EP0411993B1 - Versenkbare leichte Fliegerabwehrlafette - Google Patents

Versenkbare leichte Fliegerabwehrlafette Download PDF

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Publication number
EP0411993B1
EP0411993B1 EP90402154A EP90402154A EP0411993B1 EP 0411993 B1 EP0411993 B1 EP 0411993B1 EP 90402154 A EP90402154 A EP 90402154A EP 90402154 A EP90402154 A EP 90402154A EP 0411993 B1 EP0411993 B1 EP 0411993B1
Authority
EP
European Patent Office
Prior art keywords
plate
weapon
elevation
launcher
vehicle
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.)
Expired - Lifetime
Application number
EP90402154A
Other languages
English (en)
French (fr)
Other versions
EP0411993A1 (de
Inventor
Jean-Philippe Patrice Bernard Allais
Alain Robert Guillermond
Pascal Gérard Rouyer
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.)
Safran Transmission Systems SAS
Original Assignee
Hispano Suiza SA
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 Hispano Suiza SA filed Critical Hispano Suiza SA
Priority to AT90402154T priority Critical patent/ATE91342T1/de
Publication of EP0411993A1 publication Critical patent/EP0411993A1/de
Application granted granted Critical
Publication of EP0411993B1 publication Critical patent/EP0411993B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F41A23/00—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles
    • F41A23/20—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles for disappearing guns

Definitions

  • the invention relates to a light anti-aircraft mount capable of being mounted on the roof of a light armored vehicle.
  • Document DE-A-2 043 852 describes a rocket launcher whose deformable parallelogram structure is completely cantilevered at the front of the turntable of the vehicle, this document constituting the preamble to the present claim 1.
  • This structure does not allow the balance of the masses of the lookout during deployment and also does not provide mobility in site of the weapon from a position with negative site to a position with strongly positive site.
  • One of the aims of the present invention is therefore to produce a light mount which has a site tilt of the weapon from -15 ° to + 45 ° while allowing the air transportability of the vehicle carrying the mount.
  • the invention proposes to make a foldable mount on the roof of the vehicle and having a reduced overall mass whose center of gravity is the lowest possible, not far from the center of gravity of the naked vehicle.
  • Another object of the invention is to produce a mount, the deployment of which by the servant of the weapon is carried out quickly and almost automatically without requiring for the servant an excessive effort during the folding.
  • Another object of the invention is to provide a mounting allowing execution for the servant without excessive fatigue of the phases of rallying towards the target, and of pursuit, with reduced reaction times over 360 ° of deposit.
  • the invention proposes to produce a light deployable anti-aircraft mount mobile in 360 ° bearing and on site from -15 ° to + 45 ° and more depending on the weapon, arranged on the roof of a vehicle and capable of assuming a folded position on the roof of said vehicle and a deployed position for firing, such that said mount comprises a support plate for the weapon and its aiming system and such that said plate is carried by an articulated chair formed by a deformable double quadrilateral, the chair being fixed on a turntable on the roof of the vehicle by means of a circular toothed crown.
  • the articulated chair is itself further constituted by two transverse supports, one front and the other rear, each formed of a U-shaped tube, the base of which comprises two yokes allowing them to tilt forwards in bearings integral with the turntable, and by two horizontal crosspieces of longitudinal axis, symmetrical with respect to the axis of the circular toothed crown surrounding the member of the weapon, said crosspieces being articulated on the upper ends, respectively left and right of the front and rear cross supports.
  • the axis of rotation in elevation of the plate relative to the horizontal crosspieces is arranged in a vertical plane containing the axis of bearing of the carriage when the latter is deployed.
  • Displacement assistance means consisting of two pairs of mechanical cylinders, respectively front and rear, articulated on the turntable and having their rods articulated respectively on the yokes of the front and rear transverse supports, balance the mass of the stage equipped with its weapon when passing from the folded position to the deployed position.
  • the plate 2 comprises a rectangular armored hatch 8 opening by tilting backwards to serve as passage to the lookout attendant from inside the vehicle.
  • the plate 2 comprises four boxes serving as bearings for a deployable chair, itself made up of two transverse supports, one at the front 9 and the other at the rear 10.
  • two front boxes 11 serving as the bearing for the support transverse front
  • two rear boxes 12 serve as bearings to the rear transverse support.
  • the front left 11 and rear 12 boxes are symmetrical with the right front and rear boxes with respect to a diametrical axis of the turntable.
  • Each front 9 and rear 10 transverse support consists of a U-shaped bent tube, the base (respectively 9a, 10a) is provided with yokes (respectively 9b, 10b) equipped with articulation axes around which the supports rotate. transverse 9 and 10.
  • left 9c and 10c and right 9d, 10d are mounted, articulated on ball joints of the horizontal crosspieces (respectively left 13a and right 13b).
  • the assembly formed by the transverse supports 9 and 10 and the crosspieces 13a and 13b constitutes the articulated chair whose deployment is ensured by the shape in two deformable parallelograms constituted by the plate 2, the left uprights 9c, 10c of the transverse supports and the cross 13a (respectively the uprights 9d, 10d and the cross 13b).
  • the plate 14 On the chair thus formed is mounted the plate 14, support of the weapon (s) 15.
  • the plate 14 is rotatably mounted in elevation on a site axis YY materialized by bearings 16 of the crosspieces 13a, 13b, said site axis being arranged in the vertical plane containing the axis of deposit ZZ.
  • the plate 14 supports two weapons 15 placed laterally on either side of the servant. It also supports a sighting device 17 in front of the servant.
  • the plate thus equipped has its center of gravity located along an axis Z1 Z1 placed in front of the bearing axis and this fact increases the unbalance of the assembly to be deployed by the servant to move the carriage from its folded position to the deployed position.
  • Means for assisting the deployment of the articulated chair are therefore provided, capable of balancing the mass of the plate equipped with its weapon (s), when passing from the folded position to the deployed position.
  • the front boxes 11 may include a mechanical system for disengaging the front jacks 18.
  • the cross members 13a, 13b of the chair each support a longitudinal cylinder 20 whose body is articulated at the rear of the cross member and the rod of which actuates a cable 21 wound on a pulley integral in rotation in elevation with the plate and concentric with the pin 16 of said plate.
  • the servant of the weapon has a lower effort to provide to position his weapon in site.
  • this device improves the dynamic behavior when driving.
  • the turntable supports in its median axis in the front position a lock 31 for locking the articulated chair in each of its two folded and deployed positions, said lock cooperating with two bolts formed in the base of the front lyre 9.
  • the plate 2 also carries a bolt 22 for blocking the carriage in deposit in order to ensure that the carriage is locked in an axial position, weapon facing forward, during taxiing.
  • the bolt of said lock 22 is erased in the standby and firing position to allow the carriage to rotate 360 °. In the road position, it is unlocked to automatically engage in a keeper secured to the riser when the carriage is first moved into position longitudinal facing the front of the vehicle.
  • the plate 14 supporting the weapon comprises on its lateral edges two bolts 23 for blocking the elevation of said plate, said latches being able to cooperate with two strikes 24 carried by the longitudinal crosspieces of the chair to immobilize the plate in horizontal position especially when rolling in the folded position of the mount on the vehicle roof.
  • the second jacks 120 for compensating for the unbalance due to the eccentric position of the center of gravity of the plate equipped with its weapon relative to the axis of rotation in elevation, are arranged between the plate 14 and the crosspieces 13a 13b and below these in order to improve the size of the carriage.
  • the jacks 120 have their bodies fixed on a yoke integral with the front part of each longitudinal cross member and their rod directly actuates a yoke 116 integral in site with the plate and carried by the pin 16 of the latter.
  • the deposit locking can be automatic or manual.
  • An adjustable stop fixed on the transverse support 109 by folding the system to actuate a piston 123 which by its movement, releases a bolt 124 in the keeper 125 of the extension 3. Unlocking is performed manually after deploying the system in actuating the lock 126 downwards. The servant has the possibility of manually locking the rotating part by actuating the lock 126 upwards.
  • the carriage thus produced according to these two variants allows rapid and almost automatic implementation of the folded position to the deployed position, as well as the execution by the servant of the carriage, of the rallying phases. towards the target and pursuit without excessive fatigue, while retaining on the lookout compactness qualities allowing the preservation of the mobility and the air transportability of the support vehicle.
  • the mount according to the invention is adapted to support on its plate in place of missiles, either a machine gun or a laser type ground weapon, or a rocket launcher.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Lighting Device Outwards From Vehicle And Optical Signal (AREA)
  • Filtering Materials (AREA)
  • Air Bags (AREA)
  • Catching Or Destruction (AREA)
  • Toys (AREA)

Claims (9)

  1. Auf dem Dach eines Fahrzeugs angeordnete ausfahrbare Waffenlafette, die über einen Seitenwinkel von 360° sowie bezüglich des Höhenwinkels verstellbar ist und auf dem Fahrzeugdach eine eingefahrene Position und eine schußbereite ausgefahrene Position einnehmen kann,
       mit einer als Träger der Waffe (15) dienenden Platine (14), die von einem aus einem doppelten verformbaren Gelenkviereck gebildeten gelenkigen Rahmengestell (9, 10, 13 oder 109, 110, 113) getragen ist, das auf dem Fahrzeugdach auf einem mit Hilfe eines kreisförmigen Zahnkranzes (5) drehbaren Drehteller (2) befestigt ist und aus zwei Querträgern besteht, von denen der eine (9, 109) vorn und der andere (10, 110) hinten angeordnet ist und deren Basis (9a, 10a; 109a, 110a) zwei Gabelgelenke (9b, 10b; 109b, 110b) aufweist, die ihr Vorwärtskippen in mit dem Drehteller fest verbundenen Lagern ermöglichen, sowie aus zwei horizontalen Traversen (13a, 13b) mit zur Achse des Zahnkranzes symmetrischer Längsachse, die die Bedienungsperson der Waffe umschließen und mit den oberen linken (9a, 10a; 109a, 110a) bzw. rechten (9b, 10b; 109b, 110b) Enden der vorderen und hinteren Querträger (9, 109 bzw. 10, 110) gelenkig verbunden sind,
       dadurch gekennzeichnet,
       daß die Waffenlafette eine leichte Fliegerabwehrlafette ist, die über einen Höhenwinkel von -15° bis +45° und darüber hinaus verstellbar ist,
       daß die Platine (14) auch den Träger des Richtsystems der Waffe bildet,
       daß die Querträger jeweils aus einem U-förmigen Rohr bestehen,
       daß die Drehachse YY der Höhenwinkelverstellung der Platine (14) relativ zu den horizontalen Traversen (13a, 13b) in einer vertikalen Ebene liegt, die die Achse ZZ der Seitenwinkelverstellung der Lafette enthält, wenn diese ausgefahren ist,
       und daß Ausfahrhilfsmittel vorgesehen sind, bestehend aus zwei Paaren, nämlich einem vorderen Paar (18) und einem hinteren Paar (19), von ersten mechanischen Winden (18, 19), die an dem Drehteller (2) angelenkt sind und deren Stangen jeweils mit den beiden Gabelgelenken (9b, 10b; 109b, 110b) der vorderen und hinteren Querträger gelenkig verbunden sind, wobei diese Ausfahrhilfsmittel beim Übergang aus der eingefahrenen in die ausgefahrene Position die Masse der mit ihrer Waffe (15) ausgerüsteten Platine (14) ausgleichen.
  2. Fliegerabwehrlafette nach Anspruch 1 mit zwei zu beiden Seiten der Bedienungsperson angeordneten Waffen, dadurch gekennzeichnet, daß sie eine Vorrichtung zum mechanischen Auskuppeln der vorderen Massenausgleichswinden (18) aufweist.
  3. Fliegerabwehrlafette nach einem der Ansprüche 1 oder 2, dadurch gekennzeichnet, daß der hintere Querträger (110) höher ist als der vordere Querträger (109), so daß die longitudinalen Traversen in der ausgefahrenen Position um einen Winkel nach vom geneigt sind, der gleich dem minimalen Höhenwinkel ist.
  4. Fliegerabwehrlafette nach einem der Ansprüche 1 oder 2, dadurch gekennzeichnet, daß die vorderen und hinteren Querträger (9, 10) gleiche Höhe haben, so daß die longitudinalen Traversen in der ausgefahrenen Position horizontal angeordnet sind.
  5. Fliegerabwehrlafette nach Anspruch 4, dadurch gekennzeichnet, daß zwei zweite Winden (20) vorgesehen sind, die an den horizontalen Traversen des Rahmengestells befestigt sind und ein Kabel (21) antreiben, das auf einer bezüglich des Höhenwinkels mit der Platine fest verbundenen Scheibe aufgewickelt ist, die von den die Drehachse der Höhenwinkelverstellung der Platine verkörpernden Zapfen (16) getragen ist, um das durch die exzentrische Position des Schwerpunkts der mit ihrer Waffe ausgerüsteten Platine gegenüber der Drehachse der Höhenwinkelverstellung verursachte Ungleichgewicht zu beseitigen.
  6. Fliegerabwehrlafette nach Anspruch 3, dadurch gekennzeichnet, daß sie zwei zweite Winden (120) aufweist, deren Körper an einem mit dem vorderen Teil jeder der longitudinalen Traversen fest verbundenen Gabelgelenk befestigt ist und deren Stange ein Gabelgelenk (116) antreibt, das bezüglich des Höhenwinkels mit der Platine fest verbunden ist und von den Zapfen (16) der Platine getragen wird, um das durch die exzentrische Position des Schwerpunkts der mit ihrer Waffe ausgerüsteten Platine gegenüber der Drehachse der Höhenwinkelverstellung verursachte Ungleichgewicht zu beseitigen.
  7. Fliegerabwehrlafette nach einem der Ansprüche 1 bis 6, dadurch gekennzeichnet, daß ein von dem Drehteller getragenes Schloß (31) zur Blockierung des gelenkigen Rahmengestells in jeder ihrer beiden Positionen, d.h. der eingefahrenen und der ausgefahrenen Position, vorgesehen ist, das mit zwei an der Basis des vorderen Querträgers ausgebildeten Riegeln zusammenwirkt.
  8. Fliegerabwehrlafette nach einem der Ansprüche 1 bis 7, dadurch gekennzeichnet, daß ein von dem Drehteller getragenes Schloß (22, 122) zur Blockierung der Lafette bezüglich des Seitenwinkels vorgesehen ist, wobei der Riegel dieses Schlosses in der Wacht- und Schußposition zurückgefahren ist, um die Drehung der Lafette um 360° zu ermöglichen, und in der Fahrposition entsperrt ist, um beim ersten Übergang der Lafette in die zur Vorderseite des Fahrzeugs gerichtete Längsposition automatisch in einen mit dem Rahmen fest verbundenen Schließhaken einzufallen.
  9. Fliegerabwehrlafette nach einem der Ansprüche 1 bis 8, dadurch gekennzeichnet, daß die Trägerplatine der Waffe an ihren Seitenrändern zwei Riegel (23) zur Blockierung der Platine bezüglich des Höhenwinkels aufweist, die zur Festlegung der Platine in ihrer horizontalen Position mit zwei von den longitudinalen Traversen (13a, 13b) getragenen Schließhaken des Rahmengestells zusammenwirken können.
EP90402154A 1989-07-31 1990-07-26 Versenkbare leichte Fliegerabwehrlafette Expired - Lifetime EP0411993B1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT90402154T ATE91342T1 (de) 1989-07-31 1990-07-26 Versenkbare leichte fliegerabwehrlafette.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR898910289A FR2650385B1 (fr) 1989-07-31 1989-07-31 Affut antiaerien leger deployable
FR8910289 1989-07-31

Publications (2)

Publication Number Publication Date
EP0411993A1 EP0411993A1 (de) 1991-02-06
EP0411993B1 true EP0411993B1 (de) 1993-07-07

Family

ID=9384313

Family Applications (1)

Application Number Title Priority Date Filing Date
EP90402154A Expired - Lifetime EP0411993B1 (de) 1989-07-31 1990-07-26 Versenkbare leichte Fliegerabwehrlafette

Country Status (6)

Country Link
US (1) US5056409A (de)
EP (1) EP0411993B1 (de)
AT (1) ATE91342T1 (de)
DE (1) DE69002138T2 (de)
ES (1) ES2042243T3 (de)
FR (1) FR2650385B1 (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7231862B1 (en) 2002-11-26 2007-06-19 Recon/Optical, Inc. Dual elevation weapon station and method of use
EP3699542A1 (de) 2019-02-21 2020-08-26 CMI Defence S.A. Tarnkappenfahrzeug mit integriertem waffensystem zur raschen bereitstellung

Families Citing this family (15)

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Publication number Priority date Publication date Assignee Title
US6308610B1 (en) * 1998-10-15 2001-10-30 Ronald S. Deichmann Liquid cannon having trunnion assembly
US6907812B1 (en) 2003-01-21 2005-06-21 United Defense Lp Pop-up weapon system
US7669513B2 (en) * 2003-10-09 2010-03-02 Elbit Systems Ltd. Multiple weapon system for armored vehicle
DE102005061517B4 (de) * 2005-12-22 2008-04-03 Rheinmetall Landsysteme Gmbh Trägerfahrzeug oder dergleichen für eine Lafette
US20070251375A1 (en) * 2006-04-28 2007-11-01 Lockheed Martin Corporation Segmented gun turret for quick assembly
US8584573B2 (en) * 2010-02-04 2013-11-19 Quantum Fuel Systems Technologies Worldwide Inc. Orbital device with stowable mount
US8459170B2 (en) * 2010-03-10 2013-06-11 Oto Melara S.P.A. Vehicle provided with revolving turret
DE102010017784B4 (de) 2010-07-07 2013-08-08 Krauss-Maffei Wegmann Gmbh & Co. Kg Militärisches Fahrzeug mit einem Überrollschutz und Verfahren zur Reduktion der Fahrzeughöhe eines militärischen Fahrzeugs
ITTO20110239A1 (it) * 2011-03-18 2012-09-19 Oto Melara Spa Struttura di posizionamento per un'arma da fuoco su un veicolo
FR3004529B1 (fr) * 2013-04-11 2015-04-03 Nexter Systems Dispositif de support de tourelleau
EA024671B1 (ru) * 2013-05-24 2016-10-31 Закрытое Акционерное Общество "Цнип" Многозарядная пусковая установка
US9464856B2 (en) 2014-07-22 2016-10-11 Moog Inc. Configurable remote weapon station having under armor reload
US9568267B2 (en) * 2014-07-22 2017-02-14 Moog Inc. Configurable weapon station having under armor reload
ITUB20151137A1 (it) * 2015-05-28 2016-11-28 Oto Melara Spa Sistema di supporto per arma da fuoco, in particolare destinato ad essere montato appeso ad una superficie superiore.
CA2999996C (en) * 2015-09-29 2019-10-22 Russell FRANK Camper shell turret system

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US641872A (en) * 1899-11-01 1900-01-23 Krupp Gmbh Disappearing gun.
US769636A (en) * 1901-05-04 1904-09-06 Krupp Gmbh Carriage for disappearing guns.
FR502549A (fr) * 1916-01-03 1920-05-18 Schneider & Cie Affut à éclipse pour bouches à feu de submersibles et autres applications
BE426551A (de) * 1937-02-26
GB556002A (en) * 1941-06-12 1943-09-16 Alfred German Rose Improvements in or relating to gun mountings
US2336557A (en) * 1942-07-30 1943-12-14 Glenn L Martin Co Flush gun turret
DE2043852A1 (de) * 1969-09-04 1971-03-11 Societe Nationale Industrielle Aerospatiale Paris Versenkbare Abschußvorrichtung fur Lenkwaffen
FR2380527A2 (fr) * 1977-02-11 1978-09-08 Creusot Loire Installation de lancement de missiles
DE2902992C3 (de) * 1979-01-26 1981-09-24 Heckler & Koch Gmbh, 7238 Oberndorf Lafette zur Aufnahme leichter Maschinenwaffen mit einer Umlenkvisierung
FR2506002A1 (fr) * 1981-05-15 1982-11-19 Creusot Loire Support d'arme legere
US4667565A (en) * 1984-12-14 1987-05-26 Tetradyne Corporation Rapid response patrol and antiterrorist vehicle

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7231862B1 (en) 2002-11-26 2007-06-19 Recon/Optical, Inc. Dual elevation weapon station and method of use
EP3699542A1 (de) 2019-02-21 2020-08-26 CMI Defence S.A. Tarnkappenfahrzeug mit integriertem waffensystem zur raschen bereitstellung
WO2020169368A1 (fr) 2019-02-21 2020-08-27 Cmi Defence S.A. Vehicule furtif avec système d'arme integre a deploiement rapide
US11940236B2 (en) 2019-02-21 2024-03-26 John Cockerill Defense SA Stealth vehicle with integrated fast deployment weapon system

Also Published As

Publication number Publication date
FR2650385B1 (fr) 1994-09-09
DE69002138D1 (de) 1993-08-12
ES2042243T3 (es) 1993-12-01
FR2650385A1 (fr) 1991-02-01
ATE91342T1 (de) 1993-07-15
DE69002138T2 (de) 1994-01-05
EP0411993A1 (de) 1991-02-06
US5056409A (en) 1991-10-15

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