EP0054877B1 - Appareil autonome de lancement pour missiles guidés - Google Patents

Appareil autonome de lancement pour missiles guidés Download PDF

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Publication number
EP0054877B1
EP0054877B1 EP19810110411 EP81110411A EP0054877B1 EP 0054877 B1 EP0054877 B1 EP 0054877B1 EP 19810110411 EP19810110411 EP 19810110411 EP 81110411 A EP81110411 A EP 81110411A EP 0054877 B1 EP0054877 B1 EP 0054877B1
Authority
EP
European Patent Office
Prior art keywords
weapon
piston
main piston
container
equipment according
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.)
Expired
Application number
EP19810110411
Other languages
German (de)
English (en)
Other versions
EP0054877A1 (fr
Inventor
Hanns-Wilhelm Dr. Rer. Nat. Leuschner
Hermann Dipl.-Ing. Niermann
Joachim Ing. Grad. Voigt
Friedrich Ing. Grad. Wiggers
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.)
Ingenieurkontor Luebeck Prof Gabler Nachf GmbH
Licentia Patent Verwaltungs GmbH
Original Assignee
Ingenieurkontor Luebeck Prof Gabler Nachf GmbH
Licentia Patent Verwaltungs GmbH
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 Ingenieurkontor Luebeck Prof Gabler Nachf GmbH, Licentia Patent Verwaltungs GmbH filed Critical Ingenieurkontor Luebeck Prof Gabler Nachf GmbH
Publication of EP0054877A1 publication Critical patent/EP0054877A1/fr
Application granted granted Critical
Publication of EP0054877B1 publication Critical patent/EP0054877B1/fr
Expired legal-status Critical Current

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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
    • F41F3/08—Rocket or torpedo launchers for marine torpedoes

Definitions

  • the invention relates to a device according to the preamble of claim 1.
  • a launching and transporting container for rockets, missiles and the like in which a tube receiving a rocket is inserted into a container in such a way that the tube is centered and shock-proof stored therein.
  • the container is placed on a launcher frame and fastened so that the rocket can be fired from the tube in an alignable manner.
  • a firing device must always be present in order to use the weapon effectively.
  • a missile launching device which consists of a tubular receptacle for the missile with a solid bottom.
  • the discharge opening is provided with a removable cover. Its engine is fired to launch the missile.
  • the propellant gases hit the bottom of the container and are deflected towards the opening, causing the cap to be pushed out. This gives the missile a forward impulse.
  • the propellant gases emerging from the container opening have the task of displacing the water mass lying in front of the container opening and creating a path that is water-free for the start.
  • This effect can be intensified if a gas generator is additionally provided near the ground, which either creates the water-free space in front of the opening before the missile drive is fired or is ignited after the launch of the missile in order to keep this space water-free for a long period of time. This means that greater shooting depths can also be permitted.
  • the main deficiency of this device is that the risk of treachery rises sharply due to the propellant gases emerging from the container.
  • only missiles with launchers can be used.
  • a torpedo boat is known from DE-C-243 570, the bow tube of which accommodates a torpedo.
  • the tip of the torpedo is also the tip of the boat.
  • the torpedo is locked with its rear end in a piston filled with compressed air, which in turn is locked with the torpedo tube.
  • a firing pin is moved forward by externally supplied compressed air, which releases the lock between the piston and the tube and destroys a cutting disc, so that the compressed air enclosed in the piston can reach the rear of the torpedo. This pushes the piston forward with the torpedo until the piston is held in a pawl and the torpedo is unlocked from the piston.
  • the torpedo will continue to run after starting its propulsion.
  • the tip of the piston then forms the tip of the torpedo boat.
  • This launching device is very boat-specific, not self-sufficient and only intended for a special application - launching torpedoes in shallow water. This device is not suitable for long-term storage of the weapon.
  • the particular advantage of the invention is that an autonomous weapon system is achieved which has an extremely short reaction time because a firing mechanism is provided which is integrated in the storage and transport container and which takes effect immediately after the start signal.
  • An autonomous torpedo weapon system is described as an exemplary embodiment, which can be used, for example, on a submarine.
  • a steering body 4 (torpedo) is mounted approximately centrally on a support ring 5 and in the front tube part on guide surfaces 6.
  • the other tube end is provided with a removable bottom 8.
  • a pressurized gas volume 9 The inner wall of the pressurized gas-containing space 9 is provided with an opening, which in the storage and transport state has a valve 10 is closed. This valve is actuated via a line 11 by a start signal supplied from the outside.
  • This bottom part 8-11 and the rear pipe part are closed by a seal 13 contained in the flange 12.
  • a depth-dependent control valve 14 follows in the direction of the barrel axis, followed by a gas generator 15 for generating the pressure required to eject the weapon.
  • a compressed air bottle can also be provided.
  • the outlet opening for the compressed gas is provided with a sealing membrane 16.
  • the compressed gas acts on an inner piston 18 loading a spring 17 in a main piston 19 which causes the weapon to advance.
  • the inner piston 18 is displaceably mounted on the cylindrical inner wall of the piston 19 and on a sliding piston 20 connected to it, which at the same time receives a communication cable 21 from a termination bushing 22 to the stationary cassette.
  • the main piston 19 is held in place by a lock 23 and carries a seal 24 which, in the forward piston position, seals the drive space from the space flooded with water. Unlocking cams 25 which have the task of releasing a locking device 26 in the main piston 19 during ejection engage in this space. The piston 19 is then locked by the lock 23.
  • the space 27 for receiving the weapon 4 is filled with a protective liquid.
  • the device described above can be attached to the submarine in a suitable manner and is used as follows.
  • the boat may be at a certain depth.
  • the main piston 19 runs in the tubular container 1 up to the front guide surfaces 6. Here the movement is damped and the piston is locked.
  • the seal 24 between the main piston 19 and the pipe 1 prevents the compressed gas from escaping from the pipe.
  • This storage, transport and launching device is reusable after the shot has been fired.
  • the device can be used again by pushing back the main piston after venting the room and unlocking it by hand, inserting the new weapon with a tube closure with a membrane and replacing the gas volumes.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Ocean & Marine Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Portable Nailing Machines And Staplers (AREA)

Claims (5)

1. Dispositif autonome pour l'éjection rapide de torpilles et missiles sans étage de lancement, utilisable sur et sous l'eau, constitué par un conteneur (1) tubulaire fermé pour le stockage et le transport sans chocs de l'arme (4), des moyens de verrouillage et de propulsion de l'arme actionnés par un signal transmis de l'extérieur, un générateur de gaz (15) ou un volume de gaz compressible renouvelable assurant l'éjection de l'arme, ledit dispositif étant caractérisé en ce que l'arme (4) repose dans le conteneur (1) sur une bague d'appui (5) sensiblement centrale et est entourée par un liquide protecteur; après la délivrance d'un signal de lancement, une valve de régulation (10) d'un volume de gaz (9) est ouverte et met en service le générateur de gaz (15) par l'intermédiaire d'une autre valve de régulation (14); le gaz provenant du générateur (15) charge un piston double constitué par un piston principal et un piston intérieur (19, 18), le piston principal (19) étant déverrouillé par le piston intérieur (18) après le dépassement d'un seuil; le piston principal (19) chasse l'arme (4) hors du conteneur (1), son mouvement vers l'avant étant amorti par la bague d'appui (5) puis arrêté sur des faces de guidage (6) voisines de la bouche, avec déverrouillage simultané (26, 25) de l'arme (4); et le piston principal (19) porte un joint d'étanchéité (24) sur sa périphérie.
2. Dispositif selon revendication 1, caractérisé en ce que le seuil de déverrouillage du piston principal (19) est ajustable à l'aide d'un ressort (17).
3. Dispositif selon revendication 1, caractérisé en ce que la piston principal (19) est verrouillé dans la position avant.
4. Dispositif selon revendication 1, caractérisé en ce que l'orifice de bouche du conteneur (1) est obturé par une membrane destructible.
5. Dispositif selon revendication 1, caractérisé en ce que le piston principal (19) comporte une ouverture pour le passage d'un câble de télécommunication (21) pour armes dirigées (4) et constitue en outre le support d'une cassette de câble.
EP19810110411 1980-12-23 1981-12-14 Appareil autonome de lancement pour missiles guidés Expired EP0054877B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19803048666 DE3048666C2 (de) 1980-12-23 1980-12-23 Autarke Ausstoßeinrichtung für Lenkwaffen
DE3048666 1980-12-23

Publications (2)

Publication Number Publication Date
EP0054877A1 EP0054877A1 (fr) 1982-06-30
EP0054877B1 true EP0054877B1 (fr) 1986-04-02

Family

ID=6120081

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19810110411 Expired EP0054877B1 (fr) 1980-12-23 1981-12-14 Appareil autonome de lancement pour missiles guidés

Country Status (2)

Country Link
EP (1) EP0054877B1 (fr)
DE (1) DE3048666C2 (fr)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0110554B1 (fr) * 1982-10-28 1989-07-26 Underwater Storage Limited Systèmes à armes sous-marines
EP0116211A3 (fr) * 1982-12-10 1987-05-06 Underwater Storage Limited Systèmes d'armes sous-marines
FR2649194B1 (fr) * 1989-06-30 1994-05-13 Aerospatiale Ste Nationale Indle Dispositif d'ejection pour munition amphibie et propulseur independant en faisant partie
FR2767914B1 (fr) * 1997-08-28 1999-10-22 France Etat Conteneur de stockage et de lancement d'une arme du type torpille
RU2148773C1 (ru) * 1999-03-09 2000-05-10 Государственное унитарное предприятие "Конструкторское бюро машиностроения" Ракетно-торпедная пусковая установка
RU2172462C2 (ru) * 1999-08-30 2001-08-20 Казаков Владимир Михайлович Способ подачи снаряда или ракеты к месту назначения и устройство для его осуществления
GB0107552D0 (en) * 2001-03-27 2005-01-05 Matra Bae Dynamics Uk Ltd Improvements in and relating to the launching of missiles
RU2275579C1 (ru) * 2004-11-18 2006-04-27 Николай Яковлевич Кириленко Устройство для запуска ракет
RU2290590C1 (ru) * 2005-08-11 2006-12-27 Николай Яковлевич Кириленко Устройство для запуска ракет
RU2295689C1 (ru) * 2005-08-11 2007-03-20 Николай Яковлевич Кириленко Устройство для запуска ракет
GB0521649D0 (en) * 2005-10-24 2006-03-29 Strachan & Henshaw Ltd A payload deployment system
RU2318172C1 (ru) * 2006-08-08 2008-02-27 Николай Яковлевич Кириленко Устройство для запуска ракет
GB0625625D0 (en) * 2006-12-21 2008-01-09 Strachan & Henshaw Ltd A payload deployment system
CN103175444A (zh) * 2011-12-23 2013-06-26 刘祖学 聚能动态发射装置
DE102020211065B3 (de) 2020-09-02 2021-08-12 Thyssenkrupp Ag Torpedokassettenadapter und Torpedokassettenadapterverlängerungsstück

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE243570C (fr) *
DE809156C (de) * 1944-11-30 1951-07-23 Schermuly Pistol Rocket Appara Abschussvorrichtung mit Rakete
FR1604112A (fr) * 1964-02-26 1971-07-12
CA935681A (en) * 1970-01-02 1973-10-23 Norris Industries Disposable projectile launcher of the recoilless type
DE2029869C3 (de) * 1970-06-18 1974-04-11 Faun-Werke Kommunalfahrzeuge Und Lastkraftwagen Karl Schmidt, 8500 Nuernberg Torpedorohr, insbesondere zum Überwasserabschuß eines Torpedos von einem Schiff aus
FR2217657B1 (fr) * 1973-02-13 1976-05-14 Aerospatiale
DE2416801A1 (de) * 1974-04-06 1979-01-11 Gemmecke Kurt Ing Grad Torpedoabschussvorrichtung
US4026188A (en) * 1975-12-24 1977-05-31 Sanders Associates, Inc. Modular buoy system
DE2627505C3 (de) * 1976-06-18 1981-08-13 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Vorrichtung zur Lagerung, zum Transport und Abschuß von Flugkörpern

Also Published As

Publication number Publication date
DE3048666C2 (de) 1986-05-22
EP0054877A1 (fr) 1982-06-30
DE3048666A1 (de) 1982-07-08

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