EP0664431A2 - Véhicule de combat et son système de transport destiné à son embarquement dans un avion de transport - Google Patents

Véhicule de combat et son système de transport destiné à son embarquement dans un avion de transport Download PDF

Info

Publication number: EP0664431A2
Authority: EP; European Patent Office
Prior art keywords: frame; launcher; transport; vehicle; lifting
Prior art date: 1994-01-20
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.): Granted

Application number

EP94107517A

Other languages

German (de)

English (en)

Other versions

EP0664431B1 (fr

EP0664431A3 (fr

Inventor

Rüdiger Dipl.-Ing. Baus

Reiner Linge

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.)

Wegmann and Co GmbH

Original Assignee

Wegmann and Co 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.)

1994-01-20

Filing date

1994-05-14

Publication date

1995-07-26

1994-05-14 Application filed by Wegmann and Co GmbH filed Critical Wegmann and Co GmbH

1995-07-26 Publication of EP0664431A2 publication Critical patent/EP0664431A2/fr

1996-01-10 Publication of EP0664431A3 publication Critical patent/EP0664431A3/fr

1998-08-05 Application granted granted Critical

1998-08-05 Publication of EP0664431B1 publication Critical patent/EP0664431B1/fr

2014-05-14 Anticipated expiration legal-status Critical

Status Expired - Lifetime legal-status Critical Current

Links

Images

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
- 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

Definitions

the invention relates to a combat vehicle with the features from the preamble of claim 1 and a transport system for loading it into transport aircraft.
a problem with such combat vehicles is that the total weight of the vehicle and the launching device for artillery missiles arranged on it is so great that it is loaded into one of the usual transport aircraft used for such purposes in order to bring the combat vehicle to a far-away area of application , is not possible due to weight reasons.
the invention has for its object to design a combat vehicle of the type specified in the preamble of claim 1 in a special way and to create a transport system adapted to this configuration, with which not only a favorable weight distribution between vehicle and launcher is achieved during loading, but with a particularly simple loading of the launcher is also possible.
the design and the transport system are intended to ensure that no readjustment of the overall system for pivoting the launcher is necessary when reassembling on site.
a basic idea of the invention consists in the special arrangement of the interface between combat vehicle and launcher. It is not, as in known proposals, only the launcher frame of the launcher removed, but the entire launcher including the upper carriage, intermediate frame with slewing ring, and including the entire lifting system for pivoting the launcher.
This interface is laid out in such a way that it can be opened by locking devices which can be operated from the outside of the vehicle, so that only the separation of electrical plug-in devices is added if necessary and then the entire launching device can be lifted off the vehicle underframe.
the transport system is adapted to this configuration of the combat vehicle, the most important element of which is a mobile transport frame, as is used, for example, for transporting and loading containers.
This transport frame is so according to the further invention adapted to the special problems when lifting the launcher from the vehicle base and when transporting the launcher to a transport plane and when loading the transport frame together with the launcher into the transport plane, that the entire loading process is considerably simplified.
FIG. 1 and 2 show a combat vehicle with a vehicle undercarriage 1, on which a driver's cab 2 is arranged, and a launching device for artillery missiles, which has a launcher frame 3 for receiving the missiles.
the launcher frame 3 is pivotally mounted in elevation on an upper carriage 4, which is mounted on the vehicle underframe 1 via an intermediate frame 6 (visible in FIG. 6) and a slewing ring 7 in azimuth.
the pivoting movement in elevation is brought about by electrically driven lifting spindles 5 arranged between the upper mount 4 and the launcher frame 3.
the launcher with the launcher frame 3 and including the upper mount 4, the intermediate frame 6 and the turntable 7 is designed as an independent unit which is only coupled to the vehicle undercarriage 1 via locking devices which can be operated from the outside of the vehicle and, if appropriate, via electrical plug-in devices. It is therefore possible, after loosening the locking devices and possibly the plug-in devices, to lift the entire firing device off the vehicle underframe 1 with suitable means and to load it individually into a transport aircraft. After the launcher has been lifted off, the remaining combat vehicle can also be loaded onto another transport aircraft.
FIGS. 1A to 1F An embodiment of a locking device for coupling the launching device to the vehicle underframe is explained below with reference to FIGS. 1A to 1F.
a locking device designated overall by reference number 20 in FIG. 1B, is arranged on the vehicle underframe 1 and can be operated from the outside of the vehicle via a hand crank 20.11.
This locking device 20 is shown in more detail in FIGS. 1C and 1D. It has a total of 4 claws 20.1, 20.2, 20.3 and 20.4 designed as circular ring sections.
the claws 20.1 and 20.3 and the claws 20.2 and 20.4 are each connected to one another via a connecting piece 20.5.
the connecting pieces 20.5 are each guided via bolt guides 20.51 in elongated holes in the direction of the double arrow R, which corresponds to the longitudinal direction of the vehicle, towards and away from one another.
the locking between the firing device and the vehicle undercarriage takes place in such a way that the claws 20.1 to 20.4 on the one hand an annular flange 7.1 on the underside of the swivel headwheel when the firing device 3 is attached to the support undercarriage 1 connected to the vehicle underframe 1 7 and on the other hand comprise an annular flange 21.1 on the upper side of the support ring 21.
the locked position is shown. If the claw 20.4 shown in FIG. 1D moves from the position shown in the direction of the arrow R 'and accordingly the other claws 20.1, 20.2 and 20.3, the lock is released and the launcher 3 can be lifted upwards.
the means for loading the launcher and the method for loading are described in more detail below with reference to FIGS. 3 to 9.
the launcher is lifted off the vehicle underframe 1 and loaded into the transport plane by means of a transport frame 8, which is shown in the unloaded state in FIGS. 3, 4 and 9 and in the loaded state in FIGS. 5 to 8.
the transport frame 8 is designed as a statically determined spatial structure and has an upper frame with a cross member 9.1 arranged at the rear and one in the middle of the cross member 9.1 Articulated side members 9.2 with a side member extension 9.3.
the cross member 9.1 is supported by vertical supports 9.4 and 9.5 on two support arms 13.1 and 13.2, each of which can be raised and lowered on one of two lifting supports 10.1 and 10.2, which is described in more detail below.
the front end of the longitudinal beam 9.2 or the longitudinal beam extension 9.3 is supported via a vertical support 9.6 on a support arm 13.3 which is guided on a third lifting support 10.3 and can be raised and lowered.
the transport frame also has a subframe suspended from the vertical supports 9.4, 9.5 and 9.6 with two side members 9.7 and 9.8, two cross members 9.9 and 9.10, the rear end of the subframe being suspended via the cross member 9.9, while its front end is connected via connecting members 9.11 and 9.12 is connected to the vertical support 9.6 arranged at the center of the bow.
the upper and lower frames can be handled and broken down into individual parts by two operators by being constructed, as indicated in the drawings, from detachably connected longitudinal and transverse beams or connecting beams.
Each of the lifting props 10.1, 10.2 and 10.3 has a pair of wheels 11 which can be pivoted and braked about a vertical axis and a vertical column 12, at the lower end of which the pairs of wheels 11 are arranged.
a rack 12.1 is attached to the column 12, in which, in a manner not shown, at least one pinion engages, which is part of a reduction gear 14.1, 14.2, 14.3 arranged on or in the support arm 13.1, 13.2 and 13.3.
the input elements of the reduction gears are connected to a drive device.
the drive devices are shown as a hand crank 15.1, 15.2 and 15.3.
the reduction gears 14.1 and 14.2 are connected to one another at the rear end of the transport frame via a flexible shaft 16 such that they can each be driven synchronously from one of the two hand cranks 15.1 or 15.2.
the reduction gear 14.3 arranged at the front end of the transport frame on the support arm 13.3 can be connected via a flexible shaft (not shown) to one of the rear reduction gears 14.1 or 14.2 such that all three gears can be driven synchronously from a hand crank.
electric servomotors instead of the hand cranks for driving.
the starting point of the loading process is an adjustment of the transport frame 8 as shown in FIG. 9.
the pairs of wheels are in this position 11, which are arranged via a pivot bearing 11.1 at the lower end of the vertical columns 12 of the lifting supports 10.1, 10.2 and 10.3, rotated by 90 °, so that the transport frame can be moved transversely to its longitudinal direction. Furthermore, one side member 9.7 of the lower frame is removed. In this configuration and position, the transport frame 8, as can be seen from FIGS.
launching device 1 and 9 can be moved in the transverse direction from behind to the combat vehicle and can drive over it in the area of the launcher frame 3 if the launcher frame 3 of the launcher at elevation 0 ° is pivoted in azimuth to a position of 90 ° between the longitudinal direction of the vehicle and the direction of launch.
This position is shown in Fig. 1 and arises from the position shown in FIG. 2 by lowering the launcher frame 3.
the launcher frame 3 of the launcher is on its top via fasteners 18.1, 18.2 and 18.3 in a three-point suspension on Upper frame of the transport frame 8 attached.
the entire launching device is separated from the vehicle underframe 1 by unlocking the locking device 20 as described above and, if necessary, releasing electrical plug connections.
the longitudinal member 9.7 is now inserted again into the subframe of the transport frame 8.
the lower frame serves to support the parts of the launcher arranged below the launcher frame 3, in that the upper mount 4 is fastened to the longitudinal members 9.7 and 9.8 of the lower frame via bolts 19.
the launcher frame 3 with the remaining parts of the launching device is lifted from the vehicle underframe 1 until it is completely separated. Then the vehicle underframe 1 can be removed by moving the combat vehicle forward.
the drive devices with reduction gears 14.1 to 14.3 on the lifting supports 10.1 to 10.3 the transport frame 8 and with it the launching device is lowered into a driving position, the pairs of wheels 11 also being pivoted back into a position in which the transport frame is moved in the longitudinal direction can be locked in this position.
the transport frame is then moved away and steered in the manner of a tricycle via a drawbar 17 arranged at the front end.
the transport frame 8 can be moved together with the launcher to a transport aircraft, not shown, and loaded into the transport aircraft via a known, appropriately designed access ramp, set down and lashed there.
the vehicle underframe 1 of the combat vehicle is then loaded into another transport aircraft in a manner not described in more detail and known per se.

Landscapes

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

EP94107517A 1994-01-20 1994-05-14 Véhicule de combat et son système de transport destiné à son embarquement dans un avion de transport Expired - Lifetime EP0664431B1 (fr)

Applications Claiming Priority (2)

Application Number	Priority Date	Filing Date	Title
DE4401587		1994-01-20
DE4401587A DE4401587A1 (de)	1994-01-20	1994-01-20	Kampffahrzeug sowie Transportsystem zu seiner Verladung in Transportflugzeuge

Publications (3)

Publication Number	Publication Date
EP0664431A2 true EP0664431A2 (fr)	1995-07-26
EP0664431A3 EP0664431A3 (fr)	1996-01-10
EP0664431B1 EP0664431B1 (fr)	1998-08-05

Family

ID=6508322

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
EP94107517A Expired - Lifetime EP0664431B1 (fr)	1994-01-20	1994-05-14	Véhicule de combat et son système de transport destiné à son embarquement dans un avion de transport

Country Status (3)

Country	Link
US (1)	US5461961A (fr)
EP (1)	EP0664431B1 (fr)
DE (2)	DE4401587A1 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
EP1400773A3 (fr) *	2002-09-23	2004-03-31	Krauss-Maffei Wegmann GmbH & Co. KG	Dispositif pour adapter un conteneur pour plusieurs roquettes à un lanceur pour roquettes d'artillerie
FR2938983A1 (fr) *	2008-11-26	2010-05-28	Nexter Systems	Dispositif permettant le desacouplement automatique des deux parties d'un connecteur.
DE102010016542A1 (de)	2010-04-20	2011-10-20	Krauss-Maffei Wegmann Gmbh & Co. Kg	Vorrichtung und Verfahren zum Richten eines Abschussbehälters

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EP1092671B1 (fr) *	1999-07-23	2005-03-02	Bivas Hydraulic Industries Limited	Chargements d'aéronefs
DE29922470U1 (de) *	1999-12-22	2001-05-03	Krauss-Maffei Wegmann GmbH & Co.KG, 80997 München	Militärisches Systemmodul, insbesondere Flugabwehrsystemmodul
DE10045051A1 (de)	2000-09-12	2002-03-21	Krauss Maffei Wegmann Gmbh & C	Kampffahrzeug mit Abschußvorrichtung für Artillerieraketen
US6742435B2 (en)	2000-10-27	2004-06-01	United Defense, L.P.	High-mobility artillery cannon system
US6584881B1 (en)	2001-03-26	2003-07-01	United Defense Lp	Multi-purpose missile launcher system for a military land vehicle
DE10117007A1 (de) *	2001-04-04	2002-10-17	Buck Neue Technologien Gmbh	Verfahren und Vorrichtung zum Schutz von mobilen militärischen Einrichtungen
EP1421327B1 (fr)	2001-08-30	2010-06-30	Krauss-Maffei Wegmann GmbH & Co. KG	Canon d'artillerie comprenant une arme lourde montee sur un vehicule de soutien
DE10144366A1 (de) *	2001-09-10	2003-03-27	Rheinmetall Landsysteme Gmbh	Container-Adapter für ein gepanzertes Transportfahrzeug
DE10144375B4 (de) *	2001-09-10	2004-02-12	Rheinmetall Landsysteme Gmbh	Ablege-Adapter für ein gepanzertes Transportfahrzeug
US6907812B1 (en) *	2003-01-21	2005-06-21	United Defense Lp	Pop-up weapon system
DE10333910A1 (de) *	2003-07-25	2005-02-10	Diehl Munitionssysteme Gmbh & Co. Kg	Artillerieraketenwerfer
DE10346001B4 (de)	2003-10-02	2006-01-26	Buck Neue Technologien Gmbh	Vorrichtung zum Schützen von Schiffen vor endphasengelenkten Flugkörpern
US6820531B1 (en) *	2003-12-01	2004-11-23	Textron Systems Corporation	Positioning system with continuous-range inclination and rotation angles
RU2243478C1 (ru) *	2004-01-08	2004-12-27	Открытое акционерное общество специального машиностроения и металлургии "Мотовилихинские заводы"	Устройство для погрузки, разгрузки и заряжания реактивного снаряда
RU2262647C1 (ru) *	2004-06-29	2005-10-20	Открытое акционерное общество "Научно-производственное предприятие "Старт"	Самоходная пусковая установка
DE102004042869A1 (de) *	2004-09-04	2006-03-23	Rheinmetall Landsysteme Gmbh	Verfahren und Vorrichtung zum Transport schwerer Fahrzeuge
IL169481A (en) *	2005-06-30	2011-11-30	Rafael Advanced Defense Sys	Mobile carrier for a projectile launcher
RU2312294C2 (ru) *	2005-12-20	2007-12-10	Открытое акционерное общество "Конструкторское бюро специального машиностроения "	Самоходная пусковая установка
DE102006034688B4 (de) *	2006-07-24	2019-09-12	Rheinmetall Landsysteme Gmbh	Universales gepanzertes Unterstützungsfahrzeug
RU2331832C2 (ru) *	2006-10-05	2008-08-20	Государственное унитарное предприятие "Конструкторское бюро приборостроения"	Боевой модуль зенитного самоходного комплекса
RU2343390C1 (ru) *	2007-03-12	2009-01-10	ОАО "Конструкторское бюро машиностроения"	Самоходная пусковая установка
RU2389967C1 (ru) *	2008-09-09	2010-05-20	ОАО "Конструкторское бюро машиностроения"	Береговой ракетный противокорабельный комплекс
FR2936305B1 (fr) *	2008-09-24	2010-10-22	Nexter Systems	Tourelleau escamotable manuellement
SG183063A1 (en)	2009-03-30	2012-08-30	Director General Defence Res & Dev Org	A mobile missile launch system and method thereof
DE202010006199U1 (de)	2010-04-28	2010-08-12	Bundesrepublik Deutschland, vertreten durch das Bundesministerium der Verteidigung, vertreten durch das Bundesamt für Wehrtechnik und Beschaffung	Waffensystem für Artillerieraketen
US11015903B2 (en) *	2011-06-08	2021-05-25	American Technical Coatings, Inc.	Enhanced ballistic protective system
DE102012103353A1 (de) *	2012-04-17	2013-10-17	Krauss-Maffei Wegmann Gmbh & Co. Kg	Verfahren zum Transport eines Fahrzeugs sowie Fahrzeug
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1994
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- 1994-05-14 DE DE59406612T patent/DE59406612D1/de not_active Expired - Lifetime
- 1994-05-14 EP EP94107517A patent/EP0664431B1/fr not_active Expired - Lifetime
- 1994-12-21 US US08/361,267 patent/US5461961A/en not_active Expired - Lifetime

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
EP1400773A3 (fr) *	2002-09-23	2004-03-31	Krauss-Maffei Wegmann GmbH & Co. KG	Dispositif pour adapter un conteneur pour plusieurs roquettes à un lanceur pour roquettes d'artillerie
FR2938983A1 (fr) *	2008-11-26	2010-05-28	Nexter Systems	Dispositif permettant le desacouplement automatique des deux parties d'un connecteur.
EP2192373A1 (fr) *	2008-11-26	2010-06-02	NEXTER Systems	Dispositif permettant le désaccouplement automatique des deux parties d'un connecteur
DE102010016542A1 (de)	2010-04-20	2011-10-20	Krauss-Maffei Wegmann Gmbh & Co. Kg	Vorrichtung und Verfahren zum Richten eines Abschussbehälters
DE102010016542B4 (de)	2010-04-20	2013-01-03	Krauss-Maffei Wegmann Gmbh & Co. Kg	Vorrichtung und Verfahren zum Richten eines Abschussbehälters
DE102010016542C5 (de) *	2010-04-20	2017-08-17	Krauss-Maffei Wegmann Gmbh & Co. Kg	Vorrichtung und Verfahren zum Richten eines Abschussbehälters

Also Published As

Publication number	Publication date
US5461961A (en)	1995-10-31
EP0664431B1 (fr)	1998-08-05
DE4401587A1 (de)	1995-07-27
EP0664431A3 (fr)	1996-01-10
DE59406612D1 (de)	1998-09-10

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