EP0323484B1 - Einlage für einen gefechtskopf - Google Patents
Einlage für einen gefechtskopf Download PDFInfo
- Publication number
- EP0323484B1 EP0323484B1 EP19880902446 EP88902446A EP0323484B1 EP 0323484 B1 EP0323484 B1 EP 0323484B1 EP 19880902446 EP19880902446 EP 19880902446 EP 88902446 A EP88902446 A EP 88902446A EP 0323484 B1 EP0323484 B1 EP 0323484B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- liner
- area
- insert
- explosive
- 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
- F42B1/00—Explosive charges characterised by form or shape but not dependent on shape of container
- F42B1/02—Shaped or hollow charges
- F42B1/028—Shaped or hollow charges characterised by the form of the liner
Definitions
- the invention relates to an insert for a warhead, the type defined in the preamble of claim 1.
- a warhead with an insert which is designed as a spherical cap is known from US Pat. No. 4,356,770.
- This spherical cap creates an essentially rod-shaped projectile through explosive deformation, but due to its aerodynamically unfavorable shape it has unstable flight behavior, a high drop in speed and consequently an inadequate end-ballistic performance.
- the high drop in speed is essentially caused by the hemispherical shape of the projectile tip.
- a projectile-forming insert corresponding to the features of the preamble of patent claim 1 can be seen as known.
- this insert which consists of a basic cone
- a central area of the insert contains a cone which deviates from the basic cone and has an acute cone angle.
- this causes the tip area to break out of the remaining part of the projectile during explosive forming.
- the aim of this is to create two partial storeys, with the leading partial storey formed from the tip area penetrating the camouflage layer of armor and thus creating an opening through which the subsequent storey can fly unhindered and without impairing its penetration effect.
- the disadvantageous shape present here in particular the main part of the projectile, does not guarantee an increase in the final ballistic performance.
- FIG. 1 shows an essentially hollow-cylindrical warhead 10, in the housing 11 of which an explosive charge 13 activated by an igniter 12 is arranged.
- the explosive charge 13 is delimited on one side by a dome-shaped insert 14, from which a projectile can be formed by explosive deformation.
- the insert 14 has the shape of a spherical cap.
- the projectile shown schematically in FIG. 1 with 15 can be produced from such an insert by the explosive shaping after ignition of the explosive charge 13. Such projectiles have a strong drop in speed, which is due to the aerodynamically unfavorable shape of the tip of the projectile 15. As shown in FIG. 1, the insert 14 creates a projectile 15 with a tip in the shape of a hemisphere.
- FIG. 2 shows an insert 20 which, apart from a central area 22, essentially corresponds to the insert 14 (FIG. 1).
- the insert In the area 22 around the center of the insert, the insert has a stronger convex curvature in the direction of the explosive 13 (FIG. 1) than outside the area 22.
- the geometric change in the area 22 of the insert can have any shape (linear, square, S-shaped, etc.) such that the radial pressure components pr at the edge of the area 22 are larger within this area than the radial pressure components p'r outside of area 22 but also in the immediate vicinity of this area.
- the height ⁇ x of the curvature and the diameter d of the area 22 up to which the geometric change is made depend on the explosive used and the insert material and must each be determined experimentally.
- the maximum diameter d of the area 22 is approximately 10 to 25% of the diameter D of the insert 20 and the height ⁇ x of the bulge (indentation) must be less than 15 in this area % of the curvature of the insert 20.
- the wall thickness s of the insert within the area around the insert center can be selected to be at least in a partial area smaller than the wall thickness of the insert outside of the said area.
- a corresponding exemplary embodiment is shown in FIG. 3.
- the insert 40 was the insert and 50 the projectile resulting from the insert 40 being exploded.
- the area 42 around the insert center corresponds to the area 22 in FIG. 2.
- the insert geometry is changed in a partial area 43 such that the corresponding diameter s is smaller than the diameter S of the insert outside the area 42.
- the remaining one Wall thickness of the insert in area 43 must, however, be selected so that the insert does not burst in the case of particularly explosive explosives.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Drilling And Exploitation, And Mining Machines And Methods (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
- Inorganic Compounds Of Heavy Metals (AREA)
- Glass Compositions (AREA)
- Ceramic Products (AREA)
- Radar Systems Or Details Thereof (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3722024 | 1987-07-03 | ||
DE19873722024 DE3722024A1 (de) | 1987-07-03 | 1987-07-03 | Einlage fuer einen gefechtskopf |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0323484A1 EP0323484A1 (de) | 1989-07-12 |
EP0323484B1 true EP0323484B1 (de) | 1992-04-22 |
Family
ID=6330852
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP19880902446 Expired - Lifetime EP0323484B1 (de) | 1987-07-03 | 1988-03-05 | Einlage für einen gefechtskopf |
Country Status (8)
Country | Link |
---|---|
US (1) | US4979443A (pt) |
EP (1) | EP0323484B1 (pt) |
DE (2) | DE3722024A1 (pt) |
DK (1) | DK71089A (pt) |
GR (1) | GR1000024B (pt) |
NO (1) | NO884373L (pt) |
PT (1) | PT87331B (pt) |
WO (1) | WO1989000274A1 (pt) |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4108633C2 (de) * | 1991-03-16 | 1999-10-28 | Diehl Stiftung & Co | Verwendung des scharfen Wirkteiles einer Suchzünder-Submunition als Übungsmunition mit reduzierter Reichweite |
SE502461C2 (sv) * | 1991-07-01 | 1995-10-23 | Bofors Ab | Sätt vid projektilbildande explosiva laddningar |
US5155296A (en) * | 1992-03-18 | 1992-10-13 | The United States Of America As Represented By The Secretary Of The Army | Thermally enhanced warhead |
US5251561A (en) * | 1992-06-11 | 1993-10-12 | The United States Of America As Represented By The United States Department Of Energy | Open apex shaped charge-type explosive device having special disc means with slide surface thereon to influence movement of open apex shaped charge liner during collapse of same during detonation |
US5792977A (en) * | 1997-06-13 | 1998-08-11 | Western Atlas International, Inc. | High performance composite shaped charge |
US6349649B1 (en) * | 1998-09-14 | 2002-02-26 | Schlumberger Technology Corp. | Perforating devices for use in wells |
US6305289B1 (en) * | 1998-09-30 | 2001-10-23 | Western Atlas International, Inc. | Shaped charge for large diameter perforations |
US6244186B1 (en) | 1999-07-26 | 2001-06-12 | Joseph F. L. John Pichard | Air gun pellet |
US7222573B2 (en) * | 2005-04-01 | 2007-05-29 | Pontieri James M | Aerodynamic air gun projectile |
US8156871B2 (en) * | 2007-09-21 | 2012-04-17 | Schlumberger Technology Corporation | Liner for shaped charges |
US7954433B1 (en) * | 2008-07-24 | 2011-06-07 | Matt Bradley Barnett | Explosive shaped charge device |
JP2010169318A (ja) * | 2009-01-23 | 2010-08-05 | Ihi Aerospace Co Ltd | 成形炸薬弾頭とこれを用いたタンデム弾頭 |
CN104457433B (zh) * | 2014-10-24 | 2016-02-24 | 中国船舶重工集团公司第七〇五研究所 | 一种组合药型罩 |
FR3057868B1 (fr) | 2016-10-26 | 2018-10-26 | Arkema France | Composition a base de monomeres allyliques et de peroxyde(s) pour la fabrication de verres organiques |
KR101823819B1 (ko) * | 2017-03-31 | 2018-01-30 | 국방과학연구소 | 복합기능탄두용 이중성능관통자 라이너 |
KR102338251B1 (ko) * | 2020-08-05 | 2021-12-10 | 국방과학연구소 | 폭발 성형 관통자 |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2513233A (en) * | 1949-03-15 | 1950-06-27 | Laud Stanley Byers | Multiple jet blasting charge |
FR1170521A (fr) * | 1957-04-01 | 1959-01-15 | Schlumberger Prospection | Perfectionnements aux charges creuses utilisées pour la perforation dans des cibleshétérogènes |
NL255689A (pt) * | 1958-07-14 | |||
US3269467A (en) * | 1964-06-11 | 1966-08-30 | Schlumberger Well Surv Corp | Shaped charge apparatus |
GB1237392A (en) * | 1967-12-15 | 1971-06-30 | Messerschmitt Boelkow Blohm | Improvements in explosive charges |
DE1946959C3 (de) * | 1969-09-17 | 1974-01-10 | Rheinmetall Gmbh, 4000 Duesseldorf | Hohlladung mit Einlage progressiver oder degressiver Wandstärke |
DE2007625A1 (de) * | 1970-02-19 | 1971-09-09 | ETA Corp GmbH, 2000 Hamburg | Hohlladungsgeschoß |
DE2729517C1 (de) * | 1977-06-30 | 1985-12-05 | Rheinmetall GmbH, 4000 Düsseldorf | Rotationssymmetrische Hohlladungseinlage mit einer ueber den Radius zunehmenden oder abnehmenden Wandstaerke |
FR2488389B1 (fr) * | 1980-08-06 | 1986-04-25 | Serat | Perfectionnements aux charges creuses |
US4359943A (en) * | 1980-09-02 | 1982-11-23 | The United States Of America As Represented By The Secretary Of The Army | Shaped charge warhead including shock wave forming surface |
FI66988C (fi) * | 1981-10-28 | 1984-12-10 | Sica Ab Oy | Haolpatron med riktad spraengverkan och foerfarande foer framstaellning av en metallisk kon foer haolpatron |
FR2569473B1 (fr) * | 1984-08-21 | 1987-10-23 | Realisa Applic Techni Et | Perfectionnements apportes aux charges creuses |
NO862508L (no) * | 1985-12-12 | 1987-06-15 | Israel Defence | Bombe med formet eller hul ladning. |
DE3622680A1 (de) * | 1986-07-05 | 1988-01-14 | Diehl Gmbh & Co | Zylindrische hohlladung mit einer tulpenfoermigen einlage |
IL81097A (en) * | 1986-12-25 | 1991-06-10 | Israel Defence | Two-stage shaped charge projectile |
US4896609A (en) * | 1989-05-01 | 1990-01-30 | United States Of America As Represented By The Secretary Of The Army | Planar shock wave generator and enhancer device |
-
1987
- 1987-07-03 DE DE19873722024 patent/DE3722024A1/de not_active Withdrawn
-
1988
- 1988-03-05 US US07/332,277 patent/US4979443A/en not_active Expired - Fee Related
- 1988-03-05 WO PCT/EP1988/000171 patent/WO1989000274A1/de active IP Right Grant
- 1988-03-05 DE DE8888902446T patent/DE3870430D1/de not_active Expired - Fee Related
- 1988-03-05 EP EP19880902446 patent/EP0323484B1/de not_active Expired - Lifetime
- 1988-04-25 GR GR880100271A patent/GR1000024B/el unknown
- 1988-04-26 PT PT87331A patent/PT87331B/pt not_active IP Right Cessation
- 1988-10-03 NO NO88884373A patent/NO884373L/no unknown
-
1989
- 1989-02-15 DK DK071089A patent/DK71089A/da not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
GR880100271A (en) | 1989-04-12 |
DK71089A (da) | 1989-03-01 |
PT87331A (pt) | 1989-06-30 |
DE3870430D1 (de) | 1992-05-27 |
GR1000024B (el) | 1990-01-31 |
DK71089D0 (da) | 1989-02-15 |
DE3722024A1 (de) | 1989-01-12 |
PT87331B (pt) | 1993-09-30 |
WO1989000274A1 (en) | 1989-01-12 |
EP0323484A1 (de) | 1989-07-12 |
NO884373L (no) | 1989-01-12 |
NO884373D0 (no) | 1988-10-03 |
US4979443A (en) | 1990-12-25 |
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