EP1992901A2 - Installation d'arme pour un bateau - Google Patents

Installation d'arme pour un bateau Download PDF

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Publication number
EP1992901A2
EP1992901A2 EP08008658A EP08008658A EP1992901A2 EP 1992901 A2 EP1992901 A2 EP 1992901A2 EP 08008658 A EP08008658 A EP 08008658A EP 08008658 A EP08008658 A EP 08008658A EP 1992901 A2 EP1992901 A2 EP 1992901A2
Authority
EP
European Patent Office
Prior art keywords
rocket
cradle
hangar
rocket launcher
ship
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.)
Withdrawn
Application number
EP08008658A
Other languages
German (de)
English (en)
Other versions
EP1992901A3 (fr
Inventor
Siegfried Süss
Georg Scheidemann
Heinrich Heldmann
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.)
KNDS Deutschland GmbH and Co KG
Original Assignee
Krauss Maffei Wegmann GmbH and Co KG
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 Krauss Maffei Wegmann GmbH and Co KG filed Critical Krauss Maffei Wegmann GmbH and Co KG
Publication of EP1992901A2 publication Critical patent/EP1992901A2/fr
Publication of EP1992901A3 publication Critical patent/EP1992901A3/fr
Withdrawn legal-status Critical Current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
    • 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
    • B63G3/00—Arrangements of ammunition stores or handlers; Vessels characterised thereby
    • B63G3/04—Arrangements of ammunition stores or handlers; Vessels characterised thereby for missiles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A23/00—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles
    • F41A23/24—Turret gun mountings

Definitions

  • the invention relates to a weapon system for a ship with a rocket launcher pivotally mounted on the ship's deck in azimuth and elevation and an ammunition space for storing rocket containers configured to receive at least one rocket, the ammunition space being located within a hangar immediately adjacent to the rocket launcher is arranged.
  • An object of the invention was to arrange a rocket launcher directly on the main deck of a ship, that is, at a location which is strongly exposed to the sea state and the waves breaking over the deck. While the placement of a rocket launcher on a land vehicle always involves well-defined and predictable stresses that are often time-limited, the sea state itself is unpredictable or predictable and very high stresses may occur over extended periods of time.
  • the weapon system must be designed on a ship so that even with prolonged high stress no damage to the missile launcher itself and the ammunition space can occur with the rocket containers stored therein.
  • a basic idea of the invention is, according to the combination of features a), to design the rocket launcher itself in a particularly stable manner and to anchor it on the ship deck.
  • rocket launcher When arranged on land vehicles rocket launcher has this, as in EP 1 186 848 A1 described, generally a top mount with mounting frame for the rocket container, which pivot at one end in elevation with a lower mount is connected, which is mounted on a turntable in azimuth pivotally mounted on the vehicle under a frame.
  • the pivoting movement in elevation is effected by electromechanical lifting means arranged between lower mount and upper mount, that is, for example, a lifting spindle drive.
  • a swivel arm is arranged with a hoist for feeding the rocket container.
  • the rocket launcher according to the invention has a fundamentally known in guns rigid bending cradle, which is mounted on a trunnion bearing in elevation pivotally mounted in a weighing receptacle. This cradle mount is then pivotally mounted on azimuth via a pivot bearing on a pedestal fixedly connected to the ship's deck. As a result, a good stability in the training and storage of the rocket launcher is achieved.
  • the rocket container conveyor is not located on the rocket launcher itself, but below the ceiling of the hangar, which has an opening in the sidewall on its rocket launcher side through which the rocket containers extend the hangar out the rocket launcher are supplied.
  • the rocket launcher has two side cheeks receiving the trunnion bearing, between which at least one guide plate for the exhaust jet the missile is arranged, which is concave curved seen at least in some areas from above and in the firing direction, so that the exhaust gas jet is diverted substantially in a direction parallel to the ship's deck.
  • FIGS. 1A to 3C is a part of the ship's deck D, which is bounded by a rail R, a warship, not shown otherwise, such as a frigate, shown.
  • a weapon system On the ship's deck D a weapon system is arranged, which has a rocket launcher, which is generally designated 1 and on which in a conventional manner two ammunition container 2 can be arranged, each containing several, for example six, artillery rockets 2.1.
  • hangar Immediately adjacent to the rocket launcher 1 a designated generally by reference numeral 3 hangar is arranged, the longitudinal direction L points to the rocket launcher 1 and a ceiling 3.1, extending in the longitudinal direction L side walls 3.2 and the rocket launcher 1 facing front wall 3.3 and a non-visible rear wall has.
  • the hangar 3 several filled with rockets ammunition container 2 are stored.
  • the hangar 3 is provided on its outside with an additional cover 7, the ceiling 7.1 above the Ceiling 3.1 of the hangar and its side walls 7.2 are arranged outside the side walls 3.2 of the hangar.
  • the cover 7 is made of a in Fig. 1 B shown open position in which it is located directly above the hangar 3 and in which the rocket launcher 1 is free in an in Fig.
  • FIGS. 1A to 3C a conveyor 8 for the supply and discharge of rocket containers 2 'to the rocket launcher 1 and back installed.
  • This conveyor system can also be used to load the ammunition space in the hangar 3 from the outside.
  • the conveyor 8 is designed as a overhead crane, which has a transversely movable to the longitudinal direction L of the hangar frame 8.1, in which telescopically arranged and guided in the longitudinal direction L from the hangar boom 3 8.2 is guided, the only indicated hoists 8.3 for receiving the rocket container. 2 wearing.
  • the rocket launcher 1 facing the front wall 3.3 of the hangar 3 has an opening 3.31, through which the rocket container 2 by means of the conveyor 8 are fed to the rocket launcher 1. When launching the rockets, the opening 3.31 can be closed in a manner not specifically shown to prevent the entry of smoke and gases into the hangar.
  • the training and storage of the rocket launcher 1 is particularly in the FIGS. 4 A to 7 shown in more detail.
  • the rocket launcher 1 is arranged on a rigid cradle 4, which is mounted via a trunnion bearing 5.4 in elevation pivotally mounted in a cradle receptacle, which is generally designated by reference numeral 5 and two the trunnion bearing 5.4 receiving side walls 5.1 and 5.2, on a Base plate 5.3 are arranged.
  • the base plate 5.3 is pivotally mounted in azimuth on a base 6 via a not shown in more detail pivot bearing, which has a shock-damping device 10 (FIG. Fig. 1 A) firmly connected to the ship's deck D.
  • the movement of the rocket launcher 1 in elevation takes place by means of a known directional drive, not shown in detail, the output pinion of which engages in a rack 9 arranged on the cradle 4 and running on a circular arc around the lug axis ( Fig. 6 and 7 ).
  • baffle 5.5 is arranged.
  • the exhaust jet and flying parts such as cap are to be derived at the rocket launch on the ship's deck.
  • the baffle 5.5 is formed concave curved at least in some areas from above and in the launching direction, so that the exhaust gas jet is diverted substantially in a direction parallel to the ship's deck D.
  • Fig. 5 shows the rocket launcher 1 in a rest position in which it is in a lashing position.
  • the lashing takes place at the lashing points 11 arranged on both sides.
  • Fig. 6 shows the rocket launcher 1 in the firing position, in which a maximum elevation of 70 ° can be achieved.
  • 5 rooms for receiving electronic devices can be integrated into the cradle 4 and / or the weighing receptacle.
  • the loading and activation of the rocket launcher 1 can take place in a protected environment, ie with the cover 7 closed. Due to the special design of the conveyor short Nachladeinterle the rocket launcher can be achieved.
  • the entire construction can be designed according to maritime aspects with regard to corrosion and radar tracking.
  • the rocket containers 2 are permanently fixed within the hangar during the loading process.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
  • Warehouses Or Storage Devices (AREA)
EP08008658A 2007-05-12 2008-05-08 Installation d'arme pour un bateau Withdrawn EP1992901A3 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102007022343A DE102007022343A1 (de) 2007-05-12 2007-05-12 Waffenanlage für ein Schiff

Publications (2)

Publication Number Publication Date
EP1992901A2 true EP1992901A2 (fr) 2008-11-19
EP1992901A3 EP1992901A3 (fr) 2012-01-04

Family

ID=39645257

Family Applications (1)

Application Number Title Priority Date Filing Date
EP08008658A Withdrawn EP1992901A3 (fr) 2007-05-12 2008-05-08 Installation d'arme pour un bateau

Country Status (2)

Country Link
EP (1) EP1992901A3 (fr)
DE (1) DE102007022343A1 (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2974059A1 (fr) * 2011-04-15 2012-10-19 Joseph Pierre Ursulet Fregate et vedettes rapides equipees de gouvernails lateraux specifiques, fixes et a geometries variables, de tubes lances torpilles avant arriere sans la ligne de flottaison, d'armes offensives et defensives sous cloches
ITTO20110455A1 (it) * 2011-05-25 2012-11-26 Oto Melara Spa Assieme di torretta e arma a bassa riflessione radar.
FR3139193A1 (fr) * 2022-08-30 2024-03-01 Naval Group Système modulaire et polyvalent de lancement de munitions et plateforme navale comportant au moins un tel système
EP4715315A1 (fr) * 2024-09-19 2026-03-25 Rheinmetall Air Defence AG Véhicule militaire

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE202009007415U1 (de) 2009-05-25 2010-08-26 Rheinmetall Waffe Munition Gmbh Modularer Waffenträger
DE102010016542C5 (de) * 2010-04-20 2017-08-17 Krauss-Maffei Wegmann Gmbh & Co. Kg Vorrichtung und Verfahren zum Richten eines Abschussbehälters

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2906457A1 (de) * 1979-02-20 1980-08-21 Steinbock Gmbh Einrichtung zur bildung und handhabung von sammellasten
EP1186848A1 (fr) 2000-09-12 2002-03-13 Krauss-Maffei Wegmann GmbH & Co. KG Véhicule de combat avec lanceur de missiles

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2985072A (en) * 1953-10-07 1961-05-23 Robert E Carlberg Missile launching system
US3166975A (en) * 1958-10-22 1965-01-26 Landstrom Sven Missile launching system
US3044362A (en) * 1958-12-29 1962-07-17 Robert E Carlberg Below deck shipboard missile launching system
US3371639A (en) * 1966-11-29 1968-03-05 Gen Dynamics Corp Podule assembly method for ships
DE19726242C2 (de) * 1997-06-20 2000-07-13 Stn Atlas Elektronik Gmbh Munitioniereinrichtung
JP2004314868A (ja) * 2003-04-18 2004-11-11 Ihi Aerospace Co Ltd 艦船用ランチャ

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2906457A1 (de) * 1979-02-20 1980-08-21 Steinbock Gmbh Einrichtung zur bildung und handhabung von sammellasten
EP1186848A1 (fr) 2000-09-12 2002-03-13 Krauss-Maffei Wegmann GmbH & Co. KG Véhicule de combat avec lanceur de missiles

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2974059A1 (fr) * 2011-04-15 2012-10-19 Joseph Pierre Ursulet Fregate et vedettes rapides equipees de gouvernails lateraux specifiques, fixes et a geometries variables, de tubes lances torpilles avant arriere sans la ligne de flottaison, d'armes offensives et defensives sous cloches
ITTO20110455A1 (it) * 2011-05-25 2012-11-26 Oto Melara Spa Assieme di torretta e arma a bassa riflessione radar.
WO2013050834A1 (fr) * 2011-05-25 2013-04-11 Oto Melara S.P.A. Ensemble de tourelle et d'arme à faible degré de réflexion des ondes radar
CN103765155A (zh) * 2011-05-25 2014-04-30 奥图马股份公司 炮塔和低雷达反射武器组件
US9080828B2 (en) 2011-05-25 2015-07-14 Oto Melara S.P.A. Assembly of turret and low radar reflection weapon
FR3139193A1 (fr) * 2022-08-30 2024-03-01 Naval Group Système modulaire et polyvalent de lancement de munitions et plateforme navale comportant au moins un tel système
WO2024047051A1 (fr) * 2022-08-30 2024-03-07 Naval Group Système modulaire et polyvalent de lancement de munitions et plateforme navale comportant au moins un tel système
EP4715315A1 (fr) * 2024-09-19 2026-03-25 Rheinmetall Air Defence AG Véhicule militaire

Also Published As

Publication number Publication date
EP1992901A3 (fr) 2012-01-04
DE102007022343A1 (de) 2008-11-13

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