EP0250329B2 - Munitionstreibladung, insbesondere für Pfeilgeschosse grossen Kalibers - Google Patents

Munitionstreibladung, insbesondere für Pfeilgeschosse grossen Kalibers Download PDF

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Publication number
EP0250329B2
EP0250329B2 EP87401380A EP87401380A EP0250329B2 EP 0250329 B2 EP0250329 B2 EP 0250329B2 EP 87401380 A EP87401380 A EP 87401380A EP 87401380 A EP87401380 A EP 87401380A EP 0250329 B2 EP0250329 B2 EP 0250329B2
Authority
EP
European Patent Office
Prior art keywords
holding means
propellant charge
sleeve
projectile
charge
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
EP87401380A
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English (en)
French (fr)
Other versions
EP0250329A1 (de
EP0250329B1 (de
Inventor
Jean-Claude Sauvestre
Gérard Raymondie
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.)
Giat Industries SA
Original Assignee
Giat Industries 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
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Application filed by Giat Industries SA filed Critical Giat Industries SA
Priority to AT87401380T priority Critical patent/ATE50359T1/de
Publication of EP0250329A1 publication Critical patent/EP0250329A1/de
Application granted granted Critical
Publication of EP0250329B1 publication Critical patent/EP0250329B1/de
Publication of EP0250329B2 publication Critical patent/EP0250329B2/de
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02—Cartridges, i.e. cases with charge and missile
    • F42B5/16—Cartridges, i.e. cases with charge and missile characterised by composition or physical dimensions or form of propellant charge, with or without projectile, or powder

Definitions

  • the invention relates to a propellant charge consisting of grains of powder, intended for the propulsion of projectiles in particular with kinetic energy under calibrated of the large caliber arrow type.
  • These munitions are known to perforate targets by mechanical effect thanks to the kinetic energy delivered on impact. Therefore, in a given weapon system, therefore for a known firing pressure, this ammunition is asked to have the highest possible initial speed.
  • studies of these munitions lead to the finest possible optimization of the projectile itself and of each sub-assembly making up its propulsive system (powder, ignition, etc.).
  • the mechanical strength of the towed part is essentially linked to the value of these transverse stresses.
  • the maximum value of these constraints must be limited to the maximum so that the towed part retains its integrity at the outlet of the launching tube.
  • One of the aims of the invention consists in solving the problem of the mechanical strength of the tail unit by reducing the transverse stresses to which it is subjected.
  • the subject of the invention is a propellant charge consisting of powder, for example in the form of grains, intended for the propulsion of sub-calibrated kinetic energy projectiles of the large caliber arrow type and placed inside a socket of revolution.
  • metallic or not comprising at one end a base and at the other end the projectile, charging characterized in that it comprises holding means ensuring its compactness and its symmetry with respect to the axis of revolution of the sleeve and in that that these holding means make it possible to compact the propellant charge towards the base of the case, leaving a vacuum between the tail of the arrow-type projectile and the charge.
  • the invention relates to a propellant charge consisting of powder, for example in the form of grains, intended for the propulsion of under-calibrated kinetic energy projectiles of the large caliber arrow type and placed inside.
  • a metallic or non-metallic revolution bushing comprising at one end a base and at the other end the projectile, loading characterized in that it comprises holding means ensuring its compactness and its symmetry with respect to the axis of revolution of the sleeve and in that these holding means make it possible to compact the propellant charge towards the projectile, leaving a vacuum between the base of the sleeve and the charge.
  • the invention relates to a propellant charge consisting of powder, for example in the form of grains, intended for the propulsion of under-calibrated kinetic energy projectiles of the large caliber arrow type and disposed at the inside of a metallic or non-metallic revolution socket comprising at one end a base and at the other end the projectile, loading characterized in that it comprises holding means ensuring its compactness and its symmetry with respect to the axis of revolution of the sleeve and in that these holding means make it possible to compact the propellant charge around the axis of revolution of the sleeve, leaving a vacuum between the sleeve and the charge and / or between the igniter and the charge.
  • the holding means can be constituted by a binder disposed between the grains of powder.
  • the holding means can be made of a material chosen, for example, from: cardboard, nitrocellulose or expanded polystyrene.
  • the holding means may consist of a perforated metal sheet.
  • the holding means may include a wedging disposed at the rear of the projectile so that the load is applied towards the base of the case.
  • the holding means may include a wedging disposed at the base of the sleeve so that the load is applied towards the projectile.
  • the holding means may comprise an envelope of revolution placed longitudinally in the sleeve so that the load is disposed inside this envelope.
  • the holding means may comprise an envelope of revolution placed longitudinally in the sleeve so that the load is disposed outside of this envelope.
  • the envelope of revolution can be cylindrical.
  • Figure 1 shows a munition according to the state of the art station in a launch tube 1; it consists of an arrow sub-projectile 2 comprising an elongated bar made of heavy material and a stabilizing stabilizer 3.
  • the arrow sub-projectile 2 is guided and propelled into the launching tube 1 by a shoe 4.
  • the ammunition also includes a socket 5 to the base of which is fixed a primer holder igniter tube 6. This socket contains the propellant charge 7 consisting of loose powder.
  • the powder forms, by gravitation, an inclined powder bed 8 making the propellant charge asymmetrical.
  • the primer-carrying tube 6 ignites the propellant charge 7 by developing pressure waves moving in the direction represented by the arrow 9.
  • the pressure wave is disturbed by the asymmetry of the propellant charge and generated a force T1 substantially perpendicular to the powder bed.
  • This force T1 combined with the traction force T2, due to the inertia of the towed part of the projectile, subjects the tail of the arrow to a resulting force T3 which in the particular case of this figure is substantially perpendicular to the axis of revolution of ammunition.
  • This T3 effort tends to bend the projectile, which can have harmful consequences which can range from partial deterioration to complete rupture of the tail
  • FIG. 2 shows a munition of the type described above. However, an important modification concerning the propellant charge 7 has been made.
  • a wedging has been arranged at the front of the load, isolating the latter from the tail of the boom, and now compacting it towards the rear of the sleeve 5 so as to maintain its symmetry during the various manipulations of the ammunition before and when it is stationed.
  • the setting is carried out using a disc 10 which can, for example, consist of a block of expanded polystyrene, a cardboard or nitrocellulose plate or, a perforated metal plate.
  • the setting mode represented in FIG. 3 is said to be of the rear type.
  • the wedge 11 is disposed at the rear of the propellant charge, leaving a free space 12 at the base of the socket.
  • Figure 4 shows the combination of the two variants described above.
  • the so-called mixed timing is carried out both at the front of the load using the wedge 10, and at the rear with the wedge 11.
  • FIG. 5 Another alternative setting is shown in Figure 5.
  • the load is contained in a thin cylindrical tube 13 made of inert or combustible material such as for example celluloid, nitrocellulose or cardboard.
  • This type of configuration also requires a front setting (Figure 5), a rear setting ( Figure 6) or a mixed setting (Figure 7).
  • the propellant charge is placed outside the cylindrical tube 13.
  • All the examples described above can also be produced from propellant charges made up of grains of powder coated with a binder so as to ensure the compactness of the load.
  • Two pressure sensors were placed in zones A and B respectively located at the level of the base of the socket and near the rear of the launching shoe.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
  • Laminated Bodies (AREA)
  • Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
  • Agricultural Chemicals And Associated Chemicals (AREA)
  • Underground Structures, Protecting, Testing And Restoring Foundations (AREA)

Claims (11)

1. Treibladung (7), bestehend aus Pulver, zum Beispiel in Form von Körnern, zum Antrieb von unterkalibrierten Geschossen mit kinetischer Energie vom Typ großkalibrigem Pfeil (2), die in einer metallischen oder nicht metallischen Rotationshülse (5) angeordnet sind, mit einem Boden an einem Ende und dem Geschoß am anderen Ende, dadurch gekennzeichnet, daß sie Haltemittel zur Gewährleistung ihrer Kompaktheit und ihrer Symmetrie in bezug auf die Rotationsachse der Hülse aufweist, und daß diese Haltemittel die Kompaktierung der Treibladung zum Boden der Hülse hin ermöglichen, indem sie zwischen den Flügeln des pfeilartigen Geschosses und der Ladung einen Freiraum lassen.
2. Treibladung (7), bestehend aus Pulver, zum Beispiel in Form von Körnern, zum Antrieb von unterkalibrierten Geschossen mit kinetischer Energie vom Typ großkalibrigem Pfeil (2), die in einer metallischen oder nicht metallischen Rotationshülse (5) angeordnet sind, mit einem Boden an einem Ende und dem Geschoß am anderen Ende, dadurch gekennzeichnet, daß sie Haltemittel zur Gewährleistung ihrer Kompaktheit und ihrer Symmetrie in bezug auf die Rotationsachse der Hülse aufweist, und daß diese Haltemittel die Kompaktierung der Treibladung zum Geschoß hin ermöglichen, indem sie zwischen dem Boden der Hülse und der Ladung einen Freiraum lassen.
3. Treibladung (7), bestehend aus Pulver, zum Beispiel in Form von Körnern, zum Antrieb von unterkalibrierten Geschossen mit kinetischer Energie vom Typ großkalibrigem Pfeil (2), die in einer metallischen oder nicht metallischen Rotationshülse (5) angeordnet sind, mit einem Boden an einem Ende und dem Geschoß am anderen Ende, dadurch gekennzeichnet, daß sie Haltemittel zur Gewährleistung ihrer Kompaktheit und ihrer Symmetrie in bezug auf die Rotationsachse der Hülse aufweist, und daß diese Haltemittel die Kompaktierung der Treibladung um die Rotationsachse der Hülse herum ermöglichen, indem sie zwischen der Hülse und der Ladung und/oder zwischen dem Zünder und der Ladung einen Freiraum lassen.
4. Treibladung nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, daß das Haltemittel aus einem Binder besteht, der zwischen den Körnern des Pulvers angeordnet ist.
5. Treibladung nach einem derAnsprüche 1 bis 2, dadurch gekennzeichnet, daßdas Haltemittel zum Beispiel aus einem der folgenden Werkstoffe besteht: Pappe, Nitrozellulose oder expandiertes Polystyrol.
6. Treibladung nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, daß das Haltemittel aus einem gelochten Metallblech besteht.
7. Treibladung nach einem der Ansprüche 1 bis 6, dadurch gekennzeichnet, daß das Haltemittel einen Keil (10) aufweist, der am Heck des Geschosses angeordnet ist, so daß die Ladung in Richtung des Bodens der Hülse gedrückt wird.
8. Treibladung nach einem der Ansprüche 2 bis 7, dadurch gekennzeichnet, daß das Haltemittel einen Keil (11) aufweist, der am Boden der Hülse angeordnet ist, so daß die Ladung in Richtung des Geschosses gedrückt wird.
9. Treibladung nach einem der Ansprüche 3 bis 8, dadurch gekennzeichnet, daß das Haltemittel einen Rotationsmantel (13) aufweist, der in Längsrichtung in der Hülse angeordnet ist, so daß sich die Ladung innerhalb dieses Mantels befindet.
10. Treibladung nach einem der Ansprüche 3 bis 8, dadurch gekennzeichnet, daß das Haltemittel einen Rotationsmantel (13) aufweist, der in Längsrichtung in der Hülse angeordnet ist, so daß sich die Ladung außerhalb dieses Mantels befindet.
11. Treibladung nach einem der Ansprüche 9 oder 10, dadurch gekennzeichnet, daß der Rotationsmantel (13) zylinderförmig ist.
EP87401380A 1986-06-19 1987-06-19 Munitionstreibladung, insbesondere für Pfeilgeschosse grossen Kalibers Expired - Lifetime EP0250329B2 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT87401380T ATE50359T1 (de) 1986-06-19 1987-06-19 Munitionstreibladung, insbesondere fuer pfeilgeschosse grossen kalibers.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8608829 1986-06-19
FR8608829A FR2600411B1 (fr) 1986-06-19 1986-06-19 Chargement propulsif de munitions utilisable notamment pour les projectiles fleches de gros calibre

Publications (3)

Publication Number Publication Date
EP0250329A1 EP0250329A1 (de) 1987-12-23
EP0250329B1 EP0250329B1 (de) 1990-02-07
EP0250329B2 true EP0250329B2 (de) 1994-09-28

Family

ID=9336472

Family Applications (1)

Application Number Title Priority Date Filing Date
EP87401380A Expired - Lifetime EP0250329B2 (de) 1986-06-19 1987-06-19 Munitionstreibladung, insbesondere für Pfeilgeschosse grossen Kalibers

Country Status (6)

Country Link
EP (1) EP0250329B2 (de)
AT (1) ATE50359T1 (de)
DE (1) DE3761708D1 (de)
ES (1) ES2014026T5 (de)
FR (1) FR2600411B1 (de)
IL (1) IL82927A (de)

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE540530A (de) * 1954-08-13
US3209689A (en) * 1956-11-14 1965-10-05 Mclennan Donald Elmore Reduction of gun barrel wear
FR1354703A (fr) * 1963-04-30 1964-03-06 Agencement des charges propulsives pour armes à feu de tous types
CH579549A5 (de) * 1973-01-18 1976-09-15 Ciba Geigy Ag
GB1601661A (en) * 1978-02-21 1981-11-04 Dardick D Gas generating charge for open chamber gas powered tool
DE3442741A1 (de) * 1984-11-23 1986-05-28 Rheinmetall GmbH, 4000 Düsseldorf Ladungsanordnung

Also Published As

Publication number Publication date
EP0250329A1 (de) 1987-12-23
IL82927A (en) 1994-05-30
FR2600411A1 (fr) 1987-12-24
EP0250329B1 (de) 1990-02-07
FR2600411B1 (fr) 1990-04-20
DE3761708D1 (de) 1990-03-15
ATE50359T1 (de) 1990-02-15
IL82927A0 (en) 1987-12-20
ES2014026B3 (es) 1990-06-16
ES2014026T5 (es) 1995-08-16

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