EP3002543A1 - Projectile with a cover - Google Patents
Projectile with a cover Download PDFInfo
- Publication number
- EP3002543A1 EP3002543A1 EP15194890.8A EP15194890A EP3002543A1 EP 3002543 A1 EP3002543 A1 EP 3002543A1 EP 15194890 A EP15194890 A EP 15194890A EP 3002543 A1 EP3002543 A1 EP 3002543A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- cover
- projectile
- bore
- projectile body
- groove contour
- 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.)
- Ceased
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/38—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information of tracer type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
- F42B10/38—Range-increasing arrangements
- F42B10/40—Range-increasing arrangements with combustion of a slow-burning charge, e.g. fumers, base-bleed projectiles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B33/00—Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
- F42B33/001—Devices or processes for assembling ammunition, cartridges or cartridge elements from parts
Definitions
- the invention deals with a projectile with a cover to the cover, such as a tracer or the like, which is usually located in the rear part of a projectile body and with the theme that the tracer or such content must be hermetically sealed, since the otherwise penetrating moisture etc. may cause, for example, the tracer - Pyrotechnics- no longer or only insufficiently burned.
- a cover preferably a cover ring, proposed, which is pressed during the forming process by an axial feed movement of a (rigid) punch, preferably made of metal, radially into a preferably completely circumferential groove contour of the projectile body.
- the punch has an outer dimension that is pending from the axial position of the punch relative to the cover.
- the disadvantage of the deformation is, inter alia, that often conflicting requirements are made of the projectile body material.
- hard or hard to non-deformable material properties are presumed, while for the forming process such as crimping, caulking etc. soft or ductile material properties are the prerequisite. Therefore, the area of the projectile body material to be reshaped is made soft or ductile by applying heat treatment methods, which is however very complicated and time consuming as well as costly.
- the process stability is also to be kept at great expense.
- the formation of cracks in the material which can occur during hardening or during the forming, are themselves heat treatment processes which have been preceded by the subsequent or the forming process can not be ruled out and can lead to failure of the cover as possible sources of error.
- the screw and nut only have to be subjected to a surface treatment, for example hard anodizing, but the outlay on assembly is higher since measures for securing the screw are necessary. Guide surfaces for better installation take up a corresponding space.
- the weight of a screw to cover the tracer is higher than that of a cover ring.
- the invention has the object to show a projectile that allows better coverage, for example, the tracer.
- the invention is based on the idea not to transform the projectile body material but the cover itself.
- a part of the cover is radially pressed by a preferably rigid punch, which only needs to move axially, and is provided with a special outer contour, pressed into a circumferential groove contour in the projectile body.
- the outer contour should be matched to the groove contour (or vice versa), so that the radially outwardly formed in the forward movement stamp material of the cover can be pressed into the groove contour of the projectile body and the cover has no degrees of freedom after forming more, so this is fixed to the tracer or the like.
- the cover is preferably a cover ring.
- the cover Since the cover is deformed from the inside to the outside, this is pressed by the acceleration, mass and centrifugal forces occurring during the launch of the projectile against the projectile body, so that no flying parts arise.
- the positioning of the cover by means of a preferably rigid die guarantees high process stability, which is a prerequisite to the safety requirements in order to prevent it from flying off parts due to errors in the forming process or inadequate heat treatment.
- This idea can also be applied independently of the material properties of the projectile body and allows maximum flexibility regarding the materials to be used for the projectile body.
- the Fig. 1 shows in a simplified representation of the basic principle of the method. 1 with a rear part of a projectile 10 is designated, wherein the rear part 1 in a bore 11 a tracer 2, 3 receives.
- the tracer 2, 3 in turn consists of a flare-compact 2 and a 3 cheeks, which are preferably pressed in the bore 11.
- in the tracer 2, 3 are in this case pyrotechnic substances, which reacts with other chemical substances, such as those contained in the propellant charge powder.
- a cover 4 is used to seal the tracer 2, 3 from the environment until the time of firing of the projectile 10 from a weapon, not shown, to avoid contact of the substances with humid air, etc.
- the cover 4 is fixed by a cover 6 in the rear part 1.
- the cover 4 and the cover 6 are inserted into the recess 12 provided in the projectile body 10, as in Fig. 2 shown. Subsequently, the cover ring 6 is pressed with a punch 5, preferably made of metal, in the bore 11 of the rear part 1 of the projectile body 10 ( Fig.2 ), wherein the punch 5 in the forward movement or the axial movement and due to its (special) outer contour 7, the cover ring 6 in the preferably circumferential groove 8 in the projectile body or rear part 1 deformed. After pressing the cover ring 6 including cover 4, the cover of the tracer 2, 3 is ensured in the bore 11 relative to the environment, the forming process is completed ( Figure 3 ).
- Fig. 4 shows a sectional view of a cover 6, which is preferably designed as a cover ring. This fixes the cover 4.
- the cover 4 and the cover 6 can also form a one-piece constructive unit.
- this method is not limited to the sealing of a luminous trace in the rear part 1 of a projectile 10.
- Holes are here also understood as cavities, recesses, openings or the like in the projectile body, ammunition body, etc.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Manufacturing & Machinery (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Automatic Assembly (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
Vorgeschlagen wird ein Geschoss (10) mit einer Abdeckung (6) in einer Bohrung (11) im Geschoss (10), wobei das Geschoss (10) eine Nutkontur (8) im Geschosskörper aufweist, die Abdeckung (6) als Abdeckring ausgeführt ist, der eine Abdeckscheibe (4) der Abdeckung im Heckteil (1) fixiert, und der Abdeckring (6) in die Nutkontur (8) des Geschosskörpers hineingedrückt ist, wodurch eine luftdichte Abdeckung der Bohrung (11) gegenüber der Umgebung sichergestellt ist. Diesem Vorschlag liegt die Idee zugrunde, nicht das Geschosskörpermaterial sondern die Abdeckung (6) selbst umzuformen. Dazu wird ein Teil der Abdeckung (6) radial durch einen vorzugsweise starren Stempel (5), der sich ausschließlich nur axial zu bewegen braucht, in die umlaufende Nutkontur (8) im Geschosskörper gepresst. Die Außenkontur (7) des Stempels sollte dabei auf die Nutkontur (8) (oder umgekehrt) abgestimmt sein, damit das von dem in der Vorwärtsbewegung befindlichen Stempel (5) radial umgeformte Material der Abdeckung (6) in die Nutkontur (8) des Geschosskörpers hineingedrückt werden kann und die Abdeckung (6) nach der Umformung über keinerlei Freiheitsgrade mehr verfügt, sodass diese zur Leuchtspur (2, 3) oder dergleichen fixiert ist.Proposed is a projectile (10) with a cover (6) in a bore (11) in the projectile (10), wherein the projectile (10) has a groove contour (8) in the projectile body, the cover (6) is designed as a cover ring, a cover (4) of the cover in the rear part (1) fixed, and the cover ring (6) is pressed into the groove contour (8) of the projectile body, whereby an airtight cover of the bore (11) from the environment is ensured. This proposal is based on the idea not to transform the projectile body material but the cover (6) itself. For this purpose, a part of the cover (6) radially by a preferably rigid punch (5), which only needs to move axially, pressed into the circumferential groove contour (8) in the projectile body. The outer contour (7) of the punch should in this case be matched to the groove contour (8) (or vice versa) so that the material of the cover (6) radially deformed by the ram (5) in the forward movement moves into the groove contour (8) of the projectile body can be pressed in and the cover (6) after the deformation has no more degrees of freedom so that it is fixed to the tracer (2, 3) or the like.
Description
Die Erfindung beschäftig sich mit einem Geschoss mit einer Abdeckung zur Abdeckung, beispielsweise einer Leuchtspur oder dergleichen, die sich in der Regel im Heckteil eines Geschosskörpers befindet und mit der Thematik, dass die Leuchtspur oder derartige Inhalte luftdicht verschlossen sein muss, da die sonst eindringende Feuchtigkeit etc. dazu führen kann, dass beispielsweise die Leuchtspur - Pyrotechnik- nicht mehr oder nur unzureichend abbrennt. Dazu wird eine Abdeckung, bevorzugt ein Abdeckring, vorgeschlagen, die während des Umformprozesses durch eine axiale Vorschubbewegung eines (starren) Stempels, vorzugsweise aus Metall, radial in eine vorzugsweise vollständig umlaufende Nutkontur des Geschosskörpers gepresst wird. Der Stempel besitzt ein Außenmaß, das von der axialen Position des Stempels gegenüber dem der Abdeckung anhängig ist.The invention deals with a projectile with a cover to the cover, such as a tracer or the like, which is usually located in the rear part of a projectile body and with the theme that the tracer or such content must be hermetically sealed, since the otherwise penetrating moisture etc. may cause, for example, the tracer - Pyrotechnics- no longer or only insufficiently burned. For this purpose, a cover, preferably a cover ring, proposed, which is pressed during the forming process by an axial feed movement of a (rigid) punch, preferably made of metal, radially into a preferably completely circumferential groove contour of the projectile body. The punch has an outer dimension that is pending from the axial position of the punch relative to the cover.
In der Praxis ist vorgesehen, dass der luftdichte Verschluss durch eine Abdeckscheibe etc., in der Regel aus Messing, realisiert wird. Diese wird durch weitere Teile fixiert, wie beispielsweise einem Abdeckring. Dabei wird der Abdeckring beispielsweise durch Umformung des Geschosskörpermaterials gehalten. Weitere Lösungen sind in der Richtung bekannt, dass eine zusätzliche schraube oder Mutter in das Heckteil des Geschosskörpers geschraubt wird.In practice, it is provided that the airtight closure by a cover plate, etc., usually made of brass, is realized. This is fixed by other parts, such as a cover ring. In this case, the cover ring is held for example by deformation of the projectile body material. Other solutions are known in the direction that an additional screw or nut is screwed into the rear part of the projectile body.
Der Nachteil bei der Umformung liegt unter anderem darin, dass oftmals gegensätzliche Anforderungen an das Geschosskörpermaterial gestellt werden. Für die endballistische Wirksamkeit werden harte oder schwer bis nicht verformbare Materialeigenschaften vorausgesetzt, während für den Umformprozess wie Bördeln, Verstemmen etc. weiche oder duktile Materialeigenschaften die Voraussetzung sind. Daher wird der umzuformende Bereich des Geschosskörpermaterials durch Anwendung von Wärmebehandlungsverfahren in den Zustand weich bzw. duktil überführt, was jedoch sehr aufwändig und kosten- wie auch zeitintensiv ist. Die Prozessstabilität ist zudem unter großem Aufwand einzuhalten. Die Bildung von Rissen im Material, die beim Härten oder bei der Umformung entstehen können sind selbst durch die anschließende oder dem Umformungsprozess voran gegangene Wärmebehandlungsverfahren nicht auszuschließen und können als mögliche Fehlerquellen zum Versagen der Abdeckung führen. Schraube und Mutter müssen hingegen nur einer Oberflächenbehandlung unterzogen werden, beispielsweise Hartanodisieren, der Aufwand bei der Montage ist hingegen höher, da Maßnahmen zur Schraubensicherung notwendig sind. Führungsflächen zur besseren Montage nehmen einen entsprechenden Bauraum in Anspruch. Zudem ist das Gewicht einer Schraubverbindung zur Abdeckung der Leuchtspur höher als das eines Abdeckringes.The disadvantage of the deformation is, inter alia, that often conflicting requirements are made of the projectile body material. For end ballistic effectiveness, hard or hard to non-deformable material properties are presumed, while for the forming process such as crimping, caulking etc. soft or ductile material properties are the prerequisite. Therefore, the area of the projectile body material to be reshaped is made soft or ductile by applying heat treatment methods, which is however very complicated and time consuming as well as costly. The process stability is also to be kept at great expense. The formation of cracks in the material, which can occur during hardening or during the forming, are themselves heat treatment processes which have been preceded by the subsequent or the forming process can not be ruled out and can lead to failure of the cover as possible sources of error. On the other hand, the screw and nut only have to be subjected to a surface treatment, for example hard anodizing, but the outlay on assembly is higher since measures for securing the screw are necessary. Guide surfaces for better installation take up a corresponding space. In addition, the weight of a screw to cover the tracer is higher than that of a cover ring.
Hier stellt sich die Erfindung die Aufgabe, ein Geschoss aufzuzeigen, das eine bessere Abdeckung beispielsweise der Leuchtspur ermöglicht.Here, the invention has the object to show a projectile that allows better coverage, for example, the tracer.
Gelöst wird die Aufgabe durch die Merkmale des Patentanspruchs 1. Vorteilhafte Ausführungen sind in den Unteransprüchen aufgezeigt.The object is achieved by the features of
Der Erfindung liegt die Idee zugrunde, nicht das Geschosskörpermaterial sondern die Abdeckung selbst umzuformen. Dazu wird ein Teil der Abdeckung radial durch einen vorzugsweise starren Stempel, der sich ausschließlich nur axial zu bewegen braucht, und mit einer speziellen Außenkontur versehen ist, in eine umlaufende Nutkontur im Geschosskörper gepresst. Die Außenkontur sollte dabei auf die Nutkontur (oder umgekehrt) abgestimmt sein, damit das von dem in der Vorwärtsbewegung befindlichen Stempel radial umgeformte Material der Abdeckung in die Nutkontur des Geschosskörpers hineingedrückt werden kann und die Abdeckung nach der Umformung über keinerlei Freiheitsgrade mehr verfügt, sodass diese zur Leuchtspur oder dergleichen fixiert ist. Bei der Abdeckung handelt es sich bevorzugt um einen Abdeckring.The invention is based on the idea not to transform the projectile body material but the cover itself. For this purpose, a part of the cover is radially pressed by a preferably rigid punch, which only needs to move axially, and is provided with a special outer contour, pressed into a circumferential groove contour in the projectile body. The outer contour should be matched to the groove contour (or vice versa), so that the radially outwardly formed in the forward movement stamp material of the cover can be pressed into the groove contour of the projectile body and the cover has no degrees of freedom after forming more, so this is fixed to the tracer or the like. The cover is preferably a cover ring.
Da die Abdeckung von innen nach außen verformt wird, wird diese durch die beim Abschuss des Geschosses auftretenden Beschleunigungs-, Massen- und Fliehkräfte gegen den Geschosskörper gedrückt, sodass keine wegfliegenden Teile entstehen. Die Positionierung der Abdeckung mittels eines bevorzugt starren Stempels garantiert eine hohe Prozessstabilität, die eine Vorraussetzung an die Sicherheitsanforderungen ist, um zu verhindern, dass es von wegfliegenden Teilen aufgrund von Fehlern bei dem Umformprozess oder einer unzureichenden Wärmebehandlung kommt.Since the cover is deformed from the inside to the outside, this is pressed by the acceleration, mass and centrifugal forces occurring during the launch of the projectile against the projectile body, so that no flying parts arise. The positioning of the cover by means of a preferably rigid die guarantees high process stability, which is a prerequisite to the safety requirements in order to prevent it from flying off parts due to errors in the forming process or inadequate heat treatment.
Diese Idee kann zudem unabhängig von den Materialeigenschaften des Geschosskörpers angewandt werden und ermöglicht ein Höchstmaß an Flexibilität betreffend der einzusetzenden Materialien für den Geschosskörper.This idea can also be applied independently of the material properties of the projectile body and allows maximum flexibility regarding the materials to be used for the projectile body.
Der nunmehr einfachere Fertigungsprozess ist prozessstabil, Kosten und Zeit optimiert, da es zu einer Reduzierung der Anzahl der einzelnen Arbeitsschritte als auch der fertigungstechnischen Anforderung selbst kommt. Fehlermöglichkeiten, wie beispielsweise eine unzureichende Verformung der Abdeckung oder aber auch ein unrichtiger Sitz, sind auch per Sichtkontrolle leicht erfassbar.The now simpler manufacturing process is process stable, costs and time optimized, since it comes to a reduction in the number of individual steps and the manufacturing requirement itself. Possible errors, such as an insufficient deformation of the cover or even an incorrect seat, are easily detected by visual inspection.
Anhand eines Ausführungsbeispiels mit Zeichnung soll die Erfindung näher erläutert werden. Es zeigt:
- Fig. 1 -3
- Verfahrensschritte zur Abdeckung einer Leuchtspur,
- Fig. 4
- eine Schnittdarstellung des Abdeckringes aus den Figuren.
- Fig. 1-3
- Method steps for covering a tracer track,
- Fig. 4
- a sectional view of the cover ring of the figures.
Die
Nach dem konventionellen Einpressen der Leuchtspur 2, 3 werden die Abdeckscheibe 4 und der Abdeckring 6 in die dafür vorgesehene Aussparung 12 im Geschosskörper 10 eingelegt, wie in
Alternativ können die Abdeckscheibe 4 und der Abdeckring 6 auch eine einteilige konstruktive Einheit bilden.Alternatively, the cover 4 and the
Es versteht sind, dass dieses Verfahren nicht auf die Abdichtung einer Leuchtspur im Heckteil 1 eines Geschosses 10 beschränkt ist. So lassen sich mit diesem Verfahren in einfacher Art und Weise auch andere Komponenten, die sich in einer Bohrung oder einem Hohlraum in einem Geschoss, einer Munition etc. befinden, sicher abdichten. Unter Bohrung werden hierbei auch Hohlräume, Ausnehmungen, Öffnungen oder dergleichen im Geschosskörper, Munitionskörper etc. verstanden.It is understood that this method is not limited to the sealing of a luminous trace in the
Claims (12)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102011018475A DE102011018475A1 (en) | 2011-04-21 | 2011-04-21 | Apparatus and method for airtight covering a tracer or the like |
EP12161545.4A EP2515068B1 (en) | 2011-04-21 | 2012-03-27 | Device and method for air-tight covering of a tracer or the like |
Related Parent Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP12161545.4A Division-Into EP2515068B1 (en) | 2011-04-21 | 2012-03-27 | Device and method for air-tight covering of a tracer or the like |
EP12161545.4A Division EP2515068B1 (en) | 2011-04-21 | 2012-03-27 | Device and method for air-tight covering of a tracer or the like |
Publications (1)
Publication Number | Publication Date |
---|---|
EP3002543A1 true EP3002543A1 (en) | 2016-04-06 |
Family
ID=45954405
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP15194890.8A Ceased EP3002543A1 (en) | 2011-04-21 | 2012-03-27 | Projectile with a cover |
EP12161545.4A Active EP2515068B1 (en) | 2011-04-21 | 2012-03-27 | Device and method for air-tight covering of a tracer or the like |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP12161545.4A Active EP2515068B1 (en) | 2011-04-21 | 2012-03-27 | Device and method for air-tight covering of a tracer or the like |
Country Status (3)
Country | Link |
---|---|
US (1) | US9188415B2 (en) |
EP (2) | EP3002543A1 (en) |
DE (1) | DE102011018475A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2019243015A1 (en) * | 2018-06-22 | 2019-12-26 | Rheinmetall Waffe Munition Gmbh | Base bleed having sealing device |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11965721B2 (en) * | 2022-09-13 | 2024-04-23 | General Dynamics Ordnance and Tactical Systems—Canada, Inc. | Closure disk assembly for tracer projectile |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB191229393A (en) * | 1912-12-20 | 1913-05-29 | William John Mellersh-Jackson | Improvements in or relating to Projectiles. |
US4987672A (en) * | 1989-07-28 | 1991-01-29 | Fuji Valve Co., Ltd. | Method of partitioning the internal space of a hollow cylindrical member |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE361070C (en) | 1922-10-10 | Harry Crane Dodge | Fire pipes for projectiles | |
GB191420976A (en) * | 1914-10-14 | 1915-10-07 | Samuel Dewey Cushing | Improvements in or relating to Projectiles. |
DE707002C (en) | 1936-04-05 | 1941-06-11 | Westfaelisch Anhaltische Spren | Attachment of the sleeve containing the flare in a pressure-resistant socket of the tracer bullet |
US2336143A (en) * | 1941-01-04 | 1943-12-07 | Remington Arms Co Inc | Method of making projectiles |
US2394249A (en) * | 1941-12-23 | 1946-02-05 | Mcgahey Mfg Company | Cartridge |
US2402018A (en) * | 1943-03-11 | 1946-06-11 | Remington Arms Co Inc | Method of making incendiary bullets |
US3291049A (en) * | 1952-05-22 | 1966-12-13 | Aaron L Hitchens | Impact spotter bullet |
NL7701244A (en) * | 1976-03-23 | 1977-09-27 | Diehl Fa | SPLINTER SHELL FOR GRANATE COMBAT HEAD AND THE LIKE. |
NO137297C (en) * | 1976-07-01 | 1978-02-01 | Raufoss Ammunisjonsfabrikker | PROJECT. |
DE7628540U1 (en) * | 1976-09-11 | 1977-03-17 | Rheinmetall Gmbh, 4000 Duesseldorf | PRACTICE FLOOR |
CH622883A5 (en) * | 1977-07-21 | 1981-04-30 | Oerlikon Buehrle Ag | |
EP0072050B1 (en) | 1981-08-05 | 1985-10-09 | Werkzeugmaschinenfabrik Oerlikon-Bührle AG | Process to fasten a tracer case in a hole at the rear of a projectile |
FR2572512B1 (en) * | 1984-10-25 | 1987-09-25 | Luchaire Sa | DEVICE, ADAPTABLE ON MACHINERY OR AMMUNITION, SUCH AS ARTILLERY PROJECTILES, INTENDED TO REDUCE THEIR PANT TRAIL |
US4940375A (en) | 1989-05-19 | 1990-07-10 | Textron Inc. | Clinch type fastener structure and tooling |
DE4109371A1 (en) * | 1991-03-22 | 1992-09-24 | Bernd Buedenbender | CONTAINER MADE FROM METAL SHEET, IN PARTICULAR BARREL |
DE4415341A1 (en) | 1994-05-02 | 1995-11-09 | Teves Gmbh Alfred | Closing device for closing pressure-carrying channels in a housing |
DE19513992C2 (en) | 1995-04-13 | 1998-12-24 | Daimler Benz Ag | Axial fixation of a shaft-hub connection |
US6752085B2 (en) * | 2002-05-06 | 2004-06-22 | Lockheed Martin Corporation | Method and apparatus for releasably attaching a closure plate to a casing |
US6796244B2 (en) * | 2002-12-04 | 2004-09-28 | Denel (Proprietary) Limited | Opening and closing a container |
DE102004033017A1 (en) * | 2004-07-08 | 2006-02-09 | Ruag Ammotec Gmbh | Hard core shell with flare and process for its production |
DE102009027146A1 (en) | 2009-06-24 | 2010-12-30 | Robert Bosch Gmbh | Fuel high-pressure pump for fuel system of internal combustion engine, has suction side low pressure area, in which overflow valve is arranged, where overflow valve has valve housing with inlet, outlet, valve body and valve spring |
-
2011
- 2011-04-21 DE DE102011018475A patent/DE102011018475A1/en not_active Withdrawn
-
2012
- 2012-03-27 EP EP15194890.8A patent/EP3002543A1/en not_active Ceased
- 2012-03-27 EP EP12161545.4A patent/EP2515068B1/en active Active
- 2012-04-20 US US13/452,027 patent/US9188415B2/en active Active
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB191229393A (en) * | 1912-12-20 | 1913-05-29 | William John Mellersh-Jackson | Improvements in or relating to Projectiles. |
US4987672A (en) * | 1989-07-28 | 1991-01-29 | Fuji Valve Co., Ltd. | Method of partitioning the internal space of a hollow cylindrical member |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2019243015A1 (en) * | 2018-06-22 | 2019-12-26 | Rheinmetall Waffe Munition Gmbh | Base bleed having sealing device |
Also Published As
Publication number | Publication date |
---|---|
EP2515068B1 (en) | 2016-01-20 |
DE102011018475A1 (en) | 2012-10-25 |
US20120312148A1 (en) | 2012-12-13 |
EP2515068A3 (en) | 2013-03-27 |
US9188415B2 (en) | 2015-11-17 |
EP2515068A2 (en) | 2012-10-24 |
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