EP2078920A3 - Opercule aval déformable pour conteneur de missile - Google Patents

Opercule aval déformable pour conteneur de missile Download PDF

Info

Publication number
EP2078920A3
EP2078920A3 EP09150245A EP09150245A EP2078920A3 EP 2078920 A3 EP2078920 A3 EP 2078920A3 EP 09150245 A EP09150245 A EP 09150245A EP 09150245 A EP09150245 A EP 09150245A EP 2078920 A3 EP2078920 A3 EP 2078920A3
Authority
EP
European Patent Office
Prior art keywords
bottom closure
deformable bottom
missile container
stack
support frame
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.)
Granted
Application number
EP09150245A
Other languages
German (de)
English (en)
Other versions
EP2078920A2 (fr
EP2078920B1 (fr
Inventor
Pierre Jacques Truyman
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Naval Group SA
Original Assignee
DCNS SA
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 SA filed Critical DCNS SA
Priority to PL09150245T priority Critical patent/PL2078920T3/pl
Publication of EP2078920A2 publication Critical patent/EP2078920A2/fr
Publication of EP2078920A3 publication Critical patent/EP2078920A3/fr
Application granted granted Critical
Publication of EP2078920B1 publication Critical patent/EP2078920B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F41F3/0413—Means for exhaust gas disposal, e.g. exhaust deflectors, gas evacuation systems
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Closures For Containers (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Table Devices Or Equipment (AREA)
  • Details Of Aerials (AREA)
  • Bag Frames (AREA)
  • Packages (AREA)
  • Wind Motors (AREA)

Abstract

La présente invention concerne un opercule (56) du type déformable, destiné à équiper le fond d'un conteneur de missile (15) et apte à s'ouvrir sous la poussée des gaz de propulsion d'un missile (16) contenu dans le conteneur et à se refermer après éjection du missile, l'opercule comprenant une grille (62) et 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). Selon l'invention l'opercule comporte au moins un moyen intercalaire de glissement (67) disposé entre deux lames successives de l'empilement.
EP09150245A 2008-01-11 2009-01-08 Opercule aval déformable pour conteneur de missile Active EP2078920B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL09150245T PL2078920T3 (pl) 2008-01-11 2009-01-08 Osłona dolna kontenera pocisku

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0850160A FR2926358B1 (fr) 2008-01-11 2008-01-11 Opercule aval deformable ameliore pour conteneur de missile

Publications (3)

Publication Number Publication Date
EP2078920A2 EP2078920A2 (fr) 2009-07-15
EP2078920A3 true EP2078920A3 (fr) 2009-12-02
EP2078920B1 EP2078920B1 (fr) 2010-09-22

Family

ID=39745309

Family Applications (1)

Application Number Title Priority Date Filing Date
EP09150245A Active EP2078920B1 (fr) 2008-01-11 2009-01-08 Opercule aval déformable pour conteneur de missile

Country Status (6)

Country Link
EP (1) EP2078920B1 (fr)
AT (1) ATE482373T1 (fr)
DE (1) DE602009000191D1 (fr)
ES (1) ES2351379T3 (fr)
FR (1) FR2926358B1 (fr)
PL (1) PL2078920T3 (fr)

Citations (6)

* 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
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

Patent Citations (6)

* 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
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
DE602009000191D1 (de) 2010-11-04
EP2078920A2 (fr) 2009-07-15
EP2078920B1 (fr) 2010-09-22
ES2351379T3 (es) 2011-02-03
FR2926358A1 (fr) 2009-07-17
ATE482373T1 (de) 2010-10-15
FR2926358B1 (fr) 2010-01-15
PL2078920T3 (pl) 2011-06-30

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