[go: up one dir, main page]

EP0114591B1 - Process for the production of arm barrels - Google Patents

Process for the production of arm barrels Download PDF

Info

Publication number
EP0114591B1
EP0114591B1 EP83890232A EP83890232A EP0114591B1 EP 0114591 B1 EP0114591 B1 EP 0114591B1 EP 83890232 A EP83890232 A EP 83890232A EP 83890232 A EP83890232 A EP 83890232A EP 0114591 B1 EP0114591 B1 EP 0114591B1
Authority
EP
European Patent Office
Prior art keywords
tube
alloy
jacket tube
casing
liner
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
EP83890232A
Other languages
German (de)
French (fr)
Other versions
EP0114591A1 (en
Inventor
Manfred Gstettner
Bruno Dipl.-Ing. Hribernik
Alexander Kohnhauser
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.)
Voest-Alpine Stahl AG Te Linz Ad
Original Assignee
Vereinigte Edelstahlwerke AG
Voestalpine Stahl GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=3567024&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=EP0114591(B1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Vereinigte Edelstahlwerke AG, Voestalpine Stahl GmbH filed Critical Vereinigte Edelstahlwerke AG
Publication of EP0114591A1 publication Critical patent/EP0114591A1/en
Application granted granted Critical
Publication of EP0114591B1 publication Critical patent/EP0114591B1/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/12Both compacting and sintering
    • B22F3/1208Containers or coating used therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/06Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
    • B22F7/062Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/06Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
    • B22F7/08Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools with one or more parts not made from powder
    • 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
    • F41A21/00Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
    • F41A21/02Composite barrels, i.e. barrels having multiple layers, e.g. of different materials
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2998/00Supplementary information concerning processes or compositions relating to powder metallurgy
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12014All metal or with adjacent metals having metal particles
    • Y10T428/12028Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, etc.]
    • Y10T428/12063Nonparticulate metal component
    • Y10T428/12097Nonparticulate component encloses particles

Definitions

  • the invention relates to a method for producing gun barrels with incorporated trains for guns or handguns, the gun barrels having a core barrel and a jacket barrel made of different metallic materials.
  • Gun barrels are subject to two completely different stresses: on the one hand, the explosion of the propellant charge of a projectile creates a high pressure inside the barrel, which the gun barrel must be able to withstand, and on the other hand the projectile is driven through the barrel at high speed, thereby stabilizing the bullet trajectory the projectile is rotated by the cables in the gun barrel, which creates an extremely abrasive load on the barrel interior.
  • these two loads place different demands on the material.
  • One way to meet these different requirements is to provide the gun barrels with a correspondingly large dimension, as a result of which the mobility of the weapons suffers and an extremely high amount of material is required.
  • a method for the manufacture of gun barrels has already become known, wherein a core tube is inserted into a casing tube in a snug fit.
  • the disadvantage of this method is that particularly precise machining of both the inner hollow of the casing tube and the outer casing of the core tube is required. If the inner tube is damaged, for example as a result of cracks that can be attributed to the pressure, a major change in the caliber can occur, which can lead to the projectile being destroyed by the projectile.
  • a method is described which is suitable for lining cavities, including pipes.
  • a gap is created in a casing tube, for example made of steel, by introducing a thin-walled metal part, into which metal powder is filled, the gap is then evacuated and then the body with the metal part and powder contained therein at approx. 1150 ° C. and 103 N / mm 2 is compressed. A final post-processing is possible.
  • No. 4,327,154 discloses a method for producing tubular parts, a composite part being produced by applying a powder component to a tubular metal shell with hot isostatic pressing between 1000 ° C. to 1400 ° C. and pressures from 10 to 1000 bar.
  • the present invention had for its object to provide a method for producing gun barrels that are suitable for guns as well as for hand and handguns that have a core tube and at least one jacket tube made of different metallic materials, which allows a to produce a particularly light and resistant weapon barrel.
  • the method according to the invention for the manufacture of weapon tubes which have a core tube and at least one jacket tube made of different metallic materials, consists essentially in the fact that in a sleeve tube, which is arranged in a capsule tube, a filling made of a bulk density of a tough alloy at least 60% of the density of the compact, powdery, highly wear-resistant or corrosion-resistant material is introduced and compacted with the exception of a central hollow area by a filler made of free-cutting steel, is closed at the ends of the casing or capsule tube, whereupon the tube is evacuated and the sealed tube in a protective gas atmosphere , at least 900 ° C, but below the melting point of the metallic materials and a pressure of at least 900 bar and that after a heat treatment of the composite body thus obtained, which between a full-surface metallic composite n has a casing tube and compressed material, is then subjected to at least 1.3 times the hot deformation, mechanically processed and trains are created.
  • a weapon barrel manufactured according to this method has the
  • titanium or a titanium alloy is used as a tough material, a particularly low-weight weapon barrel can be produced.
  • high wear-resistant alloy For gun barrels for guns or the like with a particularly elongated shot trajectory is considered to be high wear-resistant alloy uses a cobalt-based alloy.
  • a nickel-based alloy is used as the material for filling the casing tube.
  • a sleeve tube which has a coating of an adhesion promoter, e.g. Nickel or the like.
  • a composite metal tube part was produced by using X40CrMoV51 (with 0.38% C, 1.1% Si, 0.38% Mn, 5.20% Cr, 1.30% Mo and 1.2% V, the rest essentially iron) of the dimension: 46 mm outer diameter, 15 mm wall thickness and 650 mm length, a rod of the same length made of free-cutting steel is inserted centrally and in the remaining cavity a metal powder made of a heat-resistant nickel-based alloy with the composition 0, 12% C, 20.0% Cr, 18.1% Co, 2.5% Ti, 1.5% Al, 1.5% Fe, the rest essentially nickel.
  • the tube ends were sealed gas-tight by welding circular sheet metal disks onto the jacket tube and the hot isostatic pressing process was carried out at 1080 ° C. and a gas pressure of 1100 bar for 3 hours.
  • the central core made of free-cutting steel was completely drilled out and then the further mechanical processing was carried out to produce the trains and to complete the run.
  • a sleeve tube made of an alloy of the following composition in wt .-% C 0.33, Si 0.28, Mn 0.50, Cr 3.0, Mo 1.2, V 0.27 and remainder iron with an outer diameter of 60 mm and an inner diameter of 40 mm and a length of 800 mm.
  • the hollow cylindrical space was filled with a powder of a cobalt-based alloy with the following composition in% by weight C 0.17, Si 0.35, Mn 0.65, Cr 28.9, Mo 5.6, Ni max. 0.5, Co 66.0 and Fe max. 0.5 filled, a density of 6.5 g / cm 3 was achieved by shaking. Degassing was carried out at 350 ° C., whereupon an upper cover with a suction opening was welded onto the capsule tube. Then it was evacuated and the suction opening was closed. The encapsulated body was hot-isostatically pressed for 3 hours in an argon atmosphere at 1150 ° C. and at a pressure of 1000 bar.
  • This composite body was then forged on a long forging machine to an outer diameter of approx. 35 mm, which corresponds to an approximate triple deformation.
  • solution annealing was carried out at 1100 ° C for one hour, after which a barrel for a heavy machine gun was made by mechanical processing and cold forging of the trains.
  • a cylindrical rod made of free-cutting steel with an outside diameter of 45 mm and a length of 900 mm was inserted in the center of the casing tube.
  • the hollow cylindrical space was filled with a powder of a cobalt-based alloy with the following composition in% by weight C 0.17, Si 0.35, Mn 0.65, Cr 28.0, Mo 5.5, Ni max. 0.5, Co 66.0 and Fe max. 0.5 filled, a density of 6.7 g / cm 3 was achieved by shaking.
  • Degassing was carried out at 340 ° C., whereupon an upper cover with a suction opening was welded on. It was then evacuated and hot-isostatically pressed according to Example 2.
  • the composite body thus obtained was forged on a long forging machine to a diameter of 105 mm or 35 mm or 23 mm and a length of 3500 mm, which corresponds to a fourfold deformation.
  • the further processing was carried out analogously to Example 2, but a tensile strength of 900-1100 N / m 2 was set by tempering the jacket tube.
  • the tube obtained had a caliber of 1 "and was used for a rapid-fire cann
  • a sleeve tube made of TiA16V4 with an outer diameter of 210 mm and an inner diameter of 160 mm and a length of 900 mm was introduced.
  • a core rod made of free-cutting steel with a diameter of 45 mm and a length of 900 mm was then introduced into this casing tube.
  • the intermediate space was filled with a powder of the following composition in% by weight C 0.34, Cr 1.2, Mo 0.2, Al 0.95, remainder Fe. It was compressed to 70% of the density.
  • the procedure was then as in Example 3 and the composite body was forged to a diameter of 105 mm or 35 mm and a length of 350 mm, which corresponds to a fourfold deformation.
  • This composite was heated at 940 ° C for one hour and then cooled in oil and tempered at 520 ° C for four hours. After processing, the inner Surface nitrided in a manner known per se to a depth of 0.3 to 0.4 mm.
  • the sleeve tube can also be welded directly to the cover, since the powder can not act radially due to the material thickness of the sleeve tube.
  • the core can also be formed by a hollow cylinder, in which case, which is particularly suitable for larger calibers, forging can be carried out using a mandrel.
  • a cladding tube can also be used which has an inner coating, e.g. B. electrodeposited from nickel or the like., which can occur as an adhesion promoter between the material of the cladding tube and the powder.
  • an inner coating e.g. B. electrodeposited from nickel or the like.

Landscapes

  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Materials Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Forging (AREA)
  • Powder Metallurgy (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Crystals, And After-Treatments Of Crystals (AREA)
  • Semiconductor Lasers (AREA)
  • Manufacture And Refinement Of Metals (AREA)
  • Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
  • Preventing Corrosion Or Incrustation Of Metals (AREA)
  • Coating With Molten Metal (AREA)
  • Glass Compositions (AREA)

Abstract

The weapon barrel comprises a liner and at least one jacket tube. The liner is made of a highly wear-resistant material, like a cobalt or nickel base alloy, and the jacket tube is made of a tough alloy, like steel. In the manufacturing process the liner material is packed into the jacket tube in the form of a powdery material which may be pre-pressed or pre-sintered. The packing is arranged such as to leave a central free space in the jacket tube, and the jacket tube may be surrounded by an encapsulating tube. The jacket tube or the encapsulating tube is closed either before or after evacuation, and the closed tube arrangement is subjected to a combined heat and pressure treatment at temperatures of at least 900 DEG C., but below the melting point of the relevant materials and at pressures of at least 900 bar. The compound body thus obtained is formed with a full-area metallic bond between the liner and the jacket tube. After eventual heat treatment the compound body is further machined and a rifling is worked thereinto as, for example, by forging.

Description

Die Erfindung betrifft ein Verfahren zur Herstellung von Waffenrohren mit eingearbeiteten Zügen für Geschütze oder Handfeuerwaffen, wobei die Waffenrohre ein Seelenrohr und ein Mantelrohr aus unterschiedlichen, metallischen Werkstoffen aufweisen.The invention relates to a method for producing gun barrels with incorporated trains for guns or handguns, the gun barrels having a core barrel and a jacket barrel made of different metallic materials.

Waffenrohre unterliegen zwei vollkommen unterschiedlichen Beanspruchungen, und zwar wird einerseits durch die Explosion der Treibladung eines Geschosses im Laufinneren ein hoher Druck aufgebaut, welchem das Waffenrohr gewachsen sein muss, andererseits wird das Projektil mit einer hohen Geschwindigkeit durch den Lauf getrieben, wobei zur Stabilisierung der Geschossbahn das Projektil durch die Züge im Waffenrohr in Rotation versetzt wird, wodurch eine extrem abrasive Beanspruchung des Laufinneren gegeben ist. Diese beiden Beanspruchungen stellen jedoch unterschiedliche Anforderungen an den Werkstoff. Eine Möglichkeit, diesen unterschiedlichen Anforderungen gerecht zu werden, besteht darin, eine entsprechend grosse Dimensionierung der Waffenrohre vorzusehen, wodurch die Mobilität der Waffen leidet und ein überaus hoher Materialeinsatz erforderlich wird.Gun barrels are subject to two completely different stresses: on the one hand, the explosion of the propellant charge of a projectile creates a high pressure inside the barrel, which the gun barrel must be able to withstand, and on the other hand the projectile is driven through the barrel at high speed, thereby stabilizing the bullet trajectory the projectile is rotated by the cables in the gun barrel, which creates an extremely abrasive load on the barrel interior. However, these two loads place different demands on the material. One way to meet these different requirements is to provide the gun barrels with a correspondingly large dimension, as a result of which the mobility of the weapons suffers and an extremely high amount of material is required.

Es ist bereits ein Verfahren zur Herstellung von Waffenrohren bekannt geworden, wobei in ein Mantelrohr ein Seelenrohr im Passsitz eingebracht wird. Nachteilig bei diesem Verfahren ist, dass eine besonders genaue Bearbeitung sowohl des Innenhohls des Mantelrohres als auch des äusseren Mantels des Seelenrohrs erforderlich ist. Bei Beschädigungen des Innenrohres, wie sie beispielsweise durch Risse, welche auf die Druckbeanspruchung zurückzuführen sind, entstehen, kann eine wesentliche Veränderung des Kalibers eintreten, womit es zur Zerstörung des Geschützrohres durch ein Projektil kommen kann.A method for the manufacture of gun barrels has already become known, wherein a core tube is inserted into a casing tube in a snug fit. The disadvantage of this method is that particularly precise machining of both the inner hollow of the casing tube and the outer casing of the core tube is required. If the inner tube is damaged, for example as a result of cracks that can be attributed to the pressure, a major change in the caliber can occur, which can lead to the projectile being destroyed by the projectile.

Es ist auch bereits bekannt geworden, zwischen einem Seelenrohr aus Stahl und einem Aussenrohr aus Stahl eine faserverstärkte Schicht als Verbindungsrohr vorzusehen. Derartige Konstruktionen sind sowohl für ein Geschützrohr als auch für Handfeuerwaffen bekannt geworden, wobei mit einer derartigen Konstruktion zwar ein Waffenrohr mit geringem Gewicht erzeugt werden kann; die Einsatzfähigkeit eines derartigen Rohres wird jedoch aufgrund der thermischen Empfindlichkeit des zwischen diesen beiden Rohren angeordneten Materials sehr beschränkt, da insbesondere im Ernstfall die thermische Beanspruchung des Laufes über das Projektil, nicht engen Grenzen unterworfen werden kann.It has also become known to provide a fiber-reinforced layer as a connecting tube between a core tube made of steel and an outer tube made of steel. Such constructions have become known both for a gun barrel and for handguns, although a gun barrel with a low weight can be produced with such a construction; However, the usability of such a tube is very limited due to the thermal sensitivity of the material arranged between these two tubes, since the thermal stress on the barrel via the projectile cannot be subject to narrow limits, particularly in an emergency.

Nach DE-3 114 659 ist ein Verfahren beschrieben, das zum Auskleiden von Hohlräumen geeignet ist, worunter auch Rohre fallen. Dabei wird in einem Hüllenrohr, z.B. aus Stahl, ein Spalt durch Einbringen eines dünnwandigen Metallteiles erstellt, in den Metallpulver gefüllt wird, der Spalt sodann evakuiert und anschliessend der Körper mit dem darin enthaltenen Metallteil und Pulver bei ca. 1150°C und 103 N/mm2 verdichtet wird. Eine abschliessende Nachbearbeitung ist möglich.According to DE-3 114 659, a method is described which is suitable for lining cavities, including pipes. In this case, a gap is created in a casing tube, for example made of steel, by introducing a thin-walled metal part, into which metal powder is filled, the gap is then evacuated and then the body with the metal part and powder contained therein at approx. 1150 ° C. and 103 N / mm 2 is compressed. A final post-processing is possible.

Aus US-4 327 154 ist ein Verfahren zur Herstellung von rohrförmigen Teilen zu entnehmen, wobei ein Verbundteil durch Aufbringen einer Pulverkomponente auf eine rohrförmige Metallschale mit heissisostatischem Verpressen zwischen 1000°C bis 1400°C und Drücken von 10 bis 1000 bar erzeugt wird.No. 4,327,154 discloses a method for producing tubular parts, a composite part being produced by applying a powder component to a tubular metal shell with hot isostatic pressing between 1000 ° C. to 1400 ° C. and pressures from 10 to 1000 bar.

Ferner ist aus US-3 753 704 bekannt, durch isostatisches Pressen hergestellte Verbundrohre vor der mechanischen Weiterverarbeitung einer Warmverformung durch Heissextrudieren zu unterwerfen.Furthermore, it is known from US Pat. No. 3,753,704 to subject composite pipes produced by isostatic pressing to hot deformation by hot extrusion prior to further mechanical processing.

Der vorliegenden Erfindung lag die Aufgabe zugrunde, ein Verfahren zur Herstellung von Waffenrohren zu schaffen, die sowohl für Geschütze als auch für Hand- und Faustfeuerwaffen geeignet sind, die ein Seelenrohr und zumindest ein Mantelrohr aus unterschiedlichen, metallischen Werkstoffen aufweisen, das es erlaubt, ein besonders leichtes und widerstandsfähiges Waffenrohr zu erzeugen.The present invention had for its object to provide a method for producing gun barrels that are suitable for guns as well as for hand and handguns that have a core tube and at least one jacket tube made of different metallic materials, which allows a to produce a particularly light and resistant weapon barrel.

Das erfindungsgemässe Verfahren zur Herstellung von Waffenrohren, die ein Seelenrohr und zumindest ein Mantelrohr aus unterschiedlichen, metallischen Werkstoffen aufweisen, besteht im wesentlichen darin, dass in ein Hüllenrohr, welches in einem Kapselrohr angeordnet wird, aus einer zähfesten Legierung eine Füllung aus einem eine Schüttdichte von zumindest 60% der Dichte des kompakten Werkstoffes aufweisenden, pulverförmigen, hochverschleissfesten oder korrosionsbeständigen Werkstoff unter Aussparung eines zentralen Hohlbereiches durch einen Füllkörper aus Automatenstahl eingebracht und verdichtet wird, an den Hüllen- bzw. Kapselrohrenden verschlossen wird, worauf evakuiert und das verschlossene Rohr in einer Schutzgasatmosphäre, bei zumindest 900°C, jedoch unterhalb der Schmelzpunkte der metallischen Werkstoffe und einem Druck von zumindest 900 bar verpresst wird und dass nach einer Wärmebehandlung der so erhaltene Verbundkörper, welcher einen vollflächigen metallischen Verbund zwischen Hüllenrohr und verdichtetem Werkstoff aufweist, sodann einer zumindest 1,3-fachen Warmverformung unterworfen wird, mechanisch bearbeitet und Züge erstellt werden. Ein nach diesem Verfahren hergestelltes Waffenrohr weist den Vorteil auf, dass es sowohl den Hochdruckbeanspruchungen als auch den abrasiven Beanspruchungen besonders günstig Rechnung trägt, wobei eine besonders vorteilhafte Kombination eines schmelzmetallurgischen und pulvermetallurgischen Verfahrens gegeben ist.The method according to the invention for the manufacture of weapon tubes, which have a core tube and at least one jacket tube made of different metallic materials, consists essentially in the fact that in a sleeve tube, which is arranged in a capsule tube, a filling made of a bulk density of a tough alloy at least 60% of the density of the compact, powdery, highly wear-resistant or corrosion-resistant material is introduced and compacted with the exception of a central hollow area by a filler made of free-cutting steel, is closed at the ends of the casing or capsule tube, whereupon the tube is evacuated and the sealed tube in a protective gas atmosphere , at least 900 ° C, but below the melting point of the metallic materials and a pressure of at least 900 bar and that after a heat treatment of the composite body thus obtained, which between a full-surface metallic composite n has a casing tube and compressed material, is then subjected to at least 1.3 times the hot deformation, mechanically processed and trains are created. A weapon barrel manufactured according to this method has the advantage that it takes account of both the high pressure and the abrasive stresses in a particularly favorable manner, a particularly advantageous combination of a melt-metallurgical and powder-metallurgical method being provided.

Wird als Füllkörper ein Rohr verwendet, so kann die Manipulation besonders einfach durchgeführt werden, da das Gewicht des Verbundkörpers besonders gering gehalten werden kann.If a tube is used as the packing, the manipulation can be carried out particularly easily, since the weight of the composite can be kept particularly low.

Wird als zähfestes Material Titan oder eine Titanlegierung verwendet, so kann ein besonders geringgewichtiges Waffenrohr erzeugt werden.If titanium or a titanium alloy is used as a tough material, a particularly low-weight weapon barrel can be produced.

Für Waffenrohre für Geschütze od. dgl. mit einer besonders gestreckten Schussbahn wird als hochverschleissfeste Legierung eine Kobaltbasislegierung verwendet.For gun barrels for guns or the like with a particularly elongated shot trajectory is considered to be high wear-resistant alloy uses a cobalt-based alloy.

Bei Geschützen, in welchen besonders korrosive Treibladungen zur Verwendung kommen, wird als Werkstoff zur Füllung des Hüllenrohres eine Nickelbasislegierung verwendet.In guns in which particularly corrosive propellant charges are used, a nickel-based alloy is used as the material for filling the casing tube.

Gemäss einem weiteren Merkmal des erfindungsgemässen Verfahrens wird ein Hüllenrohr verwendet, das auf seiner inneren Zylinderfläche eine Beschichtung aus einem Haftvermittler, z.B. Nickel od. dgl., aufweist.According to a further feature of the method according to the invention, a sleeve tube is used which has a coating of an adhesion promoter, e.g. Nickel or the like.

Im folgenden wird die Erfindung an Hand der Beispiele näher erläutert.The invention is explained in more detail below with the aid of the examples.

Beispiel 1:Example 1:

Zur Weiterverarbeitung als Gewehrlauf eines Maschinengewehres wurde ein Verbundmetall-Rohrteil hergestellt, indem in einem Hüllenrohr aus X40CrMoV51 (mit 0,38% C, 1,1% Si, 0,38% Mn, 5,20% Cr, 1,30% Mo und 1,2% V, Rest im wesentlichen Eisen) der Abmessung: 46 mm Aussendurchmesser, 15 mm Wandstärke und 650 mm Länge, ein Stab gleicher Länge aus Automatenstahl zentrisch eingesetzt und in den verbleibenden Hohlraum ein Metallpulver aus einer warmfesten Nickelbasislegierung der Zusammensetzung 0,12% C, 20,0% Cr, 18,1% Co, 2,5% Ti, 1,5% Al, 1,5% Fe, Rest im wesentlichen Nickel eingebracht wurde. Nach dem durch Evakuieren vorgenommenen Verdichten des Pulvers wurden die Rohrenden durch Aufschweissen von kreisförmigen Blechscheiben auf das Hüllenrohr gasdicht verschlossen und der Vorgang des heissisostatischen Pressens bei 1080°C und einem Gasdruck von 1100 bar 3 Stunden lang vorgenommen. Nach dem Abkühlen wurde der aus Automatenstahl bestehende zentrale Kern zur Gänze ausgebohrt und sodann die weitere mechanische Bearbeitung zur Herstellung der Züge und zur Fertigstellung des Laufes vorgenommen.For further processing as a gun barrel of a machine gun, a composite metal tube part was produced by using X40CrMoV51 (with 0.38% C, 1.1% Si, 0.38% Mn, 5.20% Cr, 1.30% Mo and 1.2% V, the rest essentially iron) of the dimension: 46 mm outer diameter, 15 mm wall thickness and 650 mm length, a rod of the same length made of free-cutting steel is inserted centrally and in the remaining cavity a metal powder made of a heat-resistant nickel-based alloy with the composition 0, 12% C, 20.0% Cr, 18.1% Co, 2.5% Ti, 1.5% Al, 1.5% Fe, the rest essentially nickel. After the powder had been compacted by evacuation, the tube ends were sealed gas-tight by welding circular sheet metal disks onto the jacket tube and the hot isostatic pressing process was carried out at 1080 ° C. and a gas pressure of 1100 bar for 3 hours. After cooling, the central core made of free-cutting steel was completely drilled out and then the further mechanical processing was carried out to produce the trains and to complete the run.

Beispiel 2:Example 2:

In ein Kapselrohr mit einem Bodenblech aus unlegiertem Baustahl mit einem Aussendurchmesser von 68 mm, einem Innendurchmesser von 62 mm und einer Länge von 800 mm wurde ein Hüllenrohr aus einer Legierung folgender Zusammensetzung in Gew.-% C 0,33, Si 0,28, Mn 0,50, Cr 3,0, Mo 1,2, V 0,27 und Rest Eisen mit einem Aussendurchmesser von 60 mm und einem Innendurchmesser von 40 mm und einer Länge von 800 mm eingebracht. In dieses Rohr wurde ein Kernzylinder aus Automatenstahl mit einem Aussendurchmesser von 18 mm und einer Länge von 800 mm zentrisch eingesetzt. Der hohlzylinderförmige Zwischenraum wurde mit einem Pulver einer Kobaltbasislegierung folgender Zusammensetzung in Gew.-% C 0,17, Si 0,35, Mn 0,65, Cr 28,9, Mo 5,6, Ni max. 0,5, Co 66,0 und Fe max. 0,5 gefüllt, wobei durch Rütteln eine Dichte von 6,5 g/cm3 erreicht wurde. Bei 350°C wurde entgast, worauf ein oberer Deckel mit Absaugöffnung an das Kapselrohr angeschweisst wurde. Sodann wurde evakuiert und die Absaugöffnung verschlossen. Der eingekapselte Körper wurde in einer Argonatmosphäre bei 1150 °C und bei einem Druck von 1000 bar 3 Stunden lang heiss-isostatisch verpresst. Dieser Verbundkörper wurde sodann auf einer Langschmiedemaschine auf einen Aussendurchmesser von ca. 35 mm geschmiedet, was einer ca. dreifachen Verformung entspricht. Nach dem Schmieden wurde bei 1100°C eine Stunde lang lösungsgeglüht, worauf durch mechanische Bearbeitung und Kaltschmieden der Züge ein Lauf für ein schweres Maschinengewehr gefertigt wurde.In a capsule tube with a base plate made of unalloyed structural steel with an outer diameter of 68 mm, an inner diameter of 62 mm and a length of 800 mm, a sleeve tube made of an alloy of the following composition in wt .-% C 0.33, Si 0.28, Mn 0.50, Cr 3.0, Mo 1.2, V 0.27 and remainder iron with an outer diameter of 60 mm and an inner diameter of 40 mm and a length of 800 mm. A core cylinder made of free-cutting steel with an outer diameter of 18 mm and a length of 800 mm was inserted centrally into this tube. The hollow cylindrical space was filled with a powder of a cobalt-based alloy with the following composition in% by weight C 0.17, Si 0.35, Mn 0.65, Cr 28.9, Mo 5.6, Ni max. 0.5, Co 66.0 and Fe max. 0.5 filled, a density of 6.5 g / cm 3 was achieved by shaking. Degassing was carried out at 350 ° C., whereupon an upper cover with a suction opening was welded onto the capsule tube. Then it was evacuated and the suction opening was closed. The encapsulated body was hot-isostatically pressed for 3 hours in an argon atmosphere at 1150 ° C. and at a pressure of 1000 bar. This composite body was then forged on a long forging machine to an outer diameter of approx. 35 mm, which corresponds to an approximate triple deformation. After forging, solution annealing was carried out at 1100 ° C for one hour, after which a barrel for a heavy machine gun was made by mechanical processing and cold forging of the trains.

Beispiel 3:Example 3:

In ein Kapselrohr mit einem Bodenblech aus unlegiertem Baustahl mit einem Aussendurchmesser 215 mm, einem Innendurchmesser von 210 mm und einer Länge von 900 mm wurde ein Hohlzylinder aus Vergütungsstahl folgender Zusammensetzung C 0,41, Si 0,3, Mn 0,7, Cr 1,1, Mo 0,2 mit einem Aussendurchmesser von 210 mm und einem Innendurchmesser von 160 mm und einer Länge von 900 mm eingebracht. Im Zentrum des Hüllenrohres wurde ein zylindrischer Stab aus Automatenstahl mit einem Aussendurchmesser von 45 mm und einer Länge von 900 mm eingebracht. Der hohlzylinderförmige Zwischenraum wurde mit einem Pulver einer Kobaltbasislegierung folgender Zusammensetzung in Gew.-% C 0,17, Si 0,35, Mn 0,65, Cr 28,0, Mo 5,5, Ni max. 0,5, Co 66,0 und Fe max. 0,5 gefüllt, wobei durch Rütteln eine Dichte von 6,7 g/cm3 erreicht wurde. Bei 340°C wurde entgast, worauf ein oberer Deckel mit Absaugöffnung angeschweisst wurde. Sodann wurde evakuiert und gemäss Beispiel 2 heiss-isostatisch verpresst. Der so erhaltene Verbundkörper wurde auf einer Langschmiedemaschine auf einen Durchmesser von 105 mm bzw. 35 mm bzw. 23 mm und einer Länge von 3500 mm geschmiedet, was einer vierfachen Verformung entspricht. Die Weiterverarbeitung erfolgte analog Beispiel 2, wobei jedoch durch Vergüten des Hüllenrohres eine Zugfestigkeit von 900 -1100 N/m2 eingestellt wurde. Das erhaltene Rohr wies ein Kaliber von 1" auf und fand Einsatz für eine Schnellfeuerkanone.In a capsule tube with a base plate made of unalloyed structural steel with an outer diameter of 215 mm, an inner diameter of 210 mm and a length of 900 mm, a hollow cylinder made of tempered steel with the following composition C 0.41, Si 0.3, Mn 0.7, Cr 1 , 1, Mo 0.2 introduced with an outer diameter of 210 mm and an inner diameter of 160 mm and a length of 900 mm. A cylindrical rod made of free-cutting steel with an outside diameter of 45 mm and a length of 900 mm was inserted in the center of the casing tube. The hollow cylindrical space was filled with a powder of a cobalt-based alloy with the following composition in% by weight C 0.17, Si 0.35, Mn 0.65, Cr 28.0, Mo 5.5, Ni max. 0.5, Co 66.0 and Fe max. 0.5 filled, a density of 6.7 g / cm 3 was achieved by shaking. Degassing was carried out at 340 ° C., whereupon an upper cover with a suction opening was welded on. It was then evacuated and hot-isostatically pressed according to Example 2. The composite body thus obtained was forged on a long forging machine to a diameter of 105 mm or 35 mm or 23 mm and a length of 3500 mm, which corresponds to a fourfold deformation. The further processing was carried out analogously to Example 2, but a tensile strength of 900-1100 N / m 2 was set by tempering the jacket tube. The tube obtained had a caliber of 1 "and was used for a rapid-fire cannon.

Beispiel 4:Example 4:

In ein mit einem Boden versehenes Kapselrohr wurde ein Hüllenrohr aus TiA16V4 mit einem Aussendurchmesser von 210 mm und einem Innendurchmesser von 160 mm sowie einer Länge von 900 mm eingebracht. In dieses Hüllenrohr wurde sodann ein Kernstab aus Automatenstahl mit einem Durchmesser von 45 mm und einer Länge von 900 mm eingebracht. Der Zwischenraum wurde mit einem Pulver folgender Zusammensetzung in Gew.-% C 0,34, Cr 1,2, Mo 0,2, AI 0,95, Rest Fe gefüllt. Es wurde auf 70% der Dichte verdichtet. Sodann wurde gemäss Beispiel 3 verfahren und der Verbundkörper auf einen Durchmesser von 105 mm bzw. 35 mm und einer Länge von 350 mm geschmiedet, was einer vierfachen Verformung entspricht. Dieser Verbundkörper wurde bei 940 °C eine Stunde erhitzt und sodann in Öl abgekühlt und vier Stunden bei 520°C angelassen. Nach erfolgter Bearbeitung wurde die innere Oberfläche in an sich bekannter Weise bis zu einer Tiefe von 0,3 bis 0,4 mm nitriert.In a capsule tube provided with a bottom, a sleeve tube made of TiA16V4 with an outer diameter of 210 mm and an inner diameter of 160 mm and a length of 900 mm was introduced. A core rod made of free-cutting steel with a diameter of 45 mm and a length of 900 mm was then introduced into this casing tube. The intermediate space was filled with a powder of the following composition in% by weight C 0.34, Cr 1.2, Mo 0.2, Al 0.95, remainder Fe. It was compressed to 70% of the density. The procedure was then as in Example 3 and the composite body was forged to a diameter of 105 mm or 35 mm and a length of 350 mm, which corresponds to a fourfold deformation. This composite was heated at 940 ° C for one hour and then cooled in oil and tempered at 520 ° C for four hours. After processing, the inner Surface nitrided in a manner known per se to a depth of 0.3 to 0.4 mm.

An Stelle des Kapselrohres kann auch das Hüllenrohr direkt mit den Deckel verschweisst werden, da keine Druckeinwirkung auf das Pulver in radialer Richtung auf Grund der Materialstärke des Hüllenrohres eintreten kann. Der Kern kann auch durch einen Hohlzylinder gebildet sein, wobei in diesem Falle, der sich insbesondere für grössere Kaliber anbietet, über einen Dorn geschmiedet werden kann.Instead of the capsule tube, the sleeve tube can also be welded directly to the cover, since the powder can not act radially due to the material thickness of the sleeve tube. The core can also be formed by a hollow cylinder, in which case, which is particularly suitable for larger calibers, forging can be carried out using a mandrel.

Es kann auch ein Hüllenrohr verwendet werden, das eine Innenbeschichtung, z. B. elektrolytisch abgeschieden aus Nickel od. dgl., aufweist, die als Haftvermittler zwischen dem Material des Hüllenrohres und dem Pulver auftreten kann.A cladding tube can also be used which has an inner coating, e.g. B. electrodeposited from nickel or the like., Which can occur as an adhesion promoter between the material of the cladding tube and the powder.

Bei allen angeführten Beispielen war ein vollflächiger Verbund zwischen dem Hüllenrohr und dem Seelenrohr eingetreten, wobei beispielsweise bei der Kobalthartlegierung gemäss Beispiel 2 folgende Eigenschaftsverbesserungen durch das heiss-isostatische Verpressen bzw. durch heissisostatisches Verpressen und Schmieden erreicht werden können.

Figure imgb0001
In all of the examples cited, a full-area bond between the cladding tube and the core tube had occurred, the following property improvements, for example in the case of the cobalt hard alloy according to Example 2, being able to be achieved by hot-isostatic pressing or by hot-isostatic pressing and forging.
Figure imgb0001

Claims (8)

1. A method for manufacturing weapon barrels with rifling for guns or manual firearms, the weapon barrels having a liner and a casing tube made of different metal materials, characterised in that a filler made of a highly-abrasion-resistant or corrosion-proof powdered material, which has a bulk density of at least 60% of the density of the compact material, is inserted and compressed in a casing, which is disposed in a capsule tube and is made of a tough alloy, by a filling body made of machining steel, hollowing out a central hollow region, the filling is sealed at the casing or capsule tube ends, then evacuated and the sealed tube is compressed in a protective gas atmosphere at a temperature of at least 900°C, but below the melting point of the metal materials, and at a pressure of at least 900 bar, and in that, after heat-treatment, the compound body thus obtained, which has a holohedral metallic connection between the casing tube and the compressed material, is subjected to at least a 1.3-fold hot-forming, machined, and riflings are provided.
2. A method according to claim 1, characterised in that a tube is used as a filling body.
3. A method according to claim 1 and 2, characterised in that titanium or a titanium alloy is used as a tough alloy.
4. A method according to one of claims 1 to 3, characterised in that steel is used as a tough alloy.
5. A method according to one of claims 1 to 4, characterised in that a cobalt-based alloy is used as a highly-abrasion-resistant alloy.
6. A method according to one of claims 1 to 5, characterised in that a nickel-based alloy is used as a highly-abrasion-resistant-alloy.
7. A method according to one of claims 1 to 6, characterised in that the powdered material is pre-compressed and/or pre-sintered.
8. A method according to one of claims 1 to 7, characterised in that the casing tube has a lining made of an ahesion agent, e.g. nickel.
EP83890232A 1982-12-23 1983-12-22 Process for the production of arm barrels Expired EP0114591B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
AT4679/82 1982-12-23
AT467982 1982-12-23

Publications (2)

Publication Number Publication Date
EP0114591A1 EP0114591A1 (en) 1984-08-01
EP0114591B1 true EP0114591B1 (en) 1988-03-30

Family

ID=3567024

Family Applications (3)

Application Number Title Priority Date Filing Date
EP83890233A Expired EP0114592B1 (en) 1982-12-23 1983-12-22 Process for treating metals by using dies
EP83890234A Withdrawn EP0114593A1 (en) 1982-12-23 1983-12-22 Process for the production of a hollow cylinder for synthetics processing machines
EP83890232A Expired EP0114591B1 (en) 1982-12-23 1983-12-22 Process for the production of arm barrels

Family Applications Before (2)

Application Number Title Priority Date Filing Date
EP83890233A Expired EP0114592B1 (en) 1982-12-23 1983-12-22 Process for treating metals by using dies
EP83890234A Withdrawn EP0114593A1 (en) 1982-12-23 1983-12-22 Process for the production of a hollow cylinder for synthetics processing machines

Country Status (6)

Country Link
US (1) US4747225A (en)
EP (3) EP0114592B1 (en)
AT (2) ATE33218T1 (en)
DE (2) DE3376100D1 (en)
ES (2) ES8501657A1 (en)
GR (2) GR79748B (en)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT385227B (en) * 1984-01-24 1988-03-10 Ver Edelstahlwerke Ag METHOD FOR THE PRODUCTION OF FORCE TRANSFERRING, IN PARTICULAR TORQUE TRANSFERRING ELEMENTS
US4640814A (en) * 1985-10-17 1987-02-03 Crucible Materials Corporation Method for producing clad tubular product
DE3881923T2 (en) * 1987-03-25 1994-01-27 Nippon Steel Corp Process for the production of coated metal pipes.
AT391105B (en) * 1988-10-07 1990-08-27 Boehler Gmbh PRE-MATERIAL FOR THE PRODUCTION OF COMPOSITES
US5277228A (en) * 1990-11-02 1994-01-11 Usui Kokusai Sangyo Kaisha Limited Welded pipe with excellent corrosion resistance inner surface
US5290507A (en) * 1991-02-19 1994-03-01 Runkle Joseph C Method for making tool steel with high thermal fatigue resistance
US5341719A (en) * 1992-12-14 1994-08-30 General Electric Company Multi-layer composite gun barrel
US5357842A (en) * 1993-07-09 1994-10-25 Reynolds Charles E Recoil reducing device
US6218026B1 (en) 1995-06-07 2001-04-17 Allison Engine Company Lightweight high stiffness member and manufacturing method thereof
US5724643A (en) * 1995-06-07 1998-03-03 Allison Engine Company, Inc. Lightweight high stiffness shaft and manufacturing method thereof
US5856631A (en) * 1995-11-20 1999-01-05 Nitinol Technologies, Inc. Gun barrel
DE19834394A1 (en) * 1998-07-30 2000-02-03 Rheinmetall W & M Gmbh Gun barrel with a wear-reducing hard chrome layer
SE516130C2 (en) * 1999-03-15 2001-11-19 Damasteel Ab Substance for metal product, process for making metal product and metal product
RU2167742C2 (en) * 1999-03-31 2001-05-27 Курский государственный технический университет Method of hard facing of metal articles
DE19926246A1 (en) * 1999-06-09 2000-12-14 Rheinmetall W & M Gmbh Process for coating the inside of a gun barrel
US6594936B1 (en) * 2002-10-03 2003-07-22 Gary Sniezak Method for lining a gun barrel
US20040226211A1 (en) * 2003-05-16 2004-11-18 Ra Brands. L.L.C. Composite receiver for firearms
US20040244254A1 (en) * 2003-06-09 2004-12-09 Barfield Christopher A.. Firearm safety device
US7922065B2 (en) 2004-08-02 2011-04-12 Ati Properties, Inc. Corrosion resistant fluid conducting parts, methods of making corrosion resistant fluid conducting parts and equipment and parts replacement methods utilizing corrosion resistant fluid conducting parts
US7963202B1 (en) * 2005-09-21 2011-06-21 The United States Of America As Represented By The Secretary Of The Army Superalloy mortar tube
US7921590B2 (en) * 2006-02-23 2011-04-12 Strum, Ruger & Company, Inc. Composite firearm barrel reinforcement
US20100236122A1 (en) * 2006-07-26 2010-09-23 Fonte Matthew V Flowforming Gun Barrels and Similar Tubular Devices
EP2046524A4 (en) * 2006-08-01 2016-05-25 Afl Telecommunications Llc Embedded metallic tubes with compression fit and method for manufacturing the same
US8910409B1 (en) 2010-02-09 2014-12-16 Ati Properties, Inc. System and method of producing autofrettage in tubular components using a flowforming process
US8869443B2 (en) 2011-03-02 2014-10-28 Ati Properties, Inc. Composite gun barrel with outer sleeve made from shape memory alloy to dampen firing vibrations
US10118259B1 (en) 2012-12-11 2018-11-06 Ati Properties Llc Corrosion resistant bimetallic tube manufactured by a two-step process
US9279633B2 (en) 2014-01-21 2016-03-08 Richard R. Hayes Multi-caliber weapon
US9796057B2 (en) * 2015-01-15 2017-10-24 Saeilo Enterprises, Inc. Gun barrel assembly
SE2300011A1 (en) * 2023-02-09 2024-08-10 Bae Systems Bofors Ab Barrel
SE547703C2 (en) * 2024-05-28 2025-11-11 Bae Systems Bofors Ab ELECTRIC PIPE AND METHOD FOR MANUFACTURING ELECTRIC PIPE SEGMENTS

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US930927A (en) * 1906-03-19 1909-08-10 Robert H Berkstresser Gun-barrel and process of producing the same.
US2372202A (en) * 1940-05-08 1945-03-27 Mallory & Co Inc P R Bearing
US2636849A (en) * 1946-12-13 1953-04-28 Us Sec War Method of electroforming gun barrels and liners
US2977666A (en) * 1954-12-29 1961-04-04 Porter H Brace Method of making gun liner elements
US3112553A (en) * 1960-06-08 1963-12-03 William H Safranek Electroforming of gun liners
US3261121A (en) * 1961-10-13 1966-07-19 Joseph R Eves Gun barrel with explosively welded liner
US3753704A (en) * 1967-04-14 1973-08-21 Int Nickel Co Production of clad metal articles
JPS50106844A (en) * 1974-01-31 1975-08-22
DE2514565C3 (en) * 1975-04-03 1979-09-20 Uralskij Nautschno-Issledovatelskij Institut Trubnoj Promyschlennosti, Tscheljabinsk (Sowjetunion) Process for the production of a composite pipe
US4016008A (en) * 1975-07-31 1977-04-05 The International Nickel Company, Inc. Clad metal tubes
DE2737248C2 (en) * 1977-08-18 1985-09-19 MTU Motoren- und Turbinen-Union München GmbH, 8000 München High strength component with a complex geometric shape and process for its manufacture
US4135286A (en) * 1977-12-22 1979-01-23 United Technologies Corporation Sputtering target fabrication method
GB2073783B (en) * 1980-04-10 1984-10-10 Cameron Iron Works Inc Lining valves by hot isotatic pressing
US4426248A (en) * 1983-05-20 1984-01-17 The United States Of America As Represented By The Secretary Of The Army Process for coating rifle tubes

Also Published As

Publication number Publication date
ES528315A0 (en) 1984-12-01
ES528317A0 (en) 1984-12-01
EP0114592A1 (en) 1984-08-01
DE3376100D1 (en) 1988-05-05
US4747225A (en) 1988-05-31
DE3376101D1 (en) 1988-05-05
EP0114593A1 (en) 1984-08-01
ES8501657A1 (en) 1984-12-01
ATE33219T1 (en) 1988-04-15
GR79748B (en) 1984-10-31
EP0114591A1 (en) 1984-08-01
ATE33218T1 (en) 1988-04-15
GR81355B (en) 1984-12-11
EP0114592B1 (en) 1988-03-30
ES8501658A1 (en) 1984-12-01

Similar Documents

Publication Publication Date Title
EP0114591B1 (en) Process for the production of arm barrels
US4756677A (en) Method of manufacturing a weapon barrel
US4961383A (en) Composite tungsten-steel armor penetrators
KR940009657B1 (en) Forming method of high density tungsten alloy projectile
DE69932720T2 (en) DEVELOPABLE METAL BALLS, AMMUNITION AND METHOD FOR THE MANUFACTURE OF SUCH ARTICLES
DE69714270T2 (en) DEVICE FOR PROCESSING CORROSIVE METAL MELT
EP0201557B1 (en) Gun barrel for use at high temperature
US3803702A (en) Method of fabricating a composite steel article
DE69332834T2 (en) LEAD-FREE CARTRIDGE
CN1332774C (en) Blank for a gun barrel, method for producing said gun barrel and said gun barrel
US6981996B2 (en) Tungsten-tin composite material for green ammunition
EP1930456A2 (en) Powder-metallurgically produced steel plate, application of such a steel plate and method for its manufacture
EP1715080B1 (en) Process for coating the inner surface of a gun barrel
DE2539684C1 (en) Splinter shell for projectiles, warheads, ammunition and the like.
DE896234C (en) X-ray tube
EP1125093B1 (en) Production of a low-polluting jacketed bullet
DE3934148C1 (en)
DE3907087A1 (en) HIGH PRESSURE TANK
DE102006025241A1 (en) Method for producing forged steel for highly stressed weapons, tube blanks and a weapon equipped therewith
EP2173507A1 (en) Method and device for producing a tubular solid body from a refractory tungsten-heavy metal alloy, particularly as a semi-finished product for the production of a penetrator for a kinetic energy projectile with fragmentation effect
EP1186847B1 (en) Method for repairing the damage in coatings or the damage caused by erosion
AT314212B (en) Process for sintering alloys with liquid phase
WO2021136755A1 (en) Method for producing a composite tube, and composite tube
DE102014006081A1 (en) Metal-metal matrix composite runs
EP1240475B1 (en) Projectile body and a method for producing radially protruding driving means

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

Designated state(s): AT BE CH DE FR GB IT LI LU NL SE

17P Request for examination filed

Effective date: 19850125

17Q First examination report despatched

Effective date: 19860411

R17C First examination report despatched (corrected)

Effective date: 19860821

ITF It: translation for a ep patent filed
GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE CH DE FR GB IT LI LU NL SE

REF Corresponds to:

Ref document number: 33218

Country of ref document: AT

Date of ref document: 19880415

Kind code of ref document: T

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

Ref document number: 3376100

Country of ref document: DE

Date of ref document: 19880505

ET Fr: translation filed
BECN Be: change of holder's name

Effective date: 19880330

PLBI Opposition filed

Free format text: ORIGINAL CODE: 0009260

26 Opposition filed

Opponent name: SEILSTORFER GMBH & CO. METALLURGISCHE VERFAHRENST

Effective date: 19881229

RAP2 Party data changed (patent owner data changed or rights of a patent transferred)

Owner name: VOEST-ALPINE STAHL AKTIENGESELLSCHAFT

NLR1 Nl: opposition has been filed with the epo

Opponent name: SEILSTORFER GMBH & CO. METALLURGISCHE VERFAHRENSTE

NLT2 Nl: modifications (of names), taken from the european patent patent bulletin

Owner name: VOEST-ALPINE STAHL AKTIENGESELLSCHAFT TE LINZ A.D.

REG Reference to a national code

Ref country code: CH

Ref legal event code: PFA

Free format text: VOEST-ALPINE STAHL AKTIENGESELLSCHAFT

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

Ref country code: AT

Payment date: 19911107

Year of fee payment: 9

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

Ref country code: GB

Payment date: 19911108

Year of fee payment: 9

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

Ref country code: CH

Payment date: 19911111

Year of fee payment: 9

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

Ref country code: FR

Payment date: 19911113

Year of fee payment: 9

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

Ref country code: SE

Payment date: 19911118

Year of fee payment: 9

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

Ref country code: LU

Payment date: 19911125

Year of fee payment: 9

REG Reference to a national code

Ref country code: GB

Ref legal event code: 732

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

Ref country code: DE

Payment date: 19911212

Year of fee payment: 9

Ref country code: BE

Payment date: 19911212

Year of fee payment: 9

ITTA It: last paid annual fee
PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: NL

Payment date: 19911231

Year of fee payment: 9

EPTA Lu: last paid annual fee
RDAG Patent revoked

Free format text: ORIGINAL CODE: 0009271

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

Free format text: STATUS: PATENT REVOKED

GBPR Gb: patent revoked under art. 102 of the ep convention designating the uk as contracting state

Free format text: 920630

27W Patent revoked

Effective date: 19920630

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

NLR2 Nl: decision of opposition
BERE Be: lapsed

Owner name: VOEST-ALPINE STAHL AKTIENGESELLSCHAFT

Effective date: 19921231

EUG Se: european patent has lapsed

Ref document number: 83890232.8

Effective date: 19930107

APAH Appeal reference modified

Free format text: ORIGINAL CODE: EPIDOSCREFNO