US3713392A - Explosive lead plug - Google Patents

Explosive lead plug Download PDF

Info

Publication number
US3713392A
US3713392A US00113866A US3713392DA US3713392A US 3713392 A US3713392 A US 3713392A US 00113866 A US00113866 A US 00113866A US 3713392D A US3713392D A US 3713392DA US 3713392 A US3713392 A US 3713392A
Authority
US
United States
Prior art keywords
channel
fuse
charge
explosive
extension
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
US00113866A
Inventor
K Parsons
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.)
US Department of Navy
Original Assignee
US Department of Navy
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 US Department of Navy filed Critical US Department of Navy
Application granted granted Critical
Publication of US3713392A publication Critical patent/US3713392A/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
    • F42B12/52Fuel-air explosive devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C19/00Details of fuzes
    • F42C19/08Primers; Detonators
    • F42C19/0838Primers or igniters for the initiation or the explosive charge in a warhead

Definitions

  • the channel is small on one end and large on the other end.
  • the small end is adjacent a fuse and the large end is adjacent a burster U.S. ..102/70, charge p detonation of the explosive material in [51] IIBLCI ..F42b 3/10 the channel, the Sma" end is sealed closed due to Fleld of Search 1 metal flow, thus preventing a backfire of the burster charge through the small end.
  • FAS fuel-air explosive
  • liquid fuel disperse into a large fuel-air cloud, Le. a cloud formed of a mixture of fuel and air, of a pancake configuration.
  • a proper fuel-air mixture result prior to detonation.
  • the present invention prevents backfire of the central burster tube by forming an extension of the fuse used to detonate the central burster tube. After the ignition passes from the fuse, through the extension and into the burster tube, the extension seals itself at the fuse end due to metal flow, thus preventing a backfire.
  • FIG. 1 shows the invention and its environment in cross-section.
  • FIG. 2 shows the invention in perspective.
  • FIG. 3 shows in cross-section the invention after detonation.
  • FIG. 1 shows a fuel-air explosive device 10.
  • a canister 12 contains a liquid fuel supply 14 surrounding a central burster charge 16.
  • the burster charge is connected to a fuse 18 through a bronze or steel fuse extension 20.
  • the fuse extension fits snugly in a round hole in the canister base 22.
  • the upper end of the fuse extension 20 is contiguous to the burster charge 16, while the lower end of the extension is contiguous to the fuse 18.
  • the fuse extension is tubular and flat on each end.
  • a channel 24 extends from one end to the other.
  • the channel is filled with an explosive material 26.
  • a signal causes the fuse to ignite.
  • the fuse causes the fuse extension explosive material 26 to detonate, thereby detonating the burster charge 16.
  • the detonation of the extension explosive material 26 also causes the extension to expand radially, thereby wedging it in place before it can be forced out by the detonation of the burster charge.
  • thf detonatitgn eria causes e of the fuse extension explosive ma metal of the extension to flow in such a manner as to seal the lower end of the extension as seen in FIG. 3. This prevents a backfire from the burster charge, thereby preventing a burning or premature detonation of the fuel-air cloud.
  • fuse extension means situated between and contiguous said charge and said fuse
  • said extension means comprising:
  • tubular body of flowable metal having a channel extending therethrough and communicating said charge with said fuse

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Dispersion Chemistry (AREA)
  • Combustion & Propulsion (AREA)
  • Feeding And Controlling Fuel (AREA)

Abstract

A metal fuse extension with an explosive-filled channel passing through it. The channel is small on one end and large on the other end. The small end is adjacent a fuse and the large end is adjacent a burster charge. Upon detonation of the explosive material in the channel, the small end is sealed closed due to metal flow, thus preventing a backfire of the burster charge through the small end.

Description

United States Patent 11 1 Parsons 1 1 Jan. 30, 1973 s41 EXPLOSIVE LEAD PLUG 3,260,202 7/1966 Bryla ..102/27 3,326,l27 6 I967 S h' l ..l02 27 1 lnvemo" Kenneth Parsons, clumbla 3,572,246 311971 1121:3321 "102427 Heights, Minn. [73] Assignee: The United States of America as Q 'T F Pendegrass represented by the Secretary of the "amey et Navy 57 ABSTRACT [22] Filed: 1971 A metal fuse extension with an explosive-filled chan- [21] Appl. No.: 113,866 nel passing through it. The channel is small on one end and large on the other end. The small end is adjacent a fuse and the large end is adjacent a burster U.S. ..102/70, charge p detonation of the explosive material in [51] IIBLCI ..F42b 3/10 the channel, the Sma" end is sealed closed due to Fleld of Search 1 metal flow, thus preventing a backfire of the burster charge through the small end. [56] References Cited 2 Claims, 3 Drawing Figures UNITED STATES PATENTS 3,238,876 3/1966 Allen ..l02/70 PATENTED JAN 30 I975 I/[III/Il/lIIIIII/lIl/l/l [Ill/ 1 l I I r I I I I I l1 FIG. I.
KENNETH C. PARSONS BY ROY MILLER ATTORNEY.
EXPLOSIVE LEAD PLUG GOVERNMENT INTEREST The invention described herein may be manufactured and used by or for the government of the United 'States of America for governmental purposes without the payment of any royalties thereon or therefor.
BACKGROUND OF THE INVENTION It is common practice to drop from aircraft, canisters of fuel which are dispersed and detonated adjacent the ground by an explosive device. Intended targets may be personnel, parked aircraft, vehicles, buildings and mined land areas. A device of this type, sometimes referred to as a FAS (fuel-air explosive) canister, is disclosed in copending U.S. patent application by William A. Gey, Ser. No. 173,077, filed Feb. 13, 1962. In said application a central burster tube is employed to disperse the surrounding liquid fuel contained within the canister.
It is desired that the liquid fuel disperse into a large fuel-air cloud, Le. a cloud formed of a mixture of fuel and air, of a pancake configuration. For optimum results, it is essential that a proper fuel-air mixture result prior to detonation.
Problems have resulted where the central burster tube backfires, causing a premature detonation or a burning of the fuel.
The present invention prevents backfire of the central burster tube by forming an extension of the fuse used to detonate the central burster tube. After the ignition passes from the fuse, through the extension and into the burster tube, the extension seals itself at the fuse end due to metal flow, thus preventing a backfire.
BRIEF DESCRIPTION OF THE DRAWING FIG. 1 shows the invention and its environment in cross-section.
FIG. 2 shows the invention in perspective.
FIG. 3 shows in cross-section the invention after detonation.
DESCRIPTION OF PREFERRED EMBODIMENT FIG. 1 shows a fuel-air explosive device 10. A canister 12 contains a liquid fuel supply 14 surrounding a central burster charge 16. The burster charge is connected to a fuse 18 through a bronze or steel fuse extension 20.
The fuse extension fits snugly in a round hole in the canister base 22. The upper end of the fuse extension 20 is contiguous to the burster charge 16, while the lower end of the extension is contiguous to the fuse 18.
The fuse extension is tubular and flat on each end. A channel 24 extends from one end to the other. The channel is filled with an explosive material 26.
OPERATION As the device 10 approaches the ground, a signal causes the fuse to ignite. The fuse, in turn, causes the fuse extension explosive material 26 to detonate, thereby detonating the burster charge 16. The detonation of the extension explosive material 26 also causes the extension to expand radially, thereby wedging it in place before it can be forced out by the detonation of the burster charge More importantly, thf detonatitgn eria causes e of the fuse extension explosive ma metal of the extension to flow in such a manner as to seal the lower end of the extension as seen in FIG. 3. This prevents a backfire from the burster charge, thereby preventing a burning or premature detonation of the fuel-air cloud.
What is claimed is:
1. In an explosive device including a burster charge and a fuse, fuse extension means situated between and contiguous said charge and said fuse;
said extension means comprising:
a tubular body of flowable metal having a channel extending therethrough and communicating said charge with said fuse;
explosive material filling said channel;
a portion of said channel near the middle of said channel being conical;
the larger end of said channel being in contact with said charge;
the smaller end of said channel being in contact with said fuse;
whereby detonation of said explosive material causes said flowable metal to flow in such a manner as to seal said channel.
2. A fuse extension as set forth in claim 1 wherein said body comprises bronze.

Claims (2)

1. In an explosive device including a burster charge and a fuse, fuse extension means situated between and contiguous said charge and said fuse; said extension means comprising: a tubular body of flowable metal having a channel extending therethrough and communicating said charge with said fuse; explosive material filling said channel; a portion of said channel near the middle of said channel being conical; the larger end of said channel being in contact with said charge; the smaller end of said channel being in contact with said fuse; whereby detonation of said explosive material causes said flowable metal to flow in such a manner as to seal said channel.
1. In an explosive device including a burster charge and a fuse, fuse extension means situated between and contiguous said charge and said fuse; said extension means comprising: a tubular body of flowable metal having a channel extending therethrough and communicating said charge with said fuse; explosive material filling said channel; a portion of said channel near the middle of said channel being conical; the larger end of said channel being in contact with said charge; the smaller end of said channel being in contact with said fuse; whereby detonation of said explosive material causes said flowable metal to flow in such a manner as to seal said channel.
US00113866A 1971-02-09 1971-02-09 Explosive lead plug Expired - Lifetime US3713392A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11386671A 1971-02-09 1971-02-09

Publications (1)

Publication Number Publication Date
US3713392A true US3713392A (en) 1973-01-30

Family

ID=22351976

Family Applications (1)

Application Number Title Priority Date Filing Date
US00113866A Expired - Lifetime US3713392A (en) 1971-02-09 1971-02-09 Explosive lead plug

Country Status (1)

Country Link
US (1) US3713392A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3776135A (en) * 1972-06-29 1973-12-04 Hercules Inc Non-electric blasting cap assembly
US3789764A (en) * 1973-02-20 1974-02-05 Us Navy Explosive lead plug
US3929072A (en) * 1974-11-26 1975-12-30 Us Navy Mild detonating fuse end termination
US4038900A (en) * 1976-07-19 1977-08-02 The United States Of America As Represented By The Secretary Of The Navy Explosive closure valve
WO1986006829A1 (en) * 1985-05-04 1986-11-20 Rheinmetall Gmbh Payload spin-stabilized projectile with propelling charge
WO2018108308A1 (en) * 2016-12-16 2018-06-21 Diehl Defence Gmbh & Co. Kg Munition module, warhead, and munition
RU2746956C1 (en) * 2019-12-30 2021-04-22 Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом" (Госкорпорация "Росатом") Detonation transmission device

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3776135A (en) * 1972-06-29 1973-12-04 Hercules Inc Non-electric blasting cap assembly
US3789764A (en) * 1973-02-20 1974-02-05 Us Navy Explosive lead plug
US3929072A (en) * 1974-11-26 1975-12-30 Us Navy Mild detonating fuse end termination
US4038900A (en) * 1976-07-19 1977-08-02 The United States Of America As Represented By The Secretary Of The Navy Explosive closure valve
WO1986006829A1 (en) * 1985-05-04 1986-11-20 Rheinmetall Gmbh Payload spin-stabilized projectile with propelling charge
WO2018108308A1 (en) * 2016-12-16 2018-06-21 Diehl Defence Gmbh & Co. Kg Munition module, warhead, and munition
US10845176B2 (en) 2016-12-16 2020-11-24 Diehl Defence Gmbh & Co. Kg Munition module, warhead and munition
RU2746956C1 (en) * 2019-12-30 2021-04-22 Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом" (Госкорпорация "Росатом") Detonation transmission device

Similar Documents

Publication Publication Date Title
US20050081706A1 (en) Device for the disruption of explosive ordnance
US3720167A (en) Rotatable rocket having means for preventing flameout due to centrifugal force created during rotation thereof
GB1271704A (en) Projectile with multiple effect
GB1533685A (en) Delay detonator device
US3013495A (en) Spotter-tracer projectile
US3713392A (en) Explosive lead plug
US2742856A (en) Burster
US3570401A (en) Explosive apparatus
US4157928A (en) Method for fuel air explosive
US2843041A (en) Deep perforation of subsurface formations
US3645208A (en) Fuzeless target practice cartridge
US3021786A (en) Blasting device
US3789764A (en) Explosive lead plug
US3541961A (en) Method and apparatus for preventing premature ignition of electro-explosive devices
US2920566A (en) Tear gas bullet
US3995549A (en) Rocket/missile motor explosive insert detonator
US2294415A (en) Grenade
US4074628A (en) Fax canister with a bottom burster charge and dispersion control ring
GB259539A (en) Improvements in or relating to bombs or the like
US3638572A (en) Delay train for ordnance fuse
US4058060A (en) Gravity-deployed munition with a mechanical gravity-controlled switch
US4132170A (en) Fuel-air type bomb
US3473472A (en) Photoflash cartridge
US2595960A (en) Explosive device
US3274933A (en) Apparatus for explosive charge drilling