EP0432362A1 - Warhead - Google Patents
Warhead Download PDFInfo
- Publication number
- EP0432362A1 EP0432362A1 EP19900115263 EP90115263A EP0432362A1 EP 0432362 A1 EP0432362 A1 EP 0432362A1 EP 19900115263 EP19900115263 EP 19900115263 EP 90115263 A EP90115263 A EP 90115263A EP 0432362 A1 EP0432362 A1 EP 0432362A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- insert
- casing
- intermediate ring
- warhead
- 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.)
- Granted
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B1/00—Explosive charges characterised by form or shape but not dependent on shape of container
- F42B1/02—Shaped or hollow charges
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B1/00—Explosive charges characterised by form or shape but not dependent on shape of container
- F42B1/02—Shaped or hollow charges
- F42B1/036—Manufacturing processes therefor
Definitions
- the invention relates to a warhead as defined in the preamble of claim 1.
- indefinable chipping effects are often observed at the edge of the insert, i.e. in the area of the separating surfaces insert / cover. These effects are particularly great if the insert and cover are not made of the same material.
- the chipping effects disrupt the symmetrical formation of the rear of the projectile resulting from the detonative shaping. The projectile mass is also reduced, thus reducing the kinetic energy of the projectile.
- the invention is therefore based on the object of further developing a warhead of the type mentioned at the outset in such a way that chipping effects from the insert in the region of the insert / casing separating surfaces are avoided.
- the invention is therefore based on the fact that the chipping effects are primarily due to the different acoustic impedances of the casing and insert or intermediate ring and insert. According to the invention, the chipping effects are prevented by an intermediate ring which encompasses the insert over the entire circumference and whose sound impedance corresponds to that of the insert.
- the warhead according to the invention is designated by 10 in FIG. It has a shell 11 which surrounds the explosive 12.
- the cover 11 is provided with a cover 13 at one end and with the projectile-forming insert 14 at the opposite end.
- the reference numeral 16 denotes the transition area insert / casing, in which an intermediate ring 17 is arranged.
- FIG. 2 shows a more detailed illustration of the cutout 16.
- the intermediate ring 17 lies against the inner surface of the casing and is connected to the casing 11 by frictional connection.
- Fig. 3 shows a corresponding embodiment in which the intermediate ring 17 'rests in a recess on the front edge of the casing and is connected to the casing 11' by force and / or positive engagement.
- the particular advantage of this arrangement is that the intermediate ring is secured against axial slipping when exposed to heat (e.g. when pouring the explosive).
- Fig. 4 shows an L-shaped intermediate ring 17 ", which surrounds the front edge of the casing and partially abuts the inner casing surface.
- the intermediate ring 17 ′′ can be connected to the sheath 11 ′′ by force and / or positive locking.
- FIG. 4 An embodiment of a detachable or non-detachable connection of the intermediate ring 17 'to the sheath 11' according to FIG. 3 is shown in FIG. 4.
- a screw 18 was used as the connecting means.
- other connecting means such as pins or rivets can also be used.
- the intermediate rings 17, 17 ', 17''and the inserts 14, 14', 14 '' should have the same acoustic impedance as possible, since the higher the impedance jump, the greater the damage or the irregular spalling of the projectile tail the larger the reflection coefficient is.
- the table below shows the reflection coefficients for some metal combinations (the upper value represents the reflection coefficient for transverse waves and the lower value for longitudinal waves).
- the chipping effect on the projectile tail could be reduced to zero with the aid of the pressing in of Ta impedance matching rings.
- the thickness of the Ta impedance matching rings was varied between 1 and 3 mm.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
Description
Die Erfindung betrifft einen Gefechtskopf, wie er im Gattungsbegriff des Anspruchs 1 definiert wird.The invention relates to a warhead as defined in the preamble of claim 1.
Bei der detonativen Umformung von Einlagen beobachtet man häufig undefinierbare Abplatzeffekte am Einlagenrand, d.h. im Bereich der Trennflächen Einlage/Hülle. Diese Effekte sind besonders groß, wenn Einlage und Hülle nicht aus dem gleichen Werkstoff bestehen. Durch die Abplatzeffekte wird eine symmetrische Heckausbildung des bei der detonativen Umformung entstehenden Projektiles gestört. Außerdem wird die Projektilmasse reduziert und somit die kinetische Energie des Projektils verringert.In the detonative forming of deposits, indefinable chipping effects are often observed at the edge of the insert, i.e. in the area of the separating surfaces insert / cover. These effects are particularly great if the insert and cover are not made of the same material. The chipping effects disrupt the symmetrical formation of the rear of the projectile resulting from the detonative shaping. The projectile mass is also reduced, thus reducing the kinetic energy of the projectile.
Aus der DE 34 41 693 ist ferner ein Gefechtskopf der gattungsgemäßen Art bekannt, bei dem Zwischenringe vorgesehen sind, mit denen die Wärmeausdehnung zwischen Hülle und Spengstoff kompensiert werden soll. Maßnahmen zur Vermeidung der vorstehend erwähnten Abplatzeffekte werden in dieser Schrift nicht erwähnt.From DE 34 41 693 a warhead of the generic type is also known, in which intermediate rings are provided with which the thermal expansion between the shell and the explosive is to be compensated. Measures to avoid the above-mentioned chipping effects are not mentioned in this document.
Der Erfindung liegt daher die Aufgabe zugrunde, einen Gefechtskopf der eingangs erwähnten Art so weiterzuentwickeln, daß Abplatzeffekte von der Einlage im Bereich der Trennflächen Einlage/Hülle vermieden werden.The invention is therefore based on the object of further developing a warhead of the type mentioned at the outset in such a way that chipping effects from the insert in the region of the insert / casing separating surfaces are avoided.
Diese Aufgabe wird erfindungsgemäß durch die Merkmale des kennzeichnenden Teiles des Anspruchs 1 gelöst.This object is achieved by the features of the characterizing part of claim 1.
Die Unteransprüche geben besonders vorteilhafte Ausgestaltungen der Erfindung wieder.The subclaims represent particularly advantageous embodiments of the invention.
Die Erfindung geht also von der Tatsache aus, daß die Abplatzeffekte in erster Linie auf die unterschiedlichen akustischen Impedanzen von Hülle und Einlage bzw. Zwischenring und Einlage zurückzuführen sind. Durch einen Zwischenring, der die Einlage am gesamten Umfang umfaßt und dessen Schallimpedanz dem der Einlage entspricht, werden erfindungsgemäß die Abplatzeffekte verhindert.The invention is therefore based on the fact that the chipping effects are primarily due to the different acoustic impedances of the casing and insert or intermediate ring and insert. According to the invention, the chipping effects are prevented by an intermediate ring which encompasses the insert over the entire circumference and whose sound impedance corresponds to that of the insert.
Weitere Einzelheiten und Vorteile der Erfindung werden nachfolgend anhand von Ausführungsbeispielen, welche mit Hilfe von Figuren erläutert werden, beschrieben.Further details and advantages of the invention are described below on the basis of exemplary embodiments which are explained with the aid of figures.
Es zeigen:
- Fig. 1
- einen Längsschnitt durch einen erfindungsgemäßen Gefechtskopf mit projektilbildender Einlage;
- Fig. 2
- bis
- Fig. 4
- verschiedene Ausführungsbeispiele der Anordnung des Zwischenringes und
- Fig. 5
- ein Ausführungsbeispiel, bei dem der Zwischenring mit Hilfe einer Schraube an der Hülle befestigt ist.
- Fig. 1
- a longitudinal section through a warhead according to the invention with projectile-forming insert;
- Fig. 2
- to
- Fig. 4
- different embodiments of the arrangement of the intermediate ring and
- Fig. 5
- an embodiment in which the intermediate ring is attached to the shell by means of a screw.
In Fig. 1 ist mit 10 der erfindungsgemäße Gefechtskopf bezeichnet. Er besitzt eine Hülle 11, die den Sprengstoff 12 umgibt. An dem einen Ende ist die Hülle 11 mit einem Deckel 13 und an dem gegenüberliegenden Ende mit der projektilbildenden Einlage 14 versehen. Über eine Übertra gungs-und Verstärkerladung 15 wird in bekannter Weise der Sprengstoff 12 des Gefechtskopfes 10 gezündet. Mit dem Bezugszeichen 16 ist der Übergangsbereich Einlage/Hülle, in dem ein Zwischenring 17 angeordnet ist, gekennzeichnet.The warhead according to the invention is designated by 10 in FIG. It has a
Fig. 2 zeigt eine detailliertere Darstellung des Auschnittes 16. Dabei liegt der Zwischenring 17 an der inneren Hüllenmantelfläche an und ist durch Kraftschluß mit der Hülle 11 verbunden.FIG. 2 shows a more detailed illustration of the
Fig. 3 zeigt ein entsprechendes Ausführungsbeispiel, bei dem der Zwischenring 17' in einer Aussparung an der Hüllenvorderkante anliegt und durch Kraft und/oder Formschluß mit der Hülle 11' verbunden ist. Der besondere Vorteil dieser Anordnung besteht darin, daß der Zwischenring gegen axiales Verrutschen bei Wärmeeinwirkung (z. B. beim Gießen des Sprengstoffes) gesichert ist.Fig. 3 shows a corresponding embodiment in which the intermediate ring 17 'rests in a recess on the front edge of the casing and is connected to the casing 11' by force and / or positive engagement. The particular advantage of this arrangement is that the intermediate ring is secured against axial slipping when exposed to heat (e.g. when pouring the explosive).
Fig. 4 zeigt einen L-förmigen Zwischenring 17'', der die Hüllenvorderkante umfaßt und an der inneren Hüllenmantelfläche teilweise anliegt. Auch in diesem Fall kann der Zwischnring 17'' durch Kraft und/oder Formschluß mit der Hülle 11'' verbunden werden.Fig. 4 shows an L-shaped
Ein Ausführungsbeispiel einer lösbaren oder unlösbaren Verbindung des Zwischenringes 17' mit der Hülle 11' gemäß Fig. 3 ist in Fig. 4 dargestellt. Dabei wurde als Verbindungsmittel eine Schraube 18 verwendet. Es können aber auch andere Verbindungsmittel wie Stifte oder Nieten benutzt werden.An embodiment of a detachable or non-detachable connection of the intermediate ring 17 'to the sheath 11' according to FIG. 3 is shown in FIG. 4. A
Erfindungsgemäß sollen die Zwischenringe 17, 17', 17'' und die Einlagen 14, 14', 14'' möglichst die gleiche Schallimpedanz aufweisen, da die Schädigung bzw. das unregelmäßige Abplatzen des Projektilhecks umso größer ist, je höher der Impedanzsprung ist, d. h. je größer der Reflexionskoeffizient ist.According to the invention, the
In der unten stehenden Tabelle sind die Reflexionskoeffizienten für einige Metallkombinationen aufgeführt (der jeweils obere Wert stellt den Reflexionskoeffizient für transversale und der untere Wert für longitudinale Wellen dar).
Aus der Tabelle ist zu entnehmen, daß die Kombinationen Fe - Cu, Fe - Ni und Ta - Mo eine sehr niedrige, dagegen Al - W und Al - Mo ein extrem großes Reflexionsverhalten aufweisen.It can be seen from the table that the combinations Fe - Cu, Fe - Ni and Ta - Mo have a very low, but Al - W and Al - Mo have an extremely high reflection behavior.
Besonders vorteilhaft sind Materialkombinationen, bei denen die Dichte des Ringes ζ R größer ist als die Dichte der Einlage ζ E. Denn in diesen Fällen ergibt sich eine Leistungssteigerung aufgrund des höhren Verdämmungseffektes am Einlagenrand. Das Projektil besitzt dadurch eine höhere Abgangsgeschwindigkeit und somit eine höhere kinetische Energie.Material combinations in which the density of the ring ζ R is greater than the density of the insert ζ E are particularly advantageous. Because in these cases there is an increase in performance due to the greater insulation effect at the edge of the insert. The projectile therefore has a higher exit speed and thus a higher kinetic energy.
Bei einem praktischen Ausführungsbeispiel, bei dem eine Ta-Einlage und ein Fe-Stahlgehäuse verwendet wurde, konnte mit Hilfe der Einpressung von Ta-Impedanzanpassungsringen der Abplatzeffekt am Projektilheck auf Null reduziert werden. Die Dicke der Ta-Impedanzanpassungsringe wurde zwischen 1 bis 3 mm variiert.In a practical exemplary embodiment, in which a Ta insert and an Fe steel housing were used, the chipping effect on the projectile tail could be reduced to zero with the aid of the pressing in of Ta impedance matching rings. The thickness of the Ta impedance matching rings was varied between 1 and 3 mm.
- 10 Gefechtskopf10 warhead
- 11, 11', 11'' Hülle11, 11 ', 11' 'case
- 12 Sprengstoff12 explosives
- 13 Deckel13 lid
- 14, 14', 14'' projektilbildende Einlage14, 14 ', 14' 'projectile-forming insert
- 15 Übertragungs- und Verstärkerladung15 Transfer and amplifier charging
- 16 Ausschnitt des Übergangsbereiches Einlage/Hülle16 Section of the transition area insert / cover
- 17, 17', 17'' Zwischenring17, 17 ', 17' 'intermediate ring
- 18 Verbindungsmittel (Schraube, Stift, Niete)18 connecting means (screw, pin, rivet)
Claims (5)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3941245A DE3941245A1 (en) | 1989-12-14 | 1989-12-14 | SKULL HEAD |
DE3941245 | 1989-12-14 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0432362A1 true EP0432362A1 (en) | 1991-06-19 |
EP0432362B1 EP0432362B1 (en) | 1993-11-03 |
Family
ID=6395429
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP90115263A Expired - Lifetime EP0432362B1 (en) | 1989-12-14 | 1990-08-09 | Warhead |
Country Status (3)
Country | Link |
---|---|
US (1) | US5153373A (en) |
EP (1) | EP0432362B1 (en) |
DE (2) | DE3941245A1 (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE501121C2 (en) * | 1992-01-29 | 1994-11-21 | Bofors Ab | Ammunition |
FR2759158B1 (en) * | 1997-02-06 | 1999-02-26 | Giat Ind Sa | CORE GENERATOR LOAD COMPRISING MEANS OF LINKING THE COATING AND THE ENVELOPE |
US6453817B1 (en) * | 1999-11-18 | 2002-09-24 | Schlumberger Technology Corporation | Shaped charge capsule |
SE524299C2 (en) * | 2003-03-26 | 2004-07-20 | Saab Ab | Effect part (1) forms part of ammunition device such as shell, missile or similar and has casing provided with socket connected to casing opening |
DE102007051345A1 (en) | 2007-10-26 | 2009-04-30 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Explosive charge |
FR3068456B1 (en) | 2017-06-28 | 2019-07-19 | Nexter Munitions | SHAPED LOAD |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3301150A1 (en) * | 1982-01-15 | 1983-07-28 | Aktiebolaget Bofors, 69180 Bofors | CHARGE |
DE3301148A1 (en) * | 1982-01-15 | 1983-07-28 | Aktiebolaget Bofors, 69180 Bofors | CHARGE |
EP0105495A1 (en) * | 1982-09-30 | 1984-04-18 | Southwest Energy Group, Ltd., | Energy transfer through a multilayer liner for shaped charges |
DE3402121A1 (en) * | 1984-01-23 | 1987-07-16 | Diehl Gmbh & Co | Hollow-charge projectile |
DE3831604A1 (en) * | 1987-10-31 | 1989-05-18 | Messerschmitt Boelkow Blohm | Device for fixing the explosive body after completion of pressing of a shaped charge |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3217650A (en) * | 1952-02-28 | 1965-11-16 | Martin A Paul | Offset liner for a cavity charge projectile |
US3913488A (en) * | 1973-09-17 | 1975-10-21 | Us Army | Ballistic disc |
FR2569473B1 (en) * | 1984-08-21 | 1987-10-23 | Realisa Applic Techni Et | IMPROVEMENTS TO HOLLOW CHARGES |
DE3441693C1 (en) * | 1984-11-15 | 1986-02-06 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Device for compensating the thermal expansion of a component |
DE3506225A1 (en) * | 1985-02-22 | 1986-08-28 | Diehl GmbH & Co, 8500 Nürnberg | Warhead arrangement |
US4862804A (en) * | 1985-05-22 | 1989-09-05 | Western Atlas International, Inc. | Implosion shaped charge perforator |
DE3901474A1 (en) * | 1989-01-19 | 1990-07-26 | Rheinmetall Gmbh | DEVICE FOR FASTENING THE INSERT OF HOLLOW LOADS OR PROJECT-FORMING LOADS |
-
1989
- 1989-12-14 DE DE3941245A patent/DE3941245A1/en not_active Withdrawn
-
1990
- 1990-08-09 EP EP90115263A patent/EP0432362B1/en not_active Expired - Lifetime
- 1990-08-09 DE DE90115263T patent/DE59003348D1/en not_active Expired - Fee Related
- 1990-12-14 US US07/626,722 patent/US5153373A/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3301150A1 (en) * | 1982-01-15 | 1983-07-28 | Aktiebolaget Bofors, 69180 Bofors | CHARGE |
DE3301148A1 (en) * | 1982-01-15 | 1983-07-28 | Aktiebolaget Bofors, 69180 Bofors | CHARGE |
EP0105495A1 (en) * | 1982-09-30 | 1984-04-18 | Southwest Energy Group, Ltd., | Energy transfer through a multilayer liner for shaped charges |
DE3402121A1 (en) * | 1984-01-23 | 1987-07-16 | Diehl Gmbh & Co | Hollow-charge projectile |
DE3831604A1 (en) * | 1987-10-31 | 1989-05-18 | Messerschmitt Boelkow Blohm | Device for fixing the explosive body after completion of pressing of a shaped charge |
Also Published As
Publication number | Publication date |
---|---|
DE59003348D1 (en) | 1993-12-09 |
US5153373A (en) | 1992-10-06 |
EP0432362B1 (en) | 1993-11-03 |
DE3941245A1 (en) | 1991-06-20 |
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