EP2078918A3 - Container for multiple missiles and versatile launcher - Google Patents

Container for multiple missiles and versatile launcher Download PDF

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Publication number
EP2078918A3
EP2078918A3 EP09150230A EP09150230A EP2078918A3 EP 2078918 A3 EP2078918 A3 EP 2078918A3 EP 09150230 A EP09150230 A EP 09150230A EP 09150230 A EP09150230 A EP 09150230A EP 2078918 A3 EP2078918 A3 EP 2078918A3
Authority
EP
European Patent Office
Prior art keywords
container
missile
cap
tube
launcher
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
EP09150230A
Other languages
German (de)
French (fr)
Other versions
EP2078918A2 (en
EP2078918B1 (en
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
Publication of EP2078918A2 publication Critical patent/EP2078918A2/en
Publication of EP2078918A3 publication Critical patent/EP2078918A3/en
Application granted granted Critical
Publication of EP2078918B1 publication Critical patent/EP2078918B1/en
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)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

Conteneur multiple (17) comportant un fond muni d'une pluralité d'opercules (56) et un cloisonnement (50) subdivisant le conteneur en une pluralité de tubes (51), chaque tube étant destiné à recevoir un missile (18) et chaque opercule étant en regard d'un tube.Multiple container (17) having a bottom provided with a plurality of lids (56) and a partition (50) dividing the container into a plurality of tubes (51), each tube being adapted to receive a missile (18) and each operculum being opposite a tube.

Chaque opercule est du type déformable, apte à s'ouvrir sous la poussée des gaz de propulsion du missile contenu dans le tube correspondant et à se refermer après éjection du missile, l'opercule comprenant un empilement de lames élastiques maintenues entre un cadre de support amont et un cadre de support aval.Each cap is of the deformable type, able to open under the thrust of the propulsion gases of the missile contained in the corresponding tube and to close after ejection of the missile, the cap comprising a stack of elastic blades held between a support frame upstream and a downstream support framework.

Le fond du conteneur est muni, du côté aval, de moyens de protection thermique aptes à protéger chaque opercule du flux de rayonnement thermique incident émis lors de l'ouverture d'un opercule voisin sous l'effet des gaz de propulsion d'un missile.

Figure imgaf001
The bottom of the container is provided, on the downstream side, with thermal protection means capable of protecting each cap of the incident thermal radiation flux emitted during the opening of a neighboring cap under the effect of the propulsion gases of a missile .
Figure imgaf001
EP09150230.2A 2008-01-11 2009-01-08 Container for multiple missiles and versatile launcher Active EP2078918B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0850159A FR2926357B1 (en) 2008-01-11 2008-01-11 MULTIPLE MISSILE CONTAINER AND VERSATILE LAUNCHER

Publications (3)

Publication Number Publication Date
EP2078918A2 EP2078918A2 (en) 2009-07-15
EP2078918A3 true EP2078918A3 (en) 2009-12-02
EP2078918B1 EP2078918B1 (en) 2016-04-27

Family

ID=39679311

Family Applications (1)

Application Number Title Priority Date Filing Date
EP09150230.2A Active EP2078918B1 (en) 2008-01-11 2009-01-08 Container for multiple missiles and versatile launcher

Country Status (4)

Country Link
EP (1) EP2078918B1 (en)
ES (1) ES2581232T3 (en)
FR (1) FR2926357B1 (en)
PL (1) PL2078918T3 (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2484408C2 (en) * 2011-08-22 2013-06-10 Открытое акционерное общество "Центральное конструкторское бюро "Титан" Device for automatic drop and catch of cover of transporter-launcher container installed on missile launcher
RU2544265C1 (en) * 2014-02-28 2015-03-20 Открытое акционерное общество Центральный научно-исследовательский институт специального машиностроения Fireproof cover of multi-barrel launching unit
CN103913099B (en) * 2014-03-12 2015-09-09 南京航空航天大学 Integral hollow composite material launching box cover
CN111086773A (en) * 2020-03-11 2020-05-01 衡阳泰豪通信车辆有限公司 Anti-ablation high-shielding container capable of being quickly separated
CN111595199B (en) * 2020-05-14 2022-12-23 湖北三江航天万峰科技发展有限公司 Heating control device for launching box
CN113074580B (en) * 2021-04-02 2022-08-12 上海机电工程研究所 Repeatable large-angle cartridge switch cover mechanism
CN115164642B (en) * 2022-07-30 2024-07-05 成都云鼎智控科技有限公司 Insert-removing supporting structure and transmitting device formed by same

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4044648A (en) * 1975-09-29 1977-08-30 General Dynamics Corporation Rocket exhaust plenum flow control apparatus
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 (en) * 1987-09-17 1989-03-24 France Etat Armement REAR OPERATOR FOR MISSILE CONTAINER
US5194688A (en) * 1992-01-31 1993-03-16 Hughes Missile Systems Company Apparatus for limiting recirculation of rocket exhaust gases during missile launch
US5327809A (en) * 1993-03-24 1994-07-12 Fmc Corporation Dual pack canister
JPH11183089A (en) * 1997-12-24 1999-07-06 Mitsubishi Electric Corp Firing apparatus for missile
US6125734A (en) * 1998-10-14 2000-10-03 The United States Of America As Represented By The Secretary Of The Navy Multi-warfare area launcher
JP2001124494A (en) * 1999-10-25 2001-05-11 Mitsubishi Electric Corp Discharger for flier
US6230604B1 (en) * 1997-01-14 2001-05-15 United Defense, L.P. Concentric canister launcher

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4044648A (en) * 1975-09-29 1977-08-30 General Dynamics Corporation Rocket exhaust plenum flow control apparatus
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 (en) * 1987-09-17 1989-03-24 France Etat Armement REAR OPERATOR FOR MISSILE CONTAINER
US5194688A (en) * 1992-01-31 1993-03-16 Hughes Missile Systems Company Apparatus for limiting recirculation of rocket exhaust gases during missile launch
US5327809A (en) * 1993-03-24 1994-07-12 Fmc Corporation Dual pack canister
US6230604B1 (en) * 1997-01-14 2001-05-15 United Defense, L.P. Concentric canister launcher
JPH11183089A (en) * 1997-12-24 1999-07-06 Mitsubishi Electric Corp Firing apparatus for missile
US6125734A (en) * 1998-10-14 2000-10-03 The United States Of America As Represented By The Secretary Of The Navy Multi-warfare area launcher
JP2001124494A (en) * 1999-10-25 2001-05-11 Mitsubishi Electric Corp Discharger for flier

Also Published As

Publication number Publication date
FR2926357A1 (en) 2009-07-17
EP2078918A2 (en) 2009-07-15
ES2581232T3 (en) 2016-09-02
PL2078918T3 (en) 2016-11-30
FR2926357B1 (en) 2013-10-25
EP2078918B1 (en) 2016-04-27

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