EP0432362A1 - Warhead - Google Patents

Warhead Download PDF

Info

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
Application number
EP19900115263
Other languages
German (de)
French (fr)
Other versions
EP0432362B1 (en
Inventor
Hendrik Robert Lips
Dr. JÀ¼rgen Böcker
Peter Tripptap
Dr. Klaus Weimann
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rheinmetall Industrie AG
Original Assignee
Rheinmetall GmbH
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Rheinmetall GmbH filed Critical Rheinmetall GmbH
Publication of EP0432362A1 publication Critical patent/EP0432362A1/en
Application granted granted Critical
Publication of EP0432362B1 publication Critical patent/EP0432362B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B1/00Explosive charges characterised by form or shape but not dependent on shape of container
    • F42B1/02Shaped or hollow charges
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B1/00Explosive charges characterised by form or shape but not dependent on shape of container
    • F42B1/02Shaped or hollow charges
    • F42B1/036Manufacturing 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.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

The invention relates to a warhead (10) having a casing (11,11',11") surrounding the explosive (12) and a projectile-forming insert (14,14',14"), the insert being arranged circumferentially on an intermediate ring (17,17',17") which is itself fastened to the casing (11,11',11"). …<??>In order, in the region of the insert/casing parting planes, to prevent the occurrence of indeterminate chipping effects which can cause an asymmetric formation of the rear of the projectile obtained as a result of the detonation deformation, it is proposed that the intermediate ring (17,17',17") and the insert (14,14',14") should have the same acoustic impedance. …<IMAGE>…

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.
Show it:
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 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. About a transfer supply and booster charge 15, the explosive 12 of the warhead 10 is detonated in a known manner. The reference numeral 16 denotes the transition area insert / casing, in which an intermediate ring 17 is arranged.

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 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 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 intermediate ring 17 ", which surrounds the front edge of the casing and partially abuts the inner casing surface. In this case too, the intermediate ring 17 ″ can be connected to the sheath 11 ″ by force and / or positive locking.

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 screw 18 was used as the connecting means. However, other connecting means such as pins or rivets can also be used.

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 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.

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).

Figure imgb0001
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).
Figure imgb0001

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.

BezugszeichenlisteReference symbol list

  • 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)

Gefechtskopf (10) mit einer den Sprengstoff (12) umgebenden Hülle (11, 11', 11'') und einer projektilbildenden Einlage (14, 14', 14''), wobei die Einlage (14, 14', 14'') umfangsseitig an einem Zwischenring (17, 17', 17'') angeordnet ist, welcher seinerseits an der Hülle (11, 11', 11'') befestigt wird, dadurch gekennzeichnet, daß der Zwischenring (17, 17', 17'') und die Einlage (14, 14', 14'') die gleiche Schallimpedanz aufweisen.Warhead (10) with a shell (11, 11 ', 11'') surrounding the explosive (12) and a projectile-forming insert (14, 14', 14 ''), the insert (14, 14 ', 14'') ) is arranged circumferentially on an intermediate ring (17, 17 ', 17''), which in turn is fastened to the casing (11, 11', 11 ''), characterized in that the intermediate ring (17, 17 ', 17'') and the insert (14, 14', 14 '') have the same sound impedance. Gefechtskopf nach Anspruch 1, dadurch gekennzeichnet, daß die Dichte ζ R des Zwischenringes (17, 17', 17'') größer ist als die DichteζE der Einlage (14, 14', 14'').Warhead according to claim 1, characterized in that the density ζ R of the intermediate ring (17, 17 ', 17'') is greater than the density ζ E of the insert (14, 14', 14 ''). Gefechtskopf nach Anspruch 1 oder 2, dadurch gekennzeichnet, daß der Zwischenring (17) an der inneren Hüllenmantelfläche anliegend durch Kraftschluß mit der Hülle (11) verbunden ist.Warhead according to claim 1 or 2, characterized in that the intermediate ring (17) is connected to the casing (11) by frictional engagement against the inner casing surface. Gefechtskopf nach Anspruch 1 oder 2, dadurch gekennzeichnet, daß der Zwischenring (17) in einer Aussparung an der Hüllenvorderkante innen anliegend durch Kraft und/oder Formschluß mit der Hülle (11') verbunden und gegen axiales Verrutschen bei Wärmeeinwirkung gesichert ist.Warhead according to claim 1 or 2, characterized in that the intermediate ring (17) in a recess on the front edge of the casing is connected to the casing (11 ') by force and / or positive locking and is secured against axial slipping under the influence of heat. Gefechtskopf nach Anspruch 1 oder 2, dadurch gekennzeichnet, daß der Zwischenring (17'') L-förmig die Hüllenvorderseite umfassend und an der inneren Hüllenmantelfläche teilweise anliegend durch Kraft und/oder Formschluß mit der Hülle (11'') verbunden ist.Warhead according to claim 1 or 2, characterized in that the intermediate ring (17 '') is connected in an L-shape to the front of the casing and is partially connected to the casing (11 '') by force and / or positive engagement.
EP90115263A 1989-12-14 1990-08-09 Warhead Expired - Lifetime EP0432362B1 (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (5)

* Cited by examiner, † Cited by third party
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

Similar Documents

Publication Publication Date Title
DE69005988T2 (en) Shielding seal for electromagnetic waves.
DE69403385T2 (en) Viscosity damper and isolator, with three parameters
WO1990002918A1 (en) Warhead
EP1569735B1 (en) Separator for purifying a fluid flow
EP0432362B1 (en) Warhead
DE2842581A1 (en) FASTENING DEVICE FOR COUPLING TWO CYLINDER-SHAPED PARTS
DE2911723A1 (en) DISC SPRING FOR AGGREGATE, AS FRICTION COUPLINGS, AND AGGREGATE EQUIPMENT WITH SUCH DISC SPRINGS
EP0219639B1 (en) Shielded casing for high frequencies
DE19758460A1 (en) Charge for forming projectile has plate which deforms less towards center than deformation of cover
EP0378749A1 (en) Apparatus for fastening the liner of a hollow charge or a charge making a projectile
DE102013004851A1 (en) Rotor for an electric motor comprising a rotating shaft and a yoke securely fitted on the rotating shaft
DE3639392A1 (en) CERAMIC ELECTRONIC COMPONENTS
DE102020104103A1 (en) ENGINE
EP1674817A1 (en) Cartridge
DE3900269C2 (en) Warhead
EP0485897B1 (en) Projectile with trajectory correction
DE2036065A1 (en) Mechanical connection
DE19730968B4 (en) Method for producing a projectile and projectile
EP0290654B1 (en) Expansion dowel for the form-locking anchorage in a borehole
DE2710169C2 (en) Broadband coaxial microwave attenuator
DE3510431C2 (en)
DE1638180A1 (en) Electrically operated twist drive
EP0027650A1 (en) Method of making stacked electrical capacitors
DE3523569C2 (en)
DE1614754B2 (en) PROTECTIVE TUBE ANCHOR CONTACT

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: A1

Designated state(s): DE FR GB IT

17P Request for examination filed

Effective date: 19910427

RAP3 Party data changed (applicant data changed or rights of an application transferred)

Owner name: RHEINMETALL GMBH

17Q First examination report despatched

Effective date: 19930304

ITF It: translation for a ep patent filed

Owner name: CALVANI SALVI E VERONELLI S.R.L.

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE FR GB IT

GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)

Effective date: 19931109

REF Corresponds to:

Ref document number: 59003348

Country of ref document: DE

Date of ref document: 19931209

ET Fr: translation filed
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
REG Reference to a national code

Ref country code: GB

Ref legal event code: IF02

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20050801

Year of fee payment: 16

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 NON-PAYMENT OF DUE FEES

Effective date: 20050809

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20050812

Year of fee payment: 16

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20060816

Year of fee payment: 17

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20060809

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20070430

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20060809

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: 20060831

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20080301