EP1170568A3 - Deflagration minimization device on a metallic container in case of accidental internal overpressure - Google Patents
Deflagration minimization device on a metallic container in case of accidental internal overpressure Download PDFInfo
- Publication number
- EP1170568A3 EP1170568A3 EP01401693A EP01401693A EP1170568A3 EP 1170568 A3 EP1170568 A3 EP 1170568A3 EP 01401693 A EP01401693 A EP 01401693A EP 01401693 A EP01401693 A EP 01401693A EP 1170568 A3 EP1170568 A3 EP 1170568A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- enclosure
- deflagration
- case
- metallic container
- internal overpressure
- 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.)
- Withdrawn
Links
- 238000004200 deflagration Methods 0.000 title 1
- 239000003380 propellant Substances 0.000 abstract 2
- 230000009172 bursting Effects 0.000 abstract 1
- 239000012634 fragment Substances 0.000 abstract 1
- 238000013467 fragmentation Methods 0.000 abstract 1
- 238000006062 fragmentation reaction Methods 0.000 abstract 1
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
- 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
- F42B39/14—Explosion or fire protection arrangements on packages or ammunition
Abstract
Pour éviter l'éclatement violent de l'enceinte (2) d'un propulseur contenant du propergol (4) lors d'un incendie accidentel de son environnement, on fixe sur cette enceinte, une composition pyrotechnique (5, 6) qui échauffe localement l'enceinte lors de cet incendie, et fragilise donc cette enceinte, qui s'ouvre à cet endroit avant que la pression intérieure soit trop importante, ce qui évite la fragmentation de l'enceinte et la projection violente de tels fragments. To avoid the violent bursting of the enclosure (2) of a propellant containing propellant (4) during an accidental fire in its environment, a pyrotechnic composition (5, 6) is fixed on this enclosure which heats up locally the enclosure during this fire, and therefore weakens this enclosure, which opens at this location before the internal pressure is too great, which avoids the fragmentation of the enclosure and the violent projection of such fragments.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0008516A FR2811053B1 (en) | 2000-06-30 | 2000-06-30 | DEVICE FOR MINIMIZING THE EXPLOSION EFFECTS OF A METAL ENCLOSURE IN THE EVENT OF ACCIDENTAL INTERNAL OVERPRESSURE |
FR0008516 | 2000-06-30 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1170568A2 EP1170568A2 (en) | 2002-01-09 |
EP1170568A3 true EP1170568A3 (en) | 2002-04-03 |
Family
ID=8851961
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP01401693A Withdrawn EP1170568A3 (en) | 2000-06-30 | 2001-06-26 | Deflagration minimization device on a metallic container in case of accidental internal overpressure |
Country Status (4)
Country | Link |
---|---|
US (1) | US20020020323A1 (en) |
EP (1) | EP1170568A3 (en) |
FR (1) | FR2811053B1 (en) |
NO (1) | NO20013225L (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6952995B2 (en) * | 2002-01-11 | 2005-10-11 | Aerojet-General Corporation | Apparatus and method for passive venting of rocket motor or ordnance case |
US7530314B2 (en) * | 2004-05-25 | 2009-05-12 | Lockheed Martin Corporation | Thermally initiated venting system and method of using same |
DE102004038039A1 (en) * | 2004-08-05 | 2006-02-23 | Diehl Bgt Defence Gmbh & Co. Kg | rocket engine |
US7472653B1 (en) * | 2006-06-15 | 2009-01-06 | United States Of America As Represented By The Secretary Of The Navy | Insensitive munitions warhead explosive venting system |
FR2908506B1 (en) | 2006-11-14 | 2008-12-19 | Protac | PROTECTIVE SYSTEM FOR DEVICE CONTAINING MATERIAL WHICH RESULTS AGAINST WARMING |
EP2113733A1 (en) | 2008-04-30 | 2009-11-04 | Saab Ab | Weapon with IM-characteristics |
US9255774B2 (en) | 2008-06-30 | 2016-02-09 | Battelle Memorial Institute | Controlled fragmentation of a warhead shell |
FR2948186B1 (en) * | 2009-07-17 | 2015-02-20 | Tda Armements Sas | AMMUNITION COMPRISING MEANS FOR NEUTRALIZING ITS EXPLOSIVE LOADING |
US10670381B1 (en) * | 2013-09-17 | 2020-06-02 | The United States Of America, As Represented By The Secretary Of The Navy | Electronic thermally-initiated venting system (ETIVS) for rocket motors |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4478151A (en) * | 1983-02-28 | 1984-10-23 | The United States Of America As Represented By The Secretary Of The Navy | Pressure vessel penetrator |
US4597261A (en) * | 1984-05-25 | 1986-07-01 | Hughes Aircraft Company | Thermally actuated rocket motor safety system |
US5129326A (en) * | 1987-04-14 | 1992-07-14 | Aerojet-General Corporation | Ordnance device with explosion protection |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5206456A (en) * | 1989-08-24 | 1993-04-27 | The United States Of America As Represented By The Secretary Of The Navy | Ordinance thermal battery |
-
2000
- 2000-06-30 FR FR0008516A patent/FR2811053B1/en not_active Expired - Fee Related
-
2001
- 2001-06-26 EP EP01401693A patent/EP1170568A3/en not_active Withdrawn
- 2001-06-27 NO NO20013225A patent/NO20013225L/en not_active Application Discontinuation
- 2001-06-29 US US09/893,448 patent/US20020020323A1/en not_active Abandoned
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4478151A (en) * | 1983-02-28 | 1984-10-23 | The United States Of America As Represented By The Secretary Of The Navy | Pressure vessel penetrator |
US4597261A (en) * | 1984-05-25 | 1986-07-01 | Hughes Aircraft Company | Thermally actuated rocket motor safety system |
US5129326A (en) * | 1987-04-14 | 1992-07-14 | Aerojet-General Corporation | Ordnance device with explosion protection |
Also Published As
Publication number | Publication date |
---|---|
EP1170568A2 (en) | 2002-01-09 |
NO20013225L (en) | 2001-12-31 |
US20020020323A1 (en) | 2002-02-21 |
FR2811053B1 (en) | 2003-06-13 |
NO20013225D0 (en) | 2001-06-27 |
FR2811053A1 (en) | 2002-01-04 |
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Legal Events
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17Q | First examination report despatched |
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STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN |
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18D | Application deemed to be withdrawn |
Effective date: 20040327 |