EP0314870A2 - Projectile porteur à stabilisation par rotation équipé d'une ceinture de rotation - Google Patents
Projectile porteur à stabilisation par rotation équipé d'une ceinture de rotation Download PDFInfo
- Publication number
- EP0314870A2 EP0314870A2 EP88109510A EP88109510A EP0314870A2 EP 0314870 A2 EP0314870 A2 EP 0314870A2 EP 88109510 A EP88109510 A EP 88109510A EP 88109510 A EP88109510 A EP 88109510A EP 0314870 A2 EP0314870 A2 EP 0314870A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- floor
- guide band
- projectile
- spin
- guide
- 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.)
- Granted
Links
Images
Classifications
-
- 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 swirl-stabilized carrier projectile provided with a guide band, as defined in more detail in the preamble of the patent claim.
- the projectiles are provided with guide bands for transmitting the swirl.
- the diameter of the guide bands is such that they press into the trains as the bullet passes through the tube.
- the guide band is usually arranged either on the floor or on the shell of the projectile. If the guide band is on the floor, the twist transmission between the floor and the casing is usually carried out via a pin or screw connection.
- the screw connection was previously used for thick-walled casings.
- the pin connection has advantages over thin-walled sleeves. A large number of pins are arranged over the circumference in order to ensure a secure swirl transmission in the pin connection. This requires a relatively large ejection charge to shear the pins when the submunitions are ejected.
- the guide band is arranged on the projectile casing, a relatively complex radial support structure of the casing in the guide band area is required. Otherwise, the sealing function of the guide band would not be guaranteed due to the large radial compressive forces of the tube on the guide band.
- the projectile is particularly sensitive to radial pressure, since large stresses on the material can occur at locations dependent on the projectile geometry.
- the present invention is therefore based on the object of specifying a carrier projectile of the type mentioned at the beginning, in which on the one hand the swirl transmission between the casing and the floor is eliminated and in which on the other hand a complex support structure of the casing in the guide band area is not required.
- the invention is therefore based on the idea of distributing the guide band over the shell and floor, so that a direct swirl transmission takes place in both storey components. Due to a guide band distribution corresponding to the axial inertia conditions, the previously required twist transmission between the shell and the bottom is eliminated.
- the connection between the shell and the bottom can therefore be designed to meet emissions requirements (e.g. only two instead of 8 dowel pins) and thus one Contributing to the minimization of the projectile load during ejection.
- 10 is a carrier floor. At the rear end of the carrier floor 10 there is a floor 11, which is connected to the shell 12 of the carrier floor 10 via shear pins 13.
- Submunition bodies may be located in the interior of the carrier projectile, the rear-side submunition body, which is only shown schematically, being indicated by 15.
- the guide band 14 is dimensioned so that it fully presses into the trains when the projectile passes through the tube. It transmits the swirl to the floor 11 via the strip guide of the trains and via the shear pins 13 to the floor case 12.
- the submunition projectiles 15 are ejected by, for example, igniting a pyrotechnic charge in the bow-side part of the carrier projectile 10, which pushes the submunition projectiles 15 backwards so that it is at a sufficiently high pressure to shear the pins 13 is coming.
- the guide band is composed of two partial guide bands 140 and 141.
- the first part guide band 140 is arranged on the floor 11 and the second part guide band 141 on the floor case 12.
- the guide band causes a direct swirl transmission both to the floor 11 and to the shell 12.
- the swirl transmission between the shell 12 and the floor 11, which is usually necessary, is therefore eliminated.
- the number of shear pins can be reduced compared to conventional carrier projectiles 10 (e.g. Only two pins may be required), and consequently the ejection charge required to shear the pins can be significantly reduced. Ultimately, this leads to a considerable reduction in the projectile load during ejection.
- the guide band 140 located on the floor 11 could e.g. B. made of copper and the guide band 141 located on the sleeve 12 are made of soft iron.
- the guide band 140 located on the floor 11 and fasten the partial guide band 141 to the cover 12 with three welds.
- the different materials and types of fastening shown by way of example are chosen because the thin wall of the casing does not allow the partial guide band 141 made of copper to be shrunk on and a soft iron guide band must be used instead.
- the floor 11, on the other hand allows the shrinking of a partial guide band 140 made of copper thanks to the greater wall thickness. In general, copper is preferred as the belt material because it causes less tube wear.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Toys (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19873734033 DE3734033A1 (de) | 1987-10-08 | 1987-10-08 | Mit einem fuehrungsband versehenes drallstabilisiertes traegergeschoss |
DE3734033 | 1987-10-08 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0314870A2 true EP0314870A2 (fr) | 1989-05-10 |
EP0314870A3 EP0314870A3 (en) | 1990-02-07 |
EP0314870B1 EP0314870B1 (fr) | 1992-03-18 |
Family
ID=6337890
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP19880109510 Expired - Lifetime EP0314870B1 (fr) | 1987-10-08 | 1988-06-15 | Projectile porteur à stabilisation par rotation équipé d'une ceinture de rotation |
Country Status (3)
Country | Link |
---|---|
US (1) | US4884508A (fr) |
EP (1) | EP0314870B1 (fr) |
DE (2) | DE3734033A1 (fr) |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4000167C2 (de) * | 1990-01-05 | 1994-04-14 | Rheinmetall Gmbh | Drallstabilisiertes Trägergeschoß mit einem metallischen Führungsband |
DE4025844C2 (de) * | 1990-08-16 | 1996-08-08 | Diehl Gmbh & Co | Geschoß-Führungsband aus Formgedächtnismetall |
DE19818411C2 (de) | 1998-04-24 | 2002-04-18 | Rheinmetall W & M Gmbh | Drallstabilisiertes Geschoß und Verfahren zu seiner Herstellung |
DE19855535A1 (de) * | 1998-12-02 | 2000-06-08 | Rheinmetall W & M Gmbh | Drallstabilisiertes Artilleriegeschoß |
DE19855536A1 (de) * | 1998-12-02 | 2000-06-08 | Rheinmetall W & M Gmbh | Drallstabilisiertes Artilleriegeschoß |
SE518516C2 (sv) * | 2001-04-19 | 2002-10-22 | Bofors Defence Ab | Sätt och anordning för förbättring av ytterballistiken för en artillerigranat |
US6763765B2 (en) * | 2001-09-27 | 2004-07-20 | Harold Crowson | Break-away gas check for muzzle-loading firearms |
DE10157667B4 (de) * | 2001-11-24 | 2007-10-04 | Rheinmetall Waffe Munition Gmbh | Aus einer Rohrwaffe verschießbares Vollkalibergeschoss |
DE10213466A1 (de) * | 2002-03-26 | 2003-10-09 | Rheinmetall W & M Gmbh | Geschoßkörper |
US6668814B1 (en) | 2002-08-12 | 2003-12-30 | The United States Of America As Represented By The Secretary Of The Navy | Mechanism for deploying cylindrical objects from a spinning container |
US7921780B2 (en) * | 2004-04-02 | 2011-04-12 | Techventure Investments Pty Ltd | Projectile |
US7748325B2 (en) * | 2005-10-21 | 2010-07-06 | Liberty Ammunition, Llc | Firearms projectile |
US8082850B2 (en) * | 2005-10-21 | 2011-12-27 | Liberty Ammunition, Inc. | Synchronized spin multi-component projectile |
NZ579812A (en) * | 2007-03-30 | 2011-05-27 | Techventure Investments Pty Ltd | A method of manufacturing a caseless projectile for a small arms weapon |
DE102010006221A1 (de) * | 2010-01-28 | 2011-08-18 | Rheinmetall Waffe Munition GmbH, 29345 | Drallstabilisiertes Geschoss |
WO2013082557A1 (fr) * | 2011-11-30 | 2013-06-06 | Alliant Techsystems Inc. | Projectile polymère présentant une ceinture de projectile intégrée |
WO2013109634A1 (fr) | 2012-01-16 | 2013-07-25 | Alliant Techsystems Inc. | Projectile non mortel stabilisé par rotation avec fluide rhéofluidifiant |
USD813974S1 (en) | 2015-11-06 | 2018-03-27 | Vista Outdoor Operations Llc | Cartridge with an enhanced ball round |
US10551154B2 (en) | 2017-01-20 | 2020-02-04 | Vista Outdoor Operations Llc | Rifle cartridge with improved bullet upset and separation |
US10690464B2 (en) | 2017-04-28 | 2020-06-23 | Vista Outdoor Operations Llc | Cartridge with combined effects projectile |
USD848569S1 (en) | 2018-01-20 | 2019-05-14 | Vista Outdoor Operations Llc | Rifle cartridge |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE53992C (de) * | H. ST. MAXIM in London | Artillerie-Geschofs mit gasdichtem Abschlufs | ||
US1345689A (en) * | 1917-06-30 | 1920-07-06 | Morris Joseph | Shell or projectile |
FR1245379A (fr) * | 1959-01-19 | 1960-11-04 | Brevets Aero Mecaniques | Perfectionnements apportés aux obus perforants comportant un noyau en matière durecoiffé d'une ogive établie au moins partiellement en matière légère, pour armesà canon rayé |
FR2087797A5 (fr) * | 1970-03-12 | 1971-12-31 | Space Res Corp | |
US3769912A (en) * | 1970-10-23 | 1973-11-06 | W Friend | Spin-stabilized projectiles |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US443101A (en) * | 1890-12-23 | maxim | ||
FR1231601A (fr) * | 1945-08-27 | 1960-09-30 | Ct D Etudes M B A Mecanqiue Ba | Projectile d'artillerie muni de ceintures éjectables |
FR1166011A (fr) * | 1957-01-17 | 1958-11-03 | Projectile surallongé | |
FR1385392A (fr) * | 1963-08-12 | 1965-01-15 | Haut Rhin Manufacture Machines | Projectiles ceinturés perfectionnés notamment pour armes automatiques de petit calibre |
DE3630000A1 (de) * | 1986-09-03 | 1988-03-17 | Rheinmetall Gmbh | Geschosskoerper mit auf der geschosshuelle angeordnetem fuehrungsband |
-
1987
- 1987-10-08 DE DE19873734033 patent/DE3734033A1/de not_active Withdrawn
-
1988
- 1988-06-15 EP EP19880109510 patent/EP0314870B1/fr not_active Expired - Lifetime
- 1988-06-15 DE DE8888109510T patent/DE3869323D1/de not_active Expired - Lifetime
- 1988-09-22 US US07/247,623 patent/US4884508A/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE53992C (de) * | H. ST. MAXIM in London | Artillerie-Geschofs mit gasdichtem Abschlufs | ||
US1345689A (en) * | 1917-06-30 | 1920-07-06 | Morris Joseph | Shell or projectile |
FR1245379A (fr) * | 1959-01-19 | 1960-11-04 | Brevets Aero Mecaniques | Perfectionnements apportés aux obus perforants comportant un noyau en matière durecoiffé d'une ogive établie au moins partiellement en matière légère, pour armesà canon rayé |
FR2087797A5 (fr) * | 1970-03-12 | 1971-12-31 | Space Res Corp | |
US3769912A (en) * | 1970-10-23 | 1973-11-06 | W Friend | Spin-stabilized projectiles |
Non-Patent Citations (1)
Title |
---|
Wehrtechnik 2/84 Seite 82 * |
Also Published As
Publication number | Publication date |
---|---|
US4884508A (en) | 1989-12-05 |
EP0314870A3 (en) | 1990-02-07 |
EP0314870B1 (fr) | 1992-03-18 |
DE3734033A1 (de) | 1989-04-20 |
DE3869323D1 (de) | 1992-04-23 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0314870B1 (fr) | Projectile porteur à stabilisation par rotation équipé d'une ceinture de rotation | |
DE3004047C2 (de) | Panzerbrechendes Geschoß | |
DE69709083T2 (de) | Verfahren und vorrichtung zur programmierung eines geschosses | |
DE3207220A1 (de) | Geschossanordnung | |
DE20320359U1 (de) | Projektildichtungsanordnung | |
EP0101795A1 (fr) | Projectile explosif à effet d'éclats | |
DE2639884A1 (de) | Geschoss fuer uebungsmunition | |
EP0072584B1 (fr) | Liaison entre l'enveloppe et la partie arrière d'un sabot pour projectile | |
DE4123649A1 (de) | Ausstossvorrichtung | |
EP0088898A1 (fr) | Projectile de calibre réduit à noyau perforant | |
DE2826497A1 (de) | Treibspiegelgeschoss mit pyrotechnischem satz | |
DE3888288T2 (de) | Treibladung für flügelstabilisierte Geschossmunition sowie Verfahren zu ihrer Herstellung. | |
EP1347262B1 (fr) | Charge propulsive pour munition de gros calibre | |
DE2143605A1 (de) | Patrone und Verfahren zu deren Her stellung | |
EP0258531B1 (fr) | Projectile et sa ceinture d'étanchéité | |
EP0378749B1 (fr) | Dispositif pour la fixation du revêtement d'une charge creuse ou d'une charge formant un projectile | |
DE2852334A1 (de) | Verfahren zur herstellung gepresster, insbesondere grosskalibriger sprengladungen | |
EP0298997B1 (fr) | Bande de guidage pour projectile | |
EP0404844B1 (fr) | Culot pour projectiles porteurs de charges | |
DE4202129B4 (de) | Kompakter Ladungskörper | |
EP0237711A2 (fr) | Allumeur pour charge propulsive d'une cartouche | |
CH598562A5 (en) | Artillery projectile with enclosing nose and base | |
DE3434847C1 (de) | Verfahren zur Montage einer Hohlladung | |
DE3323386A1 (de) | Geschoss | |
DE19650741C2 (de) | Verfahren zur Herstellung eines unterkalibrigen Geschosses |
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): DE ES FR GB IT NL |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
AK | Designated contracting states |
Kind code of ref document: A3 Designated state(s): DE ES FR GB IT NL |
|
17P | Request for examination filed |
Effective date: 19900108 |
|
17Q | First examination report despatched |
Effective date: 19901005 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): DE ES FR GB IT NL |
|
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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRE;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED.SCRIBED TIME-LIMIT Effective date: 19920318 Ref country code: ES Free format text: THE PATENT HAS BEEN ANNULLED BY A DECISION OF A NATIONAL AUTHORITY Effective date: 19920318 Ref country code: NL Effective date: 19920318 Ref country code: GB Effective date: 19920318 |
|
REF | Corresponds to: |
Ref document number: 3869323 Country of ref document: DE Date of ref document: 19920423 |
|
ET | Fr: translation filed | ||
NLV1 | Nl: lapsed or annulled due to failure to fulfill the requirements of art. 29p and 29m of the patents act | ||
GBV | Gb: ep patent (uk) treated as always having been void in accordance with gb section 77(7)/1977 [no translation filed] | ||
RAP4 | Party data changed (patent owner data changed or rights of a patent transferred) |
Owner name: RHEINMETALL GMBH |
|
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 | ||
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20060619 Year of fee payment: 19 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20070622 Year of fee payment: 20 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST Effective date: 20080229 |
|
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: 20070702 |