US3188954A - Gas ejection bomb for dispersing solid particulates - Google Patents

Gas ejection bomb for dispersing solid particulates Download PDF

Info

Publication number
US3188954A
US3188954A US735345A US73534558A US3188954A US 3188954 A US3188954 A US 3188954A US 735345 A US735345 A US 735345A US 73534558 A US73534558 A US 73534558A US 3188954 A US3188954 A US 3188954A
Authority
US
United States
Prior art keywords
bomb
cylinder
tail
primer
gas ejection
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
Application number
US735345A
Inventor
Paul G Roach
Harold C Weingartner
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to US735345A priority Critical patent/US3188954A/en
Application granted granted Critical
Publication of US3188954A publication Critical patent/US3188954A/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
    • 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

Definitions

  • This invention relates to a gas ejection bomb so constructed that it will disperse finely divided toxic solids upon impact with the ground or a solid object.
  • FIG. 1 is a longitudinal view of a carbon dioxide cyinder gas ejection bomb, a portion of the bomb casing being broken away to show certain parts in section.
  • FIG. 2 is a transverse sectional view of the gas ejection bomb taken on the line 2-2 of FIG. 1.
  • FIG. 3 is a partial longitudinal sectional view of a detonator type of air cylinder gas ejection bomb.
  • FIG. 4 is a partial longitudinal view of a shearing pin type of air cylinder gas ejection bomb with parts broken away, showing certain parts in section.
  • the bomb comprises a casing 1 which includes a cylindrical body portion 2, joined at 3 to a nose assembly 4, and conical tail section 5. Within the casing 1 is a cylindrical reinforcing sleeve 6. There is a nose base 7 at a first end and diffuser vanes 9 at a second end of the bomb.
  • the nose base 7 comprises a nose outer cup 11 and a nose inner cup 13.
  • Nose assembly 4 is secured to the nose base 7 by nose cup screws 16.
  • the nose assembly 4 supports the gas cylinder and fuse described below.
  • the hexagonal shaped nose base 7 corresponds with a hexagon formed when the tail vanes 15 at the second end are folded in to facilitate bomb clustering.
  • the tail vanes 15 fold about the conical tail section 5.
  • a pivoting rivet 19 is used to connect the tail vanes 15 to the conical tail section 5.
  • Vane bracket 20, dilfuser nut 22, and tail sleeve 24 keep the tail vanes 15 and the diffuser vanes 9 in place.
  • the fuse comprises an arming pin 23, and an arming spring 25, which is used to eject the arming pin 23.
  • An arming wire 21 is removed when the bomb is clustered with others for use.
  • Pin 23 is then held in place by clip 26.
  • Retainer balls 27 cooperate with the arming pin 23 to restrain the fuse operation.
  • the fuse body 29 forms the base for the elements which comprise the fuse.
  • a collar 31 and its attached primer firer 33 are located adjacent to the retainer balls 27.
  • a retainer spring 35 is positioned between the collar 31 and the primer 37. The retainer spring 35 circumscribes the primer firer 33 so as to prevent the primer firer 33 from accidentally striking the primer 37.
  • the primer 37 is located within the fuse plunger 39. In FIG. 1 a piston 40 is separated from the free plunger 39 by a small space.
  • the base of the firing pin 41 is secured to piston 40.
  • a piston spring 42 is located between the piston 40 and a cylinder 44 which contains liquified carbon dioxide.
  • the piston spring 42 prevents the firing pin 41, which is situated between the springs of the piston spring 42, from accidentally striking and rupturing a first shear disc 47.
  • the heater primer 49 is adjacent to the first shear 3,188,954 Patented June 15, 1965 ice disc 47 and is at a first end of heater tube 51.
  • Heater support 53 is also mounted at the first end of heater tube 51 and is adjacent to the heater primer 49.
  • the exterior of heater support is formed of flutes 55.
  • a heater sealing cup 59 is at the second end of the heater tube 51.
  • Liquid carbon dioxide 61 is contained in cylinder 44 and surrounds the heater tube 51.
  • the fluted heater support 53 passes through a cylindrical opening in the end of cylinder 44. The flutes thus form longitudinal passages, which communicate with the interior of cylinder 44. The outer ends of these passages are closed by first shear disc 47.
  • a detonator 43 is located adjacent to the fuse plunger 39.
  • the first shear disc 47 blocks the entrance to the cylinder 144 and is positioned next to the detonator 43.
  • Compressed air 161 is contained in cylinder 144 of this second type gas bomb.
  • a piston 140 is separated from the fuse plunger by a small space.
  • the base of a shearing pin 45 is secured to piston 140.
  • a piston spring 42 is located between the piston 140 and the cylinder 144.
  • the piston spring 42 prevents the shearing pin 45, which is situated between the coils of the piston spring 42, from accidentally striking and rupturing the first shear disc 47.
  • the first shear disc 47 blocks the entrance to the cylinder 144 and is positioned next to the detonator 43. Compressed air 161 is contained in cylinder 144 of this third type gas bomb.
  • first orifices 65 which are taped, 69, within the nose assembly 4. It will be noted that in all three modifications the elements lying between the orifices 65 and the opening in the end of cylinder 44 are so formed as to define a passage for the compressed gas, which passage is closed by shear disc 47.
  • the solid toxic particulates 70 are contained in the space 71 between the casing 1 and the cylinder 44 or cylinder 144.
  • a tail shear disc 73 is located within the conical tail section 5 at the second end of the bomb.
  • the shear disc ring 74 is used to firmly position the tail shear disc 73.
  • Tail orifices 75 are located at the base of difiuser vanes 9 at the second end of the bomb.
  • Explosion of primer 37 explodes detonator 43 (FIG. 3), propels firing pin 41 (FIG. 1), or propels shear pin 45 (FIG. 4).
  • explosion of primer 37 drives firing pin 41 through the first shear disk 47 and detonates heater primer 49.
  • the heater tube 51 contains a mixture of potassium perchlorate, charcoal and oil. This mixture is ignited by primer 49 and burns rapidly, evolving a large amount of heat.
  • the products of combustion are potassium chloride and carbon dioxide.
  • the heat given off by the combustion vaporizes the liquified carbon dioxide 61 in the cylinder 44.
  • the pressure developed further ruptures shear disc 47, exposing the ends of the passages formed by flutes 55.
  • the carbon dioxide in cylinder 44 and that formed by the reaction in tube 51 then flow through orifices 65, bursting tape 69 and entering the space 71 between the cylinder 44 and easing 1, in which the solid toxic particulates 70 are located.
  • the mixture, KClO and charcoal, in the heater burns rapidly at high pressure, but only slowly at low pressures. The burning therefore ceases or is retarded when pressure is released. This avoids overheating of the toxic particulates.
  • the first shear disc 47 is ruptured by the detonator 43 while in FIG. 4 the first shear disc 47 is ruptured by the shearing pin 45.
  • the tapes 69 are burst by the air pressure in the first orifices 65 and the compressed air fiows into the space 71 between the casing 1 and the cylinder 144.
  • the carbon dioxide gas or the air mixes with the solid toxic particulates and flows through the conical tail section which is converged to increase the velocity at its second end where the tail shear disc 73 is located.
  • the tail shear disc 73 bursts due to the pressure of either the carbon dioxide gas and the solid toxic particulates or the air and the solid toxic particulates depending on the type of bomb used, and the mixture flows past the ruptured tail shear disc 73 and out the tail orifices 75.
  • the difiuser vanes 9 deflect the finely divided solid particulates coming out of the tail orifices 75 into three separate low hanging clouds for maximal efiect.
  • gases can be used to disperse the solid toxic particulates, if desired.
  • carbon dioxide is preferable to certain other liquifiable gases, such as ammonia, because of its inert and odorless characteristics.
  • a gas ejection bomb for dispersing solid particulates comprising an elongated casing having a first end and a second end, a nose base at said first end of said casing, a fuze mounted within said casing adjacent said nose base, said fuze defining at least one orifice communicating with the interior of said casing, a closed cylinder mounted within said casing and having an opening adjacent said fuze means, a heater tube within said cylinder, a heater primer, in a first end of said heater tube, a heater support mounted at said first end of said heater tube and within said opening, said opening having walls surrounding and contacting the exterior of said heater support, said heater support having a plurality of longitudinal fiutes on its exterior, defining with the walls of said opening a series of passages from the interior to the exterior of said cylinder, a first shear disk mounted between said fuze and said opening and closing said passages, said fuze comprising a firing pin aligned with said heater primer, liquified carbon dioxide in said cylinder surrounding

Landscapes

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

Description

June 15, 1965 P. s. ROACH ETAL 3,188,954
GAS EJECTION BQMB FOR DISPERSING SOLID PARTICULATES Filed May 14. 1958 Fig.
u n 2 i i 70 i i l 59 i 44 i 6/ l6! 5/ i 47 i; 45 \k 140 1 29 2* INVENTORS 2 3 Paul 6. Roach 3/ 7 Harold 6. Walngarfnd BY A a I3 27 2 6 2/ 23 ATTORNEY United States Patent 3,188,954 GAS EJECTION BOMB FOR DISPERSING SOLID PARTICULATES Paul G. Roach, Dover, N.J., and Harold C. Weingartner,
Marblehead, Mass., assignors to the United States of America as represented by the Secretary of the Army Filed May 14, 1958, Ser. No. 735,345 1 Claim. (Cl. 102-6) This invention relates to a gas ejection bomb so constructed that it will disperse finely divided toxic solids upon impact with the ground or a solid object.
It is an object of this invention to develop an aerial bomb for ejecting and dispersing a toxic powder into the air in the form of a low hanging cloud, which will persist as long as possible.
It is another object of this invention to provide a means for etfectively dispersing solid toxic particulates without the use of an explosive or heating means which would seriously limit or destroy the effect of heat-sensitive solid toxic particulates.
In the accompanying drawing:
FIG. 1 is a longitudinal view of a carbon dioxide cyinder gas ejection bomb, a portion of the bomb casing being broken away to show certain parts in section.
FIG. 2 is a transverse sectional view of the gas ejection bomb taken on the line 2-2 of FIG. 1.
FIG. 3 is a partial longitudinal sectional view of a detonator type of air cylinder gas ejection bomb.
FIG. 4 is a partial longitudinal view of a shearing pin type of air cylinder gas ejection bomb with parts broken away, showing certain parts in section.
The bomb comprises a casing 1 which includes a cylindrical body portion 2, joined at 3 to a nose assembly 4, and conical tail section 5. Within the casing 1 is a cylindrical reinforcing sleeve 6. There is a nose base 7 at a first end and diffuser vanes 9 at a second end of the bomb. The nose base 7 comprises a nose outer cup 11 and a nose inner cup 13. Nose assembly 4 is secured to the nose base 7 by nose cup screws 16. The nose assembly 4 supports the gas cylinder and fuse described below.
The hexagonal shaped nose base 7 corresponds with a hexagon formed when the tail vanes 15 at the second end are folded in to facilitate bomb clustering. The tail vanes 15 fold about the conical tail section 5. A pivoting rivet 19 is used to connect the tail vanes 15 to the conical tail section 5. Vane bracket 20, dilfuser nut 22, and tail sleeve 24 keep the tail vanes 15 and the diffuser vanes 9 in place.
The fuse comprises an arming pin 23, and an arming spring 25, which is used to eject the arming pin 23. An arming wire 21 is removed when the bomb is clustered with others for use. Pin 23 is then held in place by clip 26. Retainer balls 27 cooperate with the arming pin 23 to restrain the fuse operation. The fuse body 29 forms the base for the elements which comprise the fuse. A collar 31 and its attached primer firer 33 are located adjacent to the retainer balls 27. A retainer spring 35 is positioned between the collar 31 and the primer 37. The retainer spring 35 circumscribes the primer firer 33 so as to prevent the primer firer 33 from accidentally striking the primer 37. The primer 37 is located within the fuse plunger 39. In FIG. 1 a piston 40 is separated from the free plunger 39 by a small space. The base of the firing pin 41 is secured to piston 40. A piston spring 42 is located between the piston 40 and a cylinder 44 which contains liquified carbon dioxide. The piston spring 42 prevents the firing pin 41, which is situated between the springs of the piston spring 42, from accidentally striking and rupturing a first shear disc 47.
The heater primer 49 is adjacent to the first shear 3,188,954 Patented June 15, 1965 ice disc 47 and is at a first end of heater tube 51. Heater support 53 is also mounted at the first end of heater tube 51 and is adjacent to the heater primer 49. The exterior of heater support is formed of flutes 55. A heater sealing cup 59 is at the second end of the heater tube 51. Liquid carbon dioxide 61 is contained in cylinder 44 and surrounds the heater tube 51. The fluted heater support 53 passes through a cylindrical opening in the end of cylinder 44. The flutes thus form longitudinal passages, which communicate with the interior of cylinder 44. The outer ends of these passages are closed by first shear disc 47.
In FIG. 3 a detonator 43 is located adjacent to the fuse plunger 39. The first shear disc 47 blocks the entrance to the cylinder 144 and is positioned next to the detonator 43. Compressed air 161 is contained in cylinder 144 of this second type gas bomb.
In FIG. 4 a piston 140 is separated from the fuse plunger by a small space. The base of a shearing pin 45 is secured to piston 140. A piston spring 42 is located between the piston 140 and the cylinder 144. The piston spring 42 prevents the shearing pin 45, which is situated between the coils of the piston spring 42, from accidentally striking and rupturing the first shear disc 47. The first shear disc 47 blocks the entrance to the cylinder 144 and is positioned next to the detonator 43. Compressed air 161 is contained in cylinder 144 of this third type gas bomb.
In all three cases there are first orifices 65, which are taped, 69, within the nose assembly 4. It will be noted that in all three modifications the elements lying between the orifices 65 and the opening in the end of cylinder 44 are so formed as to define a passage for the compressed gas, which passage is closed by shear disc 47. The solid toxic particulates 70 are contained in the space 71 between the casing 1 and the cylinder 44 or cylinder 144. A tail shear disc 73 is located within the conical tail section 5 at the second end of the bomb. The shear disc ring 74 is used to firmly position the tail shear disc 73. Tail orifices 75 are located at the base of difiuser vanes 9 at the second end of the bomb.
Operation In flight the three tail vanes are opened up by the air rushing up the casing 1 from the nose base 7. To produce maximum stability a maximum tail vane area is provided at a maximum distance from the bombs axis. When the cluster breaks up, clip 26 falls off and the arming pin 23 is ejected from the bomb by the ejection action of the arming spring 25. This permits the retainer balls 27 to roll freely inwardly, since the arming pin 23 is no longer between them. Upon contact with the ground or other solid object, the retainer balls 27 are pushed together by the downward sliding action of the walls of the plunger 39, which due to its inertia overcomes the resistance of spring 35 and moves downwardly, causing primer 37 to strike primer firer 33.
Explosion of primer 37 explodes detonator 43 (FIG. 3), propels firing pin 41 (FIG. 1), or propels shear pin 45 (FIG. 4).
In the modification shown in FIGURE 1, explosion of primer 37 drives firing pin 41 through the first shear disk 47 and detonates heater primer 49. The heater tube 51 contains a mixture of potassium perchlorate, charcoal and oil. This mixture is ignited by primer 49 and burns rapidly, evolving a large amount of heat. The products of combustion are potassium chloride and carbon dioxide. The heat given off by the combustion vaporizes the liquified carbon dioxide 61 in the cylinder 44. The pressure developed further ruptures shear disc 47, exposing the ends of the passages formed by flutes 55. The carbon dioxide in cylinder 44 and that formed by the reaction in tube 51 then flow through orifices 65, bursting tape 69 and entering the space 71 between the cylinder 44 and easing 1, in which the solid toxic particulates 70 are located.
The mixture, KClO and charcoal, in the heater burns rapidly at high pressure, but only slowly at low pressures. The burning therefore ceases or is retarded when pressure is released. This avoids overheating of the toxic particulates.
In FIG. 3 the first shear disc 47 is ruptured by the detonator 43 while in FIG. 4 the first shear disc 47 is ruptured by the shearing pin 45. This permits, in both cases, the compressed air 161 in the cylinder 144 to flow out past the ruptured first shear disc 47 and into the first orifices 65. The tapes 69 are burst by the air pressure in the first orifices 65 and the compressed air fiows into the space 71 between the casing 1 and the cylinder 144.
Now, in all cases, the carbon dioxide gas or the air mixes with the solid toxic particulates and flows through the conical tail section which is converged to increase the velocity at its second end where the tail shear disc 73 is located. The tail shear disc 73 bursts due to the pressure of either the carbon dioxide gas and the solid toxic particulates or the air and the solid toxic particulates depending on the type of bomb used, and the mixture flows past the ruptured tail shear disc 73 and out the tail orifices 75.
The difiuser vanes 9 deflect the finely divided solid particulates coming out of the tail orifices 75 into three separate low hanging clouds for maximal efiect. Other gases can be used to disperse the solid toxic particulates, if desired. However, carbon dioxide is preferable to certain other liquifiable gases, such as ammonia, because of its inert and odorless characteristics.
It will also be obvious that various other changes can be made. We therefore wish our invention to be limited only by the following claim.
We claim:
A gas ejection bomb for dispersing solid particulates comprising an elongated casing having a first end and a second end, a nose base at said first end of said casing, a fuze mounted within said casing adjacent said nose base, said fuze defining at least one orifice communicating with the interior of said casing, a closed cylinder mounted within said casing and having an opening adjacent said fuze means, a heater tube within said cylinder, a heater primer, in a first end of said heater tube, a heater support mounted at said first end of said heater tube and within said opening, said opening having walls surrounding and contacting the exterior of said heater support, said heater support having a plurality of longitudinal fiutes on its exterior, defining with the walls of said opening a series of passages from the interior to the exterior of said cylinder, a first shear disk mounted between said fuze and said opening and closing said passages, said fuze comprising a firing pin aligned with said heater primer, liquified carbon dioxide in said cylinder surrounding said heater tube, a conical tail section at said second end of said casing having its larger end joined to said casing and having a discharge opening at its smaller end, a tail shear disk closing said discharge opening, diffuser vanes mounted over the exterior of said discharge opening, stabilizing vanes mounted on said bomb adjacent said second end of said casing, the interior of said casing being unobstructed between said orifice and said shear disk, a charge of finely divided solid material within said casing and outside said cylinder; said fuze being impact sensitive, whereby on impact said firing pin penetrates said first shear disk and ignites said primer which thereupon ignites said heater tube, vaporizing said carbon dioxide and rupturing said first shear disk, thus permitting said carbon dioxide to flow out through said passages and said orifice into the space between said casing and said cylinder and burst said second shear disk, whereupon said carbon dioxide will flow out through said discharge opening and said difiuser vanes, carrying said solids in suspension.
References Cited by the Examiner UNITED STATES PATENTS 2,001,249 8/35 Larson 102-92 2,263,585 11/41 Moore et al. 102-6 2,367,699 1/45 Summerbell 102-77 X 2,479,570 8/49 Hayner et al 222-399 X 2,559,091 7/51 Reasenberg.
2,599,728 6/52 Seaberg 222-399 X 2,812,783 11/57 Bufogle 222-399 2,821,924 2/58 Hansen et al. 102-50 BENJAMIN A. BORCHELT, Primary Examiner.
SAMUEL BOYD, ARTHUR M. HORTON, Examiners.
US735345A 1958-05-14 1958-05-14 Gas ejection bomb for dispersing solid particulates Expired - Lifetime US3188954A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US735345A US3188954A (en) 1958-05-14 1958-05-14 Gas ejection bomb for dispersing solid particulates

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US735345A US3188954A (en) 1958-05-14 1958-05-14 Gas ejection bomb for dispersing solid particulates

Publications (1)

Publication Number Publication Date
US3188954A true US3188954A (en) 1965-06-15

Family

ID=24955381

Family Applications (1)

Application Number Title Priority Date Filing Date
US735345A Expired - Lifetime US3188954A (en) 1958-05-14 1958-05-14 Gas ejection bomb for dispersing solid particulates

Country Status (1)

Country Link
US (1) US3188954A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3496867A (en) * 1965-10-13 1970-02-24 Gilmour C Macdonald Thermal radiation weapon
US3596603A (en) * 1966-09-12 1971-08-03 Us Navy Method of dispersing bw/cw or other materials
US3596602A (en) * 1966-09-12 1971-08-03 William A Gey Distributed explosives agent dispersal system
FR2598215A1 (en) * 1986-05-05 1987-11-06 Luchaire Sa Exercise ammunition
BE1000567A4 (en) * 1987-05-19 1989-02-07 Luchaire Sa Firearms training practice round - has chambers containing powdered talc and inert gas to provide visibility on impact or detonation
US5069134A (en) * 1990-06-08 1991-12-03 Def-Tec Corporation Flameless expulsion grenade
US6349650B1 (en) * 2000-08-29 2002-02-26 Michael Brunn Launchable flameless expulsion grenade
US20070031770A1 (en) * 2005-08-08 2007-02-08 Vincent Montefusco Fireball generator
US20080202371A1 (en) * 2007-02-26 2008-08-28 Vincent Montefusco Fireball generator
US9423225B1 (en) * 2015-09-10 2016-08-23 The United States Of America As Represented By The Secretary Of The Army Non-pyrotechnic, non-lethal compressed gas disseminator

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2001249A (en) * 1934-04-13 1935-05-14 Price M Greenlaw Blow-off tank for steam boilers
US2263585A (en) * 1938-06-07 1941-11-25 Harry H Moore Float light and smoke bomb
US2367699A (en) * 1942-04-20 1945-01-23 Summerbell William Fuse
US2479570A (en) * 1945-02-24 1949-08-23 Thomas R Hayner Fluid projector
US2559091A (en) * 1945-12-01 1951-07-03 Mizzy Inc Method and solution for producing insecticidal aerosols
US2599728A (en) * 1948-12-03 1952-06-10 Carnoy Products Corp Fire extinguisher nozzle
US2812783A (en) * 1954-10-28 1957-11-12 Quentin C Bufogle Device for injecting chemicals into vehicle tires and the like
US2821924A (en) * 1954-07-09 1958-02-04 Lawrence J Hansen Fin stabilized projectile

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2001249A (en) * 1934-04-13 1935-05-14 Price M Greenlaw Blow-off tank for steam boilers
US2263585A (en) * 1938-06-07 1941-11-25 Harry H Moore Float light and smoke bomb
US2367699A (en) * 1942-04-20 1945-01-23 Summerbell William Fuse
US2479570A (en) * 1945-02-24 1949-08-23 Thomas R Hayner Fluid projector
US2559091A (en) * 1945-12-01 1951-07-03 Mizzy Inc Method and solution for producing insecticidal aerosols
US2599728A (en) * 1948-12-03 1952-06-10 Carnoy Products Corp Fire extinguisher nozzle
US2821924A (en) * 1954-07-09 1958-02-04 Lawrence J Hansen Fin stabilized projectile
US2812783A (en) * 1954-10-28 1957-11-12 Quentin C Bufogle Device for injecting chemicals into vehicle tires and the like

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3496867A (en) * 1965-10-13 1970-02-24 Gilmour C Macdonald Thermal radiation weapon
US3596603A (en) * 1966-09-12 1971-08-03 Us Navy Method of dispersing bw/cw or other materials
US3596602A (en) * 1966-09-12 1971-08-03 William A Gey Distributed explosives agent dispersal system
FR2598215A1 (en) * 1986-05-05 1987-11-06 Luchaire Sa Exercise ammunition
BE1000567A4 (en) * 1987-05-19 1989-02-07 Luchaire Sa Firearms training practice round - has chambers containing powdered talc and inert gas to provide visibility on impact or detonation
US5069134A (en) * 1990-06-08 1991-12-03 Def-Tec Corporation Flameless expulsion grenade
US6349650B1 (en) * 2000-08-29 2002-02-26 Michael Brunn Launchable flameless expulsion grenade
US20070031770A1 (en) * 2005-08-08 2007-02-08 Vincent Montefusco Fireball generator
US7543533B2 (en) * 2005-08-08 2009-06-09 Vincent Montefusco Fireball generator
US20080202371A1 (en) * 2007-02-26 2008-08-28 Vincent Montefusco Fireball generator
US7487726B2 (en) * 2007-02-26 2009-02-10 Vincent Montefusco Fireball generator
US9423225B1 (en) * 2015-09-10 2016-08-23 The United States Of America As Represented By The Secretary Of The Army Non-pyrotechnic, non-lethal compressed gas disseminator

Similar Documents

Publication Publication Date Title
US4714020A (en) Enabling device for a gas generator of a forced dispersion munitions dispenser
US2627160A (en) Rocket igniter
US3055300A (en) Rocket flare head
US3911823A (en) Pyrotechnic devices
US3188954A (en) Gas ejection bomb for dispersing solid particulates
US3137231A (en) Chaff dispenser system
US2856851A (en) Apparatus for zoning rockets
GB960178A (en) Ammunition projectile
US4132169A (en) Fuel-air type bomb
US3712224A (en) Decoy flare with traveling ignition charge
US4195572A (en) Pressurized projectile for delivering and dispensing liquids or particulates
US4157928A (en) Method for fuel air explosive
US2271280A (en) Gas producing projectile
US2592623A (en) Primer assembly for artillery ammunition
US4141294A (en) Fuel-air type bomb
US2457839A (en) Rocket
US4353303A (en) Projectile for dispensing gaseous material
US2454281A (en) Antipersonnel artillery mine
US1316607A (en) Detonator for projectiles
US3946672A (en) Rocket propelled projectile
US3994226A (en) Flueric explosive initiation device for a fuel-air explosive bomb
USH699H (en) Submunition fuse with pyrotechnic ignition
US2730046A (en) Safety device for the explosive head of a missile
US4526105A (en) Firing mechanism for projectiles
KR940004649B1 (en) Shotgun cartridge with explosive shell