US20020011173A1 - Pyrotechnic impact fuse - Google Patents
Pyrotechnic impact fuse Download PDFInfo
- Publication number
- US20020011173A1 US20020011173A1 US09/915,788 US91578801A US2002011173A1 US 20020011173 A1 US20020011173 A1 US 20020011173A1 US 91578801 A US91578801 A US 91578801A US 2002011173 A1 US2002011173 A1 US 2002011173A1
- Authority
- US
- United States
- Prior art keywords
- explosive
- cavities
- impact fuse
- impact
- pyrotechnic
- 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.)
- Abandoned
Links
- 239000002360 explosive Substances 0.000 claims abstract description 35
- 238000010304 firing Methods 0.000 claims description 10
- TZRXHJWUDPFEEY-UHFFFAOYSA-N Pentaerythritol Tetranitrate Chemical compound [O-][N+](=O)OCC(CO[N+]([O-])=O)(CO[N+]([O-])=O)CO[N+]([O-])=O TZRXHJWUDPFEEY-UHFFFAOYSA-N 0.000 claims description 4
- 229920006329 Styropor Polymers 0.000 claims description 3
- 238000005266 casting Methods 0.000 claims description 2
- 239000011521 glass Substances 0.000 claims description 2
- 238000000465 moulding Methods 0.000 claims description 2
- 229920003023 plastic Polymers 0.000 claims description 2
- 239000004033 plastic Substances 0.000 claims description 2
- 229920002635 polyurethane Polymers 0.000 claims description 2
- 239000004814 polyurethane Substances 0.000 claims description 2
- -1 ocfol Chemical compound 0.000 claims 1
- XTFIVUDBNACUBN-UHFFFAOYSA-N 1,3,5-trinitro-1,3,5-triazinane Chemical compound [O-][N+](=O)N1CN([N+]([O-])=O)CN([N+]([O-])=O)C1 XTFIVUDBNACUBN-UHFFFAOYSA-N 0.000 claims 1
- UPSVYNDQEVZTMB-UHFFFAOYSA-N 2-methyl-1,3,5-trinitrobenzene;1,3,5,7-tetranitro-1,3,5,7-tetrazocane Chemical compound CC1=C([N+]([O-])=O)C=C([N+]([O-])=O)C=C1[N+]([O-])=O.[O-][N+](=O)N1CN([N+]([O-])=O)CN([N+]([O-])=O)CN([N+]([O-])=O)C1 UPSVYNDQEVZTMB-UHFFFAOYSA-N 0.000 claims 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims 1
- 229910002804 graphite Inorganic materials 0.000 claims 1
- 239000010439 graphite Substances 0.000 claims 1
- 230000035945 sensitivity Effects 0.000 abstract description 3
- 238000005474 detonation Methods 0.000 description 7
- AGUIVNYEYSCPNI-UHFFFAOYSA-N N-methyl-N-picrylnitramine Chemical group [O-][N+](=O)N(C)C1=C([N+]([O-])=O)C=C([N+]([O-])=O)C=C1[N+]([O-])=O AGUIVNYEYSCPNI-UHFFFAOYSA-N 0.000 description 2
- 239000011888 foil Substances 0.000 description 2
- 230000000977 initiatory effect Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000004411 aluminium Substances 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 239000012634 fragment Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000009527 percussion Methods 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C1/00—Impact fuzes, i.e. fuzes actuated only by ammunition impact
- F42C1/10—Impact fuzes, i.e. fuzes actuated only by ammunition impact without firing-pin
Definitions
- the invention concerns a pyrotechnic impact fuse as set forth in the classifying portion of claim 1.
- a pyrotechnic percussion or impact fuse is known from DE 196 51 169 A1. Disposed in a ballistic cap of a high explosive shell on a so-called anvil is a secondary explosive 28 which is commercially available but which is made especially fireable or detonatable. That secondary explosive is not defined in greater detail.
- the object of the invention is to propose an explosive which explodes upon impact on a target.
- the impact detonating or firing means is a conventional explosive but with uniformly distributed, defined cavities. Due to those cavities of a diameter of from 0.2 -1.2 mm, the sensitivity of the explosive is below the sensitivity of tetryl. Tetryl is referred to as a secondary explosive and does not require any special mechanical safety means, as is required in the case of conventional explosive, fitted in fuses.
- the cavities in the primary explosive are defined in a simple manner by glass balls, styropor balls, addition of polyurethane, the addition of gas in the casting or moulding procedure or by virtue of bores which are disposed transversely with respect to the main axis of the explosive body.
- the invention is based on the operative principle that, upon impact of the projectile, shock wave initiation of explosive occurs due to imploding pores or cavities in the explosive mixture.
- FIG. 1 is a view in longitudinal section of a high explosive shell
- FIG. 2 is a phase illustration
- FIG. 3 is a simplified view of an explosive charge.
- a high explosive shell 1 comprises a casing 2 with a guide band 3 , a base-screw 4 , a main charge 5 of explosive and a cap 6 .
- the cap 6 and an anvil 7 are connected to a screw threaded ring 8 on the shell side.
- the anvil 7 has a plurality of firing or detonation passages 10 . They connect a space 11 at the cap side, to a conical recess 12 of the anvil 7 .
- the firing passages 10 are closed by foils 9 of metal such as aluminium.
- a structured explosive 13 , 15 of PETN, nitropenta, with cavities 16 is disposed in the space 11 and likewise the conical recess 12 .
- a conventional explosive can also be arranged in the recess 12 .
- the cavities 16 are defined by suitable bodies of styropor.
- FIG. 2 shows the firing or detonation progression of the explosive 13 which is structured in accordance with the invention, upon on-target impact 17 of the shell 1 .
- a shockwave 20 which is shown by way of example produces firing or detonation potentials 21 in the phase 1 which is identified by reference 22 , in the structured explosive 13 , and causes partial firing 17 in the cavities 16 , due to shockwave initiation.
- phase 2 see reference numeral 23 , the fire sources 17 . 1 have expanded and form a detonation front 25 which extends in the space 11 , see also FIG. 1.
- a test body 30 of PHX, plastic-bound explosive has bores 32 which are disposed transversely with respect to its longitudinal axis 31 . Conversion of the explosive into detonation energy occurs in the direction of the arrow 33 . That takes place in the same manner as described with reference to FIG. 2.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
Abstract
An explosive having cavities (16) is proposed for a pyrotechnic impact fuse (100) for high explosive shells (1). The sensitivity of the explosive lies in the class of secondary explosives, due to the cavities (16). Mechanical safety means can therefore be eliminated.
Description
- The invention concerns a pyrotechnic impact fuse as set forth in the classifying portion of
claim 1. - A pyrotechnic percussion or impact fuse is known from DE 196 51 169 A1. Disposed in a ballistic cap of a high explosive shell on a so-called anvil is a secondary explosive 28 which is commercially available but which is made especially fireable or detonatable. That secondary explosive is not defined in greater detail.
- There the object of the invention is to propose an explosive which explodes upon impact on a target.
- That object is attained in accordance with
claim 1. - Advantageous developments of the invention are set forth in the appendant claims.
- In accordance with the invention, the impact detonating or firing means is a conventional explosive but with uniformly distributed, defined cavities. Due to those cavities of a diameter of from 0.2 -1.2 mm, the sensitivity of the explosive is below the sensitivity of tetryl. Tetryl is referred to as a secondary explosive and does not require any special mechanical safety means, as is required in the case of conventional explosive, fitted in fuses.
- The cavities in the primary explosive are defined in a simple manner by glass balls, styropor balls, addition of polyurethane, the addition of gas in the casting or moulding procedure or by virtue of bores which are disposed transversely with respect to the main axis of the explosive body.
- The invention is based on the operative principle that, upon impact of the projectile, shock wave initiation of explosive occurs due to imploding pores or cavities in the explosive mixture.
- Embodiments of the invention are described hereinafter and illustrated in the drawing in which:
- FIG. 1 is a view in longitudinal section of a high explosive shell, FIG. 2 is a phase illustration, and FIG. 3 is a simplified view of an explosive charge.
- Referring to FIG. 1, a high
explosive shell 1 comprises acasing 2 with aguide band 3, a base-screw 4, amain charge 5 of explosive and acap 6. - The
cap 6 and an anvil 7 are connected to a screw threadedring 8 on the shell side. - The anvil 7 has a plurality of firing or
detonation passages 10. They connect aspace 11 at the cap side, to aconical recess 12 of the anvil 7. - The
firing passages 10 are closed byfoils 9 of metal such as aluminium. - A structured explosive 13, 15 of PETN, nitropenta, with
cavities 16, is disposed in thespace 11 and likewise theconical recess 12. A conventional explosive can also be arranged in therecess 12. Thecavities 16 are defined by suitable bodies of styropor. - FIG. 2 shows the firing or detonation progression of the explosive 13 which is structured in accordance with the invention, upon on-
target impact 17 of theshell 1. - A
shockwave 20 which is shown by way of example produces firing ordetonation potentials 21 in thephase 1 which is identified byreference 22, in the structured explosive 13, and causespartial firing 17 in thecavities 16, due to shockwave initiation. - In
phase 2, seereference numeral 23, the fire sources 17.1 have expanded and form adetonation front 25 which extends in thespace 11, see also FIG. 1. - When the
detonation front 25 reaches thefoils 9 at thefiring passages 10, the procedure then involves firing through to theexplosive charge 15 in theconical recess 12. That then causes detonation of themain charge 5 which breaks up thecasing 2 into fragments (not shown). - As shown in FIG. 3, a
test body 30 of PHX, plastic-bound explosive, hasbores 32 which are disposed transversely with respect to itslongitudinal axis 31. Conversion of the explosive into detonation energy occurs in the direction of thearrow 33. That takes place in the same manner as described with reference to FIG. 2. - All military explosives are suitable as the explosives.
Claims (3)
1. A pyrotechnic impact fuse (100) for high explosive shells and shells with an impact function with a pyrotechnic firing means (13) in a cap (6), and an explosive charge (5) for breaking up the shell (1), wherein the firing means (13) surrounds an anvil (7) at the shell side, characterised in that a mouldable or pressable explosive has uniformly distributed, defined cavities (16; 32) of a diameter of 0.2 to 1.2 mm.
2. An impact fuse according to claim 1 characterised in that suitable explosives are
HWC, hexogen, wax graphite,
ocfol,
octol,
PHX, plastic-bound explosive, or
PETN, nitropenta.
3. An impact fuse according to claim 1 characterised in that the cavities (16) are defined by glass balls, styropor bodies, the addition of polyurethane, the supply of gas in the casting or moulding operation or by means of bores (32) which are disposed transversely with respect to the axis (31) of the explosive body (30).
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE10036815.8 | 2000-07-28 | ||
| DE10036815A DE10036815A1 (en) | 2000-07-28 | 2000-07-28 | Pyrotechnic impact detonator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20020011173A1 true US20020011173A1 (en) | 2002-01-31 |
Family
ID=7650541
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US09/915,788 Abandoned US20020011173A1 (en) | 2000-07-28 | 2001-07-26 | Pyrotechnic impact fuse |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US20020011173A1 (en) |
| DE (1) | DE10036815A1 (en) |
| NO (1) | NO20013693L (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2845765A1 (en) * | 2002-10-12 | 2004-04-16 | Diehl Munitionssysteme Gmbh | Fuseless rifled projectile comprises sleeve, end section with base thread, front section, collar and inner operational member |
| US20110146520A1 (en) * | 2008-06-16 | 2011-06-23 | Rheinmetall Waffe Munition Gmbh | Flare with flare ignition and ejector mechanism for the same |
| US20110174182A1 (en) * | 2008-06-16 | 2011-07-21 | Rheinmetall Waffe Munition Gmbh | Activation unit for munition-free decoys |
| US20120160121A1 (en) * | 2009-06-26 | 2012-06-28 | Rheinmetall Waffle Munition GmbH | Active body |
| US8714089B2 (en) | 2009-05-08 | 2014-05-06 | Rheinmetall Waffe Munition Gmbh | Activation unit for explosive masses or explosive bodies |
| US8763533B2 (en) | 2009-06-26 | 2014-07-01 | Rheinmetall Waffe Munition Gmbh | Active body |
| US20170287468A1 (en) * | 2015-08-31 | 2017-10-05 | Cloudminds (Shenzhen) Technologies Co., Ltd. | Method and device for processing received sound and memory medium, mobile terminal, robot having the same |
| US10502537B1 (en) * | 2017-10-20 | 2019-12-10 | The United States Of America As Represented By The Secretary Of The Army | Enhanced terminal performance medium caliber multipurpose traced self-destruct projectile |
| RU2769553C1 (en) * | 2021-07-29 | 2022-04-04 | Умар Хамидович Булатов | Heat-resistant shaped charge |
| CN114777584A (en) * | 2022-02-16 | 2022-07-22 | 南京理工大学 | Triggering fuse high-sensitivity impact fire cap containing heterogeneous sensitizer |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| BE520143A (en) * | 1952-07-09 | |||
| GB1271704A (en) * | 1969-10-13 | 1972-04-26 | Raufoss Ammunisjonsfabrikker | Projectile with multiple effect |
| DE19651169A1 (en) * | 1996-12-10 | 1998-06-18 | Diehl Gmbh & Co | Lock for pyrotechnic impact igniter of ballistic explosive round |
-
2000
- 2000-07-28 DE DE10036815A patent/DE10036815A1/en not_active Withdrawn
-
2001
- 2001-07-26 US US09/915,788 patent/US20020011173A1/en not_active Abandoned
- 2001-07-27 NO NO20013693A patent/NO20013693L/en unknown
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2845765A1 (en) * | 2002-10-12 | 2004-04-16 | Diehl Munitionssysteme Gmbh | Fuseless rifled projectile comprises sleeve, end section with base thread, front section, collar and inner operational member |
| US20110146520A1 (en) * | 2008-06-16 | 2011-06-23 | Rheinmetall Waffe Munition Gmbh | Flare with flare ignition and ejector mechanism for the same |
| US20110174182A1 (en) * | 2008-06-16 | 2011-07-21 | Rheinmetall Waffe Munition Gmbh | Activation unit for munition-free decoys |
| US8770109B2 (en) | 2008-06-16 | 2014-07-08 | Rheinmetall Waffe Munition Gmbh | Flare with flare ignition and ejector mechanism for the same |
| US8695504B2 (en) | 2008-06-16 | 2014-04-15 | Rheinmetall Waffe Munition Gmbh | Activation unit for munition-free decoys |
| US8714089B2 (en) | 2009-05-08 | 2014-05-06 | Rheinmetall Waffe Munition Gmbh | Activation unit for explosive masses or explosive bodies |
| US20120160121A1 (en) * | 2009-06-26 | 2012-06-28 | Rheinmetall Waffle Munition GmbH | Active body |
| US8763533B2 (en) | 2009-06-26 | 2014-07-01 | Rheinmetall Waffe Munition Gmbh | Active body |
| US8689693B2 (en) * | 2009-06-26 | 2014-04-08 | Rheinmetall Waffe Munition Gmbh | Active body |
| US20170287468A1 (en) * | 2015-08-31 | 2017-10-05 | Cloudminds (Shenzhen) Technologies Co., Ltd. | Method and device for processing received sound and memory medium, mobile terminal, robot having the same |
| US10502537B1 (en) * | 2017-10-20 | 2019-12-10 | The United States Of America As Represented By The Secretary Of The Army | Enhanced terminal performance medium caliber multipurpose traced self-destruct projectile |
| RU2769553C1 (en) * | 2021-07-29 | 2022-04-04 | Умар Хамидович Булатов | Heat-resistant shaped charge |
| CN114777584A (en) * | 2022-02-16 | 2022-07-22 | 南京理工大学 | Triggering fuse high-sensitivity impact fire cap containing heterogeneous sensitizer |
Also Published As
| Publication number | Publication date |
|---|---|
| NO20013693D0 (en) | 2001-07-27 |
| NO20013693L (en) | 2002-01-29 |
| DE10036815A1 (en) | 2002-02-07 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: DIEHL MUNITIONSSYSTEME GMBH & CO. KG, GERMANY Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:SCHILDKNECHT, MANFRED;RUDOLF, KARL;STRAUSS, HANS;AND OTHERS;REEL/FRAME:012030/0734;SIGNING DATES FROM 20010611 TO 20010709 |
|
| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |