EP1887306B1 - Waffenanlage - Google Patents

Waffenanlage Download PDF

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Publication number
EP1887306B1
EP1887306B1 EP07014035A EP07014035A EP1887306B1 EP 1887306 B1 EP1887306 B1 EP 1887306B1 EP 07014035 A EP07014035 A EP 07014035A EP 07014035 A EP07014035 A EP 07014035A EP 1887306 B1 EP1887306 B1 EP 1887306B1
Authority
EP
European Patent Office
Prior art keywords
ammunition
rocket
accordance
weapons system
carriages
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.)
Not-in-force
Application number
EP07014035A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP1887306A3 (de
EP1887306A2 (de
Inventor
Heinrich Heldmann
Siegfried Süss
Georg Scheidemann
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.)
Krauss Maffei Wegmann 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 EP1887306A2 publication Critical patent/EP1887306A2/de
Publication of EP1887306A3 publication Critical patent/EP1887306A3/de
Application granted granted Critical
Publication of EP1887306B1 publication Critical patent/EP1887306B1/de
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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
    • F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
    • F41A9/87—Ammunition handling dollies or transfer carts
    • 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
    • F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
    • F41A9/01—Feeding of unbelted ammunition
    • F41A9/06—Feeding of unbelted ammunition using cyclically moving conveyors, i.e. conveyors having ammunition pusher or carrier elements which are emptied or disengaged from the ammunition during the return stroke
    • F41A9/09—Movable ammunition carriers or loading trays, e.g. for feeding from magazines
    • F41A9/20—Movable ammunition carriers or loading trays, e.g. for feeding from magazines sliding, e.g. reciprocating
    • F41A9/22—Movable ammunition carriers or loading trays, e.g. for feeding from magazines sliding, e.g. reciprocating in a horizontal direction
    • 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

Definitions

  • the invention relates to a weapon system, in particular for a ship. It has a rocket launcher and an ammunition room in which the rockets are stored in rocket containers. Such systems are known per se. The stored rocket containers with the rockets are fed to the rocket launcher, which fires the charged rockets. Then the empty rocket containers must be dropped off again and new rocket containers filled with rockets must be fed to the rocket launcher. It is thus necessary an ammunition storage system, which is suitable, the full rocket container to feed the rocket launcher and pick up the empty rocket containers and store.
  • the number of missiles which can be supplied to the rocket launcher depends on the design of the rocket launcher. For example, in one known embodiment, the rocket launcher can accommodate two rocket containers each containing six rockets.
  • a well-known rocket launcher which is mounted on a land vehicle is in the EP 1 186 848 A1 described. It is also described how the rocket containers standing on the ground behind the vehicle are picked up by means of a crane and fed to the rocket launcher.
  • a basic idea of the invention is that a guide device is arranged in the ammunition space, on which at least two ammunition carriages are displaceably arranged.
  • the ammunition wagons serve to receive the rocket containers. They can be moved from a parking position into a loading position, in which the rocket container is arranged substantially below a slide-in frame of the rocket launcher.
  • an ammunition car on which a full rocket container is located, is moved from the park position to the loading position.
  • the rocket container for example by means of a lifting device such as a crane, which can attack on an eye of the rocket container, lifted from the ammunition carriage and fed to the rocket launcher.
  • the limited space can be better utilized if at least two superimposed guide devices are arranged in the ammunition space, on each of which at least two ammunition cars are arranged displaceably.
  • each guide device may be at least the length of the longest ammunition carriage on the guide device longer than the length of all ammunition carriage on the guide device together, the length of an ammunition carriage is measured in the direction of displacement.
  • At least the guiding device should be longer by the length of a rocket container than the length of all ammunition carriages on the guiding device together.
  • identical ammunition cars are used, so that each guide device is at least one ammunition cart length longer than the length of all ammunition cart on the guide device together. It can also be stored several rocket containers in a correspondingly longer ammunition cart.
  • the rocket launcher can pick up two rocket containers, in a preferred embodiment three ammunition cars can be arranged on each guide device.
  • the ammunition carriage can be arranged as a carriage on two particular straight and mutually parallel guideways slidably.
  • the ammunition trolleys may in particular have four or more rollers, by means of which they are arranged displaceably on the guide device.
  • An improved guide can also be achieved if the guideway has the shape of a U-profile in which the rollers are guided.
  • the roles in Cross section have a U-profile and rest on a track-shaped track.
  • the guideways may also be designed as roller conveyors on which sliding surfaces of the ammunition carriages rest.
  • the guide device may comprise a toothed rack, in which engages a corresponding gear of the ammunition cart, so that the ammunition carriage on the guide device can be moved manually or by motor causes.
  • the ammunition cars on a crank device by means of which they are displaceable.
  • the crank device may include a load torque lock that causes movement of the munition cart to be prevented once the crank is released. Thus, the operator and the ammunition are secured, if the crank must be released by strong ship movements.
  • the ammunition room can be arranged in a hangar on the deck of the ship behind the rocket launcher.
  • the hangar can have an opening directed towards the rocket launcher, which can be closed so that the particle beam does not enter the hangar during the firing of the rockets.
  • the hangar roof may also have an opening for emergency discharge of the rocket container, for example, if the regular lifting device is defective.
  • FIGS. 1 to 10 A possible embodiment of the invention is in the FIGS. 1 to 10 described.
  • the FIG. 1 shows a weapon system with a rocket launcher 1 in the park position on a ship deck 5 of a ship.
  • the ammunition room 2, in which the ammunition is stored, is located behind the rocket launcher 1 and is surrounded by a hangar 3.
  • the operator 7 can pass through the door 4 or the floor hatch 8 in the hangar 3.
  • the rocket launcher 1 is pivotally mounted in azimuth and elevation.
  • the swivel range 6 leads partly through the hangar 3, which is therefore a lockable during rocket launch Opening in the direction of the rocket launcher 1 has.
  • In the ammunition space 2 is configured such that a plurality of rocket containers 10 can be stored.
  • the rocket launcher 1 is designed such that it can accommodate two rocket containers 10. In FIG.
  • the FIG. 2 shows the rocket launcher 1 in two possible firing positions.
  • the firing range extends over an azimuth angle range of 20 °.
  • FIG. 3 shows the ammunition space 2 in a sectional view.
  • the ammunition room 2 six identical ammunition carriages 12 are arranged in two planes, which are configured to receive the rocket containers 10.
  • the ammunition trolley 12 each have four rollers 14, which are guided in the U-profile of the guideways 9 slidably.
  • the ammunition cart 12 have a crank device 15 which is connected to a gear 21 which engages in a toothed rack 20.
  • the ammunition cart 12 can be moved manually with the crank device 15 by the operator 7.
  • the ammunition cart 12 are by means of bolts 16, which have a handy knob 24 ( Fig. 8 ), as a locking means against accidental displacement, for example due to strong swell secured.
  • the rocket containers 10 To load the rocket launcher 1, the rocket containers 10 must be inserted into the rocket launcher 1. For this they must first by means of a in Fig. 5 shown crane 19 are lifted from the ammunition carriage 12 located in the loading position to the height of the slide-in frame 18. In FIG. 4 the raised rocket containers 10 are shown. You can be threaded in this position by the operator, which is on the ladder 17 on the work platform 11, in the insertion frame 18 of the rocket launcher 1 in the intended position.
  • the rocket launcher 1 rotates from the firing position back to the park position.
  • the rocket container 10 is lowered and placed on an empty ammunition wagon 12.
  • the ammunition cart 12 with the empty rocket container 10 is cranked to the side with the bolt 16 pulled out and then lashed again by means of the bolt 16.
  • An ammunition cart 12 with a full rocket container 10 is brought from a parking position to the loading position substantially below the drawer frame 18, so that the rocket launcher 1 can be equipped with the rocket container 10.
  • the ammunition space 2 is constructed such that all stored rocket containers 10 can be fed to the rocket launcher 1. For this reason, each guideway 9, on each of which there are three ammunition wagons 12, has a length of more than four ammunition cart lengths, so that at least one ammunition cart 12 can always be displaced at least by its own length. This ensures that the outer ammunition wagon 12 can be brought from the parking position to the loading position.
  • FIG. 5 shows the weapon system in a side view without hangar 3.
  • a arranged on the rocket launcher 1 crane 19 with a telescopic boom engages with a hook in an eyelet 23 of the rocket container 10 and lifts it from the ammunition wagon 12.
  • the rocket launcher 1 is mounted on a platform 22 which can pivot the rocket launcher 1 in elevation and azimuth.
  • FIG. 6 shows the rocket launcher 1 in a preparatory firing position.
  • a rolling window 42 is brought in front of the opening of the hangar 3.
  • weapon system is shown slightly different from the previous changed.
  • tilt-free displacement of the ammunition carriage 12 is mounted on both sides of the ammunition cart 12 arranged racks 20 ', in which engage two corresponding gears. These are connected to each other via a shaft 47, which is arranged below the ammunition cart.
  • FIG. 7 shows a section of the weapon system in plan view, in which the tooth profile of the rack 20 can be seen, in which the corresponding gears 21 of the ammunition carriage 12 engage.
  • FIG. 8 shows the running in a U-profile rollers 14 of the ammunition carriage 12.
  • the displacement is effected by means of a crank mechanism 15 which has a load-torque lock (no-back system).
  • FIG. 9 and 10 the arrangement of the weapon system is shown on a ship deck 5 of a ship, wherein the rocket launcher 1 is in the firing position or in the parking position.
  • a cover 44 is brought over the rocket launcher 1 to protect against external influences.

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)
  • Warehouses Or Storage Devices (AREA)
  • Emergency Lowering Means (AREA)
  • Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
EP07014035A 2006-08-10 2007-07-18 Waffenanlage Not-in-force EP1887306B1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102006037337A DE102006037337A1 (de) 2006-08-10 2006-08-10 Waffenanlage

Publications (3)

Publication Number Publication Date
EP1887306A2 EP1887306A2 (de) 2008-02-13
EP1887306A3 EP1887306A3 (de) 2010-02-24
EP1887306B1 true EP1887306B1 (de) 2011-09-14

Family

ID=38508814

Family Applications (1)

Application Number Title Priority Date Filing Date
EP07014035A Not-in-force EP1887306B1 (de) 2006-08-10 2007-07-18 Waffenanlage

Country Status (5)

Country Link
US (1) US7878101B2 (es)
EP (1) EP1887306B1 (es)
AT (1) ATE524703T1 (es)
DE (1) DE102006037337A1 (es)
ES (1) ES2372112T3 (es)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006037337A1 (de) * 2006-08-10 2008-02-14 Krauss-Maffei Wegmann Gmbh & Co. Kg Waffenanlage
FR2933373B1 (fr) * 2008-07-03 2010-08-20 Dcns Principe d'integration, contre menaces asymetriques, de systemes d'armes missiles sur rampe fixe pour batiment de surface furtifs
DE102012207710B4 (de) * 2012-05-09 2014-09-25 Thyssenkrupp Marine Systems Gmbh Lagerungsvorrichtung in einem militärischen Wasserfahrzeug
FR3013031B1 (fr) * 2013-11-12 2016-08-26 Dcns Plate-forme navale equipee d'au moins un conteneur formant chargeur de roquettes
GB2538015B (en) * 2014-05-02 2017-07-26 Babcock Ip Man (Number One) Ltd Marine vessel magazine, marine vessel and method of operating the same
KR101592292B1 (ko) * 2014-06-12 2016-02-05 국방과학연구소 탄약 이송장치 및 그 작동방법
US9766030B2 (en) * 2015-02-23 2017-09-19 United Arab Emirates University Automatic firing apparatus and method
GB2551455B (en) * 2015-10-22 2020-02-19 Babcock Ip Man Number One Limited Munitions container, marine vessel magazine, marine vessel and method of operating the same
GB2543557B (en) * 2015-10-22 2020-04-15 Babcock Ip Man Number One Limited Marine vessel magazine, marine vessel and method of operating the same
FR3055305B1 (fr) * 2016-09-01 2019-08-23 Dcns Entrepot modulable de stockage et de manutention notamment d'armes et navire comportant un tel entrepot
RU2699327C1 (ru) * 2018-07-02 2019-09-04 Федеральное государственное казённое военное образовательное учреждение высшего образования "Военная академия материально-технического обеспечения имени генерала армии А.В. Хрулёва" Автоматизированный контейнер-стеллаж для перевозки и перезаряжания реактивных снарядов реактивных систем залпового огня "Град" и "Торнадо-Г" на шасси УРАЛ 4320-1911-40

Citations (1)

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Also Published As

Publication number Publication date
US7878101B2 (en) 2011-02-01
ES2372112T3 (es) 2012-01-16
EP1887306A3 (de) 2010-02-24
US20080156182A1 (en) 2008-07-03
EP1887306A2 (de) 2008-02-13
ATE524703T1 (de) 2011-09-15
DE102006037337A1 (de) 2008-02-14

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