EP2909570A1 - Patrone und verfahren zu seiner herstellung - Google Patents
Patrone und verfahren zu seiner herstellungInfo
- Publication number
- EP2909570A1 EP2909570A1 EP13779532.4A EP13779532A EP2909570A1 EP 2909570 A1 EP2909570 A1 EP 2909570A1 EP 13779532 A EP13779532 A EP 13779532A EP 2909570 A1 EP2909570 A1 EP 2909570A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- adhesive
- sleeve cover
- sleeve
- casing
- tail body
- 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
- 238000004519 manufacturing process Methods 0.000 title claims description 4
- 238000000034 method Methods 0.000 title description 3
- 239000000853 adhesive Substances 0.000 claims abstract description 25
- 230000001070 adhesive effect Effects 0.000 claims abstract description 25
- 239000003380 propellant Substances 0.000 claims abstract description 15
- 239000007787 solid Substances 0.000 claims abstract description 4
- 238000013016 damping Methods 0.000 claims description 7
- 239000013464 silicone adhesive Substances 0.000 claims description 7
- 229920002379 silicone rubber Polymers 0.000 claims description 3
- 239000004945 silicone rubber Substances 0.000 claims description 3
- 239000013013 elastic material Substances 0.000 claims description 2
- 239000003381 stabilizer Substances 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract 1
- 230000007613 environmental effect Effects 0.000 abstract 1
- 238000003912 environmental pollution Methods 0.000 description 4
- 229920001296 polysiloxane Polymers 0.000 description 4
- 230000001419 dependent effect Effects 0.000 description 2
- 239000003292 glue Substances 0.000 description 2
- 229920004482 WACKER® Polymers 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/18—Caseless ammunition; Cartridges having combustible cases
- F42B5/188—Manufacturing processes therefor
Definitions
- the invention relates to a training cartridge or a combat ammunition with a consisting of a sleeve sheath and a sleeve cover combustible propellant charge shell and a stabilized full scale caliber bullet with a solid headboard and a rear side of the headboard subsequent tubular tail body.
- the front, conically tapered region of the sleeve cover of the propellant charge sleeve protrudes at least partially into a correspondingly conically tapered, rear-side region of the tubular tail body and is positively connected thereto by means of an adhesive.
- the invention proposes to form the adhesive between the full-caliber bullet and the sleeve cover of the propellant charge tube as a damping element.
- DE 10 2009 009 772 A1 discloses a non-positive adhesive connection between a segmented receiving device and a driving element.
- An adhesive connection between knob-shaped extensions with a support wall is mentioned in DE 10 2008 029 397 A1.
- the bonding of a serving as a sealing ring portion of a sleeve cover on the projectile provides the DE 10 2008 015 421 A1 before.
- DE 10 2007 037 741 A1 which proposes to join the connection between the sleeve jacket and the projectile by friction welding, leads away from these adhesive bonds.
- An exercise cartridge in which a sleeve cover and a projectile casing are connected to one another via an adhesive connection is known from DE 10 2010 034 333 A1. These are ammunition which can be fired from the cannon of a tank with a a bullet caliber of, for example, 120 mm.
- the projectile casing itself is designed as a tubular tail body. so that a separate shaft with attached fin assembly can be omitted.
- the propellant charge gases produced at the time the missile is fired enter the interior of the tubular tail body and act on the rear-end region of the head part to accelerate the training projectile, which delimits the interior of the bullet head.
- the invention has for its object to provide a way in which the likelihood that it comes due to environmental pollution to damage the propellant charge through the full-caliber bullet, compared to comparable known cartridges is substantially reduced.
- a method for producing such a cartridge is to be specified.
- the invention is based essentially on the idea to arrange a damping element between the full-caliber bullet and the sleeve cover of the propellant charge sleeve.
- This is realized in a simple manner by appropriate choice and arrangement of an existing of an elastic material adhesive which connects the sleeve cover with the Vollkalibergeunter on the one hand, on the other hand serves as a damping or damping means. That is, the adhesive also serves as a damping agent or at the same time.
- a silicone adhesive preferably a silicone rubber, with a layer thickness of at least 300 ⁇ (+/-) is used as the adhesive.
- the layer thickness (s) themselves, however, is dependent on the bonded area, so that the preferred layer thickness (s) is (are) only to be regarded as the reference and empirical value (s).
- the sleeve cover is centered by means of a tool for the tail body, but radially spaced, arranged and then the silicone adhesive thick-beaded on the Au OHseite the sleeve cover applied. Subsequently, the tail body is pushed onto the sleeve cover, such that the space between the sleeve cover and tail body is completely filled by the silicone layer. Finally, the silicone layer is cured.
- the tail-stabilized full-caliber bullet is denoted by 1 and comprises a solid head part 2 and a tubular tail body 3 adjoining the head part 2 at the rear.
- the front, conically tapered region 4 of the sleeve cover 5 projects into a correspondingly conically tapering rear region 6 of the tubular body Leitmaschines stressess 3 and is connected thereto by means of an adhesive 7.
- the adhesive 7 causes both a frictional connection between sleeve cover 5 and tail body 3 as well as the function of a damping element takes over to avoid damage to the propellant charge shell by the full caliber projectile 1 in environmental pollution.
- the sleeve cover 5 is centered by means of a tool for the tail body 3, but radially spaced.
- a silicone adhesive 7 preferably silicone rubber (for example Elastosil E43 from Wacker Chemie, Kunststoff) is applied thick-beaded onto the outside 8 of the sleeve cover 5.
- the guide factory body 3 is then pushed so far on the sleeve cover 5 until the distance between the Au .seite 8 of the sleeve cover 5 and the inside 9 of the tail body 3 is about 500 ⁇ .
- the gap between sleeve cover 5 and tail body 3 can then be completely filled by the silicone adhesive 7.
- Elastosil silicone adhesives are one-component adhesives that cure by absorbing moisture - from the air.
- the specified curing time for further handling is at least 6 hours. If, on the other hand, two-component adhesives, eg Loctite, are used, the defined curing time is at least 50 minutes. As a result, the curing time can be significantly reduced.
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Buffer Packaging (AREA)
Abstract
Description
Claims
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL13779532T PL2909570T3 (pl) | 2012-10-19 | 2013-10-07 | Nabój i sposób jego wytwarzania |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102012020540.6A DE102012020540A1 (de) | 2012-10-19 | 2012-10-19 | Patrone und Verfahren zu seiner Herstellung |
PCT/EP2013/070850 WO2014060237A1 (de) | 2012-10-19 | 2013-10-07 | Patrone und verfahren zu seiner herstellung |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2909570A1 true EP2909570A1 (de) | 2015-08-26 |
EP2909570B1 EP2909570B1 (de) | 2018-05-30 |
Family
ID=49447524
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP13779532.4A Active EP2909570B1 (de) | 2012-10-19 | 2013-10-07 | Patrone und verfahren zu seiner herstellung |
Country Status (9)
Country | Link |
---|---|
EP (1) | EP2909570B1 (de) |
DE (1) | DE102012020540A1 (de) |
DK (1) | DK2909570T3 (de) |
ES (1) | ES2681977T3 (de) |
HU (1) | HUE039282T2 (de) |
PL (1) | PL2909570T3 (de) |
PT (1) | PT2909570T (de) |
TR (1) | TR201810338T4 (de) |
WO (1) | WO2014060237A1 (de) |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2323244C3 (de) * | 1973-05-09 | 1979-04-19 | Rheinmetall Gmbh, 4000 Duesseldorf | Flügelstabilisiertes Unterkalibergeschoß |
DE3716076A1 (de) * | 1987-05-14 | 1988-11-24 | Rheinmetall Gmbh | Patronierte munition mit geschoss und verbrennbarer huelse |
FR2620214B1 (fr) * | 1987-09-09 | 1990-04-13 | France Etat Armement | Bague de liaison entre un projectile et une douille |
ATE217077T1 (de) * | 1997-02-25 | 2002-05-15 | Ruag Munition | Vorrichtung für die optische markierung der flugbahn von durch triebwerke beschleunigten flugkörpern |
DE19929915A1 (de) * | 1999-06-29 | 2001-01-18 | Rheinmetall W & M Gmbh | Patrone mit einem Treibkäfiggeschoß |
DE10055068B4 (de) * | 2000-11-07 | 2006-08-17 | Rheinmetall Waffe Munition Gmbh | Patrone |
DE102007037741B4 (de) | 2007-08-09 | 2014-01-16 | Rheinmetall Waffe Munition Gmbh | Verfahren zum Verbinden eines rohrförmigen Hülsenmantels und eines Hülsendeckels einer Patrone |
DE102008015421A1 (de) | 2008-03-20 | 2009-09-24 | Rheinmetall Waffe Munition Gmbh | Verfahren zur Herstellung einer Patrone und Patrone mit einem Treibkäfiggeschoss, hergestellt nach diesem Verfahren |
DE102008029397A1 (de) | 2008-06-23 | 2009-12-24 | Rheinmetall Waffe Munition Gmbh | Treibkäfiggeschoss |
DE102009009772A1 (de) | 2009-02-20 | 2010-09-02 | Rheinmetall Waffe Munition Gmbh | Verfahren zum Einbringen von Sollbruchstellen in ein ringförmiges Halte- und Dichtungsband eines Treibkäfiggeschosses und Laborierwerkzeug zur Durchführung des Verfahrens |
US8408137B2 (en) * | 2009-05-06 | 2013-04-02 | Vin Battaglia | Spiral case ammunition |
DE102010034333B4 (de) | 2010-07-06 | 2014-12-11 | Rheinmetall Waffe Munition Gmbh | Vollkaliber-Übungsmunition |
-
2012
- 2012-10-19 DE DE102012020540.6A patent/DE102012020540A1/de not_active Withdrawn
-
2013
- 2013-10-07 EP EP13779532.4A patent/EP2909570B1/de active Active
- 2013-10-07 HU HUE13779532A patent/HUE039282T2/hu unknown
- 2013-10-07 PL PL13779532T patent/PL2909570T3/pl unknown
- 2013-10-07 TR TR2018/10338T patent/TR201810338T4/tr unknown
- 2013-10-07 PT PT137795324T patent/PT2909570T/pt unknown
- 2013-10-07 WO PCT/EP2013/070850 patent/WO2014060237A1/de active Application Filing
- 2013-10-07 DK DK13779532.4T patent/DK2909570T3/en active
- 2013-10-07 ES ES13779532.4T patent/ES2681977T3/es active Active
Non-Patent Citations (1)
Title |
---|
See references of WO2014060237A1 * |
Also Published As
Publication number | Publication date |
---|---|
HUE039282T2 (hu) | 2018-12-28 |
DE102012020540A1 (de) | 2014-04-24 |
PL2909570T3 (pl) | 2018-10-31 |
EP2909570B1 (de) | 2018-05-30 |
ES2681977T3 (es) | 2018-09-17 |
DK2909570T3 (en) | 2018-08-20 |
WO2014060237A1 (de) | 2014-04-24 |
TR201810338T4 (tr) | 2018-08-27 |
PT2909570T (pt) | 2018-07-17 |
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