WO2009092938A3 - Opercule arrière déformable pour conteneur de missile, comportant un cadre de support aval - Google Patents

Opercule arrière déformable pour conteneur de missile, comportant un cadre de support aval Download PDF

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Publication number
WO2009092938A3
WO2009092938A3 PCT/FR2009/050020 FR2009050020W WO2009092938A3 WO 2009092938 A3 WO2009092938 A3 WO 2009092938A3 FR 2009050020 W FR2009050020 W FR 2009050020W WO 2009092938 A3 WO2009092938 A3 WO 2009092938A3
Authority
WO
WIPO (PCT)
Prior art keywords
bearing frame
downstream
downstream bearing
rear disc
disc
Prior art date
Application number
PCT/FR2009/050020
Other languages
English (en)
Other versions
WO2009092938A2 (fr
Inventor
Pierre Jacques Truyman
Original Assignee
Dcns
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 Dcns filed Critical Dcns
Priority to CN2009801019981A priority Critical patent/CN101918786B/zh
Priority to EP09704545.4A priority patent/EP2229573B1/fr
Priority to US12/735,379 priority patent/US8418593B2/en
Priority to ES09704545.4T priority patent/ES2617208T3/es
Publication of WO2009092938A2 publication Critical patent/WO2009092938A2/fr
Publication of WO2009092938A3 publication Critical patent/WO2009092938A3/fr
Priority to MA33001A priority patent/MA32051B1/fr
Priority to ZA2010/04820A priority patent/ZA201004820B/en

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.
PCT/FR2009/050020 2008-01-11 2009-01-08 Opercule arrière déformable pour conteneur de missile, comportant un cadre de support aval WO2009092938A2 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
CN2009801019981A CN101918786B (zh) 2008-01-11 2009-01-08 包括下游承载框架的用于导弹容器的可变形后部盘
EP09704545.4A EP2229573B1 (fr) 2008-01-11 2009-01-08 Système de fond d'un conteneur de missile
US12/735,379 US8418593B2 (en) 2008-01-11 2009-01-08 Deformable rear disc for missile container, including a downstream bearing frame
ES09704545.4T ES2617208T3 (es) 2008-01-11 2009-01-08 Sistema de fondo de un contenedor de misil
MA33001A MA32051B1 (fr) 2008-01-11 2010-07-08 Opercule arriere deformable pour conteneur de missile, comportant un cadre de support aval
ZA2010/04820A ZA201004820B (en) 2008-01-11 2010-07-08 Deformable rear disc for missible container, including a downstream bearing frame

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0850162 2008-01-11
FR0850162A FR2926360B1 (fr) 2008-01-11 2008-01-11 Opercule arriere deformable pour conteneur de missile, comportant un cadre de support aval

Publications (2)

Publication Number Publication Date
WO2009092938A2 WO2009092938A2 (fr) 2009-07-30
WO2009092938A3 true WO2009092938A3 (fr) 2009-12-17

Family

ID=39745427

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2009/050020 WO2009092938A2 (fr) 2008-01-11 2009-01-08 Opercule arrière déformable 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)

* Cited by examiner, † Cited by third party
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
US10813811B2 (en) 2015-08-24 2020-10-27 Handi-Move Clamp and patient lifting aids using the clamp
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

Citations (7)

* Cited by examiner, † Cited by third party
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
US4683798A (en) * 1985-12-27 1987-08-04 General Dynamics, Pomona Division Gas management transition device
US4686884A (en) * 1985-12-27 1987-08-18 General Dynamics, Pomona Division Gas management deflector
FR2620808A1 (fr) * 1987-09-17 1989-03-24 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
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

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
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
US7984675B2 (en) * 2006-02-21 2011-07-26 Metal Storm Limited Propellant sealing system for stackable projectiles

Patent Citations (7)

* Cited by examiner, † Cited by third party
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
US4683798A (en) * 1985-12-27 1987-08-04 General Dynamics, Pomona Division Gas management transition device
US4686884A (en) * 1985-12-27 1987-08-18 General Dynamics, Pomona Division Gas management deflector
FR2620808A1 (fr) * 1987-09-17 1989-03-24 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
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

Also Published As

Publication number Publication date
CN101918786A (zh) 2010-12-15
FR2926360B1 (fr) 2012-10-19
KR20100122899A (ko) 2010-11-23
KR101567998B1 (ko) 2015-11-10
US8418593B2 (en) 2013-04-16
EP2229573A2 (fr) 2010-09-22
ES2617208T3 (es) 2017-06-15
PL2229573T3 (pl) 2017-05-31
FR2926360A1 (fr) 2009-07-17
US20110011251A1 (en) 2011-01-20
ZA201004820B (en) 2011-03-30
UA98686C2 (ru) 2012-06-11
WO2009092938A2 (fr) 2009-07-30
EP2229573B1 (fr) 2016-12-07
MA32051B1 (fr) 2011-02-01
CN101918786B (zh) 2013-04-24

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