EP0822382B1 - Method for coupling the barrels of rifles in the breech - Google Patents

Method for coupling the barrels of rifles in the breech Download PDF

Info

Publication number
EP0822382B1
EP0822382B1 EP96830579A EP96830579A EP0822382B1 EP 0822382 B1 EP0822382 B1 EP 0822382B1 EP 96830579 A EP96830579 A EP 96830579A EP 96830579 A EP96830579 A EP 96830579A EP 0822382 B1 EP0822382 B1 EP 0822382B1
Authority
EP
European Patent Office
Prior art keywords
barrel
casing
barrels
zones
joining
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
EP96830579A
Other languages
German (de)
French (fr)
Other versions
EP0822382A2 (en
EP0822382A3 (en
Inventor
Ugo Gussalli Beretta
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.)
Beretta SpA
Original Assignee
Fabbrica dArmi Pietro Beretta SpA
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 Fabbrica dArmi Pietro Beretta SpA filed Critical Fabbrica dArmi Pietro Beretta SpA
Publication of EP0822382A2 publication Critical patent/EP0822382A2/en
Publication of EP0822382A3 publication Critical patent/EP0822382A3/en
Application granted granted Critical
Publication of EP0822382B1 publication Critical patent/EP0822382B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • F41A21/48Barrel mounting means, e.g. releasable mountings for replaceable barrels
    • 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
    • F41A21/06Plural barrels
    • F41A21/08Barrel junctions

Definitions

  • the present invention pertains to a method for coupling the barrels of rifles in the breech and pertains to the resulting set of barrels as well.
  • the barrels are essentially coupled according to two different methods, commonly defined as semiblock (demiblock) and monoblock, respectively.
  • each pipe forming a barrel is made in one piece with a semiblock or block full of semitenons or hooks in the breech.
  • the semiblocks of the barrels to be joined are then joined lengthwise by means of complementary guides on their adjoining faces.
  • the barrels and the semiblocks are therefore made of the same material, and the stability of the mechanical coupling obtained depends on the precision of the coupling guides and is often questionable, but not reliable, as required.
  • the barrels are separated and joined together in the breech by means of a monolithic casing.
  • This monolithic casing may be in a single piece with the tenons or hooks and is provided with holes, in which the breech ends of the barrels are threaded and welded by means of welding with a filler metal such as tin or brass.
  • the barrels and the monolithic casing may be made of different materials, and a specific procedural technique that the persons skilled in the art know well, is necessary for the coupling and welding.
  • the assembly of the barrels either using one method or the other leaves visible signs of joining even though this joining is concealed as well as possible.
  • the chemical-physical structure of the materials forming the barrels and the casing becomes nonuniform at least in the joining zones.
  • the use of filler metals for the welding involves a reheating in the oven of the components up to a high temperature and with the risk of tempering and thermal stress of the barrels, especially when using brass as the filler metal for a strong welding. On the other hand, if the welding is not strong, there is less resistance to uncoupling and to tearing.
  • the primary object of the present invention is to propose a novel method for coupling the barrels of rifles in the breech, which is suitable for preventing the disadvantages and drawbacks of the prior art.
  • the method is applicable to all rifles with one or more barrels, either smooth barrels or rifled barrels, and is carried out starting from the single barrels and from a monoblock casing and by means of a laser fusion of the parts in contact for their intimate joining, without support material.
  • each barrel is machined on the outside in the breech to have an end portion 11' that is preferably but not necessarily cylindrical, starting from a shoulder 11" that is turned towards the rear end and completely at right angles to the axis of the barrel itself.
  • the casing is provided with a through hole 12' for each barrel 11 and is machined at the top so as to have a surface that is completely at right angles to the axis the hole 12' and is intended for coinciding with the shoulder 11" of each barrel 11.
  • the end portion of each barrel and each hole in the casing shall have equal diameters with a suitable machining allowance in the coupling zones.
  • the barrels 11 and the casing 12 prepared in this manner are then machined and prepared for a preliminary mechanical coupling.
  • This coupling is performed by force-fitting the end portions of the barrels in the respective holes in the casing in order to bring the shoulder 11" of the barrels into close contact with the top surface 12" of the casing as shown in Figures 2 and 2a.
  • the striking contact between the barrels and the casing may be maintained with appropriate mechanical devices and ensures the correct arrangement of the barrels. Other devices may be provided for keeping the parts dry and cleaning them.
  • the barrels and the casing are joined by means of laser fusion in their circumferential zones A and B, respectively, on the striking surface (11" and 12") between the barrels and the casing and at the rear ends of the barrels and of the casing as shown in Figures 3 and 3a.
  • the joining is thus done without material support, and with a homogenizing in the fusion zones A and B of the material that forms the barrels and the casing. In the field, this is a joining of two metal components with fusion of same in the absence of plasma and under an inert atmosphere.
  • the inert atmosphere in the form of gas injected directly close to the point of joining, eliminates the possibility of oxidation and of decarbonization of the fused zone.
  • the joining zone of the parts adapts to the level of structural stresses immediately after the fusion. This makes it possible to regulate the internal structure of the fused zone to the same extent as the surrounding, not thermally changed zone.
  • the graph of Figure 6 represents the course of the relationship between the power applied and the volume of fused material
  • the graph of Figure 7 represents the efficiency of the welding and the power/penetration ratio
  • the graph of Figure 8 shows how, though being less than 3, the depth/width ratio (essential requirement given the thickness and the geometry of the joined components), the efficiency of the joining, as well as the final aesthetic result is very good
  • Figures 4 and 5 show, on an enlarged scale, the joining zones A and B, which may appear with protuberances which are then removed.
  • the protuberances, and where provided, the starting machining allowance on the outline of the zones A and B are then removed in order to achieve predetermined finishing heights as shown in Figures 4a and 5a.
  • the result is a set of barrels and monoblock joined together by means of laser fusion in at least the zones A and B, which makes the joined components indissoluble, as in a single piece (integral), and which does not leave apparent signs of joining which show their initial contact discontinuity.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Laser Beam Processing (AREA)
  • Braking Arrangements (AREA)
  • Drilling And Boring (AREA)
  • Fixed Capacitors And Capacitor Manufacturing Machines (AREA)
  • Ceramic Products (AREA)

Description

  • The present invention pertains to a method for coupling the barrels of rifles in the breech and pertains to the resulting set of barrels as well.
  • According to the state of the art on the subject of rifles with one, two or more barrels, the barrels are essentially coupled according to two different methods, commonly defined as semiblock (demiblock) and monoblock, respectively.
  • In the first method, each pipe forming a barrel is made in one piece with a semiblock or block full of semitenons or hooks in the breech. The semiblocks of the barrels to be joined are then joined lengthwise by means of complementary guides on their adjoining faces. The barrels and the semiblocks are therefore made of the same material, and the stability of the mechanical coupling obtained depends on the precision of the coupling guides and is often questionable, but not reliable, as required.
  • In the second method, the barrels are separated and joined together in the breech by means of a monolithic casing. This monolithic casing may be in a single piece with the tenons or hooks and is provided with holes, in which the breech ends of the barrels are threaded and welded by means of welding with a filler metal such as tin or brass. In this case, the barrels and the monolithic casing may be made of different materials, and a specific procedural technique that the persons skilled in the art know well, is necessary for the coupling and welding.
  • However, the assembly of the barrels either using one method or the other leaves visible signs of joining even though this joining is concealed as well as possible. In the second coupling method, the chemical-physical structure of the materials forming the barrels and the casing becomes nonuniform at least in the joining zones. Moreover, the use of filler metals for the welding involves a reheating in the oven of the components up to a high temperature and with the risk of tempering and thermal stress of the barrels, especially when using brass as the filler metal for a strong welding. On the other hand, if the welding is not strong, there is less resistance to uncoupling and to tearing.
  • The primary object of the present invention is to propose a novel method for coupling the barrels of rifles in the breech, which is suitable for preventing the disadvantages and drawbacks of the prior art.
  • The method is applicable to all rifles with one or more barrels, either smooth barrels or rifled barrels, and is carried out starting from the single barrels and from a monoblock casing and by means of a laser fusion of the parts in contact for their intimate joining, without support material.
  • The method proposed here makes it possible to achieve advantages, such as:
    • chemical-physical uniformity of the materials of the barrels and the casing, particularly in the joining zones;
    • high increase in the resistance to tearing between the barrels and casing;
    • indissolubility of the coupled parts;
    • invisibility of the coupling lines even after the surface finishing of the parts;
    • possibility of reducing the thicknesses and resistant sections in the coupled parts for the greater resistance obtained;
    • decrease in the overall weight thanks to the reduction in the thicknesses of the parts to be coupled;
    • possibility of automating the joining process without running into unusual thermal stresses of the barrels;
    • complete control of the effectiveness of the joining of the parts.
  • Greater details of the present invention become evident from the following description with reference to the attached drawings and, for greater simplicity, with reference to the coupling of two barrels.
  • The various features of novelty which characterize the invention are pointed out with particularity in the claims annexed to and forming a part of this disclosure. For a better understanding of the invention, its operating advantages and specific objects attained by its uses, reference is made to the accompanying drawings and descriptive matter in which a preferred embodiment of the invention are illustrated.
  • In the drawings:
  • Figure 1 is a top partially cutaway view of the starting barrels and casing separated;
  • Figure 2 is a rear view of the barely coupled barrels and casing;
  • Figure 2a is a section according to the line II-II of Figure 2;
  • Figures 3 and 3a show two views similar to those of Figures 2 and 2a, but with the barrels and casing barely tightly joined;
  • Figures 4 and 5 are cross-sectional views of two enlarged coupling zones corresponding to the encircled parts IV and V in Figure 3a, respectively;
  • Figures 4a and 5a are two views similar to those of Figures 4 and 5, but of the finished coupling;
  • Figure 6 is a graph illustrating the course of the relationship between the laser power applied and the volume of fused material;
  • Figure 7 is a graph illustrating the welding efficiency based on the laser power; and
  • Figure 8 is a graph illustrating the welding efficiency based on the penetration.
  • Referring to the drawings in particular, the starting barrels 11 and the monoblock casing 12, still separated, are illustrated in Figure 1. The barrels 11 and the casing 12 are made of materials that are identical in terms of chemical composition and structural state. Each barrel is machined on the outside in the breech to have an end portion 11' that is preferably but not necessarily cylindrical, starting from a shoulder 11" that is turned towards the rear end and completely at right angles to the axis of the barrel itself. On the other hand, the casing is provided with a through hole 12' for each barrel 11 and is machined at the top so as to have a surface that is completely at right angles to the axis the hole 12' and is intended for coinciding with the shoulder 11" of each barrel 11. The end portion of each barrel and each hole in the casing shall have equal diameters with a suitable machining allowance in the coupling zones.
  • The barrels 11 and the casing 12 prepared in this manner are then machined and prepared for a preliminary mechanical coupling. This coupling is performed by force-fitting the end portions of the barrels in the respective holes in the casing in order to bring the shoulder 11" of the barrels into close contact with the top surface 12" of the casing as shown in Figures 2 and 2a.
  • The striking contact between the barrels and the casing may be maintained with appropriate mechanical devices and ensures the correct arrangement of the barrels. Other devices may be provided for keeping the parts dry and cleaning them.
  • After the preliminary coupling, the barrels and the casing are joined by means of laser fusion in their circumferential zones A and B, respectively, on the striking surface (11" and 12") between the barrels and the casing and at the rear ends of the barrels and of the casing as shown in Figures 3 and 3a.
  • The joining is thus done without material support, and with a homogenizing in the fusion zones A and B of the material that forms the barrels and the casing. In the field, this is a joining of two metal components with fusion of same in the absence of plasma and under an inert atmosphere.
  • The fusion not obtained in the absence of material support would cause a detrimental thermal-structural change for the mechanical features of the fused zone.
  • The inert atmosphere, in the form of gas injected directly close to the point of joining, eliminates the possibility of oxidation and of decarbonization of the fused zone.
  • An excellent result is obtained, e.g., with a ratio of the fused material volume to the time used ranging from 5 mm3/sec. to 10 mm3/sec.
  • The joining zone of the parts adapts to the level of structural stresses immediately after the fusion. This makes it possible to regulate the internal structure of the fused zone to the same extent as the surrounding, not thermally changed zone.
  • The optimization of the process, set up by the inventor, for the assumed purpose is confirmed by tests, whose results appear from the attached graphs. In particular, the graph of Figure 6 represents the course of the relationship between the power applied and the volume of fused material; the graph of Figure 7 represents the efficiency of the welding and the power/penetration ratio; the graph of Figure 8 shows how, though being less than 3, the depth/width ratio (essential requirement given the thickness and the geometry of the joined components), the efficiency of the joining, as well as the final aesthetic result is very good
  • The optimization sought was thus achieved.
  • Figures 4 and 5 show, on an enlarged scale, the joining zones A and B, which may appear with protuberances which are then removed. The protuberances, and where provided, the starting machining allowance on the outline of the zones A and B are then removed in order to achieve predetermined finishing heights as shown in Figures 4a and 5a.
  • The result is a set of barrels and monoblock joined together by means of laser fusion in at least the zones A and B, which makes the joined components indissoluble, as in a single piece (integral), and which does not leave apparent signs of joining which show their initial contact discontinuity.
  • While a specific embodiment of the invention has been shown and described in detail to illustrate the application of the principles of the invention, it will be understood that the invention may be embodied otherwise without departing from such principles.

Claims (10)

  1. A method for coupling the barrels of firearms in the breech starting from at least one barrel and from a monoblock casing, the method comprising the steps of:
    providing the breech of each barrel with an end portion (11') of predetermined shape and diameter, starting from a striking shoulder (11") turned towards the rear end of the said barrel and at right angles to the axis of said barrel;
    providing the monoblock casing with a through hole (12') for each barrel and with a striking surface (12") turned towards the striking shoulder (11") of the barrel, the hole having a shape and a diameter corresponding to that of the end portion of the barrel and the striking surface (12") being at a right angle to an axis of the hole;
    mechanically coupling the barrels and the casing by fitting the end portion of the barrel in the respective hole of the casing in order to bring the striking shoulder into close contact with the striking surface;
    permanently joining the barrels and the casing by means of laser fusion in at least two zones (A,B) at the level of the said shoulder and of the striking surface in close contact and of a rear end of the barrel and of the casing; and
    removing any excess material in the joining zones (A,B).
  2. A method in accordance with claim 1, wherein each barrel and the casing are prepared with a possible machining allowance in the zones intended for being joined by means of laser fusion.
  3. A method in accordance with claim 1, wherein the end portion (11') of the barrel and the hole in the casing are cylindrical and have the same diameter.
  4. A method in accordance with claim 1, wherein the barrel and the casing are machined and prepared before the mechanical coupling, and in which this mechanical coupling is maintained with locking means during the joining by means of laser fusion in the zones.
  5. A set of barrels for firearms comprising at least one barrel and a casing, into which is inserted a breech part of the barrel, characterized in that the barrel and the casing are joined together by means of laser fusion in at least two zones (A,B).
  6. A set of barrels for firearms in accordance with claim 5, wherein said joining zones are in proportion to the said opposite ends of the said casing and extend around the said barrels without apparent joining lines.
  7. A firearm comprising:
    at least one barrel and a casing, into which is inserted the said breech part of the barrel, characterized in that the barrel and the casing are joined together by the steps comprising:
    providing the breech of each barrel with an end portion (11') of predetermined shape and diameter, starting from a striking shoulder (11") turned towards the rear end of the said barrel and at right angles to the axis of said barrel;
    providing the monoblock casing with a through hole (12') for each barrel and with a striking surface (12") turned towards the striking shoulder of the barrel, the hole having a shape and a diameter corresponding to that of the end portion of the barrel and the striking surface being at a right angle to an axis of the hole;
    mechanically coupling the barrels and the casing by fitting the end portion of the barrel in the respective hole of the casing in order to bring the striking shoulder into close contact with the striking surface;
    permanently joining the barrels and the casing by means of laser fusion in at least two zones (A,B) at the level of the said shoulder and of the striking surface in close contact and of a rear end of the barrel and of the casing; and
    removing any excess material in the joining zones.
  8. A firearm according to claim 7, wherein each barrel and the casing are prepared with a possible machining allowance in the zones (A,B) intended for being joined by means of laser fusion.
  9. A firearm according to claim 7, wherein the end portion (11') of the barrel and the hole (12') in the casing are cylindrical and have the same diameter.
  10. A firearm according to claim 7, wherein the barrel and the casing are machined and prepared before the mechanical coupling, and in which this mechanical coupling is maintained with locking means during the joining by means of laser fusion in the zones (A,B).
EP96830579A 1996-08-02 1996-11-13 Method for coupling the barrels of rifles in the breech Expired - Lifetime EP0822382B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IT96BS000066A IT1288241B1 (en) 1996-08-02 1996-08-02 METHOD OF COUPLING IN CULATTA OF RIFLES
ITBS960066 1996-08-02

Publications (3)

Publication Number Publication Date
EP0822382A2 EP0822382A2 (en) 1998-02-04
EP0822382A3 EP0822382A3 (en) 1999-06-09
EP0822382B1 true EP0822382B1 (en) 2003-06-11

Family

ID=11345798

Family Applications (1)

Application Number Title Priority Date Filing Date
EP96830579A Expired - Lifetime EP0822382B1 (en) 1996-08-02 1996-11-13 Method for coupling the barrels of rifles in the breech

Country Status (10)

Country Link
EP (1) EP0822382B1 (en)
JP (1) JPH1068599A (en)
AR (1) AR005060A1 (en)
AT (1) ATE242861T1 (en)
DE (1) DE69628647T2 (en)
ES (1) ES2201164T3 (en)
IL (1) IL119664A0 (en)
IT (1) IT1288241B1 (en)
PT (1) PT822382E (en)
ZA (1) ZA9610074B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ITMI20111184A1 (en) * 2011-06-29 2012-12-30 Benelli Armi Spa STRUCTURE OF CANE FOR FIREARMS AND METHOD FOR ITS PRODUCTION
CN105444613B (en) * 2015-12-22 2017-04-19 中国兵器工业集团第二○二研究所 Segmented type barrel connecting structure

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB141540A (en) * 1919-05-27 1920-04-22 Nathaniel Chafee Walpole Improvements in the lining and relining of cannon
DE3509125A1 (en) * 1985-03-14 1986-09-25 Samuel Triesen Kindle Front-stock retention for hunting weapons

Also Published As

Publication number Publication date
ITBS960066A1 (en) 1998-02-02
EP0822382A2 (en) 1998-02-04
AR005060A1 (en) 1999-04-07
IL119664A0 (en) 1997-02-18
DE69628647D1 (en) 2003-07-17
ES2201164T3 (en) 2004-03-16
IT1288241B1 (en) 1998-09-11
ATE242861T1 (en) 2003-06-15
PT822382E (en) 2003-10-31
JPH1068599A (en) 1998-03-10
ZA9610074B (en) 1997-06-23
EP0822382A3 (en) 1999-06-09
DE69628647T2 (en) 2004-04-29

Similar Documents

Publication Publication Date Title
WO2005090862A1 (en) Alloy-coated boiler part and method of welding self-fluxing alloy-coated boiler part
JP2001038548A (en) Assembling method of camshaft and camshaft manufactured thereby
EP0822382B1 (en) Method for coupling the barrels of rifles in the breech
CN100402222C (en) Forge welding method
US4594020A (en) Welded oil well pump rod
EP2541187B1 (en) Barrel assembly for firearms and method for manufacturing it
NO20200057A1 (en) Method for manufacturing a connecting part
US3101532A (en) Self-leveling welding ring of triangular cross-section
WO1996010466A1 (en) Brazed joint for male member to female receptacle
JPH11513474A (en) Rotating stable bullet with metal band
US3120400A (en) Welded tubular attachment to a pressure member and method of making same
US6910618B2 (en) Method for preparing pipe for butt welding
US20180065205A1 (en) Method for producing a camshaft
US7641241B2 (en) Method of corrosion protection at a welded pipe joint and resulting joint
US4761873A (en) Method of manufacturing a hose stem for hydraulically loaded friction fittings or threaded fittings
CA1237275A (en) Crimpted drier drum structure
US20040256854A1 (en) Fitting for fluid conveyance
US3651594A (en) Shotgun barrel construction
JPH0256990B2 (en)
RU2064854C1 (en) Worn roll neck repair method
AU2004291562B2 (en) Method of corrosion protection at a welded pipe joint and resulting joint
JPH05222442A (en) Hearth roll
US3546417A (en) Shotgun barrel construction
Anton Procedure for the Manufacturing of Elements for Decorative Metal Structures
JPH08132229A (en) Production of split bearing

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: A2

Designated state(s): AT BE CH DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE

AX Request for extension of the european patent

Free format text: SI

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): AT BE CH DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE

AX Request for extension of the european patent

Free format text: SI

17P Request for examination filed

Effective date: 19990925

AKX Designation fees paid

Free format text: AT BE CH DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE

RBV Designated contracting states (corrected)

Designated state(s): AT BE CH DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE

17Q First examination report despatched

Effective date: 20010920

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

RBV Designated contracting states (corrected)

Designated state(s): AT BE CH DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE

AK Designated contracting states

Designated state(s): AT BE CH DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE

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

Ref country code: LI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20030611

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20030611

Ref country code: CH

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20030611

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20030611

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REF Corresponds to:

Ref document number: 69628647

Country of ref document: DE

Date of ref document: 20030717

Kind code of ref document: P

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

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20030911

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20030911

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20030911

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

Ref country code: LU

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

Effective date: 20031113

Ref country code: IE

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

Effective date: 20031113

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

Ref country code: MC

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

Effective date: 20031130

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2201164

Country of ref document: ES

Kind code of ref document: T3

ET Fr: translation filed
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

Effective date: 20040312

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

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

Ref country code: ES

Payment date: 20051006

Year of fee payment: 10

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

Ref country code: NL

Payment date: 20051018

Year of fee payment: 10

Ref country code: GB

Payment date: 20051018

Year of fee payment: 10

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

Ref country code: PT

Payment date: 20051019

Year of fee payment: 10

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

Ref country code: DE

Payment date: 20051026

Year of fee payment: 10

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

Ref country code: BE

Payment date: 20051103

Year of fee payment: 10

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

Ref country code: FR

Payment date: 20051130

Year of fee payment: 10

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

Ref country code: BE

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

Effective date: 20061130

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

Ref country code: PT

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

Effective date: 20070514

REG Reference to a national code

Ref country code: PT

Ref legal event code: MM4A

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

Effective date: 20070514

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

Ref country code: NL

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

Effective date: 20070601

Ref country code: DE

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

Effective date: 20070601

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

Effective date: 20061113

NLV4 Nl: lapsed or anulled due to non-payment of the annual fee

Effective date: 20070601

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20070731

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

Ref country code: GB

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

Effective date: 20061113

BERE Be: lapsed

Owner name: FABBRICA D'ARMI P. *BERETTA S.P.A.

Effective date: 20061130

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20061114

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: 20061130

Ref country code: ES

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

Effective date: 20061114

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

Ref country code: IT

Payment date: 20081126

Year of fee payment: 13

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

Effective date: 20091113