EP2381204A2 - Dispositif et procédé de pointage d'un conteneur lanceur de missiles - Google Patents

Dispositif et procédé de pointage d'un conteneur lanceur de missiles Download PDF

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Publication number
EP2381204A2
EP2381204A2 EP11162702A EP11162702A EP2381204A2 EP 2381204 A2 EP2381204 A2 EP 2381204A2 EP 11162702 A EP11162702 A EP 11162702A EP 11162702 A EP11162702 A EP 11162702A EP 2381204 A2 EP2381204 A2 EP 2381204A2
Authority
EP
European Patent Office
Prior art keywords
straightening
receptacle
straightening device
container
platform
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Withdrawn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
EP11162702A
Other languages
German (de)
English (en)
Other versions
EP2381204A3 (fr
Inventor
Georg Scheidemann
Siegfried Suess
Alexander Simon
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=44064963&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=EP2381204(A2) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Krauss Maffei Wegmann GmbH and Co KG filed Critical Krauss Maffei Wegmann GmbH and Co KG
Publication of EP2381204A2 publication Critical patent/EP2381204A2/fr
Publication of EP2381204A3 publication Critical patent/EP2381204A3/fr
Withdrawn legal-status Critical Current

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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
    • F41A27/00—Gun mountings permitting traversing or elevating movement, e.g. gun carriages
    • F41A27/06—Mechanical systems
    • F41A27/24—Elevating gear
    • 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
    • F41A23/02—Mountings without wheels
    • 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
    • F41A23/02—Mountings without wheels
    • F41A23/12—Tripods ; Mountings having at least three legs
    • F41A23/14—Tripods ; Mountings having at least three legs adjustable
    • 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
    • F41A23/34—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles on wheeled or endless-track vehicles
    • F41A23/42—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles on wheeled or endless-track vehicles for rocket throwers
    • 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
    • F41A23/56—Arrangements for adjusting the gun platform in the vertical or horizontal position
    • F41A23/58—Hydraulic jacks
    • 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

Definitions

  • the invention relates to an apparatus and a method for directing a launching container, in particular rocket launching container, with a directional elevation part which can be directed about an elevation axis and which has a receptacle for receiving one or more launching containers.
  • launchers for firing military launcher or launcher straightening devices which give the launching bodies, for example, several missiles to be fired, a defined launch direction for the subsequent trajectory.
  • Such straightening devices usually have a height-straightening part that can be directed around a substantially horizontally extending elevation axis.
  • the launching container provided with the launching bodies is accommodated on the height-rectifying part, in which, for example, a plurality of rockets can be arranged.
  • the elevation axis is often located in the rear end of the invokenrichtteils or arranged on the elevating part firing container to keep the impact of the launching device through the exhaust jet in the raised firing position as low as possible. Due to the arrangement of the elevation axis, which is located far to the rear, however, comparatively large directional moments result, in particular when the firing container is directed from a horizontal position into a firing position, for example, at an angle of 70 ° relative to the horizontal.
  • the object of the present invention is to specify an apparatus and a method for aligning a launching container, in which the directional moments to be overcome via the elevation directional drive are reduced without having to accept any impairment of the launching device by the exhaust gas jet.
  • This object is achieved in a device of the aforementioned type in that the receptacle with respect to the elevation axis is arranged to be movable.
  • the receptacle is arranged to be movable by means of a drive, in particular a motor drive, relative to the elevation axis.
  • a drive in particular a motor drive
  • the drive is an electric motor drive is used.
  • the center of gravity of the ierenrichtbaren mass in the direction of the elevation axis is movable.
  • the center of gravity of the euxnrichtbaren mass consisting of elevation member and shotgun thereon including the stored therein shotgun, the directional moments for the straightening process can be reduced.
  • the center of gravity of the euxnrichtbaren mass In a transport position with horizontally aligned launching container the center of gravity of the euxnrichtbaren mass can be moved advantageously in an area over the elevation axis, resulting in the subsequent straightening in elevation low directional moments.
  • the elevation direction part next to the movable receptacle has a bearing part.
  • the receptacle is arranged to be movable relative to the bearing part.
  • the recording can be configured as a carriage, telescopic rail, extension or the like.
  • the straightening device has a side straightening part which can be directed about an azimuth axis and on which the height-straightening part is arranged.
  • the side-facing part is alignable about the substantially vertical axis of azimuth and preferably at its upper end the elevation direction part about the elevation axis pivotally.
  • this can be directed via an electromotive drive.
  • An advantage is an embodiment, according to which the elevation-straightening part and the side-facing part are designed to be hydraulically free directionable. Due to the hydraulic-free design of height-straightening and side straightening the risk of flame of the hydraulic fluid is reduced especially when rockets are fired with high-temperature exhaust gases.
  • the page-directing part is arranged on a platform.
  • the platform can be received via suitable interfaces of corresponding transport or emergency vehicles.
  • a further embodiment provides that the side-facing part is arranged on the platform such that the receptacle and a launching container to be arranged thereon in a transport position do not protrude laterally beyond the contour of the platform, resulting in advantageous loading dimensions.
  • the side-facing part is arranged on the platform in such a way that the receptacle and a firing container to be arranged on it protrude laterally at least partially beyond the contour of the platform in an elevating firing position. Due to this lateral projection, the exhaust jet resulting at the rocket launch can be guided laterally past the platform.
  • the elevation axis is arranged in the region of the one end of the elevation directing part.
  • a support for supporting the nrichtteils is arranged in a transport position.
  • the support can be arranged on the platform.
  • the launching container or the height-adjusting part can rest with their underside on an upper side of the support.
  • a favorable design with regard to a secure transport of the straightening device provides that the height-straightening part can be secured by lashing means in a transport position.
  • the lashing means are arranged in the region of the support.
  • a storage space for the stowage of objects and / or for the accommodation of electronic components is arranged on the platform.
  • the functionality of the straightening device is extended.
  • the straightening device can be transported as a module and put into operation on site with just a few simple steps.
  • the straightening device has a covering hood for covering the height-rectifying part as well as the side-facing part, including a firing container accommodated in the device. Under the cover, the corresponding components are protected from external influences.
  • the cover and / or the storage space are designed such that there is a stackable outer contour.
  • the outer contour advantageously has the dimensions of standardized standard containers.
  • connecting elements may be provided in the corner regions of the cover and / or the storage space.
  • the connecting elements can be standardized connecting elements, so that not only a plurality of straightening devices can be stacked with one another, but they can also be stacked together with other standard containers.
  • the straightening device has a remote control unit via which the height-adjusting part and the side straightening part can be aligned.
  • the remote control unit may be located a greater distance from the straightening device and connected to the straightening device via a cable connection or wireless connection, in particular with the straightening drives, electronics, etc.
  • the remote control unit may also be located inside a host vehicle, such as a ballistically protected truck cab be arranged on the loading surface, the corresponding straightening device is located.
  • the straightening device has supports for support against the ground.
  • a carrier vehicle can drive by lowering its chassis, for example by venting corresponding bellows, under the straightening device and record them by subsequent venting of the bellows. The transfer from a transport to a protected running carrier vehicle can be carried out accordingly.
  • the supports are telescopic in the vertical and / or lateral direction.
  • lateral telescoping occurring during launch of the rockets firing reaction forces can be derived in a favorable manner. This may be particularly advantageous if the launching container has a comparatively low elevation relative to a carrier vehicle, which can result in comparatively large transverse forces at rocket launch.
  • the center of gravity of the ierenrichtbaren mass is shifted in the directional position in the region of the elevation axis. This results in straightening the ierenrichtbaren mass comparatively small directional moments.
  • the receptacle is first moved in a substantially horizontal position and then returned to the raised position. It is also possible to process the recording during the elevation, whereby constant Richtmomente can be achieved.
  • Fig. 1 shown is a perspective view of a straightening device 1.
  • the straightening device 1 is equipped with a launching container 2.
  • the launching container 2 is a multiple launching container, which is equipped with a number of in the embodiment a total of six launchers 3.
  • the launching bodies 3 are rockets provided with their own drive.
  • the straightening device 1 has a height-adjusting part 4.
  • Thecollectnrichtteit 4 is of elongated geometry.
  • the elevational element 4 is mounted so as to be capable of being directed in a side facing part 6 around an elevation axis E extending substantially horizontally.
  • the side-facing member 6 is rotatably mounted on a platform 7 about a substantially vertical azimuth axis A. The aiming of the launching container 2 both about the elevation axis E and about the azimuth axis A by means of electric motor drives.
  • the elevation axis E is arranged in the rear end region of the ierenrichtbaren mass of the straightening device 1, unfavorable leverage between the elevation axis E and the center of gravity S of formerly large straightening moment.
  • the launching container 2 is arranged on a receptacle 4.1 which is translationally movable relative to the elevation axis E, as will be discussed in more detail below.
  • FIG. 1 shows a transport position of the straightening device 1, in which the elevation direction part 4 and arranged on this launching container 2 are in a substantially horizontal and so far compact transport position.
  • the side facing part 6, as well as the height-adjusting part 4, including the shooting container 2 accommodated on the height-adjusting part 4 can be covered by a covering hood 11, cf. also Fig. 3 , Together with a storage space 8 results in a cubic and stackable contour of the device 1.
  • Several straightening devices 1 can be stacked like transport containers one above the other and next to each other for transport purposes. In this context, it is advantageous if the corners of the container-shaped storage space 8 and the cover 11 with standardized fastening means are provided, so that a stacking with standard containers is possible.
  • the storage space 8 are electronic elements for operating the straightening device 1 as well as other objects, such as tools and the like, housed.
  • Fig. 2 illustrated is an embodiment of the straightening device 1, in which two launching containers 2 are arranged side by side on the elevation direction part 4.
  • the launching device 1 can be received on a carrier vehicle or a ballistic protected emergency vehicle.
  • the launcher 1 is provided in its corner areas with supports 9, via which the straightening device 1 is supported relative to the ground.
  • a carrier vehicle can travel into the space below the platform 7, receive the straightening device 1 and drive to the place of use.
  • the supports 9 are telescopically formed both in the vertical direction and in the horizontal direction. Due to the vertical telescoping of the supports 9 a secure stand is guaranteed even in different soil conditions. Due to the lateral telescoping results in a favorable power dissipation during firing of the launching body. 3
  • Fig. 4 an embodiment is shown in which the straightening device 1 is stationary and arranged on a base 12.
  • the straightening device 1 can be operated remotely via a remote control unit 13.
  • the remote control unit 13 can be arranged inside the protected emergency vehicle, so that the vehicle crew does not have to leave the vehicle interior protected against military threats for directing the launching container 2.
  • Fig. 5a shows one of the illustration in Fig. 1 In this, the launching container 2 and with this the elevation direction part 4 in an approximately horizontal position above the platform 7.
  • the arrangement of the side directing part 6 on the platform 7 is chosen such that the side facing part 6, the elevation part 4 and the launching container 2 do not protrude laterally beyond the contour of the platform 7.
  • the launching container 2 is arranged in a receptacle 4.1, via which the launching container 2 and with this the center of gravity S of the formerlyrichtbaren mass in a direction transverse to the elevation axis E can be, see. Fig. 5b ,
  • the accommodatenrichtteil 4 a translationally non-movable bearing part 4.2, on which the receptacle 4.1 is arranged to be translationally movable.
  • the top of the receptacle 4.1 serves to receive the firing container 2.
  • the receptacle 4.1 is compared to the bearing part 4.2 translationally movable.
  • the movements of the receptacle 4.1 relative to the bearing part 4.2 are guided in guide rails of the bearing part 4.2, as shown in particular in the illustration Fig. 7 lets recognize.
  • an electric motor drive 5 is arranged below the receptacle 4.1, which engages with a pinion in a rack segment 14 of the receptacle 4.1 and the recording moves when energized in one or the other direction.
  • the launching container 2 can be directed about the azimuth axis A on the side facing part 6.
  • the straightening device described above and the associated straightening method are characterized by the use of comparatively small dimensioned elevation drives. Additional hydraulic straightening means are not required.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Tunnel Furnaces (AREA)
  • Furnace Charging Or Discharging (AREA)
  • Toys (AREA)
EP11162702.2A 2010-04-20 2011-04-15 Dispositif et procédé de pointage d'un conteneur lanceur de missiles Withdrawn EP2381204A3 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102010016542.5A DE102010016542C5 (de) 2010-04-20 2010-04-20 Vorrichtung und Verfahren zum Richten eines Abschussbehälters

Publications (2)

Publication Number Publication Date
EP2381204A2 true EP2381204A2 (fr) 2011-10-26
EP2381204A3 EP2381204A3 (fr) 2014-06-11

Family

ID=44064963

Family Applications (1)

Application Number Title Priority Date Filing Date
EP11162702.2A Withdrawn EP2381204A3 (fr) 2010-04-20 2011-04-15 Dispositif et procédé de pointage d'un conteneur lanceur de missiles

Country Status (2)

Country Link
EP (1) EP2381204A3 (fr)
DE (1) DE102010016542C5 (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104776754A (zh) * 2015-04-15 2015-07-15 北京航天发射技术研究所 一种火箭发射平台的8支点调平方法
EP2746715A3 (fr) * 2012-12-22 2016-07-20 Diehl BGT Defence GmbH & Co.KG Conteneur pour missile
EP2746714B1 (fr) * 2012-12-22 2017-09-06 Diehl Defence GmbH & Co. KG Conteneur pour missile
WO2019033182A1 (fr) * 2017-08-17 2019-02-21 Mac Jee Indústria Comério E Representação Comercial Ltda. Module de lancement de fusées et véhicule de lancement de fusées

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102013100392A1 (de) 2013-01-15 2014-07-17 Krauss-Maffei Wegmann Gmbh & Co. Kg Vorrichtung und Verfahren zum Richten eines Raketenabschussbehälters
WO2020093115A1 (fr) * 2018-11-09 2020-05-14 Mac Jee Indústria De Defesa Ltda. Système de ravitaillement pour véhicule de lancement de fusées
CN114777568B (zh) * 2022-05-09 2023-09-29 鲁东大学 一种四集装箱式海上发射火箭起竖装置及起竖方法

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DE4014194A1 (de) * 1990-05-03 1991-11-07 Messerschmitt Boelkow Blohm Flugkoerper-startanlage
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FR2852385B1 (fr) * 2003-03-13 2005-06-03 Giat Ind Sa Tourelleau multitube pour munition a haute energie
DE102004060779A1 (de) * 2004-12-17 2006-06-29 Krauss-Maffei Wegmann Gmbh & Co. Kg Kampffahrzeug mit Flugabwehrsystem
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IL169481A (en) * 2005-06-30 2011-11-30 Rafael Advanced Defense Sys Leads to a missile launcher
DE102007022343A1 (de) * 2007-05-12 2008-11-13 Krauss-Maffei Wegmann Gmbh & Co. Kg Waffenanlage für ein Schiff

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2746715A3 (fr) * 2012-12-22 2016-07-20 Diehl BGT Defence GmbH & Co.KG Conteneur pour missile
EP2746714B1 (fr) * 2012-12-22 2017-09-06 Diehl Defence GmbH & Co. KG Conteneur pour missile
EP2746715B1 (fr) 2012-12-22 2017-09-06 Diehl Defence GmbH & Co. KG Conteneur pour missile
CN104776754A (zh) * 2015-04-15 2015-07-15 北京航天发射技术研究所 一种火箭发射平台的8支点调平方法
CN104776754B (zh) * 2015-04-15 2016-05-18 北京航天发射技术研究所 一种火箭发射平台的8支点调平方法
WO2019033182A1 (fr) * 2017-08-17 2019-02-21 Mac Jee Indústria Comério E Representação Comercial Ltda. Module de lancement de fusées et véhicule de lancement de fusées
US11131521B2 (en) 2017-08-17 2021-09-28 Mac Jee Industria De Defesa Ltda. Rocket launch module and rocket launch vehicle

Also Published As

Publication number Publication date
DE102010016542A1 (de) 2011-10-20
DE102010016542B4 (de) 2013-01-03
EP2381204A3 (fr) 2014-06-11
DE102010016542C5 (de) 2017-08-17

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