EP2191222B1 - Canon pour tirer des projectiles gyroscopés - Google Patents
Canon pour tirer des projectiles gyroscopés Download PDFInfo
- Publication number
- EP2191222B1 EP2191222B1 EP08801812.2A EP08801812A EP2191222B1 EP 2191222 B1 EP2191222 B1 EP 2191222B1 EP 08801812 A EP08801812 A EP 08801812A EP 2191222 B1 EP2191222 B1 EP 2191222B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- sealing ring
- barrel
- guiding band
- projectile
- gun barrel
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Not-in-force
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A21/00—Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
- F41A21/12—Cartridge chambers; Chamber liners
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A21/00—Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
- F41A21/16—Barrels or gun tubes characterised by the shape of the bore
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B14/00—Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels
- F42B14/02—Driving bands; Rotating bands
Definitions
- the invention relates to a gun barrel for firing spin-stabilized projectiles with a guide band and a rear side arranged behind the guide band sealing ring, with the features specified in the preamble of claim 1.
- Such gun tubes have long been known and usually include a cargo space, a drawn pipe part and arranged between the cargo space and the drawn pipe part transition cone.
- a projectile For loading a projectile it is pushed so far through the cargo space in the rear-side region of the drawn pipe part until the guide band of the projectile is located on the field-pull profile of the drawn pipe part.
- the rear side arranged by the guide band sealing ring which usually has a slightly larger outer diameter than the guide band is still in the transition cone of the gun barrel and should prevent firing at the beginning of the gas pressure buildup in the cargo space that the hot propellant gases between the guide band and the directly flow past the transition cone subsequent field-tensile profile of the drawn pipe part.
- the GB 232 989 A discloses a way to wear ammunition from a drawn barrel either very far or very short.
- the chamber of the gun barrel has at least two pressure cone, wherein at least between the first and the second cone a smooth section is provided.
- the rear pressure ball is intended for ammunition that is closed at close range, the front pressure cone for the firing of ammunition for the other distances.
- the range change itself is achieved by the length of the projectile or cartridge case is chosen differently.
- the ammunition is located on the rear or on the front shoulder of the cartridge chamber.
- the length of the cartridge chamber is dependent on the length of the cartridge case of the ammunition.
- the sealing ring In practice, however, it has been shown that, depending on the depth of the projectile, the sealing ring often does not rest exactly on the side walls of the transition cone and a complete initial sealing is not ensured by the sealing ring when firing. If an initial seal is not provided, the hot propellant gases flow between the guide band and the field-tensile profile in the region of the transition between the cargo space and the high-speed caliber flow part and cause severe erosion damage to the cargo chamber side end of the drawn pipe member. These erosion damages then lead to the separation of the weapon barrel.
- the invention has for its object to provide a gun barrel, in which an initial seal between the projectile and the field-tensile profile of the drawn pipe part is ensured against hot propellant gases, so that erosion damage on the load-space side Minimized end of the drawn pipe part.
- the invention is based essentially on the idea to arrange between the adjoining the cargo space transition cone and the drawn pipe part designed as a smooth tube section whose inner diameter is greater than or equal to the outer diameter of the guide band, but slightly smaller than the outer diameter of the sealing ring of the projectiles to be fired is, wherein the length of the smooth tube section is at least the length of the guide band and the sealing ring (together) of the respective projectile.
- the sealing ring arranged behind the guide band ensures an excellent initial seal when firing in the smooth pipe section until the guide strip is pressed completely into the field-pull profile of the drawn pipe part.
- a gun barrel for firing a spin-stabilized projectile 2 The gun barrel 1 comprises a cargo space 3, a drawn pipe part 4 with a known field-train profile and a between the Cargo space 3 and the drawn pipe part 4 arranged transition cone. 5
- a section 6 designed as a smooth tube is arranged between the transition cone 5 directly adjoining the charge space 3 and the drawn tube part 4.
- the designated D0 inner diameter of this smooth tube section 6 is selected such that it is slightly larger than the outer diameter D1 of the guide band 7 of each projectile to be fired and approximately equal to the outer diameter of a rear side on the guide band 7 of the projectile 2 arranged sealing ring. 8
- the length of the smooth tube section 6, however, is selected such that it corresponds at least to the length L0 of the guide band 7 and the length L1 of the sealing ring 8 of the respective projectile 2. This ensures that after loading the projectile 2 of the sealing ring 8 is located within the Giattrohrabêtes 6 and located in front of the guide belt 7 of the projectile 2 area 9 of the transition between the smooth pipe section 6 and the drawn pipe part 4 at firing against the in the cargo space. 3 generated propellant gases is securely sealed.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Portable Nailing Machines And Staplers (AREA)
Claims (4)
- Système, composé d'un canon pour tirer des projectiles (2) à stabilisation gyroscopique, ainsi que projectile (2) muni d'une bande de guidage (7) et d'une bague d'étanchéité (8) disposée du côté arrière derrière la bande de guidage (7), le canon (1) comprenant une chambre de charge (3), une partie tubulaire étirée (4) et un cône de transition (5) disposé entre la chambre de charge (3) et la partie tubulaire étirée (4),
une portion (6) réalisée sous la forme d'un tube lisse étant disposée entre le cône de transition (5) qui se raccorde à la chambre de charge (3) et la partie tubulaire étirée (4), de sorte que le début du profil rayé de la partie tubulaire étirée (4) est décalé hors de la zone (9) fortement menacée par l'érosion sur le cône de transition (5),
caractérisé en ce que* le diamètre intérieur (D0) de la portion (6) réalisée sous la forme d'un tube lisse est supérieur ou égal au diamètre extérieur (D1) de la bande de guidage (7), mais approximativement égal au diamètre extérieur de la bague d'étanchéité (8) des projectiles (2) à tirer hors du canon (1), et en ce que* la longueur de la portion en tube lisse (6) correspond au moins à la longueur (L0) de la bande de guidage (7) et à la longueur (L1) de la bague d'étanchéité (8) des projectiles (2) à tirer,* la bande de guidage (7) et la bague d'étanchéité (8) étant disposées directement l'une derrière l'autre, également d'une seule pièce, ou* la bague d'étanchéité (8) se trouve dans une rainure séparée dans le projectile (2) plus loin derrière la bande de guidage (7) et* la bague d'étanchéité (8) disposée derrière la bande de guidage (7), lors du coup de feu, contribue à une étanchéité initiale dans la portion (6) réalisée sous la forme d'un tube lisse jusqu'à ce que la bande de guidage (7) soit entièrement pressée dans le profil rayé de la partie tubulaire étirée (4). - Projectile (2) pour tirer depuis un canon (1) selon la revendication 1, caractérisé en ce que la bande de guidage (7) et la bague d'étanchéité (8) sont disposées directement l'une derrière l'autre.
- Projectile selon la revendication 2, caractérisé en ce que la bande de guidage (7) et la bague d'étanchéité (8) sont d'une seule pièce.
- Projectile (2) pour tirer depuis un canon (1) selon la revendication 1, caractérisé en ce que la bague d'étanchéité (8) se trouve dans une rainure séparée dans le projectile (2) plus loin derrière la bande de guidage (7).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102007045721A DE102007045721A1 (de) | 2007-09-24 | 2007-09-24 | Geschützrohr zum Verschießen drallstabilisierter Geschosse |
PCT/EP2008/007179 WO2009039941A1 (fr) | 2007-09-24 | 2008-09-03 | Canon pour tirer des projectiles gyroscopés |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2191222A1 EP2191222A1 (fr) | 2010-06-02 |
EP2191222B1 true EP2191222B1 (fr) | 2014-04-16 |
Family
ID=40260488
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP08801812.2A Not-in-force EP2191222B1 (fr) | 2007-09-24 | 2008-09-03 | Canon pour tirer des projectiles gyroscopés |
Country Status (5)
Country | Link |
---|---|
US (1) | US20100192445A1 (fr) |
EP (1) | EP2191222B1 (fr) |
DE (1) | DE102007045721A1 (fr) |
IL (1) | IL204602A (fr) |
WO (1) | WO2009039941A1 (fr) |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1455354A (en) * | 1918-05-28 | 1923-05-15 | Winfield P Porter | Projectile |
DE4000167A1 (de) * | 1990-01-05 | 1991-07-11 | Rheinmetall Gmbh | Drallstabilisiertes traegergeschoss mit einem metallischen fuehrungsband |
DE19532745A1 (de) * | 1995-09-05 | 1997-03-06 | Rheinmetall Ind Ag | Drallstabilisiertes Geschoß |
EP1006337A2 (fr) * | 1998-12-02 | 2000-06-07 | Rheinmetall W & M GmbH | Projectile d'artillerie stabilisé par rotation |
US6536353B1 (en) * | 1998-04-24 | 2003-03-25 | Rheinmetall W & M Gmbh | Spin-stabilized projectile having a multi-part guide band and method of making the projectile |
EP1617167A1 (fr) * | 2004-07-17 | 2006-01-18 | Rheinmetall Waffe Munition GmbH | Projectile d'artillerie avec ceinture de guidage |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US997539A (en) * | 1910-02-16 | 1911-07-11 | John H Brown | Gun. |
NL22279C (fr) * | 1924-04-28 | |||
FR615566A (fr) * | 1925-05-07 | 1927-01-11 | Système de rayage des bouches à feu | |
US1944883A (en) * | 1929-12-24 | 1934-01-30 | Gerlich Hermann | Projectile propelling apparatus |
US2288604A (en) * | 1935-09-28 | 1942-07-07 | Born Waldemar | Projectile |
CH213074A (de) * | 1939-03-23 | 1941-01-15 | Deutsche Waffen & Munitionsfab | Schusswaffe mit innen zum Teil konisch gehaltenem Lauf. |
US2395044A (en) * | 1942-04-02 | 1946-02-19 | Walter T Gorton | Gun |
DE1021759B (de) * | 1954-02-16 | 1957-12-27 | Brevets Aero Mecaniques | Patrone fuer insbesondere selbsttaetige Feuerwaffen |
US2815602A (en) * | 1954-02-23 | 1957-12-10 | Remington Arms Co Inc | Barrel chamber for cartridges of different length |
US2845741A (en) * | 1955-04-27 | 1958-08-05 | Olin Mathieson | Composite firearm barrel |
US3442172A (en) * | 1959-03-13 | 1969-05-06 | Fansteel Inc | Gun barrel liner |
US4366015A (en) * | 1980-05-16 | 1982-12-28 | Murray Myles N | Rubber driving band, artillery shell employing same, and method of making the band and assembling same in the shell |
SE442550B (sv) * | 1981-03-25 | 1986-01-13 | Bofors Ab | Anordning vid eldrorskammare for grovt artilleri |
USH1365H (en) * | 1994-02-04 | 1994-11-01 | The United States Of America As Represented By The Secretary Of The Air Force | Hybrid gun barrel |
SE508696C2 (sv) * | 1995-08-23 | 1998-10-26 | Rheinmetall Ind Ag | Draget vapenrör samt förfarande för framställning av sådant rör |
DE19815295C2 (de) * | 1998-04-06 | 2003-05-15 | Rheinmetall W & M Gmbh | Aus einem Waffenrohr verschießbares drallstabilisiertes Artilleriegeschoß |
DE19855535A1 (de) * | 1998-12-02 | 2000-06-08 | Rheinmetall W & M Gmbh | Drallstabilisiertes Artilleriegeschoß |
DE10213466A1 (de) * | 2002-03-26 | 2003-10-09 | Rheinmetall W & M Gmbh | Geschoßkörper |
SE529753C2 (sv) * | 2006-03-14 | 2007-11-13 | Bae Systems Bofors Ab | Projektil eller granat med förskjutbar gördel, vilken tätar så att eldrörsslitage ej påverkar utskjutningshastigheten |
-
2007
- 2007-09-24 DE DE102007045721A patent/DE102007045721A1/de not_active Withdrawn
-
2008
- 2008-09-03 WO PCT/EP2008/007179 patent/WO2009039941A1/fr active Application Filing
- 2008-09-03 US US12/679,638 patent/US20100192445A1/en not_active Abandoned
- 2008-09-03 EP EP08801812.2A patent/EP2191222B1/fr not_active Not-in-force
-
2010
- 2010-03-18 IL IL204602A patent/IL204602A/en not_active IP Right Cessation
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1455354A (en) * | 1918-05-28 | 1923-05-15 | Winfield P Porter | Projectile |
DE4000167A1 (de) * | 1990-01-05 | 1991-07-11 | Rheinmetall Gmbh | Drallstabilisiertes traegergeschoss mit einem metallischen fuehrungsband |
DE19532745A1 (de) * | 1995-09-05 | 1997-03-06 | Rheinmetall Ind Ag | Drallstabilisiertes Geschoß |
US6536353B1 (en) * | 1998-04-24 | 2003-03-25 | Rheinmetall W & M Gmbh | Spin-stabilized projectile having a multi-part guide band and method of making the projectile |
EP1006337A2 (fr) * | 1998-12-02 | 2000-06-07 | Rheinmetall W & M GmbH | Projectile d'artillerie stabilisé par rotation |
EP1617167A1 (fr) * | 2004-07-17 | 2006-01-18 | Rheinmetall Waffe Munition GmbH | Projectile d'artillerie avec ceinture de guidage |
Also Published As
Publication number | Publication date |
---|---|
IL204602A0 (en) | 2010-11-30 |
EP2191222A1 (fr) | 2010-06-02 |
WO2009039941A1 (fr) | 2009-04-02 |
DE102007045721A1 (de) | 2009-04-02 |
IL204602A (en) | 2015-08-31 |
US20100192445A1 (en) | 2010-08-05 |
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