US3292536A - Shaped explosive charges - Google Patents
Shaped explosive charges Download PDFInfo
- Publication number
- US3292536A US3292536A US158050A US15805050A US3292536A US 3292536 A US3292536 A US 3292536A US 158050 A US158050 A US 158050A US 15805050 A US15805050 A US 15805050A US 3292536 A US3292536 A US 3292536A
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- United States
- Prior art keywords
- charge
- cavity
- liner
- explosive charges
- shaped explosive
- 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
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- 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
- F42B1/024—Shaped or hollow charges provided with embedded bodies of inert material
Definitions
- This invention relates to a shaped explosive charge.
- the purpose of the invention is accomplished by arranging the explosive unit so that the force of the explosion is efiectively directed against the sides of the shaped liner.
- FIG. 1 is a vertical sectional view of one form of the invention.
- FIGS. 2 to 4 are sectional views of other forms.
- FIG. 1 there is shown a frusto-conical or truncated container 5 for carrying the explosive charge
- the base or rear end of the charge is formed with a conoidal cavity 7 having a relation to the conical Wall of the container so that the cross-sectional area of the charge at the base is approximately equal to its cross-sectional area at the apex of the cavity.
- the front end of the charge is likewise formed with a conoidal cavity 8 receiving a complementary liner 9 retained in any suitable manner as by the ring 10.
- the dimensions and angle of the cavity and liner may be varied as is well understood in the art of shaped charges. In the illustration parameters are selected which afford an appreciable spacing between the apices of the cavities 7 and 8.
- the explosive charge is initiated at its base in any convenient manner, as by detonators 11-11.
- a cover plate 12 confining the annular base of the charge 6 may be retained by a ring 13.
- the detonation wave In operation when the charge is initiated, the detonation wave travels a converging path on an annular front until it reaches the apex of the cavity 7, where in changing from an annular to a circular front it produces accelerated and intensified action along the periphery of the charge.
- the detonation waves striking with uniformity and maximum force will eliminate the irregularity which occurs when the wave front moves axially of the charge and strikes the liner laterally.
- the charge 14 is formed with a base cavity 15 and a front cavity 16, each having a rounded apex. This arrangement increases the spacing between the apices. Obviously either one of the cavities may be as shown in FIG. 1.
- the base cavity 15 is filled with an inert substance or member 16 which serves as a positive deflecting agency to guide the detonation wave.
- the provision of the solid guide member lends itself to adaptation for use in cylindrical charges as covered in application for patent application Serial No. 160,206 filed May 5, 1950, and now abandoned.
- the front cavity 17 and liner 18 have a sharper angle to permit the explosive charge 19 to extend to and surround the base of the liner.
- the charge 20 is shown as a linear charge with converging side walls 21-21 and parallel faces 22 only the upper one being shown.
- the charge is conveniently carried in a casing 23 which may be inserted in a tubular member, such as a gun barrel, whose wall is to be perforated.
- the invention is also applicable to an explosive charge without a liner in the front cavity.
- a frusto-conical container tapering from its rear end forwardly and having a longitudinal axis of symmetry, a solid block of explosive filling said container and having first and second discrete generally conical cavities therein opening through the forward and rearward faces of said explosive block, respectively, both said cavities being symmetrical about said axis and having their apices spaced along said axis, a liner fitting said first cavity and united about its periphery with the forward periphery of said container, detonator means associated with said block at and about the outer periphery of the base of said second cavity, an inert deflector filling said second cavity, a circular cover plate fitting over and covering said second cavity, said detonator means being annular and surrounding the base of said second cavity, and means securing the rearward periphery of said container with the periphery of said plate.
Description
29, 19% .J. H. CHURCH ETAL 3,
SHAPED EXPLOSIVE CHARGES Filed April 25, 1950 LIEIEEPh H- Church Eregnry LT- Keaaenish United States Patent O 3,292,536 SHAPED EXPLOSIVE CHARGES Joseph H. Church, Austin, Minn., and Gregory J. Kessenich, Madison, Wis., assignors to the United States of America as represented by the Secretary of the Army Filed Apr. 25, 1950, Ser. No. 158,050 1 Claim. (Cl. 102-24 The invention described in the specification and claims may be manufactured and used by or for the Government for governmental purposes without the payment to us of any royalty thereon.
This invention relates to a shaped explosive charge.
In the employment of lined hollow or shaped explosive charges it has long bee-n known that maximum penetration of a target is obtained when the striking gap or standoff distance from the target has a predetermined value dependent on the characteristics of the particular change and liner. In the military and industrial applications of explosives, situations occur where the explosive charge is to be used in confined areas and restricted spaces and must accordingly be limited in size and so placed that the optimum relationship between stand-off and penetration must be ignored or compensated for.
Illustrations of such restricted applications are found where the explosive charge is placed within a tube and is to function axially of the tube as in US patents to Watson 1,534,011, 1,534,012 and Woodberry 1,810,000 or is to function transversely of the tube as in Mims 1,582,184 and Davis 2,399,211.
The purpose of the invention is accomplished by arranging the explosive unit so that the force of the explosion is efiectively directed against the sides of the shaped liner.
The invention is illustrated in the accompanying drawings, in which FIG. 1 is a vertical sectional view of one form of the invention.
FIGS. 2 to 4 are sectional views of other forms.
In FIG. 1 there is shown a frusto-conical or truncated container 5 for carrying the explosive charge The base or rear end of the charge is formed with a conoidal cavity 7 having a relation to the conical Wall of the container so that the cross-sectional area of the charge at the base is approximately equal to its cross-sectional area at the apex of the cavity.
The front end of the charge is likewise formed with a conoidal cavity 8 receiving a complementary liner 9 retained in any suitable manner as by the ring 10. The dimensions and angle of the cavity and liner may be varied as is well understood in the art of shaped charges. In the illustration parameters are selected which afford an appreciable spacing between the apices of the cavities 7 and 8.
The explosive charge is initiated at its base in any convenient manner, as by detonators 11-11. A cover plate 12 confining the annular base of the charge 6 may be retained by a ring 13.
In operation when the charge is initiated, the detonation wave travels a converging path on an annular front until it reaches the apex of the cavity 7, where in changing from an annular to a circular front it produces accelerated and intensified action along the periphery of the charge. The directional efiect on the detonation wave, imparted by the convergence or cavity 7, causes the wave front to strike the sides of the liner 9 approximately normal to these surfaces and obliquely or frontally in the direction of the liner axis. The detonation waves striking with uniformity and maximum force will eliminate the irregularity which occurs when the wave front moves axially of the charge and strikes the liner laterally.
In FIG. 2 the charge 14 is formed with a base cavity 15 and a front cavity 16, each having a rounded apex. This arrangement increases the spacing between the apices. Obviously either one of the cavities may be as shown in FIG. 1. In this form of the invention the base cavity 15 is filled with an inert substance or member 16 which serves as a positive deflecting agency to guide the detonation wave. The provision of the solid guide member lends itself to adaptation for use in cylindrical charges as covered in application for patent application Serial No. 160,206 filed May 5, 1950, and now abandoned.
In FIG. 3 the front cavity 17 and liner 18 have a sharper angle to permit the explosive charge 19 to extend to and surround the base of the liner.
In FIG. 4 the charge 20 is shown as a linear charge with converging side walls 21-21 and parallel faces 22 only the upper one being shown. The charge is conveniently carried in a casing 23 which may be inserted in a tubular member, such as a gun barrel, whose wall is to be perforated.
The invention is also applicable to an explosive charge without a liner in the front cavity.
We claim:
In a shaped explosive charge, a frusto-conical container tapering from its rear end forwardly and having a longitudinal axis of symmetry, a solid block of explosive filling said container and having first and second discrete generally conical cavities therein opening through the forward and rearward faces of said explosive block, respectively, both said cavities being symmetrical about said axis and having their apices spaced along said axis, a liner fitting said first cavity and united about its periphery with the forward periphery of said container, detonator means associated with said block at and about the outer periphery of the base of said second cavity, an inert deflector filling said second cavity, a circular cover plate fitting over and covering said second cavity, said detonator means being annular and surrounding the base of said second cavity, and means securing the rearward periphery of said container with the periphery of said plate.
References Cited by the Examiner UNITED STATES PATENTS 2,494,256 1/ 1950 Muskat et al. 10224 2,622,528 12/ 1952 Lawrence 10224 2,699,721 1/1955 Klotz 10220 FOREIGN PATENTS 610,106 10/1948 Great Britain.
OTHER REFERENCES Clark, American Institute of Mining and Metallurgical Engineers, Technical Pub. No. 2157, page 7, March 1947.
McLemore, The Oil and Gas Journal, Dec. 28, 1946, pp. 268-271.
BENJAMIN A. BORCHELT, Primary Examiner.
WILLIAM WILES, ARTHUR M. HORTON, SAMUEL BOYD, Examiners.
R. L. CAMPBELL, R. F. CUSTARD, V. R. PENDE- GRASS, Assistant Examiners.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US158050A US3292536A (en) | 1950-04-25 | 1950-04-25 | Shaped explosive charges |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US158050A US3292536A (en) | 1950-04-25 | 1950-04-25 | Shaped explosive charges |
Publications (1)
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US3292536A true US3292536A (en) | 1966-12-20 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US158050A Expired - Lifetime US3292536A (en) | 1950-04-25 | 1950-04-25 | Shaped explosive charges |
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Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2308906A1 (en) * | 1975-04-23 | 1976-11-19 | Luchaire Sa | Hollow explosive charge fuse - has air chamber between priming charge and apex of hollow charge sheathing |
US4030418A (en) * | 1975-10-30 | 1977-06-21 | The United States Of America As Represented By The Secretary Of The Army | Gravity deployed mine with combined upper clearing charge firing and delayed main charge initiation |
US4033265A (en) * | 1976-03-25 | 1977-07-05 | The United States Of America As Represented By The Secretary Of The Navy | Anti-compromise device |
US4040354A (en) * | 1975-10-30 | 1977-08-09 | The United States Of America As Represented By The Secretary Of The Army | Gravity-deployed double-ended anti-tank mine |
US4058060A (en) * | 1975-10-30 | 1977-11-15 | The United States Of America As Represented By The Secretary Of The Army | Gravity-deployed munition with a mechanical gravity-controlled switch |
DE2624927A1 (en) * | 1976-06-03 | 1977-12-15 | Messerschmitt Boelkow Blohm | HOLLOW LOAD TYPE LANDMINE |
FR2380530A1 (en) * | 1977-02-12 | 1978-09-08 | Rheinmetall Gmbh | PROCESS FOR DIRECTING THE DETONATION WAVE IN THE EXPLOSIVE MATERIAL OF LOADS WITH A PREDETERMINED ACTION DIRECTION, IN PARTICULAR HOLLOW LOADS, AND PROVISION FOR IMPLEMENTATION OF THE PROCEDURE |
DE2306423A1 (en) * | 1972-02-11 | 1981-04-16 | L'Etat Français représenté par le Délégué Général pour l'Armement, Paris | FORM LOAD MINE |
US4594947A (en) * | 1983-07-28 | 1986-06-17 | Commissariat A L'energie Atomique | Apparatus for shaping a detonation wave |
FR2581747A1 (en) * | 1985-05-07 | 1986-11-14 | Serat | IMPROVEMENTS TO HOLLOW LOADS |
US5204493A (en) * | 1978-12-04 | 1993-04-20 | Wolfgang Christmann | Inert insertion for explosive wave guidance in shaped charges |
FR2742539A1 (en) * | 1995-12-14 | 1997-06-20 | Giat Ind Sa | Multi-purpose explosive charge, e.g. for detonating mines |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB610106A (en) * | 1945-02-06 | 1948-10-12 | Ct D Etudes M B A | Improvements in blasting cartridges |
US2494256A (en) * | 1945-09-11 | 1950-01-10 | Gulf Research Development Co | Apparatus for perforating well casings and well walls |
US2622528A (en) * | 1945-04-07 | 1952-12-23 | Hercules Powder Co Ltd | Explosive cartridge |
US2699721A (en) * | 1947-02-19 | 1955-01-18 | Seismograph Service Corp | Explosive cutting device |
-
1950
- 1950-04-25 US US158050A patent/US3292536A/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB610106A (en) * | 1945-02-06 | 1948-10-12 | Ct D Etudes M B A | Improvements in blasting cartridges |
US2622528A (en) * | 1945-04-07 | 1952-12-23 | Hercules Powder Co Ltd | Explosive cartridge |
US2494256A (en) * | 1945-09-11 | 1950-01-10 | Gulf Research Development Co | Apparatus for perforating well casings and well walls |
US2699721A (en) * | 1947-02-19 | 1955-01-18 | Seismograph Service Corp | Explosive cutting device |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2306423A1 (en) * | 1972-02-11 | 1981-04-16 | L'Etat Français représenté par le Délégué Général pour l'Armement, Paris | FORM LOAD MINE |
FR2308906A1 (en) * | 1975-04-23 | 1976-11-19 | Luchaire Sa | Hollow explosive charge fuse - has air chamber between priming charge and apex of hollow charge sheathing |
US4030418A (en) * | 1975-10-30 | 1977-06-21 | The United States Of America As Represented By The Secretary Of The Army | Gravity deployed mine with combined upper clearing charge firing and delayed main charge initiation |
US4040354A (en) * | 1975-10-30 | 1977-08-09 | The United States Of America As Represented By The Secretary Of The Army | Gravity-deployed double-ended anti-tank mine |
US4058060A (en) * | 1975-10-30 | 1977-11-15 | The United States Of America As Represented By The Secretary Of The Army | Gravity-deployed munition with a mechanical gravity-controlled switch |
US4033265A (en) * | 1976-03-25 | 1977-07-05 | The United States Of America As Represented By The Secretary Of The Navy | Anti-compromise device |
DE2624927A1 (en) * | 1976-06-03 | 1977-12-15 | Messerschmitt Boelkow Blohm | HOLLOW LOAD TYPE LANDMINE |
FR2380530A1 (en) * | 1977-02-12 | 1978-09-08 | Rheinmetall Gmbh | PROCESS FOR DIRECTING THE DETONATION WAVE IN THE EXPLOSIVE MATERIAL OF LOADS WITH A PREDETERMINED ACTION DIRECTION, IN PARTICULAR HOLLOW LOADS, AND PROVISION FOR IMPLEMENTATION OF THE PROCEDURE |
US5204493A (en) * | 1978-12-04 | 1993-04-20 | Wolfgang Christmann | Inert insertion for explosive wave guidance in shaped charges |
US4594947A (en) * | 1983-07-28 | 1986-06-17 | Commissariat A L'energie Atomique | Apparatus for shaping a detonation wave |
FR2581747A1 (en) * | 1985-05-07 | 1986-11-14 | Serat | IMPROVEMENTS TO HOLLOW LOADS |
FR2742539A1 (en) * | 1995-12-14 | 1997-06-20 | Giat Ind Sa | Multi-purpose explosive charge, e.g. for detonating mines |
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