EP0764826B1 - Trägergeschoss, das ein einziges Penetratorgeschoss trägt - Google Patents
Trägergeschoss, das ein einziges Penetratorgeschoss trägt Download PDFInfo
- Publication number
- EP0764826B1 EP0764826B1 EP96114077A EP96114077A EP0764826B1 EP 0764826 B1 EP0764826 B1 EP 0764826B1 EP 96114077 A EP96114077 A EP 96114077A EP 96114077 A EP96114077 A EP 96114077A EP 0764826 B1 EP0764826 B1 EP 0764826B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- penetrator
- missile
- base
- ballistic
- projectile
- 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
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
- F42B12/56—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 for dispensing discrete solid bodies
- F42B12/58—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
- F42B12/62—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile
- F42B12/625—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile a single submissile arranged in a carrier missile for being launched or accelerated coaxially; Coaxial tandem arrangement of missiles which are active in the target one after the other
Definitions
- the invention relates to a ballistic projectile according to the preamble of the claim 1.
- FR-A-2 472 168 shows a ballistic projectile according to the preamble of claim 1.
- a penetrator guided in the ballistic projectile is in a floor guide as a so-called full floor - i.e. without guide rings - guided.
- a floating floor is firmly connected to the penetrator and has one Penetrator corresponding diameter.
- the propellant charge only fills a part the space between the floating floor and one connected to the floor Closure off.
- the effect of the penetrator is in the target, especially with concrete due to the relatively thin head and the relatively large diameter of the penetrator is not sufficient.
- GB-A-2 110 799 discloses a wing stabilized projectile with one in the Projectile casing through a front guide ring and at the rear through a caliber of the same size Guided section guided penetrator.
- the front guide ring breaks out of the shell on one front At the end of the floor arranged mouthpiece, this mouthpiece on the rear guide section of the penetrator.
- the effect of the penetrator is diminished by three factors, namely the one that breaks at the mouthpiece, front guide ring, which increases the friction on the penetrator, through the aerodynamic unfavorable, rear, caliber guide section with the thorned mouthpiece and by throttling the gas cross section between Propellant charge and the penetrator through the slotted throttle disc.
- EP-A-0 293 295 shows a projectile with the same caliber in the projectile casing guided penetrator.
- the essential compared to the penetrator diameter larger propellant space is throttled at its gas outlet cross section and corresponds approximately to the diameter of the penetrator. There is no floating floor therefore, so that the problem of the invention does not arise.
- the invention has for its object a floor of the aforementioned Way to create that in concrete u. ⁇ . a significantly improved penetration performance has, so that it to combat bunkers, shelters or the like suitable is.
- the advantages achieved with the projectile according to the invention are that it has a comparatively good penetration performance in concrete or the like, so that bunkers, shelters or the like can be optimally combated. Furthermore the projectile according to the invention has improved functional reliability, i.e. a reduced risk of bouncing through an optimized penetrator contour as well a reliable igniter function.
- the outer contour and the mass of the projectile according to the invention correspond preferably the corresponding values of common floors, i.e. the invention Projectile can be ballistic of the imported ammunition in an advantageous manner be equivalent so that the bullet boards of the imported ammunition are taken over can be. However, this means that the shooting boards are not only costly Experiments must be determined. Also the spreading behavior or the Accuracy of the projectile according to the invention can be the accuracy of the imported ammunition.
- the drawing shows an illustration of the projectile 10, which is in a shell 12 corresponding caliber has a penetrator 14.
- the shell 12 consists of a sleeve body 16 which is integrally formed with a floor 18 and from a tip section 20 of the projectile 10 Ballistic projectile hood 22.
- Ballistic projectile hood 22 On the ballistic projectile hood 22 is on the front a proximity fuse 24 is arranged.
- the proximity fuse 24 is with an electrical output 26, one of which is indicated by a dash-dotted line Line arranged connecting line 28 is connected.
- the penetrator 14 has a solid ballistic head 20 with a flattened one end face 13 with a sharp edge and one on the ballistic head 30 to the rear adjoining room 32 in which there is an explosive charge 34 located.
- the penetrator 14 has a ground impact detonator for igniting the explosive charge 34 36.
- the bottom impact igniter 36 can be equipped with a pyrotechnic or be provided with an electrical delay. It can be a variable Have a time function, i.e. the time function can be preset to a certain value or adjustable by means of a suitable acceleration sensor device be.
- the length 31 of the head 30 corresponds to 2.3 times the diameter 15 of the penetrator 14. This length 31 in conjunction with the total mass of the penetrator 14 ensures the required penetration performance in concrete.
- the penetrator 14 designed in this way is in the shell 12 by means of a moving floor 38 with a sealing ring 39 and by means of a guide ring 40 fixed exactly in the middle.
- the guide ring 40 lies with a circumferential collar 42 trained counter-stop on a trained in the floor cap 22 revolving stop 44.
- the guide ring 40 is consequently in the shell 23 fixed axially immovable.
- the projectile hood 22 is screwed to the projectile casing 12 at 43.
- the floating floor 38 is formed with a circumferential collar 46 which is used to fix the rear end portion 48 of the penetrator 14 is used.
- the drift floor 38 is in the projectile casing 12 is arranged to be axially movable.
- the space between the floating floor 38 and the floor 18 of the sleeve body 16 of the shell 12 is provided for a propellant charge 50.
- the propellant charge 50 is by means of a Propellant igniter 52 ignited, which contacts the connecting line 28 is.
- the projectile 10 thus consists of the projectile shell 12 with a ballistic one Projectile hood 22, as well as the one that is protected in the projectile casing 12, sub-caliber penetrator 14, the one with the explosive charge 34 and the ground impact detonator 36 is provided.
- the penetrator 14 is by means of the floating floor 38 and fixed by means of the guide ring 40 inside the shell 12.
- the Penetrator propellant charge 50 is used to eject the penetrator 14 from the projectile shell 12.
- the penetrator propellant 50 is by means of the propellant lighter 52 ignited, via the connecting line 28 with the proximity fuse 24th connected is.
- the proximity fuse 24 thus serves to initiate the propellant charge fuse 52.
- the shell 12, the penetrator 14 and the moving floor 38 are expediently because of the high loads occurring when shooting or when Ejection of the penetrator 14 from the shell 12 of high-strength steel, as he for example, also for highly stressed components in other ammunition Application arrives.
- the ballistic projectile hood 22 or its front section and the proximity fuse 24 can be penetrated by the penetrator 14, but it is also possible, the said front part of the ballistic projectile hood 22 and to detonate the proximity fuse 24 parallel to the ignition of the propellant charge 50.
- a space 53 for a penetrator propellant charge 50 has a diameter 54, which corresponds to 1.5 times the diameter 15 of the penetrator 14.
- the drive floor 38 is concave in the direction of the penetrator charge 50 and acts with its arched flange 56 on the floor side on the one hand as Cover for the room 53, on the other hand as a traction sheave for the penetrator 14.
- the concave shape of the floating floor 38 also results in a gain in space for the Room 53 and has a favorable tension distribution when supporting the entire floor 10 when shooting and when ejecting the penetrator 14 from the Missile shell 12 on.
- the penetrator 14 is a sub-caliber balancing bullet with high initial speed, more straightforward Trajectory and high penetration.
- the concave flange 56 increases the guide length of the penetrator 14 in the Projectile casing 12 so that the penetrator 14 leaves the projectile casing 12 coaxially, thus has no or only a small exit angle.
- the sharp-edged end face 13 of the head 30 ensures that the penetrator 14 penetrates the concrete even when it hits concrete at an angle of ⁇ 90 °.
- the proximity fuse 24 is a target made of concrete and fires at a suitable distance from the target the propellant lighter 52.
- the gases of the penetrator propellant 50 drive the propellant 38 with the penetrator 14, the penetrator 14 through the collar 46 and the guide ring 40 is guided radially.
- the penetrator 14 penetrates the proximity fuse 24 and the projectile hood 22. Then the moving floor 38 strikes the guide ring 40 and the penetrator 14 leaves the moving floor 38 and the guide ring 40.
- the ground impact detonator 36 When the target hits the time-delayed detonator function of the ground impact detonator 36 started. Penetrated by the great energy of the penetrator 14 this the goal. After the penetration process, the ground impact igniter ignites 36 the explosive charge 34, causing the head 30 and sleeve 62 of the penetrator 14 is broken down into fragments.
- the ballistic projectile 10 according to the invention is reliable in its function. It has only one component that acts on the target, namely the penetrator 14 on The penetrator propellant charge 50 is large in volume and becomes functionally reliable ignited by the proximity fuse 24.
- the penetrator 14 mainly has due to the massive head 30 that required for the target punch Dimensions.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Description
Claims (5)
- Ballistisches Geschoß (10) miteinem in der Geschoßhülle (12) koaxial geführten, unterkalibrigen Penetrator (14), der zusätzlich eine Sprengladung (34) trägt,einem Annäherungszünder (24), der eine im Geschoßboden (18) angeordnete Penetrator-Treibladung (50) elektrisch zündet, die den Penetrator (14) über einen Treibboden (38) beschleunigt, und wobei der Penetrator einen Aufschlagzünder (36) aufweist,daß der Annäherungszünder (24) an der Geschoßspitze angeordnet ist;daß der Penetrator (14) einen massiven, ballistischen Kopf (30) mit einer Länge (31) aufweist, wobei die Länge (31) dem 2 bis 5-fachen Durchmesser (15) des Penetrators entspricht,ein Raum (53) für die Penetrator-Treibladung (50) einen Durchmesser (54) aufweist, der dem 1,2 bis 2,5-fachen Durchmesser des Penetrators (14) entspricht,daß die Penetrator-Treibladung das Geschoßbodenvolume ausfüllt;der Treibboden (38) einen über den Durchmesser (15) des Penetrators (14) hinausragenden Flansch (56) besitzt,der Penetrator (14) in der Geschoßhülle (12) mittels des, in der Geschoßhülle (12) axial beweglich geführten, mit dem Penetrator (14) lösbar verbundenen Treibbodens (38) und mittels eines davon beabstandeten Führungsringes (40) angeordnet ist, undder Führungsring (40) an einem in der Geschoßhülle (12) ausgebildeten Anschlag (44) axial unbeweglich anliegt.
- Ballistisches Geschoß nach Anspruch 1,
dadurch gekennzeichnet,daß der Treibboden (38) tellerförmig ausgebildet und sein Flansch (56) geschoßbodenseitig gewölbt ist, undder Treibboden (38) den Raum (53) für die Treibladung (50) deckelförmig abschließt. - Ballistisches Geschoß nach Anspruch 1,
dadurch gekennzeichnet,
daß der Bodenaufschlagzünder (36) eine pyrotechnische Verzögerung aufweist. - Ballistisches Geschoß nach Anspruch 1,
dadurch gekennzeichnet,
daß der Bodenaufschlagzünder (36) eine elektrische Verzögerung aufweist. - Ballistisches Geschoß nach Anspruch 1,
dadurch gekennzeichnet,
daß der Bodenaufschlagzünder (36) eine variable Zeitfunktion aufweist oder die Zeitfunktion voreinstellbar oder die Zeitfunktion mittels einer Beschleunigungssensoreinrichtung einstellbar ist.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19535218 | 1995-09-22 | ||
DE19535218A DE19535218C1 (de) | 1995-09-22 | 1995-09-22 | Ballistisches Geschoß |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0764826A1 EP0764826A1 (de) | 1997-03-26 |
EP0764826B1 true EP0764826B1 (de) | 1999-03-10 |
Family
ID=7772861
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP96114077A Expired - Lifetime EP0764826B1 (de) | 1995-09-22 | 1996-09-03 | Trägergeschoss, das ein einziges Penetratorgeschoss trägt |
Country Status (3)
Country | Link |
---|---|
US (1) | US5656792A (de) |
EP (1) | EP0764826B1 (de) |
DE (2) | DE19535218C1 (de) |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE29710228U1 (de) * | 1997-06-13 | 1998-10-15 | Diehl Stiftung & Co., 90478 Nürnberg | Geschoß für Rohrwaffen |
AU763036B2 (en) * | 1997-12-11 | 2003-07-10 | Lockheed Martin Corporation | Shrouded aerial bomb |
KR100549487B1 (ko) * | 1997-12-11 | 2006-02-08 | 록히드 마틴 코포레이션 | 장갑형 투하 폭탄 |
US6389977B1 (en) | 1997-12-11 | 2002-05-21 | Lockheed Martin Corporation | Shrouded aerial bomb |
US6408762B1 (en) | 1997-12-11 | 2002-06-25 | Lockheed Martin Corporation | Clamp assembly for shrouded aerial bomb |
AU755006B2 (en) * | 1997-12-11 | 2002-11-28 | Lockheed Martin Corporation | Shrouded aerial bomb |
PT1367358E (pt) * | 1997-12-11 | 2008-10-08 | Lockheed Corp | Bomba aérea blindada |
US6135028A (en) * | 1998-10-14 | 2000-10-24 | The United States Of America As Represented By The Secretary Of The Navy | Penetrating dual-mode warhead |
DE19852626A1 (de) * | 1998-11-14 | 2000-05-18 | Diehl Stiftung & Co | Artilleriegeschoß |
NO995142A (no) * | 1999-06-04 | 2000-10-16 | Nammo Raufoss As | Fremdriftsanordning for et prosjektil i et missil |
US6374744B1 (en) * | 2000-05-25 | 2002-04-23 | Lockheed Martin Corporation | Shrouded bomb |
DE10039304A1 (de) * | 2000-08-11 | 2002-02-21 | Diehl Munitionssysteme Gmbh | Gefechtskopf für ein KE-Geschoß |
US7930624B2 (en) * | 2001-04-20 | 2011-04-19 | Avid Technology, Inc. | Editing time-based media with enhanced content |
US6598535B1 (en) * | 2001-12-31 | 2003-07-29 | The United States Of America As Represented By The Secretary Of The Army | Collapsible support frame for kinetic energy penetrator |
AU2003212584A1 (en) * | 2003-03-25 | 2004-10-18 | Ruag Munition | Projectile comprising a sub-caliber penetrator core |
FR2862378B1 (fr) * | 2003-11-17 | 2007-11-23 | Giat Ind Sa | Obus explosif ayant une tenue aux chocs amelioree |
FR2871226B1 (fr) * | 2004-06-08 | 2006-08-18 | Tda Armements Sas Soc Par Acti | Projectile, notamment bombe de penetration anti- infrastructure et procede de penetration d'un tel projectile a travers une paroi |
US7380503B2 (en) * | 2004-12-20 | 2008-06-03 | Newtec Services Group | Method and apparatus for self-destruct frangible projectiles |
US7770521B2 (en) * | 2005-06-03 | 2010-08-10 | Newtec Services Group, Inc. | Method and apparatus for a projectile incorporating a metastable interstitial composite material |
DE102008023678B4 (de) * | 2008-05-15 | 2012-11-29 | Diehl Bgt Defence Gmbh & Co. Kg | Fliegerbombe |
EP2496908B1 (de) | 2009-11-04 | 2013-09-11 | Diehl BGT Defence GmbH & Co.KG | Fliegerbombe |
IL221460A (en) * | 2012-08-14 | 2016-11-30 | Rafael Advanced Defense Systems Ltd | Bullet acceleration |
KR101891016B1 (ko) | 2014-02-11 | 2018-08-22 | 레이던 컴퍼니 | 외부 에어프레임을 갖는 군수품 |
DE102017106526A1 (de) | 2017-03-27 | 2018-10-11 | Rheinmetall Waffe Munition Gmbh | Geschoss, insbesondere im Mittelkaliberbereich |
CN110906806A (zh) * | 2019-11-17 | 2020-03-24 | 长沙深蓝未来智能技术有限公司 | 外弹道末段底爆增速侵彻穿甲弹 |
CN111595209B (zh) * | 2020-05-25 | 2022-06-28 | 宁波曙翔新材料股份有限公司 | 一种穿甲杆 |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR477375A (de) * | 1900-01-01 | |||
US555774A (en) * | 1896-03-03 | Elias m | ||
GB191510470A (en) * | 1915-07-19 | 1915-10-14 | Joseph Mccann | Improvements in Explosive Shells for Artillery. |
US2091635A (en) * | 1934-09-24 | 1937-08-31 | Kenneth L Hayden | Projectile |
FR865939A (fr) * | 1940-02-16 | 1941-06-09 | Projectile à grande puissance de pénétration | |
US4063512A (en) * | 1966-10-05 | 1977-12-20 | The United States Of America As Represented By The Secretary Of The Air Force | Armor penetrating projectile |
US3842741A (en) * | 1973-06-07 | 1974-10-22 | Us Army | Subprojectile launched from telescopic tubes |
GB1605340A (en) * | 1976-01-21 | 1992-01-02 | Messerschmitt Boelkow Blohm | Bombs and projectiles |
US4036141A (en) * | 1976-08-02 | 1977-07-19 | Korr Abraham L | Ammunition |
DE2948542A1 (de) * | 1979-12-03 | 1984-04-12 | Rheinmetall GmbH, 4000 Düsseldorf | Geschoss zum bekaempfen mehrlagiger, vorzugsweise aktiver panzerungen |
FR2472168A1 (fr) * | 1979-12-19 | 1981-06-26 | Serat | Corps d'engin lanceur de sous-projectiles |
US4580498A (en) * | 1982-07-27 | 1986-04-08 | Motorola, Inc. | Fuze actuating system having a variable impact delay |
DE3544528C1 (en) * | 1985-12-17 | 1987-04-09 | Messerschmitt Boelkow Blohm | Tandem charge system having integrated protection elements |
USH1235H (en) * | 1986-06-18 | 1993-10-05 | The United States Of America As Represented By The Secretary Of The Navy | Armor-piercing projectile |
US4803928A (en) * | 1986-08-02 | 1989-02-14 | Stefan Kramer | Tandem charge projectile |
FR2615937B1 (fr) * | 1987-05-27 | 1989-09-08 | Ladriere Serge | Perfectionnements apportes aux projectiles perforants |
DE3824524A1 (de) * | 1988-07-20 | 1990-02-08 | Wegmann & Co | Panzerbrechendes geschoss |
DE4225704A1 (de) * | 1992-08-04 | 1994-02-10 | Diehl Gmbh & Co | Gefechtskopf mit einer Tandemladung |
-
1995
- 1995-09-22 DE DE19535218A patent/DE19535218C1/de not_active Expired - Fee Related
-
1996
- 1996-09-03 EP EP96114077A patent/EP0764826B1/de not_active Expired - Lifetime
- 1996-09-03 DE DE59601410T patent/DE59601410D1/de not_active Expired - Fee Related
- 1996-09-16 US US08/714,239 patent/US5656792A/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
DE59601410D1 (de) | 1999-04-15 |
EP0764826A1 (de) | 1997-03-26 |
US5656792A (en) | 1997-08-12 |
DE19535218C1 (de) | 1997-02-27 |
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