MA32051B1 - Opercule arriere deformable pour conteneur de missile, comportant un cadre de support aval - Google Patents
Opercule arriere deformable pour conteneur de missile, comportant un cadre de support avalInfo
- Publication number
- MA32051B1 MA32051B1 MA33001A MA33001A MA32051B1 MA 32051 B1 MA32051 B1 MA 32051B1 MA 33001 A MA33001 A MA 33001A MA 33001 A MA33001 A MA 33001A MA 32051 B1 MA32051 B1 MA 32051B1
- Authority
- MA
- Morocco
- Prior art keywords
- support frame
- downstream
- downstream support
- rear door
- missile container
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
- F41F3/042—Rocket or torpedo launchers for rockets the launching apparatus being used also as a transport container for the rocket
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
- F41F3/0413—Means for exhaust gas disposal, e.g. exhaust deflectors, gas evacuation systems
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Carbon And Carbon Compounds (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Support Of The Bearing (AREA)
- Radar Systems Or Details Thereof (AREA)
- Closures For Containers (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
La présente invention concerne un opercule aval déformable amélioré (56; 156; 256), destiné à équiper le fond d'un conteneur (15) à missile (16) et comportant un empilement de lames élastiques (63), enserré entre au moins une membrane de protection thermique et une membrane d'étanchéité, amont et aval (70, 71, 72, 73), et maintenu entre un cadre de support amont (61 ) et un cadre de support aval (64), caractérisé en ce que le cadre de support aval comporte un bord intérieur (80) prolongé de manière à munir l'opercule de moyens de butée définissant une position de déformation maximale des lames élastiques.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0850162A FR2926360B1 (fr) | 2008-01-11 | 2008-01-11 | Opercule arriere deformable pour conteneur de missile, comportant un cadre de support aval |
PCT/FR2009/050020 WO2009092938A2 (fr) | 2008-01-11 | 2009-01-08 | Opercule arrière déformable pour conteneur de missile, comportant un cadre de support aval |
Publications (1)
Publication Number | Publication Date |
---|---|
MA32051B1 true MA32051B1 (fr) | 2011-02-01 |
Family
ID=39745427
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MA33001A MA32051B1 (fr) | 2008-01-11 | 2010-07-08 | Opercule arriere deformable pour conteneur de missile, comportant un cadre de support aval |
Country Status (11)
Country | Link |
---|---|
US (1) | US8418593B2 (fr) |
EP (1) | EP2229573B1 (fr) |
KR (1) | KR101567998B1 (fr) |
CN (1) | CN101918786B (fr) |
ES (1) | ES2617208T3 (fr) |
FR (1) | FR2926360B1 (fr) |
MA (1) | MA32051B1 (fr) |
PL (1) | PL2229573T3 (fr) |
UA (1) | UA98686C2 (fr) |
WO (1) | WO2009092938A2 (fr) |
ZA (1) | ZA201004820B (fr) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8300757B2 (en) * | 2008-08-08 | 2012-10-30 | Motorola Mobility Llc | Methods for detection of failure and recovery in a radio link |
US8584569B1 (en) * | 2011-12-06 | 2013-11-19 | The United States Of America As Represented By The Secretary Of The Navy | Plume exhaust management for VLS |
FR3039889B1 (fr) | 2015-08-05 | 2017-07-28 | Mbda France | Opercule flexible pour conteneur de missile |
BE1023108B1 (nl) | 2015-08-24 | 2016-11-23 | Handi-Move N.V. | Verbeterde klem en hulpmiddelen voor het optillen van patiënten met behulp van de klem |
FR3053455B1 (fr) * | 2016-07-01 | 2019-04-19 | Mbda France | Opercule flexible pour conteneur de missile |
CN112985174B (zh) * | 2021-02-10 | 2023-01-10 | 上海材料研究所 | 一种对激波反射具有整流效果的柱面正交型密封后端盖 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4324167A (en) * | 1980-04-14 | 1982-04-13 | General Dynamics, Pomona Division | Flexible area launch tube rear cover |
US4498368A (en) * | 1983-10-06 | 1985-02-12 | The United States Of America As Representedby The Secretary Of The Navy | Frangible fly through diaphragm for missile launch canister |
US4686884A (en) * | 1985-12-27 | 1987-08-18 | General Dynamics, Pomona Division | Gas management deflector |
US4683798A (en) * | 1985-12-27 | 1987-08-04 | General Dynamics, Pomona Division | Gas management transition device |
FR2620808B1 (fr) | 1987-09-17 | 1990-01-12 | France Etat Armement | Opercule arriere pour conteneur de missile |
US5194688A (en) * | 1992-01-31 | 1993-03-16 | Hughes Missile Systems Company | Apparatus for limiting recirculation of rocket exhaust gases during missile launch |
JP2001124494A (ja) * | 1999-10-25 | 2001-05-11 | Mitsubishi Electric Corp | 飛しょう体の発射装置 |
JP4338004B2 (ja) * | 2000-03-16 | 2009-09-30 | 株式会社Ihiエアロスペース | ロケットモータのノズルカバー |
JP3448648B2 (ja) * | 2000-11-27 | 2003-09-22 | 防衛庁技術研究本部長 | 飛しょう体発射筒装置 |
JP2004077038A (ja) * | 2002-08-20 | 2004-03-11 | Mitsubishi Heavy Ind Ltd | 飛しょう体用キャニスタの後蓋 |
US7984675B2 (en) * | 2006-02-21 | 2011-07-26 | Metal Storm Limited | Propellant sealing system for stackable projectiles |
-
2008
- 2008-01-11 FR FR0850162A patent/FR2926360B1/fr not_active Expired - Fee Related
-
2009
- 2009-01-08 US US12/735,379 patent/US8418593B2/en active Active
- 2009-01-08 WO PCT/FR2009/050020 patent/WO2009092938A2/fr active Application Filing
- 2009-01-08 KR KR1020107015280A patent/KR101567998B1/ko active IP Right Grant
- 2009-01-08 EP EP09704545.4A patent/EP2229573B1/fr active Active
- 2009-01-08 UA UAA201008714A patent/UA98686C2/ru unknown
- 2009-01-08 PL PL09704545T patent/PL2229573T3/pl unknown
- 2009-01-08 CN CN2009801019981A patent/CN101918786B/zh not_active Expired - Fee Related
- 2009-01-08 ES ES09704545.4T patent/ES2617208T3/es active Active
-
2010
- 2010-07-08 ZA ZA2010/04820A patent/ZA201004820B/en unknown
- 2010-07-08 MA MA33001A patent/MA32051B1/fr unknown
Also Published As
Publication number | Publication date |
---|---|
WO2009092938A2 (fr) | 2009-07-30 |
ZA201004820B (en) | 2011-03-30 |
US20110011251A1 (en) | 2011-01-20 |
EP2229573A2 (fr) | 2010-09-22 |
CN101918786A (zh) | 2010-12-15 |
UA98686C2 (ru) | 2012-06-11 |
WO2009092938A3 (fr) | 2009-12-17 |
US8418593B2 (en) | 2013-04-16 |
KR101567998B1 (ko) | 2015-11-10 |
CN101918786B (zh) | 2013-04-24 |
PL2229573T3 (pl) | 2017-05-31 |
FR2926360A1 (fr) | 2009-07-17 |
EP2229573B1 (fr) | 2016-12-07 |
KR20100122899A (ko) | 2010-11-23 |
FR2926360B1 (fr) | 2012-10-19 |
ES2617208T3 (es) | 2017-06-15 |
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