NZ625171B2 - Explosive composition - Google Patents
Explosive composition Download PDFInfo
- Publication number
- NZ625171B2 NZ625171B2 NZ625171A NZ62517112A NZ625171B2 NZ 625171 B2 NZ625171 B2 NZ 625171B2 NZ 625171 A NZ625171 A NZ 625171A NZ 62517112 A NZ62517112 A NZ 62517112A NZ 625171 B2 NZ625171 B2 NZ 625171B2
- Authority
- NZ
- New Zealand
- Prior art keywords
- explosive
- emulsion
- emulsion explosive
- regions
- sensitized
- Prior art date
Links
- 239000002360 explosive Substances 0.000 title claims abstract description 193
- 239000000203 mixture Substances 0.000 title claims abstract description 143
- 239000000839 emulsion Substances 0.000 claims abstract description 197
- 238000005474 detonation Methods 0.000 claims abstract description 55
- PAWQVTBBRAZDMG-UHFFFAOYSA-N 2-(3-bromo-2-fluorophenyl)acetic acid Chemical compound OC(=O)CC1=CC=CC(Br)=C1F PAWQVTBBRAZDMG-UHFFFAOYSA-N 0.000 claims abstract description 50
- 230000001235 sensitizing effect Effects 0.000 claims abstract description 50
- 238000009826 distribution Methods 0.000 claims abstract description 24
- 238000000034 method Methods 0.000 claims abstract description 18
- 239000011800 void material Substances 0.000 claims description 44
- 238000002156 mixing Methods 0.000 claims description 34
- 229910002651 NO3 Inorganic materials 0.000 claims description 2
- NHNBFGGVMKEFGY-UHFFFAOYSA-N Nitrate Chemical compound [O-][N+]([O-])=O NHNBFGGVMKEFGY-UHFFFAOYSA-N 0.000 claims description 2
- 239000007788 liquid Substances 0.000 description 95
- 239000000463 material Substances 0.000 description 84
- 230000035939 shock Effects 0.000 description 34
- 238000005422 blasting Methods 0.000 description 19
- 238000009472 formulation Methods 0.000 description 19
- 230000003068 static effect Effects 0.000 description 14
- 150000002500 ions Chemical class 0.000 description 12
- 239000011435 rock Substances 0.000 description 10
- 239000007787 solid Substances 0.000 description 10
- 238000006243 chemical reaction Methods 0.000 description 8
- 230000000977 initiatory effect Effects 0.000 description 8
- 238000004519 manufacturing process Methods 0.000 description 7
- 206010070834 Sensitisation Diseases 0.000 description 6
- 239000004794 expanded polystyrene Substances 0.000 description 6
- 230000009467 reduction Effects 0.000 description 6
- 230000035945 sensitivity Effects 0.000 description 6
- 230000008313 sensitization Effects 0.000 description 6
- 239000000470 constituent Substances 0.000 description 5
- 239000000126 substance Substances 0.000 description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 5
- 230000002950 deficient Effects 0.000 description 4
- LEOJDCQCOZOLTQ-UHFFFAOYSA-N dibutylcarbamothioyl n,n-dibutylcarbamodithioate Chemical compound CCCCN(CCCC)C(=S)SC(=S)N(CCCC)CCCC LEOJDCQCOZOLTQ-UHFFFAOYSA-N 0.000 description 4
- 239000012530 fluid Substances 0.000 description 4
- 238000013467 fragmentation Methods 0.000 description 4
- 238000006062 fragmentation reaction Methods 0.000 description 4
- 239000000446 fuel Substances 0.000 description 4
- 239000007789 gas Substances 0.000 description 4
- 239000011159 matrix material Substances 0.000 description 4
- 238000005065 mining Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- LPXPTNMVRIOKMN-UHFFFAOYSA-M sodium nitrite Chemical compound [Na+].[O-]N=O LPXPTNMVRIOKMN-UHFFFAOYSA-M 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 230000007246 mechanism Effects 0.000 description 3
- 239000007800 oxidant agent Substances 0.000 description 3
- 239000004033 plastic Substances 0.000 description 3
- 229920002223 polystyrene Polymers 0.000 description 3
- 230000000750 progressive effect Effects 0.000 description 3
- 239000000243 solution Substances 0.000 description 3
- 238000012360 testing method Methods 0.000 description 3
- HZTVIZREFBBQMG-UHFFFAOYSA-N 2-methyl-1,3,5-trinitrobenzene;[3-nitrooxy-2,2-bis(nitrooxymethyl)propyl] nitrate Chemical compound CC1=C([N+]([O-])=O)C=C([N+]([O-])=O)C=C1[N+]([O-])=O.[O-][N+](=O)OCC(CO[N+]([O-])=O)(CO[N+]([O-])=O)CO[N+]([O-])=O HZTVIZREFBBQMG-UHFFFAOYSA-N 0.000 description 2
- 101150034533 ATIC gene Proteins 0.000 description 2
- QGZKDVFQNNGYKY-UHFFFAOYSA-O Ammonium Chemical compound [NH4+] QGZKDVFQNNGYKY-UHFFFAOYSA-O 0.000 description 2
- 239000004793 Polystyrene Substances 0.000 description 2
- 239000003795 chemical substances by application Substances 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000014509 gene expression Effects 0.000 description 2
- 239000011521 glass Substances 0.000 description 2
- 238000005086 pumping Methods 0.000 description 2
- 238000005215 recombination Methods 0.000 description 2
- 230000006798 recombination Effects 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 235000010288 sodium nitrite Nutrition 0.000 description 2
- 230000009897 systematic effect Effects 0.000 description 2
- 230000017105 transposition Effects 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 241000220317 Rosa Species 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 239000007864 aqueous solution Substances 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 238000009412 basement excavation Methods 0.000 description 1
- 239000011324 bead Substances 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000003245 coal Substances 0.000 description 1
- 239000000356 contaminant Substances 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000003995 emulsifying agent Substances 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 230000007717 exclusion Effects 0.000 description 1
- 239000012634 fragment Substances 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
- 230000006870 function Effects 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 238000000691 measurement method Methods 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 230000008520 organization Effects 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 238000003359 percent control normalization Methods 0.000 description 1
- 239000012266 salt solution Substances 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 239000004449 solid propellant Substances 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B23/00—Compositions characterised by non-explosive or non-thermic constituents
- C06B23/002—Sensitisers or density reducing agents, foam stabilisers, crystal habit modifiers
- C06B23/003—Porous or hollow inert particles
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B23/00—Compositions characterised by non-explosive or non-thermic constituents
- C06B23/002—Sensitisers or density reducing agents, foam stabilisers, crystal habit modifiers
- C06B23/004—Chemical sensitisers
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B31/00—Compositions containing an inorganic nitrogen-oxygen salt
- C06B31/28—Compositions containing an inorganic nitrogen-oxygen salt the salt being ammonium nitrate
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B31/00—Compositions containing an inorganic nitrogen-oxygen salt
- C06B31/28—Compositions containing an inorganic nitrogen-oxygen salt the salt being ammonium nitrate
- C06B31/285—Compositions containing an inorganic nitrogen-oxygen salt the salt being ammonium nitrate with fuel oil, e.g. ANFO-compositions
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B45/00—Compositions or products which are defined by structure or arrangement of component of product
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42D—BLASTING
- F42D1/00—Blasting methods or apparatus, e.g. loading or tamping
Abstract
The disclosure relates to an explosive composition comprising an emulsion explosive and sensitizing voids, wherein the sensitizing voids are present in the emulsion explosive with a non-random distribution, wherein the emulsion explosive comprises regions of a first emulsion explosive and regions of a second emulsion explosive, wherein the first emulsion explosive is sensitized with sufficient sensitizing voids to render it detonable and wherein the second emulsion explosive has different detonation characteristics from the sensitized first emulsion explosive and wherein the explosive composition does not contain ammonium nitrate prill. Also disclosed is a method of varying the energy release characteristics of a first emulsion explosive sensitized with sufficient sensitizing voids to render it detonable which comprises formulating an explosive composition comprising regions of the first emulsion explosive and regions of a second emulsion explosive, wherein the second emulsion explosive has different detonation characteristics from the sensitized first emulsion explosive, wherein the sensitizing voids are present in the explosive composition with a non-random distribution and wherein the explosive composition does not contain ammonium nitrate prill. a second emulsion explosive, wherein the first emulsion explosive is sensitized with sufficient sensitizing voids to render it detonable and wherein the second emulsion explosive has different detonation characteristics from the sensitized first emulsion explosive and wherein the explosive composition does not contain ammonium nitrate prill. Also disclosed is a method of varying the energy release characteristics of a first emulsion explosive sensitized with sufficient sensitizing voids to render it detonable which comprises formulating an explosive composition comprising regions of the first emulsion explosive and regions of a second emulsion explosive, wherein the second emulsion explosive has different detonation characteristics from the sensitized first emulsion explosive, wherein the sensitizing voids are present in the explosive composition with a non-random distribution and wherein the explosive composition does not contain ammonium nitrate prill.
Description
ive Composition
TECHNICAL FIELD
The present invention relates to explosive compositions, in ular to explosiVe
compositions that are tailored to provide desired blasting properties, and to a method of
blasting using explosive compositions of the invention. The t ion also relates
to the manufacture of such itions and to their use in blasting operations. The
present invention also s to the design and formulation of explosive compositions that
allows the shock and heave energies to be manipulated as required based on intended use
in a particular blasting.
BACKGROUND
'15 Detonation energy of commercial explosives can be broadly divided into two forms -
shock energy and heave energy. Shock energy fractures and fragments rock. Heave
energy moves blasted rock after fracture and ntation, generally as a function of gas
behind the CJ zone during detonation. In general the higher the velocity of
‘ produced
detonation (VOD) of an explosive the higher proportion of shock energy of the explosive
is likely to exhibit.
Certain mining applications require the use of explosives that exhibit a combination of low
shock energy and high heave energy. This allows fragmentation to be controlled (high
shock energy produces significant amounts of dust sized fines) and in turn reduces
excavation costs. In softer rock and coal mining applications, for example, the use of
explosives that provide a relatively high proportion of heave energy can lead to significant
savings downstream for the mine operation because tion of d rock then
becomes easier. In quarry applications, fragmentation control and reduction of fines is also
very attractive.
Current commercial explosives offer a range of shock and heave energies. -For example,
ANFO (ammonium nitrate/fuel oil)' tends to provide low shock energy and high heave
WO 86572
energy. In fact, ANFO with all of its ammonium nitrate present as prill ts what is
tionally believed to be an excellent ation of shock (fragmentation) and heave
properties for many rock blasting and tion situations. In st, (ammonium
nitrate) emulsion explosives tend to provide high shock energy and low heave energy. It is
well known that such emulsion explosives tend to have relatively high velocities of
detonation and correspondingly high pressure in the al reaction zone, This results in
a high shock explosive that is well suited to fragmenting rock, but that has relatively low
heave energy to move fragmented rock.
In practice, materials that modify explosive teristics, such as ammonium nitrate
(AN) prill are conventionally added to emulsion explosives to enhance their overall heave
properties. Prills are understood to bute to a late burn in the detonation post CJ zone
and this manifests itself as heave energy rather than shock energy.
The explosive properties of prill-containing explosive compositions are y related to
the ive characteristics of the prill itself and, in turn, the explosive characteristics are
influenced by factors including the physical features, internal structures and chemical
composition of the prill. However, such factors may vary within a wide range depending
on such things as the manufacturing technology used to produce the prill, the type and/or
content of additives (and/or contaminants) present in the prill, the manner in which the prill
is stored and/or transported, and the context of use of the explosive? including the degree of
confinement and environmental factors, such as temperature and humidity, As a result, the.
detonation performance (including the energy release characteristics) of conventional prill-
containing explosives tends to be highly variable. Explosive formulations with'a high
concentration ofprillare also very difficult to pump into a blasthole.
A further eration in relation to the use of ANFO and AN prill—containing emulsion
explosives is the cost of manufacture of AN prill. AN prill manufacturing towers represent
a significant fraction of capital expenditure associated with an ammonium nitrate
production facility. Prilling is also a highly energy intensive s that adds
significantly to the carbon footprint associated with these type of explosives.
Against this background it would be desirable to provide an explosive for commercial
blasting operations that does not require the use of ammonium nitrate prill and that
therefore does not suffer the potential problems associated with the use of prill, but that
can achieve at least comparable rock blasting performance as currently used ANFO and
AN containing explosives. The present invention seeks to provide an explosive
composition that exhibits the desirable features of conventional ANFO and AN prillcontaining
explosives in terms of detonation energy balance as between shock and heave
energies, but that is free of the practical (and economic) constraints ated with the use
of such prill-containing conventional ives.
SUMMARY OF THE INVENTION
In accordance with a first ment of the invention there is provided an explosive
composition comprising an emulsion explosive and sensitizing voids, wherein the
sensitizing voids are present in the emulsion ive with a non-random distribution,
wherein the emulsion explosive comprises regions of a first emulsion explosive and
regions of a second emulsion explosive, n the first emulsion explosive is sensitized
with sufficient sensitizing voids to render it detonable and n the second emulsion
explosive has different detonation characteristics from the ized first emulsion
explosive and wherein the explosive composition does not contain ammonium nitrate prill.
In the following discussion the term “liquid energetic material” refers to an emulsion
ive.
The explosive composition of the present ion is defined with reference to its internal
structure. A charge made up (entirely) of liquid energetic material in which the sensitizing
voids are sufficiently trated to render the liquid energetic material detonable will
have different tion characteristics when compared with a charge made up (entirely)
of liquid energetic material in which the izing voids are not so concentrated. The
(regions of) liquid energetic material having lower concentration of sensitizing voids (i.e.
those regions" in which the sensitizing voids are not so concentrated" may be per se
detonable but with reduced detonation sensitivity when compared with (those s of)
liquid energetic material including higher concentration of sensitizing
voids. atively, (the regions of) liquid energetic material having lower concentration
of sensitizing voids may be per se non—detonable.
Herein differences in detonation sensitivity relate to the intrinsic sensitivity of the
individual‘ regions, and also concentration of the sensitizing voids t within the
regions, of liquid energetic material. It is generally accepted that the sensitivity of an
energetic material to shock wave initiation is governed by the ce of the sensitizing
voids. Shock-induced void collapse due to application of a shock wave is a l
mechanism for hot spot fOrmation and subsequent detonation initiation in tic
als. The generation of the shock induced hotspots, or regions of localized energy
release, are crucial processes in shock initiation of energetic materials. The iveness of
the shock tion further depends on the amplitude and duration of the shock wave,
It is to be appreciated that the explosive composition of this first embodiment is
distinguished. from conventional explosive. compositions that are formulated by blending
sensitizing voids with a liquid tic material to provide a sensitized explosive product.
In that case the voids will be distributed in the liquid energetic material with a random
distribution (no amount of mixing will result in a uniform andom) spaced
distribution of voids). With this random arrangement of voids it may be possible-to identify
regions in which voids are t in greater concentrations than in others, but the void
distribution is nevertheless random in character and there is no structural or atic
consistency within the tic material with respect to void distribution.
This is to, be contrasted with the present invention in which the voids are‘present with a
non—random distribution to provide regions that are void rich and regions that are void
deficient. In accordance with this aspect of the invention the voids are present in the liquid
energetic material as clusters, and in this respect the explosive compositions of the
invention have some structural and systematic consistency with respect to the organization
of the voids. In the context of the t invention the term "clusters" is intended to
denote a deliberate, grouped arrangement of voids. This arrangement is non-random in
character and is not arbitrary in nature.
In on to this first embodiment of the invention it will be appreciated that regions of
liquid energetic material having a high concentration of voids, i.e. including clusters of
voids, will per se have different detonation characteristics form regions which have a
lower concentration of voids, or no voids at all. It is a requirement of the invention that the
explosive composition includes regions in which the sensitizing voids are sufficiently
concentrated to render those regions detonable, and this means that those regions would be
per se detonable. In other words an ive composition having a bulk structure
corresponding to that of these regions would be detonable in its own right. As e
influences detonation characteristics, it follows that those s in the explosive
compositions of the invention that have a lower concentration of voids will per se exhibit
different detonation characteristics from those regions in which the voids are more highly
concentrated. In accordance with the invention it has been found that providing in a single
formulation regions of liquid energetic material that per se have different detonation
teristics allows the bulk detonation characteristics of the explosive composition to be
influenced and controlled.
In accordance with the ion the explosive composition comprises regions of a first
liquid energetic material and regions of a second liquid energetic material, wherein the first
liquid energetic material is sensitized with sufficient sensitizing voids to render it
detonable and wherein the second energetic liquid has different detonation characteristics
from the sensitized first liquid energetic material. The (base) liquid energetic materials
may be the same or different, although typically the same liquid tic al is used.
When different they will have different physical and chemical properties, such as density
and composition.
In embodiments of the invention the explosive compositions of the t invention do
not need to rely on ammonium nitrate prill or like al to modify the blasting
properties of the explosive composition. Rather, the blasting properties of the explosive
ition are directly attributable to the individual regions (and possibly to the liquid
energetic material used in those regions where le energetic liquids are employed)
from which the composition is made up. In accordance with the present invention this.
approach allows explosive compositions to be formulated that have energy release
characteristics (in terms of shock and heave energies) that are at least comparable to
conventional prill-containing ive formulations.
In an embodiment the ive compositions of the invention do not need to contain any
'solid oxidiser components or fuels, such as priil, and this means that they Can be pumped
with ve ease. Thus, related to the first embodiment of the ion, the invention
provides an explosive composition consisting of, or consisting essentially of, a liquid
energetic material and sensitizing voids, wherein the sensitizing voids are provided in the
liquid energetic material with a non-random distribution, and wherein the liquid energetic
material comprises (a) regions in which the sensitizing voids are sufficiently concentrated
to render those regions detonable and (b) regions in which the sensitizing voids are not so'
concentrated.
Related to the second ment of the invention, the explosive ition may consist
of, or consist essentially of, regions of a first liquid energetic material and regions of a
'second liquid energetic material, wherein the first liquid energetic material is sensitized
with ent sensitizing voids to render it detonable and wherein the second tic
liquid has different detonation characteristics from the sensitized first liquid energetic
In these embodiments the expressions “consisting of” and variations thereof are ed
to mean that the explosive composition contains the stated components and nothing else.
The expressions “consisting essentially of” and variations f are intended to mean that
the explosive composition must contain the stated components but that other components
may be present provided that theSe components do not materially affect the properties and
performance of the explosive composition.
The present ion also provides a method of producing an explosive composition, the
method comprising providing sensitizing voids in a liquid energetic material, wherein the
izing voids are provided in the liquid energetic material with a ndom
distribution, and such that the liquid tic material comprises (or consists of or
consists essentially of) (a) regions in which the sensitizing voids are sufficiently
concentrated to render those regions detonable and (b) regions in which the sensitizing
voids are not so concentrated.
Consistent with the second embodiment of the invention, there is also provided a method
of producing an explosive composition, the method comprising (or consisting of or
consisting essentially of) blending together a first emulsion explosive and a second
emulsion explosive to provide regions of the first emulsion ive and regions of the
second emulsion explosive, wherein the first emulsion explosive is sensitized with
ient sensitizing voids to render it ble and wherein the second emulsion
explosive has different tion characteristics from the sensitized first emulsion
explosive, and wherein the explosive composition does not contain ammonium nitrate prill.
As another variant, the present invention enables explosive compositions to be formulated
with d quantities of ammonium e prill when compared with conventional prillcontaining
explosives, whilst achieving the same detonation energy balance as such
conventional ives. Accordingly, the present invention also provides an explosive
composition as defined, wherein the composition further comprises no more than 25
weight %, preferably no more than 15 weight % and, most preferably, no more than 10
weight %, of solid ammonium nitrate (as AN prill or ANFO) based on the total weight of
composition. This represent somewhere between 20 to 50 % of the amount of solid AN or
ANFO used in conventional explosive compositions.
In this embodiment the solid (prill) component should generally be provided in higher
density s of the liquid tic material making up the explosive composition, i.e.
those regions that do not include sensitizing voids or a reduced level of sensitizing voids
when compared with other regions that (are designed to) have a higher tration of
sensitizing voids. For example, this embodiment may be implemented by premixing solid
AN prill or ANFO with an unsensitized liquid energetic material prior to blending the
unsensitized liquid energetic material with a sensitized liquid energetic material consistent
with the general principles underlying the ion.
In this embodiment the detonation characteristics of the ive composition can be
tailored in accordance with the underlying principles of the invention by lling how
voids are placed and concentrated within the liquid energetic material so it is possible to
e an intended detonation energy outcome without needing to include as much prill as
one would do normally. The inclusion of relatively small amounts of AN prill may also be
applied to influence detonation teristics, however. Some applications may benefit
from the generation of additional energy from decomposition of the solid component
or/and utilizing its free oxygen in further reactions with available fuels. Inclusion of the
solid component in void-free regions of liquid energetic material may lead to an increase in
the total energy of the composition h reduction of the water content in those regions
of liquid tic material.
The present invention also provides a method of varying the energy e characteristics
of a first liquid energetic material sensitized with sufficient sensitizing voids to render it
detonable which comprises formulating an explosive composition comprising (or
consisting of or consisting essentially of) regions of the first emulsion explosive and
regions of a second emulsion ive, wherein the second emulsion explosive has
ent detonation characteristics from the sensitized first emulsion explosive, wherein
the sensitizing voids are present in the explosive composition with a non-random
distribution and n the ive composition does not contain ammonium nitrate
prill.
The present invention also provides a method of (commercial) blasting using an ive
composition in ance with the present invention. The explosive composition is used
in exactly the same manner as conventional explosive compositions. The explosive
compositions of the invention are intended to be detonated using conventional initiating
systems, for example using a detonator and a booster and/or primer.
The context of use of the explosive composition of the present invention will depend upon
the blasting properties of the ition, especially with regard to the heave and shock
energies of the composition. It will be appreciated r that it is envisaged that, in
view of their desirable energy release characteristics, the t invention will provide
explosive compositions that can be used instead of conventional ANFO or AN prillcontaining
formulations. Explosive compositions of the invention may have particular
utility in mining and quarrying applications.
Herein the term "liquid energetic material" is intended to mean a liquid explosive that has
stored chemical energy that can be released when the material is detonated. Typically, a
liquid energetic material would require some form of sensitization to render it per se
detonable. Thus, the term excludes materials that are inherently benign and that are nondetonable
even if sensitized, such as water. It should be noted however that this does not
mean that each liquid energetic al in the explosive compositions of the invention are
in fact sensitized. Indeed, in ments of the invention, one of the liquid energetic
als is sensitized and another liquid energetic material is not sensitized at all. That
said, in other embodiments one of the liquid energetic als is sensitized and another
liquid energetic al is sensitized to a lesser extent.
The energetic materials used in the invention are in liquid form, and here specific mention
may be made of explosive ons. Such emulsions are well known in the art in terms
of components used and formulation.
In the context of the present invention, the term "explosive ition" means a
composition that is detonable per se by conventional initiation means at the charge
diameter being employed.
Throughout this specification and the claims which follow, unless the context requires
otherwise, the word "comprise", and ions such as "comprises" and "comprising", will
be understood to imply the inclusion of a stated integer or step or group of integers or steps
but not the exclusion of any other integer or step or group of integers or steps.
The reference in this specification to any prior-publication (or information derived from it),
or to any matter which is known, is not, and should not be taken as an acknowledgment or
admission or any form of tion that that prior publication (or information derived
from it) or known matter forms part of the common general knowledge in the field of
endeavour to which this specification relates.
BRIEF DISCUSSION OF FIGURES
Figure l is a schematic showing le arrangements of voids in a liquid energetic
material;
Figure 2 is a schematic illustrating how a ensitized liquid energetic material in
accordance with an embodiment of the invention may be produced, as referred to in the
examples
Figure 3 is a schematic illustrating a mixing t that may be used to produce a void-
sensitized liquid» energetic material in accordance with an embodiment of the invention;
Figurei4 is a schematic illustrating the distribution of two emulsions in an explosive
composition in aCcordance with an embodiment of the invention;
Figure 5 is a photograph g an experimental arrangement employed in the examples;
s 6-8 are graphs illustrating results obtained in the examples.
DETAILED DISCUSSION OF THE INVENTION
In accordance ' with the present invention it - has been found that the detonation
characteristics of a void sensitized liquid energetic material can be controlled by
controlling how the voids are arranged within the liquid energetic material. in ular it
has been found that the ratio ofheave energy to shock energy delivered by detonation of
liquid energetic materials ized withxvoids can be significantly increased, compared
with existing void sensitized “all ” energetic materials, by lling how the voids
are distributed With respect to each other. It is also possible to achieve a high heave to
shock energy ratio whilst maintaining higher total energy densities than is available from
tional “all liquid" systems.
Prior to the present invention much has been reported on the use ofdifferent types of voids
and voidage levels, but there is not believed to have been any systematic igation of
the effect of relative void spatial distribution. Existing void sensitized liquid energetic
materials have a similar (random) l bution of the voids with respect to each
other. Only by using voids which provide fuel, such as expanded yrene, and with
void diameters of 500 um or more, have higher heave energies been achieved. With the
present invention unconventionally high ratios of heave to shock energies with voids sizes
from 20 pm to 5 mm can be achieved, and high total energies similar to solid AN prill-
' containing formulations, can be achieved.
Without wishing to be bound by theory, the mechanisms involved when an ive
composition of the invention is initiated are believed to be as follows. Distribution of the
cxplosive energy between shock and heave is governed by the speed of reactions within
the individual sensitized and itized regions. The chemical reactions within the hot
.spots are fast and exothermic and thus enable detonations by large number of
interconnected, small l ions. The number and size of the hot spots controls
the sensitivity and speed of detonation reactions within the sensitized region. In this way
the sensitized region contributes to the magnitude of the shock energy output. The
insufficient number or total absence of hot spots leads to relatively slow reactions
.25: (burning) in unsensitized region of energetic liquid. The grain burning mechanism controls
the rate ofenergy release within unsensitized regions of the energetic material. The process
hence determines output of the heave . Importantly, in accordance with the
invention, the energy release characteristics of the explosive composition can be controlled
and tailored by varying the void distribution, void volume, the combination of liquid
energetic components used and/or the arrangement of the liquid energetic components
within the bulk of the explosive ition. In turn, this enables the detonation properties
of the explosive composition to be tailored to particular rock/ground types and to particular
mining applications.
The present invention may be of particular interest when applied to the use of emulsion
explosives as liquid energetic materials. on-based bulk explosives do not have
blasting characteristics, such as velocity of detonation (VOD), lent to conventional
ANFO or AN prill-containing explosives. However, emulsion ives do have desirable
ties in terms of water resistance and the y to be . Accordingly,
emulsion-based explosive compositions of the present invention may be used as an
alternative to ANFO and AN-containing products. This will allow such tional
explosives compositions to be replaced with products that are emulsion-only based.
Accordingly, the present invention also provides the use of an emulsion explosive
composition in ance with the present invention in a ng operation as an
alternative to ANFO or AN prill-containing product.
In this context the emulsion explosives are typically water-in-oil emulsions comprising a
tinuous oxidizer salt solution (such as ammonium nitrate) dispersed in a continuous
fuel phase and stabilized with a suitable emulsifier. Sensitization is ed in
conventional manner by inclusion of "voids" such as gas bubbles or micro-balloons, e.g.
glass or polystyrene micro-balloons. This will influence the density of the on.
Central to the present invention is the arrangement with which voids are distributed within
a liquid energetic material. Thus, the explosive compositions of the present invention
include regions that are void rich (i.e. relatively concentrated) and regions that are void
deficient (i.e. not so trated), these regions per se having different detonation
characteristics. Combining such regions results in a bulk product having novel detonation
characteristics as compared to the detonation characteristics of the individual s that
are present. As will become apparent there is great scope for modifying the internal
structure of the bulk product based on its constituent components/regions and in turn this
advantageously provides great scope for tailoring the explosive characteristics of the
product.
In accordance with the present invention it may be possible to achieve one or more of the
following cal benefits ise not able with a homogeneous emulsion-only
void sensitized explosive compositions:
0 Excellent ation of heave properties and fragmentation.
o Steady low VOD during detonation.
0' Ability to adj ust/match detonation energy/properties to rock properties.
0 Control of energy release rate by proportion of differcnt components in the
ive composition. This enables the ion to deliver high heave or high ,
shock performance to match customer specific applications.
15_ When compared with solid AN-containing formulations, explosive compositions of the
ion that are prill-free offer the following benefits:
0 Water resistance.
0 Liquid explosives enable pumping at higher flow rates and lower pumping
pressures leading to faster loading of water filled holes.
In the first embodiment of the invention the explosive composition comprises a 'liquid
energetic material and sensitizing voids, wherein the sensitizing voids are present in the
liquid energetic material with a non-random distribution, and wherein 'the liquid energetic
material comprises (a) regions in which the sensitizing voids are sufficiently concentrated
to render those regions detonable and (b) regions in which the sensitizing voids are not so
trated. In this embodiment the internal structure of the explosive composition is
characterized by the distribution of voids, the volume ratio of the various regions and the
arrangement of the regions. The void diStribution may y be understood with
reference to Figure 1. This figure shows three types of void butions in a liquid
energetic material (matrix).
Figure 1(a) shoWs a uniform spaced distribution of voids as would arise with ideal mixing
of voids in a liquid energetic material. It will be appreciated that this is arrangement is
ideal/hypothetical and would not be found in real systems.
Figure 1(b) shows a random arrangement of voids as would arise in practice when
formulating a conventional explosive ition by mixing of voids into a liquid
energetic material. It might be possible to identify regions that are void rich and ent
regions that are void deficient but the ement is nevertheless random and g
deliberate has been done at achieve regions having these structural features in. terms of
void distribution.
Figure 1(c) on the other hand shows an example of clusters of voids distributed throughout
a matrix of liquid energetic material, as per the first embodiment of the invention. This
arrangement is deliberate rather than arbitrary, and there is some structural and atic
consistency. Figure 1(c) suggests that the regions of void tration are approximately
the same size and occur with an even distribution, but this is not essential. Furthermore,
Figure 1(c) shows the use of a single liquid energetic material (matrix). However, this is
not essential and the regions differing in void concentration may be achieved by the use of
different liquid energetic materials sensitized to ent extents.
In another (second) embodiment of the invention the explosive composition comprises
regions of a first liquid energetic material and regions of a second liquid tic material,
wherein the first liquid energetic material is sensitized with sufficient sensitizing voids to
render it detonable and wherein the second energetic liquid has different detonation
characteristics from the sensitized first liquid energetic material. It will be appreciated that
this embodiment is d to the first embodiment in that in the second embodiment
individual. liquid energetic materials are combined to provide the regions having the
itevoid concentrations referred to in the first embodiment.
<15-
With respect to the second—embodiment of the invention, the (internal) structure of the
explosive composition is characterized by the volume ratio of each ent (liquid
energetic material) and the structural arrangement/distribution of the components relative
to each other. In the explosive compositions of this’embodiment the two components are
generally present as ete) regions. ‘
In accordance with this embodiment the first and second liquid energetic als have
ent detonation characteristics, such as VOD and tion sensitivity. In one
embodiment the first and second liquid energetic materials (e.g. emulsion explosives) are
derived from the same base source (e.g. emulsion). For example, in this case, the first
emulsion may be produced by void sensitizing a base emulsion, thereby reducing its
density, and the second emulsion may be the base emulsion itself. In this case the
explosive composition will include discrete regions of basic (unsensitized) emulsion and
regions of the ized emulsion. The y and blasting characteristics of the resultant
explosive composition will be determined and influenced by the individual components
from which the composition is formed.
Advantageously, in this second embodiment of the invention the make up and structural
characteristics of the explosive composition may be varied in a number of ways and this
may provide significant flexibility in terms of ing particular blast outcomes that
have ise not been achievable using conventional emulsion-based void sensitized
explosive products. Thus, in the embodiment described, where an unsensitized emulsion is
provided in combination with a ized emulsion, numerous possibilities exist within the
spirit of the present invention. The following are given by way of example. It will be
appreciated that combinations of the following ts may be employed.
0 The relative proportions of the first and second emulsions may be varied.
o The geometry of the individual regions may be varied. For example, for a given
volume of emulsion, the first emulsion may be present as small dispersed
droplets/domains/zones ted from one r by intervening regions of the
second emulsion. Alternatively, the second emulsion may be present as small
—1'6—
dispersed ts/domains/zones separated from one another by intervening
regions of the first composition. As a further ative, the first and second
emulsions may be present as discrete domains/zones arranged as a bi-continuous
mixture of the two compositions. In an embodiment of the invention the
unsensitized phase may be in the form of globules, sheets, rods or bi—continuous
structures, such that the smallest dimension of the unsensitized phase is 3 to 5000,
for example 5 to 50 times, times the mean diameter of the sensitizing voids.
o The emulsions may be derived from the same or different “base” emulsion.
- One emulsion may form a discontinuous phase and the other emulsion may form a
uous phase. In the example given above, the unsensitized emulsion may form
the matrix and the void sensitized emulsion the discontinuous phase.
0 It is essential that one of the emulsions that is used be void sensitized (for
detonation using the intended initiating system) but the other emulsion does not
need to be non-sensitized. Both emulsions may be void sensitized, although in this
case the dual emulsions must nevertheless exhibit different blasting
characteristics.
0 When both ons are void sensitized, each emulsion may be sensitized in a
different way. For example, one emulsion may be gassed and the other on
include micro-balloons, such as ed polystyrene. As another example, each
emulsion may be sensitized with different sizes of micro-balloons.
It will be appreciated from this that the formulation flexibility associated with the present
invention allows the production of explosive compositions that have detonation
characteristics, such as VOD, to be substantially different from homogeneous emulsion-
only void sensitized ive ts having similar composition in terms of liquid
energetic material and void sensitization.
WO 86572
The sensitizing voids may be gas bubbles, glass micro-balloons, plastic micro—balloons,
expanded polystyrene beads, or any other tionally used sensitizing agent. The
density of the sensitizing agent is typically below 0.25 g/cc although polystyrene s
may have a y as low as 0.03 -0.05 g/cc, and the voids generally have mean diameters
in the range 20 to 2000 um, for example in the range 40 to 500 um.
Noting the scope for variation in composition formulation that , it would in fact be
possible to e a comprehensive suite of explosive compositions tailored to meet
different blasting requirements using only a limited number of base emulsion formulations.
In turn this may lead to more streamlined logistics, while at the same time possibly lead to
lower formulation and operational costs.
Furthermore, the present invention may render useful products that have previously been
' thought to be able in the explosives context. For example, by using ammonium
nitrate as melt grade only, a range of previously unacceptable ammonium nitrate sources
could be used, leading to lower cost explosives.
The present invention also provides a method of (commercial) blasting using an explosive
composition in accordance with the present invention. The explosive itions of the
' ion are ed to be detonated using conventional initiating systems, for example
comprising a detonator and a booster and/or primer. The present invention may be applied
to produce explosive ition that detonate at a steady predetermined velocity, with a
minimum VOD of 2000 m/s, for example from 2000—6000 m/s in either a confined bore
hole, or under unconfined conditions. It will be appreciated that the VOD of an explosive
composition in accordance with the invention will be less than the VOD of the component
(or region) of the composition having the highest VOD. It is well known that the amount
of shock energy at a given explosive density is proportional to the VOD, and as such.
reduction in the VOD results in a decrease in shock energy and ponding increase in
heave energy,
Advantageously, the present invention may be used to provide an emulsion-based
explosive composition that matches ANFO or an AN prill based product with respect to
WO 86572
~18?
density and velocity of detonation. For example, if a commercially available product
containing AN prill has a density of 1.2 g/cc, this same density could be achieved by using
an explosive composition in accordance with the invention in which a non-sensitized
emulsion having a density of 1.32g/cc is used in ation with a void—sensitized
emulsion having a density of 0.8 g/cc at a volume ratio of 78:22. The same density could
of course be achieved using different volume tions of emulsions having different
densities. For example, a density of 1.32 g/cc could beachieved using the following
combinations of ies and volume ratios for the non—sensitized and sensitized
emulsions respectively: 1.32 g/cc and 1.0 g/cc at 67:33; 1.32 g/cc and 0.9 g/cc at 73:27;
and 1.32 g/cc and 0.8 g/cc at 78:22. The VOD of each explosive composition will be
different, and a target VOD may be achieved by varying the volume ratio and density of
the emulsion components whilst maintaining density matching with the prill—containing
product. In proceeding in this way it is possible to provide emulsion-based explosive
compositions that offer similar blasting performance to prill—based products.
Explosive compositions in accordance with the present invention may be made by
ng together a first liquid energetic material and a second liquid energetic material to
provide regions of the first liquid energetic materials and regions of the second liquid
energetic material, wherein the first liquid tic material is sensitized with ent
2,0 sensitizing voids to render it detonable and wherein the second energetic liquid has
different detonation teristics from. the sensitized first liquid tic material.
ng of the individual liquid energetic als may take place during loading into a
blasthole but this is not essential and blending may be undertaken in advance provided that
delivery into a blasthole does not disrupt the intended structure of the explosive
composition The liquid energetic materials used may be the same or different.
In an embodiment of the invention an explosive composition may be prepared by mixing
of streams of individual components using a static miXer (see Figure 3 and the sion
below). By this mixing methodology the streams of the individual components are split
into sheets that have a mean thickness typically in the range 2 to 20 mm. The
characteristics of the sheets can be adjusted by ing the mixing methodology, for
example by varying the number of mixing elements in the static mixer. The corresponding
2012/001527
process diagram is shown in Figure 2. With reference to that figure the experimental rig
comprises two emulsion holding s ANEl and A'NEZ. Two progressive cavity (PC)
metering pumps PC Pump 1 and PC Pump 2 supply streams of the emulsions into an interchangeable
mixing head. The maSs flow of the individual fluid streams is set up by
calibration of the metering pumps and cross-checking against the total mass flow via into
the inter-changeable mixing head. Blending is done in a continuous manner in the closed
pipe of an interchangeable mixing head module.
By way of e, in the fluid stream (1), a void-free ammonium nitrate emulsion
(ANEl) is mixed in line with an aqueous solution of sodium nitrite in a gasser (mixing
point using an arrangement of SMX type static mixers. After completion of the gassing
reaction the emulsion stream (1) will have a particular density. The second fluid stream
(2) may consistof a voidcfrec ammonium nitrate emulsion having a higher density than the
gassed on stream (1).
The inter-changeable mixing head is comprised of two parts; The first part has two
separate inlet channels for the entry of each emulsion stream and a baffle just before the
entrance to the first static mixer t to ensure separation of the individual streams in
the mixing section. The changeable mixing head is 50 mm diameter and length of
228 mm.
A helical static mixer (having 3 elements; see Figure 3) was used for layering the void
sensitized on into the void—free high density emulsion continuum. Altematingv
layers of void rich. and void free are achieved by repeated division, transposition and
recombination of liquid layers around a static mixer, Addition of further static mixer
elements (for example No 4, 5& 6) reduces the thicknessof the layers produced,
Embodiments of the present invention are rated with reference to the following non—
limiting examples.
. 30
.
Example 1
In the absence of AN prill, bulk emulsion explosives rely on the inclusion of voids for
ization. In such ons the oxidizer salt used is typically ammonium nitrate.
When an um nitrate emulsion (ANE) is sensitized with voids, for example by
chemical gassing or by using balloon (mb) inclusion, the void size is approximately
—500 um in diameter. When voids are used to sensitize such emulsion explosives they
reduce the formulation density. However, homogeneous ization of emulsions with
voids will result in much higher velocity of detonation (VOD) than c0rrespond-ing
formulations of a similar density containing AN prill.
This example details explosive compositions made up of two emulsion components: a non—
sensitized ammonium nitrate on ) and a sensitized ammonium nitrate
emulsion (s—ANE). The non-sensitized emulsion in this example has an. ammonium nitrate
concentration of approximately 75 wt% and a density of approximately 1.32 g/cc. The
s-ANE has an ammonium nitrate concentration of approximately 75 wt% and a variable
density from 0.8—1.2 g/cc using either chemical gassing or micro-balloons of a er. of
approximately 40 um. Various explosive compositions in accordance with the invention
can be fornied by blending these emulsions and by adjusting the ratio of n—ANEzs-ANE in
the formulation. As the ratio is adjusted from the es of 100% n-ANE to 100%
s-ANE in a ‘200 mm diameter cardboard cylinder, the VOD ranges from a failure to
detonate for the non-sensitized emulsion to over 6000 m/s for 100% s-ANE. However, the
ability to isolate discrete regions of s—ANE (or n-ANE) Within a bulk charge of n-ANE (or
s-ANE) allows a geometric formulation variable to l detonation velocity and blasting
. teristics between these extremes.
The method of manufacturing explosive compositions in accordance with the invention is
based on blending two liquid energetic materials. The first phase is conventionally
sensitized with voids, the second phase with no or very few added voids, the blending
being such that the two phases remain largely distinct from each other, and the diameter.
sheet thickness, etc. of the distinct phases are typically in the range from 0.2 mm to
100 mm.
es of Homogeneous s-ANE charges
To fy how homogeneous s-ANE would perform without any n-ANE inclusions, a.
series of control charges were measured for VOD. The control shots contained ammonium
e emulsion and plastic Expancel micro-balloons of approximate 40 um average
diameter. The emulsion and micro—balloons were mixed to form a homogeneous blend
ranging in density from 0.8 g/cc to 1.2 g/cc based on the amount of micro—balloons used.
The VOD results can be seen in Table 1 below. A standard VOD measurement technique
was used in which compositions were submitted for a tion test in various unconfined
diameters. Charges were detonated using Pentolite primers that were initiated with a No8
industrial strength detonator. The velocity of detonation (VOD) of the charges was
measured by utilising a micro—timer unit and optical fibres.
Table 1
Charge VOD
Density
Name (km/s)
(g/cc)
Control 0.9 09
Control 1.0
As the density increased from 0.8 to 1.2 g/cc the VOD sed from 4.5%).3 km/s.
y, the homogeneous sensitization of emulsion with 40 mm diameter voids produces
an emulsion explosive of higher velocity of detonation at increasing densities as would be
2‘0 I expected.
In accordance with the t invention it is possible to reduce the VOD of these
on only eXplosives for each of the above densities, using the same size voidage, i.e.
40 um diameter micro—balloons. To do this, regions of non-sensitized emulsion (n-ANE)
WO 86572
were introduced into the sensitized on to reduce the bulk VOD. The non—sensitized
ammonium nitrate emulsion has a density of approximately 1.32 g/cc and consequently
increases the overall density of the charge upon simple addition. ore to compare
s of equal density to the ls, sensitized emulsion (s—ANE) density must be
sufficiently low that subsequent ton-ANE inclusion, the overall charge density is that_
desired.
The experimental arrangement is shown schematically in Figure 4 and by way of
photograph (from above) in Figure 5 where a continuous phase of s-ANE (light colour) has
small 120 ml volume cups of n—ANE (dark colour) distributed within the charge. The
s—ANE (0.8 g/cc) and the n-ANE (1.32 g/cc) combine to give a mixture of emulsions
having acharge density of 1.0 g/cc. Shown in Table 2 below are the results of shots fired
at this overall charge density. The first explosive composition is the control (as described
above)' consisting of only neous phase of ammonium nitrate emulsion and
Expancel micro-balloons. This explosive ation had a VOD of 5.6 km/s.
The charge labeled M1.0,SO.9 in Table 2 below has an l charge density of 1.0 g/cc,
and contains two te emulsion phases as per the present invention. A continuous
phase of s-ANE (emulsion + micro—balloons, density of 0.9 g/cc) occupying a total of
76.2 % of the charge volume, and within this continuous phase are dispersed regions of
n-ANE (density of 1.32 g/cc) which occupy the remaining 23.8 % of the charge volume.
For the purposes of laboratory testing these dispersed regions are in fact 120 ml cardboard
cups filled with the n—ANE and placed randomly within the continuous emulsion, thus
allowing a physical boundary for isolation of discrete emulsion phases. The combined
density of the s—ANE and n-ANE in the charge was 1.0 g/cc. However, the VOD was
found to be 4.9 km/s. This is a 131.2% ion in VOD ed with control 1.0.
Indeed, the VOD of charge M1.0,S0.'9 is closer to the VOD of the l 0.9 detailed
above in Table 1 which is the same density as the continuous emulsion phase of this
charge.
The charge labeled 'M1.0,SO.8 has an overall charge density of 1.0 g/cc, and a continuous
s-ANE of 0.8 g/cc (615 vol%). Again, the charge has distributed cups (120ml each) of
' n-ANE (38.5 vol%). The VOD of this charge
was found to be 4.2 km/s, which is a 25%
reduction in VOD compared to control 1.0. Once again the VOD for charge M1.0,SO.8
more closely matches the control shot at the same density as the continuous emulsion
phase, i.e. l 0.8 (Table l) 4.5 km/s.
Table 2
Charge Continuous Emulsion Dispersed Emulsion
. Density density
Name Const1tuents_ Constituents.
' (g/cc) °o
14—10309-(g/cc) 1.0
ML,.OS08 1.0 .NE+mb .1.4'62 '
. _
HANFO 1. 0 ANE + prill 1..0
VGlOO ANE + EPS
Also shown in Table 2 is the VOD for heavy ANFO (HANFO 1.0). This heavy ANFO is a
homogeneous blend of emulsion (23 wt%) and ANFO(77 wt%), and as such does not have
discrete continuous or sed on phases as described for the mixtures of emulsion
systems in'accordance with the present invention. However, similar to the mixtures of
emulsion and control 1.0 charges the heavy ANFO, HANFO 1.0, also has an overall
charge density of 1.0 g/cc. Heavy ANFO charges rely on porous nitrOpril for sensitization,
and the resulting VOD ed was found to be 3.6 km/s. The last charge listed in Table 2
gives the results for VGlOO which consists of emulsion (99.62 wt%) homogeneously
mixed with expanded polystyrene (EPS, 0.38 wt%) of approximately 4 mm diameter for
sensitization. As ’with heavy ANFO, the on and expanded polystyrene are a
homogeneous blend throughout the bulk charge and therefore have no discrete dispersed or
uous phases. The VOD for this product was found to be 3.6 km/s.
An important feature of the above charges is that the Control 1.0, M1.0,SO.9 and
M1.0,SO.8 s all have the same total quantity of emulsion and small 40 um voids in
the overall charges. Naturally, having equivalent formulation, they also have the same
WO 86572
density, 1.0 g/cc. However, when the internal structure of the explosive charge contains
two distinct phases of s-ANE and n-ANE, the VOD of the charge is reduced from the
homogeneously mixed analogue such as Control 1.0. One important aspect of the invention
is that emulsion only explosives utilizing small 40 um voids can be formulated to have
VOD characteristics of prill and EPS containing products.
Mixtureof Emulsion (MOE) Charges of overall density 1.1 g/cc
As shown in Table 3 below, all charges have an l density of 1.1 g/cc. The Control
1.1 was a single phase of s—ANE having a density of 1.1 g/cc. The VOD of this control shot
was found to be 6.0 km/s. The charge labeled Ml.1, 81.0 has a continuous s-ANE phase of
y 1.0 g/cc occupying 68.4 % of the total charge volume. The remaining volume of
the charge was made up of n-ANE in 120ml cups distributed throughout the charge. The .
VOD for charge M1.l,Sl.0 was found to be 5.1 km/s. rly, charge ML], $09 was
made up of a continuous emulsion phase of s—ANE having a density of 0.9 g/cc occupying
52.4 % of the total charge volume and distributed therein 120 ml cups of n-ANE
accounting for the ing 47.6 % of total charge volume. Charge M1,], $09 was found
‘to have a VOD of 4.6 km/s.
Charge M1.1,SO.8 was the first charge loaded with n—ANE as the continuous emulsion
. Therefore, charge M1.1,SO.8 has nsitized continuous emulsion phase
accounting for 58.8 % of the total charge volume. Distributed within this charge was
s—ANE having a density of 0.8 g/cc contained in 120ml cups and accounting for the
remaining 41.2 vol% of the total . The VOD for charge M1.l,SO.8 was found to be
3.2 km/s. This is a significant reduction to Control 1.1 charge. In addition this’low VOD is
also lower than heavy ANFO charge HANFO 1.1, thus confirming that mixtures of
emulsions in accordance with the invention can achieve low detonation velocities down to
levels not previously achievable by small 20—100 um diameter voids, and comparable to
nitropril containing emulsion products.
Table 3
Continuous Emulsion Dispersed Emulsion _l VOD
Density density ‘ density Vol
Name Constituents Constltuents. '
, (km/s)
(g/cc) (g/cc) (g/cc) %
Control 1 - 1 ANE + mb m 6.0
—-—m--47.6 4.6
M1 1 so 8 ANE 1.32 58.8 ANE + mb 41.2 3.2
HANFO 1.1 ANE + prill 1oo 3.8
Mixture of Emulsion (MOE) Charges of overall y 1.2 g/cc’
A series of charges all having an overall density of 1.2 g/cc is detailed in Table 4 below.
The control charge was a homogenous blend of ammonium nitrate on and micro-
balloons of density 1.2 g/cc, and having a VOD of 6.3 km/s. The ing s
detailed in Table 4 had a continuous emulsion phase of n-ANE. Charge M1.2,Sl.0 had a
continuous n-ANE phase accounting for 63.9 % of the total charge volume. The s-ANE
used had a density of 1.0 g/cc and was distributed within the n—ANE in 120 ml cups
occupying remaining 361 % of the total charge volume. Charge Ml.2,Sl.0 'had a
measured VOD of4.3 km/s.
Charge M1.2,SO.9 included a continuous emulsion phase of n-ANE. This accounted for
73.1 vol% of the total charge. The remaining 26.9 vol% was made up of a s—ANE of
y 0.9 g/cc. M1 2809 had a VOD of only 2.3 km/s. This low VOD could be close to
failure as a consequence of such a high volume of n-ANE. Indeed M1.2,SO.8 with 78.0
vol% of n-ANE failed to initiate and over half of the test charge remained after attempted
initiation with a 400g Pentolite booster.
Table 4
Charge uous Emulsion Dispersed Emulsion
Density density Vol y Vol
Name Constituents Constituents (km/s)
(g/cc) (g/cc) (g/cc)
M1.2,Sl.0_63.9 ANE+mb 361 4.3
L«1.2,.309 1.2 73.1 ANE+mb m- 2.3
M1.,.2308 1.2 132 78.0 ANE+mb “--
HANFO 1. 2 1. 2 ANE + prill
. --
gh not experimentally measured, there are clearly opportunities to incorporate solid
oxidizers, such as AN prill, in one or both of the phases to further fine tune ,the total energy
available and the heave energy/shock energy balance. There are also clearly opportunities
to incorporate sub-mm energetic solid fuels, such as aluminum, in one or both of the
phases to further significantly enhance the heave energy while achieving exceptionally low
shock es.
Example 2 - Gassed emulsion at 1.22 g/cm3
This example serves as a baseline to trate the features of the invention.
Experimental samples were prepared in a specially designed emulsion experimental rig.
The corresponding process diagram is shown in Figure 2. With reference to that figure the
experimental rig comprises two on holding hoppers ANEl and ANEZ. Two
metering pumps PC Pump 1 and PC Pump 2 supply streams of the emulsions into ane
inter—changeable mixing head. The mass flow of the individual fluid streams is set up by
calibration of the metering pumps and cross-checking against the total mass flow via into
the inter—changeable mixing head. Blending is done in a continuous manner in the closed
pipe of a interchangeable mixing head module.
The inter—changeable mixing head is sed of two parts. The first part has two
separate inlet channels for the entry of each emulsion stream and a baffle just before the
>27-
entrance to the first static mixer t to ensure separation of the individual streams in
the mixing section. The inter—changeable mixing head is 50 mm diameter and length of
228 mm.
A Kenics static mixer (having 3 elements; see Figure 3) was used for ng the void
sensitized emulsion into the void-free high density emulsion. Alternating layers of void
rich and void free emulsions are achieved by ed division, transposition and
recombination of liquid layers around a static mixer. In this way, the components of
emulsion to be mixed are spread into a large number of layers. A y d and
uniform shear field is generated through mixing. Addition of further static mixer elements
(for example No 4, 5 & 6) reduces the ess of the layers produced.
The starting emulsion at a density of 1.32 g/cm3 was delivered by a progressive cavity
pump at a rate of 3 kg/min. A 4% mass sodium nitrite solution was injected into the
flowing emulsion stream at a rate of 16 g/min by means of a gasser (gear) pump and
‘ sed in a series of static mixers. 1 m long cardboard tubes with internal diameters
ranging from 40 to 180 mm were loaded with emulsion and allowed to gas.
The density change of the gassing emulsion was determined in a plastic cup of known
mass and volume. The emulsion was initially filled to the top of the cup and levelled off.
As the. gassing reaction progressed, the-emulsion rose out of the top of the cup and was
levelled off periodically and weighed. The density was determined by dividing the mass of
emulsion in the cup by the cup volume. Charges were fired once the sample cup reached
the target density of 1.22 g/cm3.
Charges larger than 70 mm were ted with a single 400 g Pentex PPP booster, whist
smaller charges were initiated with a l50 g Pentex H booster. ityflof tion
(VOD) was determined using an MREL Handitrap VOD recorder. The VOD ranged from
2.9 km/s for the 70 mm diameter charge to 4.3 km/s at 180 mm. Charges smaller than
‘30 70 mm failed to sustain detonation. The results are shown in Figure 6.
_ 23 _
Example” 3 _. MOE 25 at 1.22 g/cm3
This example demonstrates the performance of MOE25, i.e. a mixture of emulsion with
%, mass gassed and 75% ungassed emulsion
MOE25 was prepared. using the apparatus mentioned in Example 2. The base emulsion
ty 1.32 g/cm3‘) was delivered by two ssive cavity pumps, PCI and PC2. The
base emulsion formulation was identical to Example 2 and was the same for both pumps.
PCl pumped ungassed emulsion at a flow rate of 4 kg/min. PC2 delivered emulsion at
1.3 kg/min with gasser (4% NaNOz solution) injected by a gasser '(gear) pump. The
emulsion was blended by a static mixer consisting of three helical mixing elements and
loaded into cardboard tubes with internal diameters ranging from 70 to 1.80 mm. The
gassed emulsion target density was 0.99 g/cm3 providing an overall density of 1.22 g/cm3
for the e of gassed and ungassed emulsion.
Charges were initiated with a single 400 g Pentex PPP booster with VOD measured with
an MREL handitrap VOD recorder. The VOD ranged from 2.5 km/s for the 90. mm charge
to 3.7 km/s at 180 mm, a cant reduction relative to the regular gassed emulsion
described in Example 2. Charges with diameters smaller than 90 mm. failed to sustain
detonation. The results are shown in Figure 7. The d VO__D of MOE25 indicates
that this formulation, sing a e of void rich and void nt materials,
exhibits a lower shock energy and higher heaveenergy relative to regular gassed emulsion
containing randomly dispersed voids at the same overall density.
Example 4 - MOE 50 at 1.22 g/cm3
This example demonstrates the performance of MOESO, i.e. a mixture of emulsion with
50% mass gassed and 50% ungassed emulsion
MOESO was prepared using the apparatus mentioned in Example 2. The base emulsion
(density 1.32 g/cm3) was delivered by two progressive cavity pumps, PCI and PC2 and
was identical to the us two examples. PCl pumped ungassed emulsion at a flow rate
'of 3' kg/min. PC2 delivered emulsion at 3 kg/min with gasser (4% NaNOz solution)
injected by a gasser (gear) pump. The void rich and void'free emulsions were blended by a
static mixer consisting of three helical mixing elements and loaded into cardboard tubes
with internal diameters ranging from 70 to 180 mm. The gassed on target density
was 1.13 g/cm3 providing an overall y of 1.22 g/cm3 for the mixture of gassed and
, ungassed emulsion.
Charges were initiated with a single 400 g Pentex PPP booster with VOD measured with
an MREL rap VOD recorder. The VOD ranged from 2.8 km/s for the 80 mm charge
to 3.9 km/s at'180 mm. Charges with diameters smaller than 80 mm failed to sustain
detonation. The results are shown in Figure 8. VOD results for MOESO were between
those of gassed emulsion and M01325, indicating ediate shock and heave energies.
This demonstrates that explosive performance can be tailored to suit different blasting
applications by. adjusting the tion of void rich and void deficient materials at the
same overall density.
Claims (6)
1. An explosive composition sing an emulsion explosive and sensitizing voids, wherein the sensitizing voids are present in the emulsion explosive with a non-random distribution, wherein the emulsion explosive comprises regions of a first emulsion explosive and regions of a second emulsion explosive, wherein the first emulsion explosive is sensitized with sufficient sensitizing voids to render it detonable and wherein the second emulsion explosive has different detonation teristics from the ized first emulsion ive and wherein the explosive composition does not contain ammonium nitrate prill.
2. The explosive ition of claim 1 consisting essentially of the emulsion explosive.
3. The explosive composition of claim 1 consisting of the emulsion explosive.
4. The explosive composition of any one of the ing claims, wherein the average void size is from 20 µm to 5 mm.
5. The explosive composition of any one of claims 1 to 4, that has been formulated to match ANFO or a AN prill based explosive product with respect to density and velocity of detonation.
6. A method of producing an ive composition, the method comprising blending together a first emulsion explosive and a second emulsion explosive to provide regions of the first emulsion explosive and regions of the second emulsion explosive, wherein the first emulsion explosive is sensitized with sufficient sensitizing voids to render it detonable and wherein the second emulsion explosive has different detonation characteristics from the sensitized first emulsion explosive, and n the ive composition does not contain um nitrate prill.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AU2011905262A AU2011905262A0 (en) | 2011-12-16 | Method of blasting | |
| AU2011905262 | 2011-12-16 | ||
| PCT/AU2012/001527 WO2013086572A1 (en) | 2011-12-16 | 2012-12-13 | Explosive composition |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| NZ625171A NZ625171A (en) | 2016-11-25 |
| NZ625171B2 true NZ625171B2 (en) | 2017-02-28 |
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