EP2293974B1 - Prinzip zur integration von flugkörper-basierten waffensystemen auf einer festen rampe für getarnte oberflächenwasserfahrzeuge zum entgegnen von asymmetrischen bedrohungen - Google Patents

Prinzip zur integration von flugkörper-basierten waffensystemen auf einer festen rampe für getarnte oberflächenwasserfahrzeuge zum entgegnen von asymmetrischen bedrohungen Download PDF

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Publication number
EP2293974B1
EP2293974B1 EP09772733A EP09772733A EP2293974B1 EP 2293974 B1 EP2293974 B1 EP 2293974B1 EP 09772733 A EP09772733 A EP 09772733A EP 09772733 A EP09772733 A EP 09772733A EP 2293974 B1 EP2293974 B1 EP 2293974B1
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EP
European Patent Office
Prior art keywords
ship
missile
ditch
bulwarks
launch
Prior art date
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Active
Application number
EP09772733A
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English (en)
French (fr)
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EP2293974A2 (de
Inventor
Stéphane GOASDUFF
Jean-Jacques Milin
Bruno Le Gall
Georges Pensec
Serge Philippe
Xavier Le Gourlay
Yvan Paulmery
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Naval Group SA
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DCNS SA
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Publication date
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Publication of EP2293974A2 publication Critical patent/EP2293974A2/de
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63G—OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
    • B63G1/00—Arrangements of guns or missile launchers; Vessels characterised thereby
    • 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

Definitions

  • the present invention relates to a device for launching a missile from a ship and to a vessel equipped with such a device.
  • missile launching devices consisting of integrated launching ramps to launch missiles over the ship's side, usually to either port or starboard, at inclinations less than or equal to 45 ° with the ship's po nt.
  • These missiles which are often contained in containers are launched for example from fixed ramps arranged on the outer deck of the ship.
  • Such fixed ramps on the deck have the drawback of being visible and of having a significant radar signature, and of being vulnerable to asymmetric threats of the small-caliber artillery type. or others.
  • In order to reduce the visual and radar signature of these missile ramps there are sometimes bulwarks around these ramps that hide them from these threats.
  • these orifices may be closed by lids adapted to be ejected at the time of firing missiles under the effect of the gases released by the thrusters. These lids can also be closed by plating doors that can be opened when the missiles are fired.
  • deflectors behind the missile launching ramps so as to orient the propulsion gases towards the openings provided in the bulwarks or above the bulwarks if the height of these bulwarks is limited.
  • Solutions based lids or plating doors have the disadvantage of being expensive, complex to achieve and difficult to use especially for the lids which must necessarily be manipulated by operators to be replaced.
  • the signature of the ship is changed until the closing of the door or until replacement of the covers.
  • this provision has the drawback of do not provide good protection against asymmetric threats and degrade visual and radar signatures.
  • the document FR 2 626 242 which is considered to be the closest state of the art, describes a surveillance patrol having guns arranged in truncated conical bowls.
  • the object of the present invention is to overcome these drawbacks by proposing a missile launching device from a ship that provides good missile protection against asymmetric threats of the small caliber artillery type or other, which ensure a low radar signature and device in such a way as to be compatible with the conditions imposed on a stealthy military building, and that meet the functional constraints imposed by missile weapon systems both under normal conditions of use and in cases of misuse. fire, this device meets the operational requirements of permanent availability of weapon systems.
  • the invention relates to a device for launching missiles from a ship of the type comprising at least one missile launching ramp. It includes a pit delimited by side walls, at least two of which extend on the periphery of the ship and constitute bulwarks, the pit being open above the outer deck of the ship.
  • the launching ramp is placed in the pit so that it can be used to launch a missile over a side bulwark of the pit.
  • the device comprises a means for evacuating the propulsion gases of a missile comprising a sheath opening onto an orifice provided in a side bulwark of the pit, and the side bulwarks of the pit have a height adapted to mask missiles arranged on the ramp, for an incidence close to the horizontal of the building.
  • the height of the bulwarks of the pit is adapted to hide missiles arranged on the ramp for an incidence between 0 ° and -5 ° relative to the horizontal of the ship.
  • the side bulwarks of the pit, the gas evacuation opening and the gas evacuation duct are adapted to minimize the radar and visual signatures of the device.
  • the side bulwark of the pit are adapted so as to withstand at least small artillery type attacks.
  • the gas evacuation device comprises walls coated with refractory material.
  • the missile launching ramp is fixed.
  • the device is adapted to launch a missile in a direction forming an angle with the ship's bridge less than or equal to 45 °.
  • the invention also relates to a ship of the type comprising a missile launching device above its outer bridge, the missile launching device was according to the invention.
  • the missile launching device is adapted for launching missiles laterally with respect to the ship.
  • the missile launch device 3 consists of a pit 4 of missile launching whose bottom is constituted by the outer deck 2 which extends over the entire width of the hull between the port plating 5 and the starboard plank 6 and which is laterally delimited by side walls 7 and 8 which constitute bulwarks.
  • These bulwarks are made of shielded steel sheet so as to protect the missiles by resisting at least attacks by low-power weapons such as light artillery.
  • These bulwarks are tilted slightly inward to minimize the radar signature for threats having an incidence between the horizontal and - 3 °, and preferably, -5 °, relative to the horizontal.
  • horizontal means the surface of the ship's deck, which corresponds to the geographical horizontal when the ship does not have a cottage.
  • a fixed missile launching ramp 9 is located inside the pit 4.
  • This missile launch pad consists of a support 10, a sun protection hood 10A, holding cradles 11, of missile containers 12 inclined.
  • the missile launching device comprises a means generally marked 14 for the evacuation of the missile propulsion gases during a nominal or sustained fire, that is to say resulting from the inadvertent ignition of the missile thrusters.
  • This means 14 of evacuation of gases is located opposite the rear end 13 of the missile containers.
  • This gas evacuation means comprises a deflector 15 consisting of sheets covered with a layer 16 of refractory material, flanked by lateral flanges 17 and whose upper part is partially covered by louvres 18 so as to constitute a sheath 19 opening on the outside by an opening 20 provided in the side wall 7.
  • the geometry of the opening 20 and the different walls of the sheath 19, are adapted so as firstly to ensure a good evacuation of gases whether at the time the launching of a missile or in case of unintentional ignition of a missile or even of several missiles, and at the same time to ensure a weak radar signature related to the opening.
  • Those skilled in the art know how to determine the optimal geometries both to ensure good gas evacuation and to ensure a low radar signature.
  • bulwark 7 and the louvers 18 may be made of armor steel or of sufficient thickness so as to provide protection against attacks by means of moderate power such as small caliber artillery.
  • the side walls 7 and 8 that is to say the bulwarks, have heights adapted to mask the missile launching ramp equipped with its missiles in view and radar observers which are at the horizontal or slightly above the horizontal.
  • the gas evacuation duct defined by the deflector 15, the flanges 17 and the louvers 18, has a geometry adapted to mask the missile launching ramp equipped with its missiles. the view and observers radars that are at the horizontal or slightly above the horizontal.
  • the bulwarks 7 and 8 have inner flaps 21 and 22 ( fallen edge) which are inclined with angles adapted to provide a reflection of the radar waves in different directions of the direction of arrival.
  • the height of the bulwarks as well as the position of the launching ramps and the inclination of the missile containers on these launching ramps are adapted so that the missile clearance cone 23 passes over the upper edge of the bulwarks.
  • this provision assumes that the ship is large enough to be able to dispose all the equipment while ensuring both good operation and good protection against asymmetric aggression, good optical concealment and a weak signature radar.
  • the evacuation pipe gas defined by the deflector 15, the flanges 17 and the louvers 18 is partially covered with refractory materials. The installation of these coatings ensures the safety of the platform and personnel by ensuring the integrity of the device during and after firing. Reuse of the device is still possible.
  • missile launching devices are mounted on ships such as frigates that are large enough to be able to implement two missile ramps one oriented to be able to send missiles on the port side and the other way to be able to send missiles by starboard.
  • the launching ramp 9 is completed by a gas evacuation means, not visible in the figure, which opens out through an opening 20 provided in the bulwark 7 which extends the plating 5 located on the port side of the ship.
  • This launching pad is intended to launch missiles over the bulwark 8 which extends the shelled 6 starboard.
  • the bulwark 8 has a notch 24 which allows to respect the missile clearance cone while keeping a margin to overcome or lack of positioning and manufacturing.
  • the missile launching pit 4 has a second missile launching ramp 9 'oriented so that it can launch missiles over the bulwark 7 located on the port side.
  • This missile launching ramp 9 ' is disposed in front of a gas evacuation means 14' consisting of a deflector 15 'bordered by lateral flanges 17' and whose upper part is covered by louvres 18 so as to constitute a exhaust duct 19 'of the gases.
  • the missile launching device that has just been described and that can equip ships such as frigates is suitable for launching missiles either to port or starboard of the ship.
  • the pit of the missile launching device is delimited by lateral walls which extend to the periphery of the ship.
  • walls which extend to the periphery of the vessel means walls which extend at least partially on the port or starboard sides or on the stern of the ship.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Claims (9)

  1. Vorrichtung für den Abschuss von Flugkörpern von einem Schiff aus, das mindestens eine Abschussrampe für Flugkörper (9, 9') umfasst, dadurch gekennzeichnet, dass sie einen Graben (4) aufweist, der von Seitenwänden begrenzt ist, von denen mindestens zwei (7, 8) Schilde bilden, die sich am Umfang des Schiffes erstrecken, wobei der Graben über dem Außendeck des Schiffes offen ist, dass die Abschussrampe (9, 9') in dem Graben in der Weise angeordnet ist, dass sie dazu dienen kann, einen Flugkörper über ein Seitenschild (7, 8) des Grabens, das sich am Umfang des Schiffes erstreckt, abzuschießen, dass sie ein Mittel zur Beseitigung von Treibgasen eines Flugkörpers umfasst, das eine Umhüllung (19, 19') aufweist, die in eine Öffnung (20) mündet, die im sich am Umfang des Schiffes erstreckenden Seitenschild (7) des Grabens vorgesehen ist, und dass die Seitenschilde (7, 8) des Grabens eine Höhe aufweist, die angepasst ist, um die auf der Rampe angeordneten Flugkörper abzuschirmen für einen Einfall benachbart zur Horizontalen des Schiffes.
  2. Vorrichtung nach Anspruch 1, dadurch gekennzeichnet, dass die Höhe des Schildes (7, 8) des Grabens angepasst ist, um Flugkörper abzuschirmen, die auf der Rampe (9,9') für einen Einfall zwischen 0° und -5° in Bezug auf die Brücke des Schiffes angeordnet sind.
  3. Vorrichtung nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass die Seitenschilde (7, 8) des Grabens, die Öffnung (20) der Beseitigung der Gase und der Kanal (19) zur Beseitigung des Gases angepasst sind, um die visuelle und Radarsignatur der Vorrichtung zu minimieren.
  4. Vorrichtung nach einem beliebigen der Ansprüche 1 bis 3, dadurch gekennzeichnet, dass die Seitenschilde (7, 8) des Grabens derart angepasst sind, dass sie mindestens Aggressionen des Typs Artillerie mit kleinem Kaliber widerstehen kann.
  5. Vorrichtung nach einem beliebigen der Ansprüche 1 bis 4, dadurch gekennzeichnet, dass die Vorrichtung (14, 14') zur Beseitigung des Gases Wände (15, 15') umfasst, die mit einem hitzebeständig Material überzogen sind.
  6. Vorrichtung nach einem beliebigen der Ansprüche 1 bis 5, dadurch gekennzeichnet, dass die Abschussrampe (9, 9') der Flugkörper feststehend ist.
  7. Vorrichtung nach einem beliebigen der Ansprüche 1 bis 6, dadurch gekennzeichnet, dass die Vorrichtung angepasst ist, einen Flugkörper in eine Richtung abzuschießen, die mit der Brücke des Schiffes einen Winkel von kleiner oder gleich 45° bildet.
  8. Schiff, das eine Vorrichtung zum Abschießen eines Flugkörpers über seine Außendeck, dadurch gekennzeichnet, dass die Vorrichtung zum Abschießen eines Flugkörpers eine solche nach einem beliebigen der Ansprüche 1 bis 7 ist.
  9. Schiff nach Anspruch 8, dadurch gekennzeichnet, dass die Vorrichtung zum Abschießen von Flugkörpern angepasst ist, um Flugkörper seitlich in Bezug auf das Schiff abzuschießen.
EP09772733A 2008-07-03 2009-07-01 Prinzip zur integration von flugkörper-basierten waffensystemen auf einer festen rampe für getarnte oberflächenwasserfahrzeuge zum entgegnen von asymmetrischen bedrohungen Active EP2293974B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0854521A FR2933373B1 (fr) 2008-07-03 2008-07-03 Principe d'integration, contre menaces asymetriques, de systemes d'armes missiles sur rampe fixe pour batiment de surface furtifs
PCT/FR2009/051276 WO2010001051A2 (fr) 2008-07-03 2009-07-01 Principe d'intégration, contre menaces asymétriques, de systèmes d'armes missiles sur rampe fixe pour bâtiments de surface furtifs

Publications (2)

Publication Number Publication Date
EP2293974A2 EP2293974A2 (de) 2011-03-16
EP2293974B1 true EP2293974B1 (de) 2013-03-27

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EP09772733A Active EP2293974B1 (de) 2008-07-03 2009-07-01 Prinzip zur integration von flugkörper-basierten waffensystemen auf einer festen rampe für getarnte oberflächenwasserfahrzeuge zum entgegnen von asymmetrischen bedrohungen

Country Status (6)

Country Link
US (1) US8181562B2 (de)
EP (1) EP2293974B1 (de)
ES (1) ES2412235T3 (de)
FR (1) FR2933373B1 (de)
RU (1) RU2497713C2 (de)
WO (1) WO2010001051A2 (de)

Families Citing this family (8)

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US11015903B2 (en) * 2011-06-08 2021-05-25 American Technical Coatings, Inc. Enhanced ballistic protective system
RU2577743C1 (ru) * 2015-01-12 2016-03-20 Николай Яковлевич Кириленко Стартовая позиция для самоходных пусковых установок для запуска ракеты под углами, близкими к вертикальному углу
FR3069522A1 (fr) * 2017-07-27 2019-02-01 Dcns Plateforme navale du type comportant une fosse a missile
CN107478106A (zh) * 2017-08-16 2017-12-15 董兰田 轨道发射地效翼对海导弹
US11143489B2 (en) * 2018-02-07 2021-10-12 Raytheon Company Rail-launching munition release
CN110319734B (zh) * 2019-07-11 2020-06-19 北京航空航天大学 地埋式伪装小型运载火箭发射系统
CN110319733B (zh) * 2019-07-11 2020-06-19 北京航空航天大学 地埋式伪装导弹发射系统
CN113148003A (zh) * 2021-04-25 2021-07-23 上海机电工程研究所 防止失控发射的甲板舱盖结构和甲板舱

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Also Published As

Publication number Publication date
US8181562B2 (en) 2012-05-22
ES2412235T3 (es) 2013-07-10
FR2933373A1 (fr) 2010-01-08
WO2010001051A2 (fr) 2010-01-07
RU2011103757A (ru) 2012-08-10
FR2933373B1 (fr) 2010-08-20
US20110167995A1 (en) 2011-07-14
WO2010001051A3 (fr) 2010-12-29
EP2293974A2 (de) 2011-03-16
RU2497713C2 (ru) 2013-11-10

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