WO2011106803A1 - Detonator initiator - Google Patents
Detonator initiator Download PDFInfo
- Publication number
- WO2011106803A1 WO2011106803A1 PCT/ZA2011/000008 ZA2011000008W WO2011106803A1 WO 2011106803 A1 WO2011106803 A1 WO 2011106803A1 ZA 2011000008 W ZA2011000008 W ZA 2011000008W WO 2011106803 A1 WO2011106803 A1 WO 2011106803A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- tinder
- thermite
- shell
- detonator
- open
- Prior art date
Links
- 239000003999 initiator Substances 0.000 title claims abstract description 16
- 239000000203 mixture Substances 0.000 claims abstract description 42
- 239000003832 thermite Substances 0.000 claims abstract description 35
- 239000002360 explosive Substances 0.000 claims abstract description 15
- WMWLMWRWZQELOS-UHFFFAOYSA-N bismuth(iii) oxide Chemical compound O=[Bi]O[Bi]=O WMWLMWRWZQELOS-UHFFFAOYSA-N 0.000 claims abstract description 13
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 5
- 239000010703 silicon Substances 0.000 claims abstract description 4
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims abstract description 3
- 239000002245 particle Substances 0.000 claims description 20
- 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 13
- 239000004411 aluminium Substances 0.000 claims description 12
- 229910052782 aluminium Inorganic materials 0.000 claims description 12
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 12
- 239000007858 starting material Substances 0.000 claims description 9
- 230000007704 transition Effects 0.000 claims description 4
- 239000000843 powder Substances 0.000 claims description 3
- 239000000026 Pentaerythritol tetranitrate Substances 0.000 description 12
- 229960004321 pentaerithrityl tetranitrate Drugs 0.000 description 12
- 238000004455 differential thermal analysis Methods 0.000 description 5
- IWOUKMZUPDVPGQ-UHFFFAOYSA-N barium nitrate Chemical compound [Ba+2].[O-][N+]([O-])=O.[O-][N+]([O-])=O IWOUKMZUPDVPGQ-UHFFFAOYSA-N 0.000 description 4
- 230000000977 initiatory effect Effects 0.000 description 4
- 238000002844 melting Methods 0.000 description 4
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 3
- 239000005864 Sulphur Substances 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 3
- 238000004880 explosion Methods 0.000 description 3
- 230000008018 melting Effects 0.000 description 3
- 238000007254 oxidation reaction Methods 0.000 description 3
- 230000035945 sensitivity Effects 0.000 description 3
- SDGKUVSVPIIUCF-UHFFFAOYSA-N 2,6-dimethylpiperidine Chemical compound CC1CCCC(C)N1 SDGKUVSVPIIUCF-UHFFFAOYSA-N 0.000 description 2
- PEDCQBHIVMGVHV-UHFFFAOYSA-N Glycerine Chemical compound OCC(O)CO PEDCQBHIVMGVHV-UHFFFAOYSA-N 0.000 description 2
- ATUOYWHBWRKTHZ-UHFFFAOYSA-N Propane Chemical compound CCC ATUOYWHBWRKTHZ-UHFFFAOYSA-N 0.000 description 2
- 239000000470 constituent Substances 0.000 description 2
- 238000004200 deflagration Methods 0.000 description 2
- 238000005474 detonation Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000011835 investigation Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000002105 nanoparticle Substances 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000000274 aluminium melt Substances 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 150000001553 barium compounds Chemical class 0.000 description 1
- 238000005422 blasting Methods 0.000 description 1
- 239000011362 coarse particle Substances 0.000 description 1
- 238000004090 dissolution Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 235000011187 glycerol Nutrition 0.000 description 1
- 231100000086 high toxicity Toxicity 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000005543 nano-size silicon particle Substances 0.000 description 1
- 239000012286 potassium permanganate Substances 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 239000001294 propane Substances 0.000 description 1
- 238000004513 sizing Methods 0.000 description 1
- 238000010561 standard procedure Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 230000008016 vaporization Effects 0.000 description 1
- 238000009834 vaporization Methods 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06C—DETONATING OR PRIMING DEVICES; FUSES; CHEMICAL LIGHTERS; PYROPHORIC COMPOSITIONS
- C06C7/00—Non-electric detonators; Blasting caps; Primers
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B33/00—Compositions containing particulate metal, alloy, boron, silicon, selenium or tellurium with at least one oxygen supplying material which is either a metal oxide or a salt, organic or inorganic, capable of yielding a metal oxide
- C06B33/12—Compositions containing particulate metal, alloy, boron, silicon, selenium or tellurium with at least one oxygen supplying material which is either a metal oxide or a salt, organic or inorganic, capable of yielding a metal oxide the material being two or more oxygen-yielding compounds
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06C—DETONATING OR PRIMING DEVICES; FUSES; CHEMICAL LIGHTERS; PYROPHORIC COMPOSITIONS
- C06C9/00—Chemical contact igniters; Chemical lighters
Definitions
- This invention relates to a detonator and to an initiating system for a detonator.
- detonators can use thermite-based compositions as initiators that will preclude the use of primary explosives.
- a thermal shock generated by a suitable thermite charge can under certain circumstances (e.g. narrow particle size distribution, confinement and specific tamped pressures) initiate an explosive such as pentaerythritol tetranitrate (PETN) from deflagration to detonation in a very short period of time.
- PETN pentaerythritol tetranitrate
- a difficulty with a thermite-based initiator is that ignition thereof requires a high temperature, for example about 940°C for an AI-CuO thermite comprising coarse particles.
- Known techniques to ignite thermite compositions include the use of a propane torch, magnesium metal strips, and a reaction between KMnO 4 and glycerine. These approaches are however unreliable and are not suited for use in a commercial detonator. Ignitors such as exploding bridge wires and laser techniques are effective but are expensive to implement. [0005] It has been proposed to add a tinder mixture to the thermite to address the problems of the high temperature, and of the relatively long delay to ignition time periods. Barium nitrate and sulphur have been used as tinder for pyrotechnic compositions because of their excellent sensitivity to heat.
- barium nitrate to a thermite composition increases the thermal effect, creates flame in burning and reduces the ignition temperature.
- a drawback, however, is that a barium compound also has a high toxicity that is exacerbated when inhalation occurs.
- Sulphur also acts as a tinder to facilitate ignition of a pyrotechnic but the presence of the low-melting volatile sulphur fuel tends to retard the burning rate because the melting and vaporization steps of the endotherms absorb heat that would otherwise be available to raise the temperature of the unreacted mixture.
- An object of the present invention is to provide a detonator initiator in which the ignition temperature is significantly reduced.
- the invention provides a detonator which includes an explosive and an initiator for igniting the explosive, wherein the initiator includes a thermite composition and a tinder mixture which includes silicon and dibismuth trioxide.
- the thermite composition is preferably AI-CuO, in a stoichiometric ratio.
- thermite is formed primarily from micron-sized particles.
- the aluminium may be provided in powder form with the particles being smaller than 25 pm (800 mesh).
- the CuO is preferably micron-sized particles, typically less than 25 pm.
- the Bi 2 0 3 and the Si may also be micron-sized particles at less than 34 ⁇ and 64 ⁇ , respectively.
- thermite composition may be present in a weight percentage range of from 70% to 90% and the tinder may be present in a weight percentage range of from 10% to 30%.
- thermite composition constitutes approximately 80 wt % of the initiator and the tinder approximately 20 wt %.
- Figures 1 and 2 are DTA responsive curves as a function of temperature produced upon ignition of respective thermite compositions.
- FIGS 3 and 4 illustrate respectively from one side and in cross-section detonators according to different forms of the invention.
- the invention is concerned with a detonator which includes an initiator which is readily initiated by the application of heat.
- the applicant has selected the pyrotechnic Si-Bi 2 O 3 system as tinder for the thermite AI-CuO system because of the excellent sensitivity of the tinder to fire.
- the Si-Bi 2 O3 is sensitive to fire and can also be used as a short period delay with a burning speed of 150 mm per second in a composition comprising 80 wt % B12O3 and 20 wt % Si.
- the temperature of the tinder reaction is sufficient to ignite a thermite reaction.
- Experimental work was conducted to determine an optimal composition of an AI-CuO thermite system mixed with Si and B12O3 (the tinder).
- Table 1 reflects ignition temperature data which were obtained for specific mixtures of thermite (80 wt %) and tinder (20 wt %) formed from particles of different sizes.
- "coarse” denotes micrometer-sized ( ⁇ ) particles for all types.
- “nano” applies only to the thickness dimension of the flakes. This type of aluminium material is referred to in Table 1 as fine.
- the nano silicon has a surface weighted mean particle size of 910 nm and a BET surface area of 10,1 m 2 /g. The sizing boundaries of the nano CuO particles were established as being less than 10 nm. Mixing of the thermite with the tinder in each case was accomplished using standard techniques. After adequate processing the initiator compositions were ignited. Appropriate instruments were used to perform a differential thermal analysis (DTA).
- DTA differential thermal analysis
- Figure 1 is a DTA response curve as a function of temperature for a stoichiometric AI-CuO mixture comprising coarse aluminium and nano-sized CuO particles.
- a first endotherm has an onset temperature of 647°C - this corresponds to the melting of the aluminium metal (literature Al mp. 660.45°C).
- a second endotherm which occurred with an onset temperature of about 880°C is presumed to correspond to the melting and dissolution of the CuO in the aluminium melt (literature CuO mp. 1326°C). This is followed by a fast exotherm with an onset temperature of about 939°C which is associated with the ignition temperature of the composition leading to the aluminium oxidation reaction.
- Figure 2 is a curve of a DTA response of an initiator mixture, according to the invention which, as shown in Table 1 , contains 80 wt % thermite (AI-CuO) and 20 wt % of the tinder mixture (Si-Bi 2 03).
- AI-CuO thermite
- Si-Bi 2 03 the tinder mixture
- FIG. 3 illustrates a detonator 20 according to a first form of the invention which is based on the inventive principles described herein.
- the detonator includes a metallic tube 22, e.g. of aluminium, with an inner holder 24, also of aluminium.
- a charge 26 of PETN is located at a blind end of the tube and tamped in position at 130kg.
- the holder 24 includes an outlet 30 and an inlet 32.
- a charge 34 of PETN, pressed at 70kg, is adjacent the outlet.
- a charge 36 made up of the thermite/tinder composition referred to and pressed at 90kg, is adjacent the charge 34.
- a time delay element 40 is loaded into the holder.
- a starter 42 typically a mixture of red lead and silicon, is adjacent the inlet 32 and pressed at 130kg.
- the detonator 20 is used substantially in a conventional manner in that the starter 42 is fired by means of the energy output from a shock tube, not shown. If the delay element 40 is used then, after a predetermined delay period, the thermite/tinder composition 36 is ignited. The firing impulse from the thermite composition leads to deflagration to detonation of the smaller PETN charge 34 which causes initiation of the larger PETN charge 26.
- FIG. 4 shows a detonator 50 which does not include a delay element.
- the detonator has an aluminium tubular shell 52 with an open upper end and a closed lower end 54. Contained in the shell is base charge 56 made up of 400mg of PETN pressed at 130kg (56A) and 400mg of loose PETN (56B).
- An initiating element in the form of a tubular steel sleeve 60, is positioned inside the aluminium shell.
- the sleeve has an open first end which opposes the open upper end of the shell 52, and an opposed open second end.
- the sleeve contains a starter composition 62 which is similar to the starter 42 shown in Figure 3, a mixture 64 of tinder, thermite and PETN and a transition portion 66 of PETN.
- the mixture 64 consists of 20% AI-CuO thermite/tinder and 80% PETN (75 to 180 micron particle size). The constituents are dry mixed and pressed at 90kg.
- the transition portion 66 comprises 140mg of PETN (75 to 180 micron particle size) pressed at 70kg.
- the detonator 50 illustrates similar desirable characteristics as the detonator 20.
- the ignition temperature of the detonator is reduced, for the reasons which have been given and, although the starter in each case includes red lead, overall the lead requirement is also reduced.
Landscapes
- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Catching Or Destruction (AREA)
- Agricultural Chemicals And Associated Chemicals (AREA)
- Air Bags (AREA)
Abstract
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU2011220386A AU2011220386A1 (en) | 2010-02-24 | 2011-02-18 | Detonator initiator |
BR112012020907A BR112012020907A2 (en) | 2010-02-24 | 2011-02-18 | detonator initiator |
AP2012006417A AP3479A (en) | 2010-02-24 | 2011-02-18 | Detonator initiator |
ZA2012/05851A ZA201205851B (en) | 2010-02-24 | 2012-08-03 | Detonator intiator |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ZA2010/01343 | 2010-02-24 | ||
ZA201001343 | 2010-02-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2011106803A1 true WO2011106803A1 (en) | 2011-09-01 |
Family
ID=43937562
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/ZA2011/000008 WO2011106803A1 (en) | 2010-02-24 | 2011-02-18 | Detonator initiator |
Country Status (6)
Country | Link |
---|---|
AP (1) | AP3479A (en) |
AU (1) | AU2011220386A1 (en) |
BR (1) | BR112012020907A2 (en) |
CL (1) | CL2012002269A1 (en) |
WO (1) | WO2011106803A1 (en) |
ZA (1) | ZA201205851B (en) |
Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2452091A (en) * | 1942-11-23 | 1948-10-26 | David L Woodberry | Incendiary material |
US3498857A (en) * | 1966-12-06 | 1970-03-03 | Ethyl Corp | Aluminum iron oxide incendiary composition containing a (cyclopentadienyl) iron compound |
US5035756A (en) * | 1989-01-10 | 1991-07-30 | United States Of America As Represented By The Secretary Of The Navy | Bonding agents for thermite compositions |
EP0599792A1 (en) * | 1992-11-27 | 1994-06-01 | Nitro Nobel Ab | Delay charge and element, and detonator containing such a charge |
WO1997022571A1 (en) * | 1995-12-20 | 1997-06-26 | Nitro Nobel Ab | Pyrotechnical charge for detonators |
US5945627A (en) * | 1996-09-19 | 1999-08-31 | Ici Canada | Detonators comprising a high energy pyrotechnic |
WO2001018482A1 (en) * | 1999-09-06 | 2001-03-15 | Dyno Nobel Sweden Ab | Detonator |
WO2004011396A2 (en) * | 2002-07-29 | 2004-02-05 | The Regents Of The University Of California | Lead-free electric match compositions |
WO2006083379A2 (en) * | 2004-11-30 | 2006-08-10 | South Dakota School Of Mines And Technology | Nanoenergetic materials based on aluminum and bismuth oxide |
WO2007098271A2 (en) * | 2006-02-27 | 2007-08-30 | Ensign-Bickford Aerospace & Defense Company | Solid hydrogen fuel elements and methods of making the same |
-
2011
- 2011-02-18 WO PCT/ZA2011/000008 patent/WO2011106803A1/en active Application Filing
- 2011-02-18 AP AP2012006417A patent/AP3479A/en active
- 2011-02-18 BR BR112012020907A patent/BR112012020907A2/en not_active Application Discontinuation
- 2011-02-18 AU AU2011220386A patent/AU2011220386A1/en not_active Abandoned
-
2012
- 2012-08-03 ZA ZA2012/05851A patent/ZA201205851B/en unknown
- 2012-08-17 CL CL2012002269A patent/CL2012002269A1/en unknown
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2452091A (en) * | 1942-11-23 | 1948-10-26 | David L Woodberry | Incendiary material |
US3498857A (en) * | 1966-12-06 | 1970-03-03 | Ethyl Corp | Aluminum iron oxide incendiary composition containing a (cyclopentadienyl) iron compound |
US5035756A (en) * | 1989-01-10 | 1991-07-30 | United States Of America As Represented By The Secretary Of The Navy | Bonding agents for thermite compositions |
EP0599792A1 (en) * | 1992-11-27 | 1994-06-01 | Nitro Nobel Ab | Delay charge and element, and detonator containing such a charge |
WO1997022571A1 (en) * | 1995-12-20 | 1997-06-26 | Nitro Nobel Ab | Pyrotechnical charge for detonators |
US5945627A (en) * | 1996-09-19 | 1999-08-31 | Ici Canada | Detonators comprising a high energy pyrotechnic |
WO2001018482A1 (en) * | 1999-09-06 | 2001-03-15 | Dyno Nobel Sweden Ab | Detonator |
WO2004011396A2 (en) * | 2002-07-29 | 2004-02-05 | The Regents Of The University Of California | Lead-free electric match compositions |
WO2006083379A2 (en) * | 2004-11-30 | 2006-08-10 | South Dakota School Of Mines And Technology | Nanoenergetic materials based on aluminum and bismuth oxide |
WO2007098271A2 (en) * | 2006-02-27 | 2007-08-30 | Ensign-Bickford Aerospace & Defense Company | Solid hydrogen fuel elements and methods of making the same |
Also Published As
Publication number | Publication date |
---|---|
AU2011220386A1 (en) | 2012-08-30 |
ZA201205851B (en) | 2013-05-29 |
CL2012002269A1 (en) | 2013-03-08 |
AP2012006417A0 (en) | 2012-08-31 |
AP3479A (en) | 2015-12-31 |
BR112012020907A2 (en) | 2016-05-03 |
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Tulis | combustible materials, such as starch dust in starch-processing plants and coal dust in coal-mining operations, are legion. |
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