GB2236582A - A device for stabilising the projectile of a hollow charge - Google Patents

A device for stabilising the projectile of a hollow charge Download PDF

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Publication number
GB2236582A
GB2236582A GB9019320A GB9019320A GB2236582A GB 2236582 A GB2236582 A GB 2236582A GB 9019320 A GB9019320 A GB 9019320A GB 9019320 A GB9019320 A GB 9019320A GB 2236582 A GB2236582 A GB 2236582A
Authority
GB
United Kingdom
Prior art keywords
insert
ring
projectile
bearing ring
casing
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
GB9019320A
Other versions
GB9019320D0 (en
GB2236582B (en
Inventor
Karl Rudolf
Gunther Hofmann
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.)
Diehl Verwaltungs Stiftung
Original Assignee
Diehl GmbH and Co
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 Diehl GmbH and Co filed Critical Diehl GmbH and Co
Publication of GB9019320D0 publication Critical patent/GB9019320D0/en
Publication of GB2236582A publication Critical patent/GB2236582A/en
Application granted granted Critical
Publication of GB2236582B publication Critical patent/GB2236582B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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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

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Earth Drilling (AREA)
  • Portable Nailing Machines And Staplers (AREA)

Abstract

Upon transformation of an insert 2 of a hollow charge 10 into a projectile, an additional tamping with regard to the casing 11 is achieved by a bearing ring 3 made of heavy metal. The consequences are a symmetrically formed projectile and an error-free departure flight of the projectile. <IMAGE>

Description

A DEVICE FOR STABILISING THE PROJECTILE OF A HOLLOW CHARGE This invention
relates to a device for stabilising the projectile of a hollow charge which has a projectileforming insert.
A device for compensating for the different thermal expansion of the explosive and of the casing of a hollow charge is shown in DE 34 41 693. This device consists of at least rings. The rings have conical contact surfaces, and one ring consists of a material which has a lower coefficient of thermal expansion than the material of the other ring. A funnel-shaped insert of the hollow charge is supported against one surface of one ring, and said surface of the ring lies at a right angle to the axis of the hollow charge. This ring consists of a special steel having a low coefficient of thermal expansion.
In the case of a hollow charge for the production of a projectile, it is important that the projectile is formed coaxially-to the axis of the charge. In the event of small deviations from the axis of the charge, an unsymmetrical projectile having a somewhat unstable flight path and deviating from the axis of the hollow charge is formed. An improvement in the aforesaid parameters may be effected upon appropriately large tamping of the casing of the hollow charge.
2 In DE 34 41 693 Cl, the Insert Is Indeed supported in the axial direction against a steel ring, but there is a lack of a suitable tamping at a right angle to the axis of the hollow charge. Upon transformation of the insert 6 into a hollow-charge jet, the forces exerted by the insert on the casing - namely at a right angle to the hollow charge - are low, since the angle of the insert with regard to the wall of the hollow charge amounts to about 45. Therefore, no pointer with regard to the set or problems realised in accordance with the present invention emerges from the said document.
An aim of the present invention is to provide a device which makes possible a projectile formation which is coaxial with the axis of the hollow charge.
According to the present invention there is provided a device for stabilising the projectile of a hollow charge, said hollow charge having a casing containing explosive, a proj ectile- forming insert and rings having conical contact surfaces, which rings support and secure the insert in the casing, characterised in that one of said rings is a bearing ring consisting of heavy metal guided axially in a recess of the casing, the bearing 25- ring having a conical guide surface butting directly against a conical surface of the insert fastened by wedge effect, and another one of said rings being a supporting ring which supports (in the axial direction of the hollow 3 charge) the insert at the explosive side relative to a shoulder of the recess on the casing side (in said axial direction), and a further fixing ring fastenable in the recess fastens the insert, the supporting ring and the 5 bearing ring.
Upon transformation of the insert into the projectile, an additional tamping with regard to the casing wall is achieved by the heavy-metal ring. In this respect, the transformation and folding or forming of the insert is influenced advantageously. An additional stabilisation of the projectile is effected.
Different strength portions of the casing in the region supporting the insert are eliminated or largely. avoided by the present invent-on. The projectile is formed in the longitudinal axis of the hollow charge. Thus, at least the f irst portion of the f light of the projectile is coaxial with the axis of the charge. Also the formation of the projectile is symmetrical to the said charge axis, since all the mass particles of the insert contribute---to the formation of the projectile. An eccentric centre of mass (that is to be avoided) of the projectile is therefore avoided.
25- A further advantage is that, upon securing the insert in the casing, the insert is urged or pressed under pressure against the explosive, i.e. the insert 4 exerts a pressure on the explosive. This pressure is selected to be so high that, on the one hand, no gap (gap freedom) exists between the explosive and the insert and, on the other hand, the bias force is so great that in the predetermined temperature range of -400C up to +760C no gap (gap freedom) exists between the explosive and the insert. A reduction in performance of the hollow charge by reason of an existing gap is, therefore, likewise avoided.
Advantageous further developments of the present invention will be apparent from the sub-claims.
In accordance with the arrangement provided for in

Claims (10)

Claim 2, tolerances of the bearing ring with respect to its dimensions in the direction of the main axis of the hollow charge are compensated for by way of the plastics ring. In accordance with the arrangement provided for in Claim 3, there is a durable fastening of the bearing ring in the recess of--- the easing. The type of fastening is cost-favourable and does not lead to any further weakening of the casing, as would be the -case with a 2T threaded connection. An exemplified embodiment of the present invention is shown with reference to a single Figure of the drawing. Referring to the drawing, a hollow charge 10 consists of a casing 11 made of steel with explosive 12 and of a proj ectile- forming insert 2 made of iron or tantalum. The casing 11 has a recess 6 with an a shoulder 61. The following rings are arranged in the recess 6. A supporting- ring 1 made of plastics material, a bearing ring 3 made of a heavy or hard material or metal (Schwermetall) or metal carbide or the like, namely tungsten carbide or titanium/iron composition, a plastics ring 4 and a fixing ring 5 made of a high-strength steel. The fixing ring 5 is, by reason of a press or force fit with respect to the recess 6, pressed into this and by way of the plastics ring 4 presses (urges) the bearing ring 3 against the supporting ring 1. The supporting ring 1 butts against the shoulder 61 of the recess 6. By reason of its elastic deformability - dictated by the compressive forcds exerted on it by the bearing ring 3 by way of the insert 2 - the supporting ring 1 butts annularly with the surface 17 against the insert 2. The 25" insert 2 is, therefore, uniformly supported relative to the casing 11. Conical surf aces 15, 16 on the insert 2 and on the bearing ring 3 centre the insert with respect to a hollow-charge axis 13. An angular spacing 31 exists 6 between the supporting ring 1 and the bearing ring 3. The insert 2 is therefore fastened or secured by being wedged in the casing 11. An angle of 1250 exists between a tangent 21 of the insert 2 and of the surface 16. The 5 plastics ring 4 ensures temperature compensation. Upon detonation of the explosive 12, the detonationwaves produced by the explosive form (from the insert 2) a projectile, not shown, lying in the hollow-charge axis 13. During the transformation of the insert 2 into the projectile, compressive and tensile stresses are superimposed (on one another) in the insert 2, in which respect the compressive stresses are reflected by the heavy-metal ring 3 until it fractures. By reason of its comparatively large mass with small dimensions, the bearing ring 3 has a good reflection behaviour for the compressive stresses and ensures, compared with the prior art, a comparatively long intact existence of a casing portion 14 during the transformation procedure. Thus, the heavy-metal ring 3 has, upon detonation of the explosive 12, the function of reflecting the compressive stresses, whereby-a complete transformation of the insert into a. projectile is ensured. The good reflection ability Is provided by a large specific density Thus, 25' tungsten carbide is better suited than a titanium ferroalloy although both have been found to be successful in practice. 7 The projectile is, therefore, formed symmetrically, i.e. all the mass particles of the insert 2 contribute to a centre of mass lying on the hollow-charge axis 13. An.angle of departure 33 of the projectile is avoided. The press or push f it of the f ixing ring 5 in the casing 11 could also be replaced by a threaded connection, not shown. This has, however, the disadvantage that the cross-section of the casing is weakened by the thread and therefore premature breakage of the casing in this region may occur. The weight of the hollow charge being greater than in accordance with the prior art, caused by the bearing ring 3 consisting of heavy metal, is more than balanced by the advantage of the centric projectile formation and of the error-free departure flight of the projectile. It is to be understood that the scope 6f the present invention is not to be unduly limited by the particular choice of terminology and that a specific term may be replaced by any equivalent or generic term where sensible. Further it is to be understood that individual features, method or functions related to the hollow charge, bearing ring or projectile formation might be individually patentably inventive. In particular, any disclosure in this specification of a range for a variable or parameter shall be taken to include a 8 disclosure of any selectable or derivable sub-range within that range and shall be taken to include a disclosure of any value for the variable or parameter lying within or at an end of the range. The singular 5 may include the plural and vice versa where sensible. The present invention may be that defined in the characterising clause of Claim 1. It is to be understood that any word or phrase derived from the German language of the priority document may be replaced or supplemented by a different English meaning where appropriate. The term 19conical surface" as used throughout the specification and claims is meant to include part-conical surfaces. Therefore, further according to the present invention there is provided a hollow charge comprising a casing in which is located a projectile-forming insert and an explosive, said hollow charge having a plurality of rings in a recess in the casing, a f irst one of said rings having a conical surface matching a conical surface of said insert and being a bearing ring for said insert, a second one of said rings supporting the insert against movement in the axial direction of.the hollow charge, the insert being wedged between the bearing ring and the 2T supporting ring, the bearing ring acting to ensure a symmetrical projectile formation coaxial with said axis or a complete transformation of the insert into a projectile. Said bearing ring may be of a heavy metal and a further fastening ring or rings may be provided in said recess. The supporting ring may be of plastics. The angle of said matching conical surfaces of the insert and bearing ring is, preferably, 33 + 5(or + 1W) to 5 the axis of the hollow charge.
1.
25- CLAIMS 1. A device for stabilising the projectile of a hollow charge, said hollow 'charge having a casing containing explosive, a proj ectileforming insert and rings having conical contact surfaces, which rings support and secure the insert in the casing, characterised in that one of said rings is a bearing ring consisting of heavy or hard metal guided axially in a recess of the casing, the bearing ring having a conical guide surface butting directly against a conical surface of the insert fastened by wedge ef fect, and another one of said rings being a supporting ring which supports (in the axial direction of the hollow charge) the insert at the explosive side relative to a shoulder of the recess on the casing side (in said axial direction), and a further f ixing ring fastenable in the recess fastens the insert, the supporting ring and the bearing ring.
2. A device according to Claim 1, in which a plastics ring is provided between the bearing ring and the fixing ring.
3. A device according to Claim 1 or Claim 2, in which 25" the fixing ring is pressed or is a force f it into the recess.
4. A device for stabilising the projectile of a hollow charge substantially as herein described with reference to the FIGURE of the accompanying drawing.
5. A hollow charge Including a device as claimed in any 5 one of the preceding claims.
6. A hollow charge comprising a casing in which Is located a projectileforming insert and an explosive, said hollow charge having a plurality of rings in a recess in the casing, a first one of said rings having a conical surface matching a conical surface of said insert and being a bearing ring for said insert, a second one of said rings supporting the insert against movement in the axial direction of the hollow charge, the insert being wedged between the bearing ring and the supporting ring, the bearing ring acting to ensure a symmetrical projectile formation coaxial with said axis or a complete transformation of the insert into a projectile.
7. A hollow charge as claimed in Claim 6 in which said bearing ring is of a heavy or hard metal or metal carbide.
8. A hollow charge as claimed in Claim 6 or Claim 7 in " which a further fastening ring or rings are provided in said recess.
9. A hollow charge as claimed in any one of Claims 6 to 12 8 in which the supporting ring is of plastics.
10. A hollow charge as claimed in any one of Claims 6 to 9 in which the angle of said matching conical surfaces of the insert and bearing ring is 33+ 5 (or + 10) to the axis of the hollow charge.
25" k Published 1991 atThePatentOfrice. State House. 66171 High Holbom. London WC1R4TP. Further copies may be obtained from Sales Branch. Unit 6. Nine Mile Point CWmielinfach, Cross Keys. Newport. NPI 7HZ. Printed y Multiplex techniques lid. St Mary Cray, Kent.
GB9019320A 1989-09-19 1990-09-05 A hollow charge Expired - Fee Related GB2236582B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3931169A DE3931169A1 (en) 1989-09-19 1989-09-19 DEVICE FOR STABILIZING THE PROJECTILE OF A SLEEVE

Publications (3)

Publication Number Publication Date
GB9019320D0 GB9019320D0 (en) 1990-10-17
GB2236582A true GB2236582A (en) 1991-04-10
GB2236582B GB2236582B (en) 1993-09-22

Family

ID=6389687

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9019320A Expired - Fee Related GB2236582B (en) 1989-09-19 1990-09-05 A hollow charge

Country Status (3)

Country Link
DE (1) DE3931169A1 (en)
FR (1) FR2652155B3 (en)
GB (1) GB2236582B (en)

Families Citing this family (1)

* 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

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB578845A (en) * 1942-11-11 1946-07-15 James Taylor Improvements in or relating to projectiles for use against armour plate and the like
GB947202A (en) * 1958-11-28 1964-01-22 Latham Valentine Stewart Black Improvements in self-propelled missiles fired from spigot projectors
EP0255130A1 (en) * 1986-07-31 1988-02-03 DIEHL GMBH &amp; CO. Ignition for a hollow charge
GB2221285A (en) * 1988-07-27 1990-01-31 Alford Sidney C Linear cutting charge and kit-of-parts for making same

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2198817B (en) * 1981-12-08 1988-10-26 Royal Ordnance Plc Hollow charge and liner assemblage
DE3441693C1 (en) * 1984-11-15 1986-02-06 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Device for compensating the thermal expansion of a component
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
DE3838581A1 (en) * 1988-11-14 1990-05-17 Kurt Weber Pressed shaped charge

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB578845A (en) * 1942-11-11 1946-07-15 James Taylor Improvements in or relating to projectiles for use against armour plate and the like
GB947202A (en) * 1958-11-28 1964-01-22 Latham Valentine Stewart Black Improvements in self-propelled missiles fired from spigot projectors
EP0255130A1 (en) * 1986-07-31 1988-02-03 DIEHL GMBH &amp; CO. Ignition for a hollow charge
GB2221285A (en) * 1988-07-27 1990-01-31 Alford Sidney C Linear cutting charge and kit-of-parts for making same

Also Published As

Publication number Publication date
FR2652155A3 (en) 1991-03-22
DE3931169A1 (en) 1991-03-28
DE3931169C2 (en) 1993-07-01
GB9019320D0 (en) 1990-10-17
GB2236582B (en) 1993-09-22
FR2652155B3 (en) 1991-08-16

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Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19950905