EP0036811B1 - Granatwerfer mit hoher Feuergeschwindigkeit - Google Patents

Granatwerfer mit hoher Feuergeschwindigkeit Download PDF

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Publication number
EP0036811B1
EP0036811B1 EP81400425A EP81400425A EP0036811B1 EP 0036811 B1 EP0036811 B1 EP 0036811B1 EP 81400425 A EP81400425 A EP 81400425A EP 81400425 A EP81400425 A EP 81400425A EP 0036811 B1 EP0036811 B1 EP 0036811B1
Authority
EP
European Patent Office
Prior art keywords
firing
mortar
mortar according
stop
barrel
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
Application number
EP81400425A
Other languages
English (en)
French (fr)
Other versions
EP0036811A1 (de
Inventor
Bernard Marie André Jugue
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.)
Direction General pour lArmement DGA
Original Assignee
Direction General pour lArmement DGA
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 Direction General pour lArmement DGA filed Critical Direction General pour lArmement DGA
Priority to AT81400425T priority Critical patent/ATE4748T1/de
Publication of EP0036811A1 publication Critical patent/EP0036811A1/de
Application granted granted Critical
Publication of EP0036811B1 publication Critical patent/EP0036811B1/de
Expired legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F1/00Launching apparatus for projecting projectiles or missiles from barrels, e.g. cannons; Harpoon guns
    • F41F1/06Mortars
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A9/00Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
    • F41A9/01Feeding of unbelted ammunition
    • F41A9/24Feeding of unbelted ammunition using a movable magazine or clip as feeding element
    • F41A9/26Feeding of unbelted ammunition using a movable magazine or clip as feeding element using a revolving drum magazine
    • F41A9/27Feeding of unbelted ammunition using a movable magazine or clip as feeding element using a revolving drum magazine in revolver-type guns

Definitions

  • the present invention relates to rapid-fire mortars, that is to say curved parts of medium caliber and high firepower and, more particularly, rear-loading mortars.
  • a mortar of this type is known, but with manual unit loading without a magazine, which makes this loading painful and slows down the rate, especially in vertical shooting.
  • this mortar on a protected carrier vehicle the interior of the latter and the explosion chamber are placed in communication when the cylinder head is opened, which involves the disadvantages of inhaling toxic gases.
  • drawbacks which we try to remedy by a strong suction of these gases or by the creation of an overpressure inside the vehicle.
  • the size of the breech box is large and constitutes a drawback in vertical shooting.
  • French Patent No. 2163932 describes another mortar of this type, equipped with one or more unitary loading pots, integral with the movable part of a wedge breech, placing itself, in the firing position, in the rear extension of the tube and being filled by gravity.
  • These loading pots are therefore movable relative to the mounting of the barrel and, therefore, do not make it possible to remedy the difficulties of evacuation of the combustion gases if the mortar is loaded from an enclosed space, for example the interior of a light carrier vehicle.
  • GB N ⁇ 2004037 discloses a rapid-fire mortar with an ammunition barrel, the chambers of which, when they are in turn in the firing position, are sealed at their ends. But the tube of this mortar is not movable relative to the lookout, and is therefore not adaptable on a light carrier vehicle. This patent therefore does not solve the aforementioned difficulties in evacuating gases from the enclosed space formed by the interior of the vehicle where the servants are located.
  • the subject of the invention is a mortar of the type comprising, on the one hand, a tube movable during firing with respect to a support and, on the other hand, an ammunition barrel , integral in translation with the tube, and having at least two chambers which can be placed one at a shooting station and the other at a feeding station, this mortar being characterized in that the chambers comprise means for ensuring their fixity with respect to the support when they are placed at at least one station other than the shooting station.
  • the means for ensuring the fixity of the chamber comprise a fur, preferably cylindrical, sliding in a barrel between a rest position and a recoil position during firing.
  • a gas evacuation station is located between the firing station and the supply station, in the direction of rotation of the barrel.
  • one of the abutments of the evacuation station may advantageously include means for evacuating gases to the outside.
  • the invention therefore makes it possible to obtain a rapid-fire mortar having excellent loading ergonomics, due to the fixity of the chamber placed at the corresponding station, and capable of being used from an enclosed space without the clearances of abundant toxic gases at high rate inconvenience the loading staff.
  • the space requirement at the rear of the weapon is reduced to a minimum, which is particularly favorable in the case of installation on a protected vehicle.
  • the mortar according to fig. 1 comprises a frame, or support, suspended by trunnions 2, or a ball joint, from the roof 3 of a casemate or a turret, thus delimiting an enclosed space occupied by the servants of the weapon.
  • the mortar comprises a tube 4 integral with the cylinder head 5 which supports the percussion mechanism (not shown), and which comprises an axis 6, parallel to the axis of the tube 4, on which a barrel 7 can rotate.
  • Letube4 is movable in translation relative to the support 1 via an elastic link 12 comprising recuperating springs 4a.
  • the barrel 7 has three identical chambers 8, 9 and 10 (fig. 5) equidistant from the axis 6 and which, in the embodiment shown tee, are placed 120 ° from each other with respect to it.
  • a rotary drive mechanism (not shown) rotates it 120 ° in the direction of arrow H when the tube 4 returns to the battery after a shot.
  • the chamber 8 is placed at a shooting station X where it is in line with the tube 4, the chamber 9 at a gas evacuation station Y and the chamber 10 at a loading Z.
  • Each of the chambers 8, 9 and 10 comprises a fur 11 a, 11 b or 11 sliding in the barrel 7 parallel to the axis 6.
  • the interior diameters of the furs 11 a, 11 b and 11 c are equal to that of the tube 4 .
  • the frame 1 At its rear part, the frame 1 comprises a casing 13 for protecting the part of the barrel 7 which is located outside the cylinder head 5.
  • the casing 13 has at its front, or upper part, a bearing face 13a constituting a front stop for the furs 11 a, 11 b and 11 c when they are outside the cylinder head 5. Solid with the frame 1, the stop 13a is therefore fixed relative to it.
  • the bearing face 13a is pierced with an orifice 13b for admission of ventilation air, while to the right of the Zelle loading station is pierced with an opening of load 18 allowing the passage of a munition, and aligned with that of the furs 11a, 11b or 11 c which is at station Z.
  • the casing 13 also includes a rear stop 14 for the loading station Z, on which the fur 11 a, 11 b or 11 c which is in Z carries, as well as a tubular rear stop 15 for the discharge station Y .
  • the stop 15 is applied in a sealed manner to the fur 11 a, 11 b or 11 c which is in Y, and it is pierced with a discharge orifice 19 connected to means for sucking the gases towards the exterior (not shown).
  • the assembly is then in the position shown in FIGS. 1 and 2.
  • the chamber placed at the shooting station X that is to say here the chamber 8, contains ammunition ready for shooting (fig. 1 and 2), while the chamber 9, placed at the shooting station evacuation Y, purges the burnt gases from the previous stroke thanks to the entry of fresh air through the orifice 13b and the gas outlet through the orifice 19 of the tubular stop 15.
  • the chamber 10, which is located at loading station Z, is ready to receive new ammunition.
  • Figs. 3 and 4 show the beginning of the installation of a new munition 17 in the chamber 10 at the loading station Z as well as the continuation of the evacuation of the burnt gases from the chamber 9 at the station Y:
  • the evacuation of the gases remaining in the chamber after firing is also carried out in masked time and the toxic emissions of the weapon are eliminated without reduction of the rate.
  • the procedure to follow is to introduce an ammunition at the loading station Z then to turn the barrel 7 by 120 ° to bring the corresponding chamber to the shooting station. We are then brought back to the situation of figs. 1 and 2 and the previously exposed shooting sequence can begin.
  • the mortar can in particular be journalled in a manner different from that which has been indicated, the axis of rotation possibly being closer and even possibly beyond the cylinder head 5, and not be placed in a casemate.
  • the barrel can also include more than three stations, the additional stations being able to be used for various functions, such as the adjustment of the loads or the adjustment of the rockets.
  • the gas evacuation station can be designed so as to move back with the barrel, which makes it possible to eliminate the corresponding rear stop at the cost of a certain complication of the gas extraction means.
  • the means for immobilizing the chambers during retraction can be different from the stops described and include for example rods or retractable fingers, and the means for driving the barrel in rotation can be controlled - possibly manually - separately instead of be automatically.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Medicines Containing Plant Substances (AREA)
  • Curing Cements, Concrete, And Artificial Stone (AREA)
  • Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
  • Conveying And Assembling Of Building Elements In Situ (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • On-Site Construction Work That Accompanies The Preparation And Application Of Concrete (AREA)
  • Devices For Post-Treatments, Processing, Supply, Discharge, And Other Processes (AREA)
  • Furnace Charging Or Discharging (AREA)
  • Acyclic And Carbocyclic Compounds In Medicinal Compositions (AREA)

Claims (8)

1. Schnellschussmörser,dereinerseitseinwäh- rend des Schusses im Verhältnis zu einem Träger (1) bewegliches Rohr (4) und andererseits einen in der Rohrverschiebung formschlüssig verbundenen Munitionsbehälter (7), mit mindestens zwei Kammern (8, 10) umfasst, von denen die eine an einem Schussposten (X) und die andere an einen Ladeposten (Z) angebracht werden kann, dadurch gekennzeichnet, dass die Kammern die Mittel (11 a, 11 b, 11 c) aufweisen, die ihre Befestigung am Träger gewährleisten, wenn sie an mindestens einem anderen als am Schussposten angebracht sind.
2. Mörser gemäss Anspruch 1, dadurch gekennzeichnet, dass die Mittel zur Gewährleistung der Befestigung eine zylindrische Hülse (11) umfassen, die im Behälter zwischen einer Ruhestellung und einer Rückwärtsposition beim Schuss gleitet.
3. Mörser gemäss Anspruch 2, dadurch gekennzeichnet, dass die sich vom Schussposten (X) unterscheidenden Posten (Y, Z) einen vorderen Anschlag (13a) und einen rückwärtigen Anschlag (14) umfassen, die mit dem Trägerformschlüssig verbunden sind und zusammenarbeiten, wenn sich die Kammer an diesem Posten mit der entsprechenden Gleithülse befindet.
4. Mörser gemäss einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, dass der Ladungsposten (Z) eine im Vergleich zum Träger feste Öffnung (18) aufweist und ermöglicht, eine Munition in die Kammer einzuführen, die sich am Posten befindet, wobei diese ebenfalls im Vergleich zum Träger fest ist.
5. Mörser gemäss einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, dass er einen Gasentleerungsposten (Y) aufweist, der sich zwischen dem Schussposten (X) und dem Ladungsposten (Z) in Drehrichtung des Behälters befindet.
6. Mörser gemäss Anspruch 5, aus einem geschlossenen Raum schiessend, dadurch gekennzeichnet, dass die Kammer am Gasentleerungsposten (Y) in Verbindung mit den Entleerungsmitteln (13b) des Gases nach aussen steht.
7. Mörsar gemäss den Ansprüchen 3 bis 6, dadurch gekennzeichnet, dass einer der Anschläge (13a) des Gasentleerungspostens (Y) dicht auf der Hülse am Posten sitzt und eine Lufteinlassöffnung aufweist, während der andere Anschlag (15) eine Rohrform hat, deren eines Ende auf dem entsprechenden Hülsenabschnitt sitzt, und eine Saugöffnung (19) nach aussen aufweist.
8. Mörser gemäss Anspruch 7, dadurch gekennzeichnet, dass der vordere Anschlag (13a) des Entleerungspostens (Y) dicht auf der Hülse am Posten aufsitzt und eine Lufteinlassöffnung (13b) aufweist, während der rückwärtige Anschlag eine Rohrform besitzt, deren Ende auf dem rückwärtigen Abschnitt der Hülse aufsitzt, wobei dieser rohrförmige Anschlag eine Öffnung (19) für die Gasabsaugung nach aussen aufweist.
EP81400425A 1980-03-26 1981-03-19 Granatwerfer mit hoher Feuergeschwindigkeit Expired EP0036811B1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT81400425T ATE4748T1 (de) 1980-03-26 1981-03-19 Granatwerfer mit hoher feuergeschwindigkeit.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8006654 1980-03-26
FR8006654A FR2479442A1 (fr) 1980-03-26 1980-03-26 Mortier a tir rapide

Publications (2)

Publication Number Publication Date
EP0036811A1 EP0036811A1 (de) 1981-09-30
EP0036811B1 true EP0036811B1 (de) 1983-09-21

Family

ID=9240096

Family Applications (1)

Application Number Title Priority Date Filing Date
EP81400425A Expired EP0036811B1 (de) 1980-03-26 1981-03-19 Granatwerfer mit hoher Feuergeschwindigkeit

Country Status (5)

Country Link
EP (1) EP0036811B1 (de)
AT (1) ATE4748T1 (de)
DE (1) DE3160920D1 (de)
FR (1) FR2479442A1 (de)
NO (1) NO148831C (de)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3207138A1 (de) * 1982-02-27 1985-11-28 Diehl GmbH & Co, 8500 Nürnberg Panzerfahrzeug mit eingebautem moerser
FR2674950B1 (fr) * 1991-04-04 1993-06-11 Giat Ind Sa Mortier a barillet.
US6637310B2 (en) * 2001-03-01 2003-10-28 United Defense L.P. Rotatable breech gun
RU2616093C1 (ru) * 2015-12-16 2017-04-12 Николай Евгеньевич Староверов Миномёт Староверова - 3 /варианты/

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2004037A (en) * 1977-09-10 1979-03-21 Rheinmetall Gmbh Mortar
DE2837995A1 (de) * 1978-08-31 1980-03-13 Rheinmetall Gmbh Steilfeuerrohrwaffe

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2163932A5 (de) * 1971-12-07 1973-07-27 France Etat

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2004037A (en) * 1977-09-10 1979-03-21 Rheinmetall Gmbh Mortar
DE2837995A1 (de) * 1978-08-31 1980-03-13 Rheinmetall Gmbh Steilfeuerrohrwaffe

Also Published As

Publication number Publication date
FR2479442B1 (de) 1982-04-02
DE3160920D1 (en) 1983-10-27
FR2479442A1 (fr) 1981-10-02
EP0036811A1 (de) 1981-09-30
NO811010L (no) 1981-09-28
NO148831C (no) 1983-12-21
ATE4748T1 (de) 1983-10-15
NO148831B (no) 1983-09-12

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