete Llc Self assembling/quick assembly structure using shape memory alloy materials
US7373885B2 (en) * 2005-10-28 2008-05-20 Lockheed Martin Corporation Device for venting a container housing an energetic material and method of using same
US8720722B2 (en) * 2005-12-15 2014-05-13 Cornerstone Research Group, Inc. Venting mechanism for containers
ES2322773T3 (es) * 2006-01-13 2009-06-26 Saab Ab Cierre de municiones insensibles para armas con proyectiles precargados.
DE602006021528D1 (de) * 2006-01-17 2011-06-09 Saab Ab Eine Vorrichtung zum Anlassen des inneren Druckes für Panzerabwehrwaffe
US8356727B2 (en) * 2007-03-07 2013-01-22 Cornerstone Research Group, Inc. Venting mechanisms for containers
US7762195B2 (en) * 2007-05-14 2010-07-27 Aerojet - General Corporation Slow cook off rocket igniter
GB0714440D0 (en) 2007-07-25 2007-10-17 Qinetiq Ltd Rupturing device
FR2931874B1 (fr) * 2008-05-29 2010-06-25 Snecma Dispositif de blocage axial d'un palier de guidage d'arbre dans une turbomachine.
US7743752B2 (en) * 2008-07-18 2010-06-29 Ford Global Technologies, Llc System and method for improving fuel vapor purging for an engine having a compressor
ES2624906T3 (es) * 2008-10-10 2017-07-18 Saab Ab Vaina de cartucho y cartucho que comprende tal vaina de cartucho
WO2010041987A1 (en) * 2008-10-10 2010-04-15 Saab Ab A cartridge case and a round comprising such a cartridge case
FR2948186B1 (fr) * 2009-07-17 2015-02-20 Tda Armements Sas Munition comprenant des moyens pour neutraliser son chargement explosif
US8578855B2 (en) 2009-08-21 2013-11-12 General Dynamics Armament And Technical Products, Inc. Rocket motor tube with safety features
US8925463B1 (en) * 2009-09-03 2015-01-06 Kms Consulting, Llc Pressure relief system for gun fired cannon cartridges
US8230682B1 (en) 2009-09-24 2012-07-31 The United States Of America As Represented By The Secretary Of The Navy Thermally activated initiator assembly
US9482185B1 (en) * 2014-02-20 2016-11-01 The United States of America as Reprented by the Secretary of the Navy Thermal rocket initiator mechanism and rocket system incorporating same
DK3129743T3 (en) * 2014-04-11 2019-01-21 Saab Ab ARRANGEMENT BLOCKING ARRANGEMENT
DE102014013316B4 (de) 2014-09-08 2016-04-07 Diehl Bgt Defence Gmbh & Co. Kg Behältnis zur Aufbewahrung eines Explosivstoffs
US10113846B2 (en) 2016-07-07 2018-10-30 General Dynamics Ordnance and Tactical Systems-Canada, Inc. Systems and methods for reducing munition sensitivity
US10801822B2 (en) * 2018-06-29 2020-10-13 Goodrich Corporation Variable stand-off assembly
IL260886B (en) * 2018-07-30 2021-04-29 Rafael Advanced Defense Systems Ltd Rocket armament that can be launched from a tubular launcher with non-ignition security outside the launcher and engine separation in flight
CN110985237A (zh) * 2019-11-13 2020-04-10 上海新力动力设备研究所 基于记忆合金技术高温下失效的连接固定装置及应用方法

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FR540418A (fr) 1919-01-13 1922-07-11 Dispositif de contrôle pour moteurs à combustion interne
US3776466A (en) * 1973-01-19 1973-12-04 W Ray Polyurethane foam insert for overexpanded rocket engine nozzles to prevent start transient sideloads
US4022129A (en) * 1976-01-16 1977-05-10 The United States Of America As Represented By The Secretary Of The Air Force Nozzle ejection system
US4084512A (en) 1976-10-18 1978-04-18 The United States Of America As Represented By The Secretary Of The Navy Pressure relief construction for controlled combustion of ordnance items
US4272956A (en) * 1979-01-22 1981-06-16 Thiokol Corporation Time delay device for deployable rocket nozzle skirts
FR2503794B1 (fr) * 1981-04-13 1986-04-25 Europ Propulsion Chambre de combustion de propulseur-fusee a divergent multiple
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FR2699663B1 (fr) * 1992-12-18 1995-02-24 Giat Ind Sa Dispositif d'initiation pour un système pyrotechnique.
US5394803A (en) * 1994-02-14 1995-03-07 Bel Electronics, Inc. Joint construction between military rocket motor and warhead and releasable by melting of fusible eutectic wedging ring for operating flexible locking fingers
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FR2742221B1 (fr) 1995-12-12 1998-02-27 Soc D Ateliers Mecaniques De P Dispositif de deconfinement pour munition
US5779151A (en) * 1996-05-28 1998-07-14 Regents Of The University Of California Stepped nozzle
FR2754566B1 (fr) * 1996-10-11 1999-02-05 Europ Propulsion Tuyere de moteur-fusee a inserts ejectables
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JP3940893B2 (ja) * 2001-12-14 2007-07-04 石川島播磨重工業株式会社 ロケットとペイロードとのクランプバンド
US6752085B2 (en) * 2002-05-06 2004-06-22 Lockheed Martin Corporation Method and apparatus for releasably attaching a closure plate to a casing

Also Published As

Publication number Publication date
US7051511B2 (en) 2006-05-30
SE519561C2 (sv) 2003-03-11
NO20030006D0 (no) 2003-01-02
DE60116309T2 (de) 2006-08-24
EP1297303B1 (en) 2005-12-28
SE0002504D0 (sv) 2000-07-03
DE60116309D1 (de) 2006-02-02
US20040244358A1 (en) 2004-12-09
WO2002003019A1 (en) 2002-01-10
NO327421B1 (no) 2009-06-29
IL153630A (en) 2006-10-31
EP1297303A1 (en) 2003-04-02
AU2001274759A1 (en) 2002-01-14
ATE314622T1 (de) 2006-01-15
SE0002504L (sv) 2002-01-04
IL153630A0 (en) 2003-07-06

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Legal Events

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