US3311055A - Toroidal booster with cylindrically symmetrical output - Google Patents

Toroidal booster with cylindrically symmetrical output Download PDF

Info

Publication number
US3311055A
US3311055A US451699A US45169965A US3311055A US 3311055 A US3311055 A US 3311055A US 451699 A US451699 A US 451699A US 45169965 A US45169965 A US 45169965A US 3311055 A US3311055 A US 3311055A
Authority
US
United States
Prior art keywords
booster
explosive
lengths
toroidal
metal cased
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
US451699A
Inventor
Jr Richard H Stresau
Raymond L Degner
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 US451699A priority Critical patent/US3311055A/en
Application granted granted Critical
Publication of US3311055A publication Critical patent/US3311055A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • F42C19/0846Arrangements of a multiplicity of primers or detonators, dispersed within a warhead, for increased efficiency
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S102/00Ammunition and explosives
    • Y10S102/701Charge wave forming

Definitions

  • the present invention relates to explosives and more particularly to an improved booster which will initiate a cylindrical symmetrical detonation wave.
  • booster applications call for a symmetrical detonation wave in order to produce the desired fragmentation patterns.
  • the booster will initiate a cylindrically symmetrical detonation Wave although the booster has a central hole through which inert components such as electrical initiators, control wires and cables can be passed.
  • a Mild Detonating Fuze distribution system is used to induce multiple point simultaneous initiation of the main booster charge.
  • Another object of the invention is to provide an improved booster for producing a cylindrically symmetrical output.
  • a further object of the invention is to provide an improved explosive initiator system using a plurality of equal-length explosive paths from a common initiation point to equally distributed terminal points about the inner diameter of a toroidal shaped booster charge for initiating a cylindn'cally symmetrical detonation wave.
  • FIG. 1 is a cross-sectionalview of the toroidal booster taken along line 1-1 of FIG. 2 showing a plurality of equally distributed explosive paths.
  • FIG. 2 is a cross-sectional view of the embodiment of the invention shown in FIG. 1 taken along line 2-2.
  • An essential feature of the invention is a multiple branched distribution system of metal cased explosive 10 so arranged that the explosive paths from a common point of initiation 12 to each of several terminal points 14 are equal to each other.
  • the terminal points 14, at which the main booster charge 16 is initiated, are equally distributed in a circle close to the inner diameter of the main booster charge.
  • metal cased explosive 10 such as, for example, Mild Detonating Fuze, a product of the Du Pont Company
  • the principle of such metal cased explosive patterns is that the lengths 10 are arranged in such a pattern that there are equal length explosive paths between a single initiation point 1-2 and a plurality of output points 14.
  • the remaining spaces in grooves 20, 21 and 22 not occupied by lengths of metal cased explosive 10 are completely filled with a potting compound so that the explosive paths between initiation point 12 and points 14 are potted in a plastic resin.
  • a sub-booster charge 27, of SPX-2 for example, may be used for initiating the main booster charge 16, of CH-6 for example.
  • metal cased explosive pattern with several output leads for initiating a sub-booster explosive which in turn initiates the main booster charge has the advantage of using relatively little explosive and weight in proportion to the main booster charge.
  • metal casing, a lead sheath for example, of the metal cased explosive lengths 10 absorb and attenuate the radial output of the explosive in the lengths 10, thus reducing any undesirable effects upon the main booster charge.
  • the main booster charge 16 is initiated simultaneously at the several terminal points 14.
  • the spherically expanding detonation wave fronts join to approach a surface of revolution. This nearly symmetrical detonation wave results in more nearly ideal performance of a warhead which is initiated by such a booster.
  • both position and timing of the terminal points may be adjusted to give a wide variety.
  • a booster for initiating a symmetrical detonation wave comprising:

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Portable Nailing Machines And Staplers (AREA)

Description

March 1967 R. H. STRESAU, JR. ETAL 3,311,055
TOROIDAL BOOSTER WITH CYLINDRICALLY SYMMETRICAL OUTPUT Filed April 23, 1965 FIG. 2
RICHARD H. STRESAU, JR m RAYMOND L DEGNER INVENTOR.
W $kM ATTORNEY United Statesv Patent The present invention relates to explosives and more particularly to an improved booster which will initiate a cylindrical symmetrical detonation wave.
Many booster applications call for a symmetrical detonation wave in order to produce the desired fragmentation patterns. In the instant invention the booster will initiate a cylindrically symmetrical detonation Wave although the booster has a central hole through which inert components such as electrical initiators, control wires and cables can be passed. A Mild Detonating Fuze distribution system is used to induce multiple point simultaneous initiation of the main booster charge.
It is an object of the present invention to provide a toroidal booster system for detonation of a Warhead.
Another object of the invention is to provide an improved booster for producing a cylindrically symmetrical output.
A further object of the invention is to provide an improved explosive initiator system using a plurality of equal-length explosive paths from a common initiation point to equally distributed terminal points about the inner diameter of a toroidal shaped booster charge for initiating a cylindn'cally symmetrical detonation wave.
Other objects and many of the attendant advantages of this invention will become readily appreciated as the same becomes better understood by reference to the following detailed description When considered in connection with the accompanying drawings wherein:
FIG. 1 is a cross-sectionalview of the toroidal booster taken along line 1-1 of FIG. 2 showing a plurality of equally distributed explosive paths.
FIG. 2 is a cross-sectional view of the embodiment of the invention shown in FIG. 1 taken along line 2-2.
Referring now to the drawings, like characters refer to like parts in each of the figures.
An essential feature of the invention is a multiple branched distribution system of metal cased explosive 10 so arranged that the explosive paths from a common point of initiation 12 to each of several terminal points 14 are equal to each other. The terminal points 14, at which the main booster charge 16 is initiated, are equally distributed in a circle close to the inner diameter of the main booster charge.
Lengths of metal cased explosive 10, such as, for example, Mild Detonating Fuze, a product of the Du Pont Company, are placed in concentric grooves 20, 21 and 22, in a housing 23, of acrylic plastic for example. From initiating point 12, two lengths of metal cased explosive 10 in groove 20 lead to T-joints in groove 21. The T- joints are formed by splicing the end of one length of metal cased explosive at the center of another length of metal cased explosive. From each T-joint 25 in groove 21 lengths of metal cased explosive lead to twice as many T-joints 25 in groove 22 which again in turn lead through more lengths of metal cased explosive to terminal points 14. The principle of such metal cased explosive patterns is that the lengths 10 are arranged in such a pattern that there are equal length explosive paths between a single initiation point 1-2 and a plurality of output points 14. The remaining spaces in grooves 20, 21 and 22 not occupied by lengths of metal cased explosive 10 are completely filled with a potting compound so that the explosive paths between initiation point 12 and points 14 are potted in a plastic resin.
At output points 14, a sub-booster charge 27, of SPX-2 for example, may be used for initiating the main booster charge 16, of CH-6 for example.
A cylindrical ring 28, of plastic for example, forms the inner wall of the toroidal booster housing. An outer cylindrical tubing ring 29, of aluminum for example, forms the outer wall of the booster. This wall is crimped over outer plates 30 and 31 of the booster.
The use of a metal cased explosive pattern with several output leads for initiating a sub-booster explosive which in turn initiates the main booster charge has the advantage of using relatively little explosive and weight in proportion to the main booster charge. In addition, the metal casing, a lead sheath for example, of the metal cased explosive lengths 10 absorb and attenuate the radial output of the explosive in the lengths 10, thus reducing any undesirable effects upon the main booster charge.
Because of the equal path lengths and the uniform detonation rate of the metal cased explosive 10, the main booster charge 16 is initiated simultaneously at the several terminal points 14. The spherically expanding detonation wave fronts join to approach a surface of revolution. This nearly symmetrical detonation wave results in more nearly ideal performance of a warhead which is initiated by such a booster.
If other wave front configurations are desired, both position and timing of the terminal points may be adjusted to give a wide variety.
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.
What is claimed is:
A booster for initiating a symmetrical detonation wave, comprising:
(a) a toroidal housing having a chamber therein,
(b) a main booster charge in said chamber,
(c) an annular sub-booster charge adjacent said booster charge,
((1) a plurality of concentric ring shaped grooves in a wall of said housing,
(e) said grooves being connected by passageways therebetween,
(f) a plurality of metal cased explosive lengths in said concentric grooves to form explosive paths, all remaining space in said grooves and passages not occupied by said lengths of metal cased explosive being completely filled with a potting compound thus potting the explosive paths,
(g) a common point of initiation in the outermost of said concentric grooves at which one end of each of a first pair of said metal cased explosive lengths are initiated,
(h) the other ends of said first pair of metal cased explosive lengths passing through the passageways between the outermost concentric groove into the next inner groove,
(i) said other ends being spliced to other lengths of metal cased explosive midway along their length in said next inner groove forming a T-junction of metal cased explosive,
(j) the end of said other lengths of metal cased explosive in turn passing through the passageways to following inner grooves in turn and also in turn being spliced at T-junctions to the lengths of metal cased explosive in the innermost concentric groove terminating at a plurality of output points symmetrically positioned about and opening onto said of the explosive therein on detonation thus reducing sub-booster charge, any undesirable eifects upon the booster charge, on (k) said spliced lengths of metal cased explosive forrndetonation of said main booster spherically expanding a plurality of equal length paths from said coming detonation wave fronts join to approach a cylinmon point of initiation to said plurality of output 5 drically symmetrical detonation Wave.
points for initiating said sub-booster charge simultaneously at each of said plurality of output points, References Cited y the Examiner saidi metal tcased explosivte lengths detonatilng at a UNITED STATES PATENTS uni orm ra e upon initia ion causlng sirnu taneous multiple point detonation of said sub-booster which 10 2 22 pi 1O2 85'2 in turn uniformly detonates said main booster charge, 9 ac e0 102M70 said metal cased explosive lengths and sub-booster 3 23131 33 using relatively little explosive and Weight in proportion to said main booster charge, (1) said metal casing of the metal cased explosive r BENJAMIN BORCHELT P'lmary Exammer' 0 lengths absorbing and attenuating the radial output V. R. PENDEGRASS, Assistant Examiner.
US451699A 1965-04-23 1965-04-23 Toroidal booster with cylindrically symmetrical output Expired - Lifetime US3311055A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US451699A US3311055A (en) 1965-04-23 1965-04-23 Toroidal booster with cylindrically symmetrical output

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US451699A US3311055A (en) 1965-04-23 1965-04-23 Toroidal booster with cylindrically symmetrical output

Publications (1)

Publication Number Publication Date
US3311055A true US3311055A (en) 1967-03-28

Family

ID=23793354

Family Applications (1)

Application Number Title Priority Date Filing Date
US451699A Expired - Lifetime US3311055A (en) 1965-04-23 1965-04-23 Toroidal booster with cylindrically symmetrical output

Country Status (1)

Country Link
US (1) US3311055A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3430564A (en) * 1967-05-03 1969-03-04 Us Navy Explosive gate,diode and switch
US3443518A (en) * 1967-09-26 1969-05-13 Donald W Cross Multi-point ignition system for shaped charges
US3496868A (en) * 1967-05-29 1970-02-24 Us Navy Explosive elements
US3680054A (en) * 1970-07-06 1972-07-25 Ibm Input/output channel
US3847080A (en) * 1971-02-22 1974-11-12 R Eckels Remote rock breaking method apparatus therefor
US3896731A (en) * 1970-09-22 1975-07-29 Us Navy Explosive initiator device
US4430939A (en) * 1980-11-19 1984-02-14 Gordon Harrold Linear shaped charges
US4510870A (en) * 1981-07-27 1985-04-16 The United States Of America As Represented By The Secretary Of The Army Charge liner construction and method
EP0255130A1 (en) * 1986-07-31 1988-02-03 DIEHL GMBH & CO. Ignition for a hollow charge
EP0310160A1 (en) * 1987-09-30 1989-04-05 FABRIQUE NATIONALE HERSTAL en abrégé FN Société Anonyme Anti-vehicle grenade
US9303966B1 (en) 2015-01-29 2016-04-05 The United States Of America As Represented By The Secretary Of The Navy Symmetical initiation distributor for use in explosive detonation trains with an offset orientation

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US830948A (en) * 1905-12-01 1906-09-11 Krupp Ag Burning time-fuse.
US2774306A (en) * 1951-11-06 1956-12-18 Norman A Macleod Means for initiating explosion
US2982210A (en) * 1958-06-25 1961-05-02 Ensign Bickford Co Connecting cord
US3170402A (en) * 1956-10-16 1965-02-23 Harold S Morton Equal length detonating cords for warhead detonation

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US830948A (en) * 1905-12-01 1906-09-11 Krupp Ag Burning time-fuse.
US2774306A (en) * 1951-11-06 1956-12-18 Norman A Macleod Means for initiating explosion
US3170402A (en) * 1956-10-16 1965-02-23 Harold S Morton Equal length detonating cords for warhead detonation
US2982210A (en) * 1958-06-25 1961-05-02 Ensign Bickford Co Connecting cord

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3430564A (en) * 1967-05-03 1969-03-04 Us Navy Explosive gate,diode and switch
US3496868A (en) * 1967-05-29 1970-02-24 Us Navy Explosive elements
US3443518A (en) * 1967-09-26 1969-05-13 Donald W Cross Multi-point ignition system for shaped charges
US3680054A (en) * 1970-07-06 1972-07-25 Ibm Input/output channel
US3896731A (en) * 1970-09-22 1975-07-29 Us Navy Explosive initiator device
US3847080A (en) * 1971-02-22 1974-11-12 R Eckels Remote rock breaking method apparatus therefor
US4430939A (en) * 1980-11-19 1984-02-14 Gordon Harrold Linear shaped charges
US4510870A (en) * 1981-07-27 1985-04-16 The United States Of America As Represented By The Secretary Of The Army Charge liner construction and method
EP0255130A1 (en) * 1986-07-31 1988-02-03 DIEHL GMBH & CO. Ignition for a hollow charge
EP0310160A1 (en) * 1987-09-30 1989-04-05 FABRIQUE NATIONALE HERSTAL en abrégé FN Société Anonyme Anti-vehicle grenade
BE1000944A3 (en) * 1987-09-30 1989-05-23 Nat Herstal Fn Sa Fab Granada anti-char.
AU603931B2 (en) * 1987-09-30 1990-11-29 Fn Herstal Anti-vehicle grenade
US9303966B1 (en) 2015-01-29 2016-04-05 The United States Of America As Represented By The Secretary Of The Navy Symmetical initiation distributor for use in explosive detonation trains with an offset orientation

Similar Documents

Publication Publication Date Title
US3311055A (en) Toroidal booster with cylindrically symmetrical output
US3724383A (en) Lasser stimulated ordnance initiation device
CA1251541A (en) Electronic explosive delay igniter
US3853059A (en) Configured blast fragmentation warhead
US3896731A (en) Explosive initiator device
US4658727A (en) Selectable initiation-point fragment warhead
US3796159A (en) Explosive fisheye lens warhead
US3820461A (en) Initiation aimed explosive devices
US3170402A (en) Equal length detonating cords for warhead detonation
US4145972A (en) Dual-mode warhead initiation system
US3332350A (en) Electric blasting cap having heatshrinkable plastic-covered match assembly
US3831523A (en) Electroexplosive device
US3973499A (en) Safe rocket motor igniter using sequenced initiation to an explosive logic network
US3714897A (en) Directed warhead
US3326125A (en) Sequenced initiation-a technique for explosive wave shaping
US5359935A (en) Detonator device and method for making same
US4291624A (en) Explosive charges
US3021786A (en) Blasting device
US2464181A (en) Rocket device
US3264990A (en) Focused exploding bridge wire
GB1152173A (en) Improvements in Apparatus for Perforating the Casings of Cased Wells
US4282814A (en) Dual-end warhead initiation system
US3180263A (en) Static electricity desensitizing device
CN212458148U (en) One-rotation multi-explosion transfer connecting device
GB2065840A (en) Detonator