EP0463904B1 - Patronenhülsenelement mit verbrennbarer Hülse, mit einem solchen Element versehene halbverbrennbare Munition und Verfahren zum Laden dieser Munition - Google Patents

Patronenhülsenelement mit verbrennbarer Hülse, mit einem solchen Element versehene halbverbrennbare Munition und Verfahren zum Laden dieser Munition Download PDF

Info

Publication number
EP0463904B1
EP0463904B1 EP91401507A EP91401507A EP0463904B1 EP 0463904 B1 EP0463904 B1 EP 0463904B1 EP 91401507 A EP91401507 A EP 91401507A EP 91401507 A EP91401507 A EP 91401507A EP 0463904 B1 EP0463904 B1 EP 0463904B1
Authority
EP
European Patent Office
Prior art keywords
combustible
tube
base
semi
case
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
EP91401507A
Other languages
English (en)
French (fr)
Other versions
EP0463904A1 (de
Inventor
Bernard Conil
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.)
Societe Nationale des Poudres et Explosifs
Original Assignee
Societe Nationale des Poudres et Explosifs
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 Societe Nationale des Poudres et Explosifs filed Critical Societe Nationale des Poudres et Explosifs
Publication of EP0463904A1 publication Critical patent/EP0463904A1/de
Application granted granted Critical
Publication of EP0463904B1 publication Critical patent/EP0463904B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

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
    • F42B5/18—Caseless ammunition; Cartridges having combustible cases
    • F42B5/181—Caseless ammunition; Cartridges having combustible cases consisting of a combustible casing wall and a metal base; Connectors therefor
    • 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
    • F42B5/18—Caseless ammunition; Cartridges having combustible cases
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C19/00—Details of fuzes
    • F42C19/08—Primers; Detonators
    • F42C19/0823—Primers or igniters for the initiation or the propellant charge in a cartridged ammunition
    • F42C19/083—Primers or igniters for the initiation or the propellant charge in a cartridged ammunition characterised by the shape and configuration of the base element embedded in the cartridge bottom, e.g. the housing for the squib or percussion cap
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S102/00—Ammunition and explosives
    • Y10S102/70—Combustilbe cartridge

Definitions

  • the present invention relates to the field of combustible ammunition. More precisely, the invention relates to a socket element with a combustible tube as well as a semi-combustible socket munition incorporating this element. The invention also relates to a method for loading such semi-combustible ammunition.
  • the metal case has certain advantages in terms of robustness and sealing at the rear of the shell at the time of firing, it does however have many disadvantages.
  • one solution consists in using fully combustible sockets.
  • the combustible case has the double advantage of participating in the combustion of the propellant charge and, in so doing, of providing additional energy and of leaving, after combustion, no solid volume containing toxic gases.
  • it is widely used in modern ammunition with fully combustible casings.
  • the latter have, compared to the sockets metal, a drawback in terms of sealing when firing at the rear of the shell.
  • the combustible sockets do not provide, by the very fact that they destroy themselves at the time of the firing, of additional sealing to that presented by the breech closure device.
  • the closing device In conventional weapon systems, the closing device generally provides an effective seal up to 3 ⁇ 108 Pa, ie 3000 bars. This limit is perfectly acceptable for most traditional shells and allows the use of a fully combustible cartridge case. However, this limit is insufficient for certain shells such as the arrow-shells intended to pierce armor and which must be fired at higher pressures, up to 7 ⁇ 108 Pa or 7000 bars. In this case the metal socket has the advantage, if one does not want to modify and weigh down the breech of the weapon system, to bring by its metallic base the essential complement of sealing.
  • the semi-combustible sockets constituted on the one hand by a combustible element in the form of a case and by a metal base.
  • the combustible case participates in the combustion of the propellant charge by providing additional energy and avoiding the retention of a large quantity of toxic gases while the metal base ensures an effective seal at the rear of the projectile even at very high pressures.
  • the metal base ensures an effective seal at the rear of the projectile even at very high pressures.
  • the combustible element is simply a combustible tube, advantageously obtained by spiraling of combustible paper, the junction with the metal base being effected by means of a complementary bottom piece, as described for example in the addition 87,428 to French patent 1,349,818.
  • the fuel element comprises both a tubular part and a bottom which can be embedded directly in the metal base.
  • Such a combustible element is preferably obtained by felting from an aqueous slurry containing the materials constituting the element. combustible.
  • the fixing of the fuel element to the metal base is done by means of a fixing part, in general a fixing ring, coming to wedge the bottom of the element fuel around a hollow internal neck carried by the metal base.
  • This solution is practical but necessarily implies that the interior of the fuel element is cleared at the time of fixing the metal base to allow the introduction and positioning of said fixing part. Consequently, in the semi-combustible sockets currently known, the propellant powder can only be introduced after the metal base has been put in place.
  • correct ignition of large caliber ammunition requires the presence of an ignition tube which is an extension of said hollow neck carried by the metal base and which, for obvious safety reasons, should preferably be put in place. place before the introduction of the powder.
  • the object of the present invention is precisely to eliminate the difficulties set out above by proposing a socket element with a combustible tube which can be loaded with powder from the bottom after the shell and the ignition tube have been installed, or of the reservation of the latter but before installation of the metal base so as to allow easy and automated manufacture of semi-combustible munitions with arrow shells.
  • the invention therefore relates to a fuel tube socket element comprising in particular a fuel tube and a bottom having a central opening, as is known from document FR-A-2 365 096, characterized in that said bottom comprises at side of said central opening, a separate lateral opening and in that is secured to said bottom a hollow part which penetrates into said bushing element through said central opening without closing said lateral opening and which comprises over its entire height a central recess delimited by an internal wall on which are provided means allowing the fixing of a separate part inside said central recess.
  • said bottom consists of an elastic material chosen from the group consisting of polymerization products of chloroprene, neoprene, or mixtures based on ethylene and propylene and comprises a lip d sealing.
  • the invention also relates to an ammunition comprising in particular a semi-combustible shell, a projectile and an ignition tube.
  • said semi-combustible socket is constituted by a socket element according to the invention and by a metal base which carries a central end piece which penetrates into the recess of said hollow part and which comprises complementary fixing means of those carried by said hollow part.
  • the invention also relates to a method of assembling a munition according to the invention characterized in that, after having reserved the space necessary for the ignition tube inside said element and having fixed the projectile to the end of the combustible tube opposite said bottom, said element is filled with propellant powder thanks to said lateral opening and in that only after the metal base is put in place.
  • the ignition tube can thus be put in place after loading and fitting of the metal base, which allows transport and storage of the un-primed ammunition.
  • FIG. 1 shows, in partial section, the lower part of a semi-combustible socket 1 according to the invention.
  • This socket is mainly constituted by a metal base 2, an element 3 with a combustible tube and by a hollow part 4.
  • the semi-combustible socket is filled with propellant powder 5.
  • the socket element 3 with a combustible tube comprises in particular a combustible tube 6 and an also combustible bottom 7 forming a single piece.
  • This unique piece is advantageously obtained by a felting technique from an aqueous slurry containing a mixture of nitrocellulose fibers and cellulose fibers.
  • the bottom 7 has a circular central opening 8.
  • the bottom 7 comprises, next to said central opening 8, a separate lateral opening 9.
  • a hollow part 4 enters said socket element 3 through the said central opening without closing said lateral opening 9 and is secured to said bottom 7.
  • Said hollow part 4 has over its entire height a central recess delimited by an internal wall on which are provided means allowing the fixing of a separate part inside said central recess.
  • FIGS. 2 and 3 show a preferred hollow part 4 according to the invention which has the shape of a ferrule of revolution.
  • This ferrule which is in one piece has a lower cylindrical part 10 whose external diameter is equal to that of the central opening 8 of the bottom 7, a central cylindrical part 11 of the same internal diameter as the part 10 and an upper cylindrical part 12 whose internal diameter is equal to the diameter of the ignition tube which will be used in the ammunition or its reservation.
  • An external stop 13 is advantageously provided at the junction of the parts 10 and 11 so as to allow the part 4 to take a firm support on the bottom 7 and to allow easy joining, for example by gluing.
  • the hollow part 4 is advantageously constituted by an elastic material such as a rubber.
  • an elastic material such as a rubber.
  • rubbers we prefer those which satisfy the following conditions: resist 3000 ° C for 10 milliseconds, be waterproof up to 7x108 Pa or 7000 bars and be compatible with nitroglycerin.
  • the epoxy or cyanoacrylic type necks are recommended by the applicant.
  • the hollow part 4 has a central recess 14 delimited by the internal walls of the parts 10, 11 and 12.
  • the internal wall 15 of the upper part 12 advantageously carries an internal stop 16 intended to facilitate the positioning the ignition tube or its reservation.
  • These means 18 are advantageously constituted by two rectilinear openings 19 and 20 made over the entire thickness of the wall of the middle part 11 so as to be parallel and arranged on either side of the axis of said shell in a same plane perpendicular to said axis, as shown in FIG. 3, and by an elastic metal ring 21 comprising two rectilinear parts 22 and 23 forming bars and engaged respectively in the openings 19 and 20.
  • Such a metal ring 21 is represented in the figure 5.
  • the metal base 2 typically carries a hollow central end piece 24 whose end 25 is frustoconical and which carries a circular groove 26.
  • the end piece 24 enters the recess 14 of the part 4, its frustoconical end 25 repels the elastic bars 22 and 23 which resume, after complete insertion of the endpiece their initial position by being inserted into the groove 26 of the base, then prohibiting any withdrawal of the latter, the groove 26 of the endpiece 24 thus constituting a fixing means complementary to those carried by the hollow part 4.
  • the metal base 2 has a flange 27 terminated by a seal 28 coming to bear against the combustible tube 6.
  • a metal washer 29 is advantageously placed between the bottom 7 and the base 2.
  • FIG 4 there is shown in Figure 4, in partial section, the lower part of a semi-combustible sleeve 101 according to a preferred embodiment of the invention.
  • This socket is mainly constituted by a metal base 102, by a socket element 103 with a combustible tube and by a hollow part 104.
  • the semi-combustible socket is filled with propellant powder 105.
  • the element 103 of the socket is constituted by a combustible tube 106 and by the bottom 107 which is constituted by an elastic material chosen from the group of polymerization products of chloroprene, neoprene or mixtures based on ethylene and propylene such as EPDM (ethylene - propylene - diene monomer).
  • EPDM ethylene - propylene - diene monomer
  • the combustible tube 106 is advantageously obtained by spiraling sheets of combustible paper containing nitrocellulose.
  • the polymer constituting the bottom 107 preferably has a shore hardness of between 40 and 90 shores with an elongation greater than 50%. It is also imperative that the material constituting the bottom 107 has a temperature resistance greater than 1200 ° C. for a few seconds. For this reason we will prefer elastic materials containing a refractory filler such as silica fibers.
  • the materials preferred by the applicant are polychloroprene rubbers containing between 20 and 60% by weight of silica.
  • a preferred embodiment of the bottom 107 is that shown in FIG. 4 according to which the bottom 107 has a flat base provided with a circular central opening 108 and a separate lateral opening 109 and has a lateral rim 130 extended by a lip. 131.
  • the combustible tube 106 is then placed in abutment on the upper part of the lateral flange 130 and against the inner surface of the sealing lip 131. Bonding with an epoxy or cyanoacrylic adhesive makes it possible to effectively join the tube 106 and the bottom 107.
  • the sealing lip 131 is advantageously provided on its external surface with at least one external dye 132.
  • a hollow part 104 similar to the part 4 described above enters the bottom 107 through the central opening 108 and is secured to the latter.
  • the elastic bars 122 and 123 placed in the piece 104 can be constituted by simple metal rods in the shape of a "V" placed in the rectilinear openings made in the piece 104 and retained by a shoulder 133 of the bottom 107 molded against the Exhibit 104.
  • FIG. 6 shows a bar 122 according to this preferred embodiment. The two arms of this bar make between them an angle ⁇ (alpha) of 175 °.
  • the metal base 102 then has a very simple shape since it essentially has the form of a flat disc provided with a central opening 108 and extended by a hollow end piece 124, similar to the hollow end piece 24 described above, and which carries a circular groove 126 constituting the complementary fixing means of the bars 122 and 123.
  • a semi-combustible case according to this preferred variant of the invention has the double advantage of a very great simplicity of manufacture and a very high efficiency in terms of the seal at the rear of the shell during firing. Indeed, at the time of firing, the sealing lip 131, especially when it is provided with flanges 132, ensures by plating against the chamber of the weapon the sealing at low pressure, then the side wall 130 of the bottom 107 similarly, provides medium pressure sealing and finally the metal base 102 provides high pressure sealing. There is thus a socket ensuring perfect sealing in all pressure ranges.
  • the shell elements according to the invention can also be used for fully combustible shell with combustible base, in particular when the bottom 7 of said element is itself combustible.
  • a semi-combustible shell munition according to the invention essentially consists of a shell and a semi-combustible shell (1,101) according to the invention.
  • a semi-combustible socket consists of a socket element 3 or 103 as described above, of a metal base 2 or 102 carrying a central tip 24 or 124 hollow which enters the recess of the hollow part 4 or 104 and which comprises fixing means 26 or 126 complementary to those carried by said hollow part.
  • the semi-combustible socket contains, as already said above, an ignition powder 5 or 105, an ignition tube as well as an igniter plug.
  • the ignition tube is shown under the reference 34 in Figure 1 and under the reference 134 in Figure 4.
  • the igniter plug has not been shown, for clarity, in the figures but is housed in the 'central opening 8 or 108 of the base 2 or 102 respectively.
  • An essential advantage provided by the invention is the simplicity of production and powder loading of an arrow shell munition having a tail unit penetrating deep into the combustible tube.
  • FIG. 7 schematically illustrates the assembly process and loading according to the invention of such ammunition.
  • a munition 40 with an arrow shell.
  • the arrow shell consists of arrow 41, a shoe 42 fixed to a combustible tube 44 and a tail 43 penetrating deep into the combustible tube 44 of a socket element according to the invention.
  • This tube 44 is obtained by spiraling strips of combustible paper and ends with a bottom 45 made of elastic material according to a preferred variant of the invention.
  • the tube 44 and the bottom 45 constitute the socket element according to the invention.
  • a hollow part 46 In the torn-off part of the bottom 45, a hollow part 46 according to the invention is recognized.
  • the propellant powder has not yet been introduced into the socket element but the space necessary for the ignition tube has been reserved by fixing a tube 47 in the extension of the hollow part 46.
  • This tube 47 can be the ignition tube itself or a protective tube inside which will be housed the ignition tube carried by the igniter plug.
  • the ammunition 40 thus formed being positioned as shown in Figure 7, that is to say the shell down, on a support 51, it is then easy to fill with propellant powder the entire free volume of l 'socket element by means of a funnel 49 penetrating into the lateral opening 48 carried by the bottom 45.
  • a funnel 49 penetrating into the lateral opening 48 carried by the bottom 45.
  • the igniter plug can then be fixed to the base 50 so as to obtain the semi-combustible ammunition ready for use.
  • An additional advantage of the invention exists when the reservation of the space necessary for the ignition tube is made by a protective tube which does not allow the powder to pass. In this case, the ammunition 40 can be transported or stored un-primed without an igniter plug, the latter being incorporated into the ammunition only at the time of use, which increases the safety presented by the munitions according to the invention.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Air Bags (AREA)
  • Lighters Containing Fuel (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)

Claims (12)

  1. Patronenhülsenelement (3) mit verbrennbarer Hülse, bestehend insbesondere aus einer verbrennbaren Hülse (6), einem Boden (7) mit einer zentralen Öffnung (8),
    dadurch gekennzeichnet, daß der genannte Boden neben der genannten zentralen Öffnung (8) eine davon getrennte seitliche Öffnung (9) aufweist und daß mit dem genannten Boden (7) ein hohles Teil (4) fest verbunden ist, das in das genannte Patronenhülsenelement durch die genannte zentrale Öffnung (8) eindringt, ohne die genannte seitliche Öffnung (9) zu verschließen, und über seine gesamte Höhe eine zentrale Vertiefung (14) aufweist, die von einer Innenwandung (17) umgrenzt ist, an der Mittel (18) ausgeführt sind, mit denen ein separates Teil im Inneren der genannten zentralen Vertiefung (14) befestigt werden kann.
  2. Patronenhülsenelement nach Anspruch 1,
    dadurch gekennzeichnet, daß das genannte hohle Teil (4) ein elastisches Teil ist.
  3. Patronenhülsenelement nach Anspruch 2,
    dadurch gekennzeichnet, daß das genannte hohle Teil (4) ein Rotationsring ist.
  4. Patronenhülsenelement nach Anspruch 3,
    dadurch gekennzeichnet, daß die Innenwandung (17) des genannten hohlen Teils einen Innenanschlag (16) aufweist und daß die genannten Befestigungsmittel (18) zwischen dem genannten Boden (7) und dem genannten Innenanschlag (16) angeordnet sind.
  5. Patronenhülsenelement nach Anspruch 3,
    dadurch gekennzeichnet, daß die genannten Befestigungsmittel (18) von zwei parallelen, geradlinigen Öffnungen (19, 20), die zu beiden Seiten der Achse des genannten Rings in derselben, zu der genannten Achse senkrecht stehenden Ebene angeordnet sind, und von zwei elastischen Stegen (22, 23), die in den genannten Öffnungen angeordnet sind, gebildet werden.
  6. Patronenhülsenelement nach Anspruch 1,
    dadurch gekennzeichnet, daß die genannte Hülse (6) und der genannte Boden (7) ein einziges verbrennbares Teil bilden.
  7. Patronenhülsenelement nach Anspruch 1,
    dadurch gekennzeichnet, daß die genannte Hülse (106) eine verbrennbare Hülse ist und daß der genannte Boden (107) aus einem elastischen Material besteht, das aus der Gruppe der Polymerisationsprodukte von Chloropren, Neopren oder Mischungen auf Ethylen- und Propylenbasis gewählt wird.
  8. Patronenhülsenelement nach Anspruch 7,
    dadurch gekennzeichnet, daß das genannte elastische Material, aus dem der Boden (107) besteht, mit hitzebeständigem Mineral angereichert ist.
  9. Patronenhülsenelement nach Anspruch 7,
    dadurch gekennzeichnet, daß der genannte Boden (107) mit einer Dichtungslippe (131) versehen ist.
  10. Patronenhülsenelement nach Anspruch 9,
    dadurch gekennzeichnet, daß die genannte Lippe (131) mit mindestens einem Außenkragen (132) versehen ist.
  11. Munition, die insbesondere aus einer halbverbrennbaren Patronenhülse, einem Geschoß und einer Zündhülse besteht, dadurch gekennzeichnet, daß die halbverbrennbare Patronenhülse (1, 101) im wesentlichen aus einem Patronenhülsenelement nach einem der Ansprüche 1 bis 10 sowie aus einem Metallsockel (2, 102) besteht, der ein zentrales, hohles Ansatzstück (24, 124) aufweist, das in die Vertiefung des genannten hohlen Teils (4, 104) eindringt und Befestigungsmittel (26, 126) aufweist, die komplementär zu denen des genannten hohlen Teils sind.
  12. Verfahren zum Zusammensetzen einer halbverbrennbaren Munition (40) nach Anspruch 11, die ein Geschoß (41), einen Metallsockel (50) und ein Patronenhülsenelement umfaßt, das von einer verbrennbaren Hülse (44), einem Boden (45) mit einer seitlichen Öffnung (48) und einem hohlen Teil (46) gebildet wird,
    bestehend darin, daß, nachdem der für die Zündhülse benötigte Raum freigehalten und das Geschoß (41) an dem vom genannten Boden (45) abgewandten Ende der verbrennbaren Hülse (44) befestigt wurde, das genannte Element durch die genannte seitliche Öffnung (48) mit Schießpulver gefüllt wird und daß erst danach der Metallsockel (50) angebracht wird.
EP91401507A 1990-06-25 1991-06-10 Patronenhülsenelement mit verbrennbarer Hülse, mit einem solchen Element versehene halbverbrennbare Munition und Verfahren zum Laden dieser Munition Expired - Lifetime EP0463904B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9007928A FR2663730B1 (fr) 1990-06-25 1990-06-25 Element de douille a tube combustible, munition a douille semi-combustible incorporant cet element et procede de chargement de cette munition.
FR9007928 1990-06-25

Publications (2)

Publication Number Publication Date
EP0463904A1 EP0463904A1 (de) 1992-01-02
EP0463904B1 true EP0463904B1 (de) 1994-10-26

Family

ID=9397957

Family Applications (1)

Application Number Title Priority Date Filing Date
EP91401507A Expired - Lifetime EP0463904B1 (de) 1990-06-25 1991-06-10 Patronenhülsenelement mit verbrennbarer Hülse, mit einem solchen Element versehene halbverbrennbare Munition und Verfahren zum Laden dieser Munition

Country Status (8)

Country Link
US (2) US5247888A (de)
EP (1) EP0463904B1 (de)
JP (1) JPH081360B2 (de)
KR (1) KR940011930B1 (de)
DE (1) DE69104781T2 (de)
ES (1) ES2065636T3 (de)
FR (1) FR2663730B1 (de)
IL (1) IL98343A0 (de)

Families Citing this family (68)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4318740C2 (de) * 1993-06-05 1998-03-12 Rheinmetall Ind Ag Munitionseinheit
US5770815A (en) * 1995-08-14 1998-06-23 The United States Of America As Represented By The Secretary Of The Navy Ammunition cartridge with reduced propellant charge
US5681526A (en) * 1996-04-23 1997-10-28 Usx Corporation Method and apparatus for post-combustion of gases during the refining of molten metal
FR2799831B1 (fr) 1999-10-13 2001-11-30 Giat Ind Sa Dispositif de fixation d'un culot obturateur sur un etui de munition et culot adapte a un tel dispositif
FR2806789B1 (fr) * 2000-03-23 2002-06-07 Giat Ind Sa Tube allumeur pour une munition d'artillerie
US6343552B1 (en) * 2000-06-06 2002-02-05 Alliant Techsystems Inc. Solvent application system
US6748870B2 (en) * 2001-10-22 2004-06-15 Armtec Defense Products Company Ammunition round assembly with combustible cartridge case
KR20030039764A (ko) * 2001-11-14 2003-05-22 엘지이노텍 주식회사 전파 고도계 점검 시스템
US6857370B1 (en) * 2002-04-10 2005-02-22 General Dynamics Ordnance And Tactical Systems, Inc. Primer body
US7913625B2 (en) 2006-04-07 2011-03-29 Armtec Defense Products Co. Ammunition assembly with alternate load path
US20120260814A1 (en) 2008-04-25 2012-10-18 Alliant Techsystems Inc. Advanced Muzzle Loader Ammunition
US20120318123A1 (en) 2011-06-14 2012-12-20 Alliant Techsystems Inc. Muzzle Loader Powder Increment using Celluloid Combustible Container
JP5199002B2 (ja) * 2008-09-25 2013-05-15 旭化成ケミカルズ株式会社 少なくとも２層から構成された焼尽性容器
US10480915B2 (en) 2010-11-10 2019-11-19 True Velocity Ip Holdings, Llc Method of making a polymeric subsonic ammunition cartridge
US11231257B2 (en) 2010-11-10 2022-01-25 True Velocity Ip Holdings, Llc Method of making a metal injection molded ammunition cartridge
US10081057B2 (en) 2010-11-10 2018-09-25 True Velocity, Inc. Method of making a projectile by metal injection molding
US10190857B2 (en) 2010-11-10 2019-01-29 True Velocity Ip Holdings, Llc Method of making polymeric subsonic ammunition
US11047664B2 (en) 2010-11-10 2021-06-29 True Velocity Ip Holdings, Llc Lightweight polymer ammunition cartridge casings
US11047663B1 (en) 2010-11-10 2021-06-29 True Velocity Ip Holdings, Llc Method of coding polymer ammunition cartridges
US10048049B2 (en) 2010-11-10 2018-08-14 True Velocity, Inc. Lightweight polymer ammunition cartridge having a primer diffuser
US8561543B2 (en) 2010-11-10 2013-10-22 True Velocity, Inc. Lightweight polymer ammunition cartridge casings
US11340050B2 (en) 2010-11-10 2022-05-24 True Velocity Ip Holdings, Llc Subsonic polymeric ammunition cartridge
US10408592B2 (en) 2010-11-10 2019-09-10 True Velocity Ip Holdings, Llc One piece polymer ammunition cartridge having a primer insert and methods of making the same
US11209252B2 (en) 2010-11-10 2021-12-28 True Velocity Ip Holdings, Llc Subsonic polymeric ammunition with diffuser
US11313654B2 (en) 2010-11-10 2022-04-26 True Velocity Ip Holdings, Llc Polymer ammunition having a projectile made by metal injection molding
US10048052B2 (en) 2010-11-10 2018-08-14 True Velocity, Inc. Method of making a polymeric subsonic ammunition cartridge
US10352670B2 (en) 2010-11-10 2019-07-16 True Velocity Ip Holdings, Llc Lightweight polymer ammunition cartridge casings
US10591260B2 (en) 2010-11-10 2020-03-17 True Velocity Ip Holdings, Llc Polymer ammunition having a projectile made by metal injection molding
US11118875B1 (en) 2010-11-10 2021-09-14 True Velocity Ip Holdings, Llc Color coded polymer ammunition cartridge
US10429156B2 (en) 2010-11-10 2019-10-01 True Velocity Ip Holdings, Llc Subsonic polymeric ammunition cartridge
US10876822B2 (en) 2017-11-09 2020-12-29 True Velocity Ip Holdings, Llc Multi-piece polymer ammunition cartridge
US11300393B2 (en) 2010-11-10 2022-04-12 True Velocity Ip Holdings, Llc Polymer ammunition having a MIM primer insert
US9885551B2 (en) 2010-11-10 2018-02-06 True Velocity, Inc. Subsonic polymeric ammunition
US10041770B2 (en) 2010-11-10 2018-08-07 True Velocity, Inc. Metal injection molded ammunition cartridge
US11293732B2 (en) 2010-11-10 2022-04-05 True Velocity Ip Holdings, Llc Method of making polymeric subsonic ammunition
USD861118S1 (en) 2011-11-09 2019-09-24 True Velocity Ip Holdings, Llc Primer insert
US9587918B1 (en) 2015-09-24 2017-03-07 True Velocity, Inc. Ammunition having a projectile made by metal injection molding
US9551557B1 (en) * 2016-03-09 2017-01-24 True Velocity, Inc. Polymer ammunition having a two-piece primer insert
US9869536B2 (en) * 2016-03-09 2018-01-16 True Velocity, Inc. Method of making a two-piece primer insert
US9518810B1 (en) * 2016-03-09 2016-12-13 True Velocity, Inc. Polymer ammunition cartridge having a two-piece primer insert
US9506735B1 (en) * 2016-03-09 2016-11-29 True Velocity, Inc. Method of making polymer ammunition cartridges having a two-piece primer insert
US9523563B1 (en) * 2016-03-09 2016-12-20 True Velocity, Inc. Method of making ammunition having a two-piece primer insert
US9835427B2 (en) 2016-03-09 2017-12-05 True Velocity, Inc. Two-piece primer insert for polymer ammunition
US10760882B1 (en) 2017-08-08 2020-09-01 True Velocity Ip Holdings, Llc Metal injection molded ammunition cartridge
USD886937S1 (en) 2017-12-19 2020-06-09 True Velocity Ip Holdings, Llc Ammunition cartridge
USD886231S1 (en) 2017-12-19 2020-06-02 True Velocity Ip Holdings, Llc Ammunition cartridge
US11435171B2 (en) 2018-02-14 2022-09-06 True Velocity Ip Holdings, Llc Device and method of determining the force required to remove a projectile from an ammunition cartridge
WO2020010100A1 (en) 2018-07-06 2020-01-09 True Velocity Ip Holdings, Llc Three-piece primer insert for polymer ammunition
US11733015B2 (en) 2018-07-06 2023-08-22 True Velocity Ip Holdings, Llc Multi-piece primer insert for polymer ammunition
US10704880B1 (en) 2019-02-14 2020-07-07 True Velocity Ip Holdings, Llc Polymer ammunition and cartridge having a convex primer insert
US10704872B1 (en) 2019-02-14 2020-07-07 True Velocity Ip Holdings, Llc Polymer ammunition and cartridge having a convex primer insert
US10704879B1 (en) 2019-02-14 2020-07-07 True Velocity Ip Holdings, Llc Polymer ammunition and cartridge having a convex primer insert
US10731957B1 (en) 2019-02-14 2020-08-04 True Velocity Ip Holdings, Llc Polymer ammunition and cartridge having a convex primer insert
US10921106B2 (en) 2019-02-14 2021-02-16 True Velocity Ip Holdings, Llc Polymer ammunition and cartridge having a convex primer insert
USD893666S1 (en) 2019-03-11 2020-08-18 True Velocity Ip Holdings, Llc Ammunition cartridge nose having an angled shoulder
USD893667S1 (en) 2019-03-11 2020-08-18 True Velocity Ip Holdings, Llc Ammunition cartridge nose having an angled shoulder
USD893665S1 (en) 2019-03-11 2020-08-18 True Velocity Ip Holdings, Llc Ammunition cartridge nose having an angled shoulder
USD893668S1 (en) 2019-03-11 2020-08-18 True Velocity Ip Holdings, Llc Ammunition cartridge nose having an angled shoulder
USD891568S1 (en) 2019-03-12 2020-07-28 True Velocity Ip Holdings, Llc Ammunition cartridge nose having an angled shoulder
USD891567S1 (en) 2019-03-12 2020-07-28 True Velocity Ip Holdings, Llc Ammunition cartridge nose having an angled shoulder
USD892258S1 (en) 2019-03-12 2020-08-04 True Velocity Ip Holdings, Llc Ammunition cartridge nose having an angled shoulder
USD891569S1 (en) 2019-03-12 2020-07-28 True Velocity Ip Holdings, Llc Ammunition cartridge nose having an angled shoulder
USD891570S1 (en) 2019-03-12 2020-07-28 True Velocity Ip Holdings, Llc Ammunition cartridge nose
WO2020197868A2 (en) 2019-03-19 2020-10-01 True Velocity Ip Holdings, Llc Methods and devices metering and compacting explosive powders
USD894320S1 (en) 2019-03-21 2020-08-25 True Velocity Ip Holdings, Llc Ammunition Cartridge
EP3999799A4 (de) 2019-07-16 2023-07-26 True Velocity IP Holdings, LLC Polymermunition mit ausrichthilfe, patrone und verfahren zu deren herstellung
DE102020001052A1 (de) 2020-02-19 2021-08-19 Nitrochemie Aschau Gmbh Hülsenmantel
FR3119231B1 (fr) 2021-01-26 2023-10-20 Nexter Munitions Dispositif de liaison entre un moyen d'allumage d'une charge propulsive et un etui combustible d'une munition, etui combustible et rondelle elastique associes a un tel dispositif de liaison.

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE524909A (de) *
FR1006140A (fr) * 1947-11-21 1952-04-21 Perfectionnements aux douilles de munitions
FR1078338A (fr) * 1952-07-16 1954-11-17 Douille à culot amovible pour armes de chasse
BE524509A (de) * 1952-11-26
US2812958A (en) * 1955-11-07 1957-11-12 Stile Craft Mfg Inc Cam release pipe coupler
US2935945A (en) * 1958-03-28 1960-05-10 James J Brady Pressure sealing plug for cartridge case
US3170401A (en) * 1962-09-11 1965-02-23 Walter T Johnson Cartridge case
US3224373A (en) * 1963-05-01 1965-12-21 Aerojet General Co Igniter device for solid body of pyrotechnic material
FR1391733A (fr) * 1963-10-10 1965-03-12 Douille souple ou semi-rigide, combustible ou non, avec éjection par la bouche, pour les munitions de canons
FR1405996A (fr) * 1964-06-04 1965-07-16 Baronne Von Thyssen Bornemisza Douille d'artillerie en deux pièces, l'une combustible, l'autre en métal
US3401632A (en) * 1965-05-03 1968-09-17 Trojan Powder Co Packaged booster explosive
US3320886A (en) * 1965-08-31 1967-05-23 Hawley Products Co Cartridge case and method for the manufacture thereof
US3741121A (en) * 1971-09-03 1973-06-26 Olin Corp Fusee cover
ES211994Y (es) * 1975-04-29 1976-11-01 Cartucho mejorado.
US3978793A (en) * 1975-06-30 1976-09-07 The United States Of America As Represented By The Secretary Of The Army Muzzle-expellable cartridge
DE2641665C2 (de) * 1976-09-16 1984-03-01 Rheinmetall GmbH, 4000 Düsseldorf Treibladungshülse
DE2902145A1 (de) * 1979-01-16 1980-08-07 Ultrafin S A Patronenhuelse
US4526411A (en) * 1980-10-29 1985-07-02 Proprietary Technology, Inc. Swivelable quick connector assembly
JPS5858598A (ja) * 1981-10-02 1983-04-07 株式会社日立製作所 音声認識方式
FR2536804B1 (fr) * 1982-11-25 1986-03-07 Moussaian Gregoire Dispositif de liaison perfectionne a assemblage et demontage rapides
DE3409017A1 (de) * 1984-03-13 1985-09-26 Rheinmetall GmbH, 4000 Düsseldorf Patronierte munition fuer rohrwaffen
US4884829A (en) * 1986-09-16 1989-12-05 Johannes Schaefer Vorm. Stettiner Schraubenwerke Gmbh & Co. Kg Plug-in connection for connecting tube and host lines in particular for use in tube-line systems of motor vehicles
DE3924986A1 (de) * 1989-07-28 1991-01-31 Rheinmetall Gmbh Treibladungsbehaelter

Also Published As

Publication number Publication date
ES2065636T3 (es) 1995-02-16
EP0463904A1 (de) 1992-01-02
IL98343A0 (en) 1992-07-15
JPH081360B2 (ja) 1996-01-10
US5247888A (en) 1993-09-28
US5277118A (en) 1994-01-11
DE69104781D1 (de) 1994-12-01
KR920001173A (ko) 1992-01-30
FR2663730A1 (fr) 1991-12-27
DE69104781T2 (de) 1995-03-09
FR2663730B1 (fr) 1992-09-11
JPH0618197A (ja) 1994-01-25
KR940011930B1 (ko) 1994-12-27

Similar Documents

Publication Publication Date Title
EP0463904B1 (de) Patronenhülsenelement mit verbrennbarer Hülse, mit einem solchen Element versehene halbverbrennbare Munition und Verfahren zum Laden dieser Munition
FR2526151A1 (fr) Munition encartouchee constituee par un projectile et une douille combustible ou partiellement combustible reliee a celui-ci
FR2702555A1 (fr) Etui pour une munition de type télescopée.
FR2799832A1 (fr) Dispositif d'allumage pour un chargement propulsif
FR2679993A1 (fr) Munition, en particulier du type telescope.
EP2297545B1 (de) Nicht tödliche munition
EP0307307B1 (de) Verbindungsring zwischen Geschoss und Geschosshülse
EP1181498B1 (de) Anzündrohr für artilleriemunition
FR2705772A1 (fr) Projectile d'exercice.
EP1712873A1 (de) Adapter für ein Mörsergeschoss in einem Geschützlauf
FR2622687A1 (fr) Chargement propulsif pour munition comportant un projectile empenne ainsi que son procede de realisation
FR2748318A1 (fr) Dispositif d'injection de plasma
EP0499500B1 (de) Behälter, vorgesehen mit elektrischen Verbindungsmitteln
WO1994021981A1 (fr) Dispositif d'etancheite aux gaz de propulsion pour munitions d'artillerie
FR2614096A1 (fr) Objets combustibles en forme d'etui borgne
EP0691520B1 (de) Vorrichtung zur Verbindung von zwei Behältern und Behälter dafür
EP1103780B1 (de) Verbindungsteil zwischen Geschoss und Geschosshülse und Methode zur Montage eines Dichtringes mittels eines derartigen Verbindungteiles
FR2463382A1 (fr) Tete de contact pour projectiles tires par des lanceurs a commande electrique
EP0147314B1 (de) Kunststoffbodenkörper
FR2679991A1 (fr) Perfectionnements apportes a une munition en particulier du type telescope.
BE524509A (de)
EP1023573B1 (de) Treibkäfig mit verbesserter gasabdichtung für submunitionskörper
EP1586852A1 (de) Hülsenlose Munition und Herstellungsverfahren dafür
FR2710975A1 (fr) Elément de munition d'artillerie et munition obtenue par assemblage d'une pluralité de tels éléments.
EP0763707A1 (de) Befestigte Abdichtungsvorrichtung zwischen der Umhüllung und dem Hülsenboden eines Trägergeschosses

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): DE ES FR GB IT

17P Request for examination filed

Effective date: 19920515

17Q First examination report despatched

Effective date: 19940208

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE ES FR GB IT

ITF It: translation for a ep patent filed
REF Corresponds to:

Ref document number: 69104781

Country of ref document: DE

Date of ref document: 19941201

GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)

Effective date: 19941103

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2065636

Country of ref document: ES

Kind code of ref document: T3

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
REG Reference to a national code

Ref country code: GB

Ref legal event code: IF02

REG Reference to a national code

Ref country code: FR

Ref legal event code: CD

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20040609

Year of fee payment: 14

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20040611

Year of fee payment: 14

REG Reference to a national code

Ref country code: FR

Ref legal event code: TP

REG Reference to a national code

Ref country code: GB

Ref legal event code: 732E

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20040830

Year of fee payment: 14

REG Reference to a national code

Ref country code: ES

Ref legal event code: PC2A

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED.

Effective date: 20050610

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20050610

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20060103

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20060228

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20050610

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20060228

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: ES

Payment date: 20060622

Year of fee payment: 16

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20070611

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20070611