US3498218A - Bomblet - Google Patents

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US3498218A
US3498218A US711470A US3498218DA US3498218A US 3498218 A US3498218 A US 3498218A US 711470 A US711470 A US 711470A US 3498218D A US3498218D A US 3498218DA US 3498218 A US3498218 A US 3498218A
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Prior art keywords
bomblet
chemical
containers
tubules
container
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Expired - Lifetime
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US711470A
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Jack A Myers
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US Department of Navy
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US Department of Navy
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/36Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
    • F42B12/46Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing gases, vapours, powders or chemically-reactive substances
    • F42B12/50Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing gases, vapours, powders or chemically-reactive substances by dispersion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/36Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
    • F42B12/56Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies
    • F42B12/58Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles

Definitions

  • FIG. 1 is an isometric view of an assembled bomblet
  • FIG. 2 is an exploded view of FIG. 1, a portion being broken away;
  • FIG. 3 is a longitudinal section through one of the tubules shown in FIG. 2;
  • FIG. 4 depicts a manner of dispersion of tubules upon ground impact of a bomblet.
  • the assembled bomblet comprises a pair of frusto-conical containers 12, 12a, secured together at their bases by a plurality of U-shaped frangible clips 14, the containers having angularly spaced recesses 16, forming vanes 18, which cause the bomblet to spin about its longitudinal axis as it falls through the air, as illusrtated by arrow 20.
  • each half of the bomblet is closed by a diaphragm 22, the periphery of which is sealed to same in any suitable manner, such as by welding, cementing or the like.
  • An explosive network 24 is disposed between the diaphragms and is initiated by a fuze 26.
  • the fuze which forms no part of the inventioni per se, is preferably of the type which arms when the bomblet reaches a predetermined speed of rotation and which is impact sensitive to initiate the explosive network.
  • tubules 30 of various lengths, one of which is illutsrated in FIG. 3, each tubule having an end wall 32 disposed adjacent a diaphragm and an opposite open end forming a jet propulsion nozzle 34.
  • Each tubule and the space surrounding all of the tubules is filled with a ice gelled or slurried chemical 36 containing a volatile gas which may rapidly expand when the pressure within the bomblet halves is suddenly released.
  • a cluster of bomblets is released from an air dropped module (not shown) and they rotate as they fall, arming the fuze.
  • the fuze Upon ground impact, as depicted in FIG. 4, the fuze initiates the explosive network, rupturing the clips and peripherally severing the diaphragms and releasing the pressure within the bomblet containers.
  • the volatile gas within the chemical now rapidly expands, issuing with the chemical from the open end of each tubule and propelling it away from the locus of the bomblet.
  • the tubules are of various lengths and thus contain various amounts of propulsive energy, they will be projected various distances from the point of impact.
  • the remaining chemical surrounding the modules also issues from each container by the ex pending gas contained therein, dispersing it in a cloud projecting from the now open end of same.
  • a bomblet comprising;
  • frangible means securing the containers together in base-to-base relationship
  • each tubule and the surrounding space being filled with a chemical material and a volatile gas under pressure
  • each tubule having a closed end adjacent the diaphragm and an opposite open end
  • a bomblet in accordance with claim 1 wherein the outside surface of each container is provided with angular- 1y spaced cut-outs, forming rotating air vane surfaces within its frusto-conical envelope, thereby permitting stacking of a plurality of bomblets in a minimum of space.
  • a bomblet in accordance with claim 2 wherein said cut-outs are so shaped to form radially extending flanges at the base of each container and a plurality of frangible U-shaped clips securing the flanges together.
  • a bomblet in accordance with claim 1 Wherein said explosive network is disc shaped, having a plurality of spokes joined to a rim portion disposed contiguous with the periphery of the diaphragms. l
  • a bomblet in accordance with claim 1 wherein a portion of the tubules of each container are nested Within a cylindrical volume approximately of the minor inner diameter of the container and substantially its axial length and the remainder are nested concentrically thereof in annuli of increasing diameter and smaller axial length, whereby the tubles contain various amounts of chemical and gas.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Dispersion Chemistry (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Description

J. A. MYERS Mal c'h 3, I970 BOMBLET Filed March 6, 1968 III/1111111111, F G n 3 IIIIIIIIIIIIII m m NM w. WA K m .J 4 m M F V. C. MULLER ROY MILLER ATTORNEYS.
United States Patent 3,498,218 BOMBLET Jack A. Myers, China Lake, Calif., assignor to the United States of America as represented by the Secretary of the Navy Filed Mar. 6, 1968, Ser. No. 711,470 Int. Cl. F42b 25/12 US. Cl. 102-6 Claims ABSTRACT OF THE DISCLOSURE Bomblet formed of two frusto-conical containers separably secured togther at their bases, the containers being substantially filled with cylindrical tubes of various lengths, each closed at one end, and containing a gelled chemical and volatile gas under pressure. Upon ground impact, the containers are explosively separated and the gas and chemical particles issuing from the tubes project them by jet propulsion, dispersing the chemical particles to various loci.
Background of the invention In the delivery of chemical particles to a ground target, one of the practices proposed is to release modules from an aircraft, each containing a plurality of bomblets or submuntions which contain a chemical agent, the bomblets dispersing in a pattern continquous wtih the desired target area, the patent to Myers et al. 3,332,348 being exemplary of such technique. In the further development of this general technique, it has been found desirable to provide more uniform dispersal of the bomblets, improved penetration of same through foilage, and variable distances of propagation of the chemical from the locus of ground impact of a bomblet.
Brief description of the drawing FIG. 1 is an isometric view of an assembled bomblet;
BIG. 2 is an exploded view of FIG. 1, a portion being broken away;
FIG. 3 is a longitudinal section through one of the tubules shown in FIG. 2; and
FIG. 4 depicts a manner of dispersion of tubules upon ground impact of a bomblet.
Description of the preferred embodiment Referring first to FIG. 1, the assembled bomblet comprises a pair of frusto-conical containers 12, 12a, secured together at their bases by a plurality of U-shaped frangible clips 14, the containers having angularly spaced recesses 16, forming vanes 18, which cause the bomblet to spin about its longitudinal axis as it falls through the air, as illusrtated by arrow 20.
Referring now to FIG. 2, the base of each half of the bomblet is closed by a diaphragm 22, the periphery of which is sealed to same in any suitable manner, such as by welding, cementing or the like. An explosive network 24 is disposed between the diaphragms and is initiated by a fuze 26. The fuze, which forms no part of the inventioni per se, is preferably of the type which arms when the bomblet reaches a predetermined speed of rotation and which is impact sensitive to initiate the explosive network.
The space between a diaphragm 22 and an end wall 28 is filled with tubules 30 of various lengths, one of which is illutsrated in FIG. 3, each tubule having an end wall 32 disposed adjacent a diaphragm and an opposite open end forming a jet propulsion nozzle 34. Each tubule and the space surrounding all of the tubules is filled with a ice gelled or slurried chemical 36 containing a volatile gas which may rapidly expand when the pressure within the bomblet halves is suddenly released.
In operation, a cluster of bomblets is released from an air dropped module (not shown) and they rotate as they fall, arming the fuze. Upon ground impact, as depicted in FIG. 4, the fuze initiates the explosive network, rupturing the clips and peripherally severing the diaphragms and releasing the pressure within the bomblet containers. The volatile gas within the chemical now rapidly expands, issuing with the chemical from the open end of each tubule and propelling it away from the locus of the bomblet. As Will be apparent, since the tubules are of various lengths and thus contain various amounts of propulsive energy, they will be projected various distances from the point of impact. The remaining chemical surrounding the modules also issues from each container by the ex pending gas contained therein, dispersing it in a cloud projecting from the now open end of same.
Gelled chemicals and the volatile gas contained therein are manufactured by Technidyne, Inc., West Chester, Pa. In the filling of the bomblet, it is first assembled as shown in FIG. 1, and the chemical-gas mixture under pressure is delivered to each bomblet half through sutiable pipe fit tings (not shown) after which the fittings are closed. Closable bleed ports may also be provided in each bomblet half to exhaust entrapped air or alternatively the bomblet halves may be evacuated prior to filling of same.
Obviously many modifications and variations of the present invention are possible in the light of the above teachings. It is therefore to be understood that within the scope of the appended claims the invention may be practiced otherwise than as specifically described.
The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes wtihout the payment of any royalties thereon or therefor.
What is claimed is:
1. A bomblet, comprising;
(a) a pair of frusto-conical containers,
(1)) frangible means securing the containers together in base-to-base relationship,
(c) a diaphragm sealingly closing the base of each container,
(d) an explosive network disposed between the diaphragms adapted to peripherally sever same and rupture the frangible means.
(e) a plurality of cylindrical tubules of various lengths filling each container and extending axially thereof,
(f) each tubule and the surrounding space being filled with a chemical material and a volatile gas under pressure,
(g) each tubule having a closed end adjacent the diaphragm and an opposite open end, and
(h) a fuze disposed centrally of said explosive network adapted to initiate same,
(i) the construction and arrangement being such that when the explosive network severs the diaphragms and ruptures the frangible means the containers separate and the tubules are jet propelled therefrom to various distances, dispersing their contained chemical along their trajectories.
2. A bomblet in accordance with claim 1 wherein the outside surface of each container is provided with angular- 1y spaced cut-outs, forming rotating air vane surfaces within its frusto-conical envelope, thereby permitting stacking of a plurality of bomblets in a minimum of space.
3. A bomblet in accordance with claim 2 wherein said cut-outs are so shaped to form radially extending flanges at the base of each container and a plurality of frangible U-shaped clips securing the flanges together.
3, v 4. A bomblet in accordance with claim 1 Wherein said explosive network is disc shaped, having a plurality of spokes joined to a rim portion disposed contiguous with the periphery of the diaphragms. l
5. A bomblet in accordance with claim 1 wherein a portion of the tubules of each container are nested Within a cylindrical volume approximately of the minor inner diameter of the container and substantially its axial length and the remainder are nested concentrically thereof in annuli of increasing diameter and smaller axial length, whereby the tubles contain various amounts of chemical and gas.
References Cited STATES PATENTS Bettica 1027.2 Blum l027.2 Kanode et al 1026 Berlin et a1. 1027.2 Lidmalm et al 1027.2 Myers et a1 102-6 10 SAMUEL W. ENGLE, Primary Examiner US. Cl. X.R.
US711470A 1968-03-06 1968-03-06 Bomblet Expired - Lifetime US3498218A (en)

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3611931A (en) * 1969-05-05 1971-10-12 Murell J Bessey Sequential burst air drop cluster
US4218064A (en) * 1979-01-23 1980-08-19 Sobbe Donald A Aerial bomb simulating device for model aircraft
US5267501A (en) * 1992-12-14 1993-12-07 Shillig Vance R R/C paint ball drop system
GB2356444A (en) * 1984-04-25 2001-05-23 British Aerospace Weapon cases
US6382105B1 (en) 2001-02-28 2002-05-07 Lockheed Martin Corporation Agent defeat warhead device
WO2003040645A1 (en) * 2001-11-06 2003-05-15 Anciens Ets Clamagirand S.A. Explosive device comprising numerous components
US8495959B2 (en) * 2006-05-15 2013-07-30 Exquadrum, Inc. Kinetic fireball incendiary munition

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1367938A (en) * 1919-01-25 1921-02-08 Bettica Alberto Bomb for aeroplanes
US1382166A (en) * 1917-05-22 1921-06-21 Blum Charles Torpedo
US2653541A (en) * 1949-10-07 1953-09-29 Glenn L Martin Co Container for inflammable liquids
US2920561A (en) * 1956-04-18 1960-01-12 Aaron S Berlin Explosive gas bomb suitable for clustering
US3172330A (en) * 1962-07-06 1965-03-09 Svenska Aeroplan Ab Jettisonable end cone for aircraft rocket missile pods
US3332348A (en) * 1965-01-22 1967-07-25 Jack A Myers Non-lethal method and means for delivering incapacitating agents

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1382166A (en) * 1917-05-22 1921-06-21 Blum Charles Torpedo
US1367938A (en) * 1919-01-25 1921-02-08 Bettica Alberto Bomb for aeroplanes
US2653541A (en) * 1949-10-07 1953-09-29 Glenn L Martin Co Container for inflammable liquids
US2920561A (en) * 1956-04-18 1960-01-12 Aaron S Berlin Explosive gas bomb suitable for clustering
US3172330A (en) * 1962-07-06 1965-03-09 Svenska Aeroplan Ab Jettisonable end cone for aircraft rocket missile pods
US3332348A (en) * 1965-01-22 1967-07-25 Jack A Myers Non-lethal method and means for delivering incapacitating agents

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3611931A (en) * 1969-05-05 1971-10-12 Murell J Bessey Sequential burst air drop cluster
US4218064A (en) * 1979-01-23 1980-08-19 Sobbe Donald A Aerial bomb simulating device for model aircraft
GB2356444A (en) * 1984-04-25 2001-05-23 British Aerospace Weapon cases
GB2356444B (en) * 1984-04-25 2001-08-29 British Aerospace Weapon cases
US5267501A (en) * 1992-12-14 1993-12-07 Shillig Vance R R/C paint ball drop system
US6382105B1 (en) 2001-02-28 2002-05-07 Lockheed Martin Corporation Agent defeat warhead device
WO2003040645A1 (en) * 2001-11-06 2003-05-15 Anciens Ets Clamagirand S.A. Explosive device comprising numerous components
US8495959B2 (en) * 2006-05-15 2013-07-30 Exquadrum, Inc. Kinetic fireball incendiary munition
US9423224B2 (en) 2006-05-15 2016-08-23 Exquadrum, Inc. Kinetic fireball incendiary munition
US9791249B2 (en) 2006-05-15 2017-10-17 Exquadrum, Inc. Kinetic fireball incendiary munition

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