U.S. patent application number 16/087440 was filed with the patent office on 2019-02-21 for energetic materials.
This patent application is currently assigned to Nederlandse Organisatie voor toegepast-natuurweten schappelijk onderzoek TNO. The applicant listed for this patent is Nederlandse Organisatie voor toegepast-natuurweten schappelijk onderzoek TNO. Invention is credited to Michiel Hannes STRAATHOF, Aafke Tessa TEN CATE, Christoffel Adrianus VAN DRIEL.
Application Number | 20190055171 16/087440 |
Document ID | / |
Family ID | 55588130 |
Filed Date | 2019-02-21 |
United States Patent
Application |
20190055171 |
Kind Code |
A1 |
STRAATHOF; Michiel Hannes ;
et al. |
February 21, 2019 |
ENERGETIC MATERIALS
Abstract
The invention is directed to a radiation curable energetic
composition, to a method of forming a three-dimensional energetic
object, to a three-dimensional energetic object, and to uses of the
radiation curable energetic composition. The radiation curable
energetic composition of the invention comprises (a) one or more
polymerisable components, (b) one or more polymerisation
photoinitiators, and (c) one or more energetic components.
Inventors: |
STRAATHOF; Michiel Hannes;
(Delft, NL) ; VAN DRIEL; Christoffel Adrianus;
(Delft, NL) ; TEN CATE; Aafke Tessa;
(?s-Hertogenbosch, NL) |
|
Applicant: |
Name |
City |
State |
Country |
Type |
Nederlandse Organisatie voor toegepast-natuurweten schappelijk
onderzoek TNO |
's-Gravenhage |
|
NL |
|
|
Assignee: |
Nederlandse Organisatie voor
toegepast-natuurweten schappelijk onderzoek TNO
's-Gravenhage
NL
|
Family ID: |
55588130 |
Appl. No.: |
16/087440 |
Filed: |
March 22, 2017 |
PCT Filed: |
March 22, 2017 |
PCT NO: |
PCT/NL2017/050174 |
371 Date: |
September 21, 2018 |
Current U.S.
Class: |
1/1 |
Current CPC
Class: |
C06B 21/0083 20130101;
B29C 64/124 20170801; C06B 21/0025 20130101; C06B 25/34 20130101;
C06B 45/10 20130101; C06B 21/0058 20130101; B33Y 70/00 20141201;
B33Y 10/00 20141201; C06B 45/00 20130101 |
International
Class: |
C06B 45/10 20060101
C06B045/10; C06B 25/34 20060101 C06B025/34; C06B 21/00 20060101
C06B021/00; B29C 64/124 20060101 B29C064/124; B33Y 10/00 20060101
B33Y010/00; B33Y 70/00 20060101 B33Y070/00 |
Foreign Application Data
Date |
Code |
Application Number |
Mar 22, 2016 |
EP |
16161647.9 |
Claims
1. A radiation curable energetic composition, comprising (a) one or
more polymerisable components, (b) one or more polymerisation
photoinitiators, and (c) one or more energetic components.
2. The radiation curable energetic composition of claim 1, wherein
said one or more polymerisable components comprise fuel and
oxidiser.
3. The radiation curable energetic composition of claim 1, wherein
said polymerisable components comprise (al) one or more free
radical polymerisable components, and said polymerisation
photoinitiators comprise (bl) one or more polymerisation
photoinitiators for free radical polymerisation.
4. The radiation curable energetic composition of claim 3, wherein
said free radical polymerisable components comprise one or more
components selected from the group consisting of an aliphatic
(meth)acrylate, an aromatic (meth)acrylate, a cycloaliphatic
(meth)acrylate, an arylaliphatic (meth)acrylate, and a heterocyclic
(meth)acrylate.
5. The radiation curable energetic composition of claim 1, wherein
said polymerisable components comprise (a2) one or more
cationically polymerisable components, and said polymerisation
photoinitiators comprise (b2) one or more polymerisation
photoinitiators for cationic polymerisation.
6. The radiation curable energetic composition of claim 5, wherein
said cationically polymerisable component comprises one or more
components selected from the group consisting of cyclic ether
compounds, cyclic acetal compounds, cyclic thioether compounds,
spiro-orthoester compounds, cyclic lactone compounds, and vinyl
ether compounds.
7. The radiation curable energetic composition of claim 5, wherein
said cationically polymerisable component comprises one or more
components selected from the group consisting of a diglycidyl ether
compound, an epoxy compound, and an oxetane compound.
8. The radiation curable energetic composition of claim 1, wherein
at least part of said energetic component comprises one or more
components selected from the group consisting of
2,4,6-trinitrotoluene (TNT),
cyclo-1,3,5-trimethylene-2,4,6-trinitramine (RDX),
cyclotetramethylenetetranitramine (HMX), pentaerythrol tetranitrate
(PETN), 3-nitro-1,2,4-triazol-5-one (NTO), nitroglycerine (NG),
nitrocellulose (13% N) (NC), ammonium nitrate (AN), ammonium
perchlorate (AP),
2,4,6,8,10,12-(hexanitro-hexaaza)tetracyclododecane (CL20 or HNIW),
1,3,3-trinitroazetidine (TNAZ), octanitrocubane (ONC),
1,1-diamino-2,2-dinitroethene (FOX-7), ammonium dinitramide (ADN),
2,2,2-trinitroethylacrylate, 2,2,2-trinitroethylmethacrylate
(TNEM), 2,2-dinitropropylacrylate (DNPA), 2-nitroethylacrylate, and
pentaerythritoltrinitrate acrylate.
9. The radiation curable energetic composition of claim 1, wherein
at least part of said energetic components are polymerisable
components.
10. The radiation curable energetic composition of claim 1, wherein
at least part of said energetic component is solid.
11. The radiation curable energetic composition of claim 10,
wherein said solid energetic component is in the form of
particulates having an average particle size as determined by laser
diffraction of 0.5-100 .mu.m.
12. The radiation curable energetic composition of claim 10,
wherein said solid energetic component is in the form of
particulates having an average particle size as determined by laser
diffraction of 1-60 .mu.m.
13. The radiation curable energetic composition of claim 10,
wherein said solid energetic component is in the form of
particulates having an average particle size as determined by laser
diffraction of 2-40 .mu.m.
14. The radiation curable energetic composition of claim 10,
wherein said solid energetic component is in the form of
particulates having an average particle size as determined by laser
diffraction of 2-10 .mu.m.
15. The radiation curable energetic composition of claim 1, wherein
said at least part of said energetic component is radiation
curable.
16. The radiation curable energetic composition of claim 1, further
comprising a hydroxy functional component.
17. The radiation curable energetic composition of claim 1,
comprising 5-45% by total weight of the composition of
polymerisable components; 0.05-3% by total weight of the
composition of polymerisation photoinitiators; 30% or more by total
weight of the composition of energetic components; and 0-10% by
total weight of the hydroxy functional component.
18. The radiation curable energetic composition of claim 1,
comprising 10-40% by total weight of the composition of
polymerisable components; 0.1-2% by total weight of the composition
of polymerisation photoinitiators; 40-95% by total weight of the
composition of energetic components; and 0.5-8% by total weight of
the hydroxy functional component.
19. The radiation curable energetic composition of claim 1,
comprising 15-35% by total weight of the composition of
polymerisable components; 0.2-1.5% by total weight of the
composition of polymerisation photoinitiators; 45-90% by total
weight of the composition of energetic components; and 1-5% by
total weight of the hydroxy functional component.
20. The radiation curable energetic composition of claim 1, further
comprising one or more dyes and/or pigments.
21. The radiation curable energetic composition of claim 20,
wherein the amount of dyes and/or pigments in the radiation curable
energetic composition is 0-0.1% by total weight of the
composition.
22. The radiation curable energetic composition of claim 20,
wherein the amount of dyes and/or pigments in the radiation curable
energetic composition is 0.005-0.02% by total weight of the
composition.
23. The radiation curable energetic composition of claim 1, further
comprising one or more selected from photosensitisers, fillers,
stabilisers, antioxidants, wetting agents, defoamers, and
surfactants.
24. A method of forming a three-dimensional energetic object
comprising the steps of forming and selectively curing a layer of
the radiation curable energetic composition of claim 1 with actinic
radiation and repeating the steps of forming and selectively curing
said layer of the radiation curable energetic composition a
plurality of times to obtain a three-dimensional energetic
object.
25. A three-dimensional energetic object formed from the radiation
curable energetic composition of claim 1.
26. A method of preparing ballistics, pyromechanical devices,
fireworks or propellant rockets, said method comprising using a
radiation curable energetic composition of claim 1.
27. A ballistic, pyromechanical device, firework or propellant
rocket prepared from the radiation curable energetic composition of
claim 1.
Description
[0001] The invention is directed to a radiation curable energetic
composition, to a method of forming a three-dimensional energetic
object, to a three-dimensional energetic object, and to uses of the
radiation curable energetic composition.
[0002] Propellant charges are used in pyrotechnics and ballistics
in order to accelerate a piston or a projectile. Typically, the
propellant charge is ignited by a primer, which is a small amount
of sensitive explosive. Gases produced by combustion of the
propellant charge cause a rapid build-up of pressure. When a
certain pressure is reached, the projectile begins to move, thereby
causing an increase in chamber volume. After a pressure maximum is
reached, typically the pressure decreases relatively rapidly due to
the expansion of the chamber volume.
[0003] A propellant charge is an amount of relatively insensitive
but powerful energetic material that propels the projectile out of
the gun barrel. Various types of propellant charges having
different composition and geometries are used for different
applications and purposes.
[0004] The propellants used are typically solid. Examples of
propellants that are in use today include gun powders, including
smokeless powders. Smokeless powders may be considered to be
classed as either single or multi-base powders. Conventional
smokeless powders consist mainly of nitrocellulose. Typical
production processes include drying of water-wet nitrocellulose,
mixing and kneading with ether and alcohol and other constituents,
pressing the propellant dough through a die, cutting the obtained
strand into propellant grains, and drying these grains. Although
called powders, they are not in powder form, but in granule
form.
[0005] In single-base propellants, nitrocellulose is the main
energetic material present. Other ingredients and additives are
added to obtain suitable form, desired burning characteristics, and
stability.
[0006] The multi-base propellants may be divided into double-base
and triple-base propellants, both of which contain typically
nitroglycerin to facilitate the dissolving of the nitrocellulose
and enhance its energetic qualities. The nitroglycerin also
increases the sensitivity, the flame temperature, burn rate, and
tendency to detonate. The higher flame temperature serves to
decrease the smoke and residue, but increases flash and gun-tube
erosion.
[0007] Triple-base propellants are double-base propellants with the
addition of nitroguanidine to lower the flame temperature, which
produces less tube erosion and flash. The major drawback is the
limited supply of the raw material nitroguanidine.
[0008] In the multi-base propellants, the multiple ingredients are
evenly distributed in the propellant charge.
[0009] Once ignition is achieved, it is desirable to have the
propellant burn in a controlled manner from the surface of the
propellant charge inwardly. As the propellant is initially ignited
and gases are being generated, the projectile is either at rest or
moving relatively slowly. Thus, gases are being generated faster
than the volume of the chamber is increasing. As a result of this,
the pressure experienced increases. As the projectile accelerates,
the volume of the chamber increases at a rate which ultimately
surpasses the rate of gas generation by the burning of the
propellant material. The transition corresponds to the point of
maximum pressure in the combustion chamber. Thereafter the pressure
decreases as the projectile continues to accelerate thus increasing
the volume of the chamber at a rate faster than the increase in
volume of gases being generated by the propellant burn.
[0010] Solid propellants are designed to produce a large volume of
gases at a controlled rate. Gun barrels and some rocket casings are
designed to withstand a fixed maximum gas pressure. The pressure
generated can be limited to this maximum value by controlling the
rate of burning of the propellant. In the art, the burn rate is
controlled by varying the following factors: [0011] (1) the size
and shape of the grain, including perforations, [0012] (2) the web
thickness or amount of solid propellant between burning surfaces;
the thicker the web, the longer the burning time., [0013] (3) the
linear burn rate, which depends on the gas pressure and the
chemical composition of the propellant, including volatile
materials, inert matter, and moisture present.
[0014] When a propellant burns in a confined space, the rate of
burning increases as both temperature and pressure rise. Since
propellants burn only on exposed surfaces, the rate of gas
evolution or changes in pressure will also depend upon the area of
propellant surface ignited.
[0015] The use of perforations in a propellant charge so as to
control the rate of burning is for instance known from U.S. Pat.
No. 4,386,569. This patent is based on the insight that the burn
rate of the propellant material, i.e. the burn characteristics of
the propellant charge, not only depends on the physical and
chemical characteristics of the propellant material itself, but
also depends on the shape of the propellant charge. U.S. Pat. No.
4,386,569 accordingly describes a propellant grain of generally
cylindrical shape having a plurality of longitudinal substantially
parallel perforations extending there through, the cross-sectional
locations of said perforations being such that the interstitial
distances between adjacent perforations is substantially equal and
substantially equals the extrastitial distances between the
perimetric perforations and the outer surface of the grain wall.
With the conventional preparation methods (such as extrusion), only
charges of limited geometries heretofore could be economically
manufactured. Consequently, the number of variables that could be
manipulated to achieve a given specified performance was limited.
It would therefore be desirable to find improved preparation
methods that allow further variables to be manipulated in order to
create a prolonged maximum pressure. Such improved preparation
methods, however, may also require special energetic
compositions.
[0016] Curable energetic compositions have been explored in the art
as well. For example, both U.S. Pat. No. 4,050,968 and U.S. Pat.
No. 4,283,237 describe a curable explosive composition that may be
cured using heat. As understood, curing energetic compositions by
heat may lead to undesirable safety issues because of proximity to
the decomposition temperature of energetic materials that are
present. Additionally, heat curing can lead to bad resolution in
additive manufacturing processing, and in general yields a process
that is difficult to control.
[0017] Object of the present invention is to overcome one or more
of the disadvantages of the prior art.
[0018] The inventors found that this objective can, at least in
part, be met by providing an energetic composition that is suitable
for additive manufacturing, and may also be useful for other
processing techniques. This allows manufacturing of propellant
charges or grains with remarkable degrees of freedom. For example,
such an energetic composition allows manufacturing propellant
charges or grains having linear burn rate gradients in multiple
directions. Accordingly, in a first aspect the invention is
directed to a radiation curable energetic composition, comprising
[0019] (a) one or more polymerisable components, [0020] (b) one or
more polymerisation photoinitiators, and [0021] (c) one or more
energetic components.
[0022] The term "energetic component" as used in this application
is meant to refer to any substance or mixture of substances that,
through chemical reaction, is capable of rapidly releasing energy.
In the context of this application, an energetic component
comprises fuel and oxidiser. Typically, energetic materials are
solid, liquid or gaseous substances or mixtures which are capable
of very fast chemical reactions without the use of additional
reactive species (e.g. oxygen). The reaction can be initiated by
means of mechanical, thermal or shock wave stimuli. Generally the
reaction products are gaseous. Energetic components can be applied
in explosives, rocket and gun propellants, pyrotechnics, gas
generators etc. The energetic components of the present invention
are distinguished from solid propellants used in hybrid rockets,
which are only capable of a chemical reaction once they are brought
into contact with the additional liquid (or gas) propellant that is
initially kept separate from the solid propellant. Such propellants
for hybrid rockets are, for instance, known from US-A-2009/0 217
525 and US-A-2013/0 042 596.
[0023] The term "energetic composition" as used in this application
is meant to refer to a composition that comprises one or more
energetic components.
[0024] The term "burn rate" as used in this application is meant to
refer to the rate at which a propellant charge releases gas during
combustion.
[0025] The burn rate is commonly measured as the mass of
pyrotechnic composition consumed per unit time, e.g., g/s. The term
"linear burn rate" as used in this application on the other hand is
meant to refer to the distance the burning surface of a pyrotechnic
composition advances inwardly (perpendicular to the burning
surface) per unit time. The linear burn rate is commonly reported
as distance per unit time, e.g., mm/s.
[0026] The term "additive manufacturing" as used in this
application is meant to refer to a method of making a
three-dimensional solid object from a digital model. Additive
manufacturing is achieved using an additive process, where
successive layers of material are laid down in different shapes.
Additive manufacturing is sometimes known as "3D printing",
"additive layer manufacturing" (ALM) or "rapid prototyping". More
in particular, additive manufacturing is a group of processes
characterised by manufacturing three-dimensional components by
building up substantially two-dimensional layers (or slices) on a
layer by layer basis. Each layer is generally very thin (for
example between 20-1000 .mu.m, 20-800 .mu.m, 20-500 .mu.m, or even
20-100 .mu.m) and many layers are formed in a sequence with the
two-dimensional shape varying on each layer to provide the desired
final three-dimensional profile. In contrast to traditional
"subtractive" manufacturing processes where material is removed to
form a desired component profile, additive manufacturing processes
progressively add material to form a net shape or near net shape
final component.
[0027] Advantageously, the invention allows to better regulate the
burning of the propellant charge or grain so as to prolong the
period of maximum pressure at which the projectile is accelerated.
As a result of the prolonged period of maximum pressure, the
projectile will be given a higher speed. Further, the production of
energetic objects by means of additive manufacturing allows to
provide the end product with specific properties that were
heretofore not possible. The composition may also be extruded,
followed by curing. This provides further degrees of freedom for
manufacturing new end products.
[0028] The energetic composition of the invention is curable by
means of radiation, more particular electromagnetic radiation. The
electromagnetic radiation can be selected from the group consisting
of X-rays, ultraviolet light, visible light, infrared radiation and
combinations thereof.
[0029] In a preferred embodiment, the one or more polymerisable
components comprise one or more energetic polymerisable
components.
[0030] The radiation curable energetic composition of the invention
can comprise a free radical polymerisation system consisting of
(a1) one or more free radical polymerisable components and (b1) one
or more polymerisation photoinitiators for free radical
polymerisation.
[0031] Alternatively, or in addition, the radiation curable
composition of the invention can comprise a cationic polymerisation
system consisting of (a2) one or more cationically polymerisable
components and (b2) one or more polymerisation photoinitiators for
cationic polymerisation.
[0032] The amount of polymerisable components in the composition
can suitably be 5-45% by total weight of the composition,
preferably 10-40%, more preferably 15-35%. These polymerisable
components can include free radical polymerisable components and
cationically polymerisable components. Preferably, the
polymerisable component at least comprises a free radical
polymerisable component.
[0033] Suitable free radical polymerisable components include
aliphatic (meth) acrylates, aromatic (meth)acrylates,
cycloaliphatic (meth) acrylates, arylaliphatic (meth)acrylates, and
heterocyclic (meth)acrylates, (cyclo)aliphatic vinyl ethers,
aromatic vinyl ethers, (cyclo)aliphatic allyl ethers, unsaturated
polyesters, alkenes, styrene, or combinations thereof.
[0034] The free radical polymerisable components may comprise
monomers, oligomers, and/or polymers. They may be monofunctional or
polyfunctional, i.e. have one or more functional groups that can
polymerise by free radical polymerisation.
[0035] Examples of monofunctional free-radical polymerisable
components include isobornyl (meth)acrylate, bornyl (meth)acrylate,
tricyclodecanyl (meth)acrylate, dicyclopentanyl (meth)acrylate,
dicyclopentenyl (meth)acrylate, cyclohexyl (meth)acrylate, benzyl
(meth)acrylatea, 4-butylcyclohexyl (meth) acrylate, acryloyl
morpholine (meth)acrylic acid, 2-hydroxyethyl (meth) acrylate,
2-hydroxypropyl (meth) acrylate, 2-hydroxybutyl (meth)acrylate,
methyl (meth)acrylate, ethyl (meth) acrylate, propyl (meth)
acrylate, isopropyl (meth)acrylate, butyl (meth) acrylate, amyl
(meth)acrylate, isobutyl (meth)acrylate, t-butyl (meth) acrylate,
pentyl (meth) acrylate, caprolactone acrylate, isoamyl (meth)
acrylate, hexyl (meth)acrylate, heptyl (meth) acrylate, octyl
(meth) acrylate, isooctyl (meth) acrylate, 2-ethylhexyl
(meth)acrylate, nonyl (meth) acrylate, decyl (meth) acrylate,
isodecyl (meth)acrylate, tridecyl (meth) acrylate, undecyl
(meth)acrylate, lauryl (meth)acrylate, stearyl (meth) acrylate,
isostearyl (meth) acrylate, tetrahydrofurfuryl (meth)acrylate,
butoxyethyl (meth)acrylate, ethoxydiethylene glycol (meth)acrylate,
benzyl (meth)acrylate, phenoxyethyl (meth)acrylate, polyethylene
glycol mono(meth)acrylate, polypropyolene glycol
mono(meth)acrylate, methoxyethylene glycol (meth) acrylate,
ethoxyethyl (meth) acrylate, methoxypolyethylene glycol
(meth)acrylate, methoxypolypropylene glycol (meth) acrylate,
diacetone (meth)acrylamide,.beta.-carboxyethyl (meth)acrylate,
phthalic acid (meth)acrylate, dimethylaminoethyl (meth)acrylate,
butylcarbamylethyl (meth) acrylate, n-isopropyl (meth) acrylamide
fluorinated (meth)acrylate, 7-amino-3,7-dim4thyloctyl (meth)
acrylate, and phosphoric acid (meth)acrylates. Further, vinyl
ethers and allyl ethers can also be used.
[0036] Examples of polyfunctional free radical polymerisable
components include those with (meth)acryloyl groups such as
trimethylolpropane tri(meth)acrylate, pentaerythritol
(meth)acrylate, ethylene glycol di(meth)acrylate, diethylene glycol
di(meth)acrylate, triethylene glycol diacrylate, bisphenol A
diglycidyl ether di(meth)acrylate, dicyclopentadiene dimethanol
di(meth)acrylate,
[2-[1,1-dimethyl-2-[(1-oxoallyl)oxy]ethyl]-5-ethyl-1,3-dioxan-5-yl]methyl
acrylate,
3,9-bis(1,1-dimethyl-2-hydroxyethyl)-2,4,8,10-tetraoxaspiro[5.5-
]undecane di(meth)acrylate, dipentaerythritol
monohydroxypenta(meth)acrylate, proposylated trimethylolpropane
tri(meth)acrylate, propoxylated neopentyl glycol di(meth)acrylate,
tetraethylene glycol di(meth)acrylate, polyethylene glycol
di(meth)acrylate, 1,4-butanediol di(meth)acrylate, 1,6-hexanediol
di(meth)acrylate, neopentyl glycol di(meth)acrylate, polybutanediol
di(meth)acrylate, tripropyleneglycol di(meth)acrylate, glycerol
tri(meth)acrylate, phosphoric acid di(meth)acrylates,
C.sub.7-C.sub.20 alkyl di(meth)acrylates, tris (2
-hydroxyethyl)isocyanurate tri(meth) acrylate,
tris(2-hydroxyethyl)isocyanurate di(meth)acrylate, pentaerythritol
tri(meth)acrylate, pentaerythritol tetra(meth)acrylate,
dipentaerythritol hexa(meth)acrylate, tricyclodecane diyl dimethyl
di(meth)acrylate and alkoxylated versions (e.g., ethoxylated and/or
propoxylated) of any of the above-mentioned monomers, and also
di(meth)acrylates of a diol which is an ethylene oxide or propylene
oxide adduct to bisphenol A, di(meth)acrylate of a diol which is an
ethylene oxide or propylene oxide adduct to hydrogenated bisphenol
A, epoxy (meth)acrylate which is a (meth)acrylate adduct to
bisphenol A of diglycidyl ether, diacrylate of polyoxyalkylated
bisphenol A, and triethylene glycol divinyl ether, and adducts of
hydroxyethyl acrylate. Preferred free radical polymerisable
components include trimethylolpropane tri(meth)acrylate and
triethylene glycol di(meth)acrylate.
[0037] It is particularly advantageous if the one or more
polymerisable components in the radiation curable energetic
composition of the invention comprises one or more energetic free
radical polymerisable components.
[0038] Suitable examples of energetic free radical polymerisable
components include 2,2,2-trinitroethyl (meth) acrylate,
2,2-dinitropropyl (meth) acrylate, 2,2-dinitropropyl
di(meth)acrylate, 2-nitroethyl (meth) acrylate, beta-nitratoethyl
(meth)acrylate, and pentaerythritol trinitrate (meth)acrylate.
Further examples of energetic free radical polymerisable components
include fluoroacrylates, such as
1,1,7-trihydroperfluoroheptyl(meth)acrylate,
1,1-dihydroperfluorooctyl(meth)acrylate,
1,2,4,5-tetrakis(difluoroamino)amyl (meth) acrylate,
2,3-bis(difluoroaminopropyl) (meth) acrylate,
2-(N-butyl)-perfluorooctane sulphonamide ethylacrylate,
2,-fluoro-2,2-dinitroethylacrylate. Any combination of the above
mentioned free radical polymerisable components may be used.
[0039] The free radical polymerisable component may be present in
the composition in an amount of 5-45% by total weight of the
composition, preferably 10-40%, more preferably 15-35%.
[0040] A free radical polymerisable component is used together with
a polymerisation photoinitiator for free radical polymerisation.
Such photoinitiators can be classified in photoinitiators that form
radicals by cleavage, known as "Norrish type I", and
photoinitiators that form radicals by hydrogen abstraction, known
as "Norrish type II". The Norrish type II photoinitiators require a
hydrogen donor, which serves as the free radical source. Photolysis
of aromatic ketones, such as benzophenone, thioxanthones, benzyl,
and quinones, in the presence of hydrogen donors, such as alcohols,
amines, or thiols leads to the formation of a radical produced from
the carbonyl compound (ketyl-type radical) and another radical
derived from the hydrogen donor. The photopolymerisation of vinyl
monomers is usually initiated by the radicals produced from the
hydrogen donor. The ketyl radicals are usually not reactive toward
vinyl monomers because of the steric hindrance and the
delocalisation of an unpaired electron.
[0041] Examples of photoinitiators for free radical polymerisation
include 2,4,6-trimethylbenzoyl diphenyl phosphine oxide,
2,4,6-trimethylbenzoyl phenyl ethoxy phosphine oxide,
bis(2,4,6-trimethylbenzoyl)-phenyl phosphine oxide,
2-methyl-1-[4-(methylthio)phenyl]-2-morpholinoprop anone-1,
2-benzyl-2-(dimethylamino)-1[4-(4-moprholinyl)phenyl]-1-butanone- ,
2-dimethylamino-2-(4-methyl-benzyl)-1-(4-morpholin-4-yl-benzyl)-butan-1--
one, 4-benzoyl-4'-methyl diphenyl sulphide,
4,4'-bis(diethylamino)benzophenone, and
4,4'-bis(N,N'-dimethylamino)benzophenone (Michler's ketone),
benzophenone, 4-methyl benzophenone, 2,4,6-trimethyl benzophonene,
dimethoxybenzophenone, 1-hydroxycyclohexyl phenol ketone, phenyl
(1-hydroxyisopropyl)ketone,
2-hydroxy-1-[4-(2-hydroxyethoxy)phenyl]-2-methyl-1-propanone,
4-isopropylphenyl (1-hydroxyisopropyl)ketone,
oligo-[2-hydroxy-2-methyl-1-[4-(1-methylvinyl)phenyl]propanone],
camphorquinone, 4,4'-bis(diethylamino)benzophenone, benzyl dimethyl
ketal, bis(eta 5-2-4-cyclopentadien-1-yl)
bis[2,6-difluoro-3-(1H-pyrrol-1-yl)phenyl] titanium, and
combinations thereof. Preferred photoinitiators for free radical
polymerisation include 2,4,6-trimethylbenzoyl diphenyl phosphine
oxide, 2,4,6-trimethylbenzoyl phenyl ethoxy phosphine oxide, and
bis(2,4,6-trimethylbenzoyl)-phenyl phosphine oxide.
[0042] The polymerisation photoinitiator for free radical
polymerisation may be present in the composition in an amount of
0.05-3% by total weight of the composition, such as 0.1-2%, or
0.2-1.5%.
[0043] Examples of cationically polymerisable components include
cyclic ether compounds such as epoxy compounds and oxetanes, cyclic
lactone compounds cyclic acetal compounds, cyclic thioether
compounds, spiro orthoester compounds and vinyl ether compounds.
Specific examples of cationically polymerisable components include
bisphenol A diglycidyl ether, bisphenol F diglycidyl ether,
bisphenol S diglycidyl ether, brominated bisphenol A diglycidyl
ether, brominated bisphenol F diglycidyl ether, brominated
bisphenol S diglycidyl ether, epoxy novolac resins, hydrogenated
bisphenol A diglycidyl ether, hydrogenated bisphenol F diglycidyl
ether, hydrogenated bisphenol S diglydicyl ether,
3,4-epoxycyclohexylmethyl-3',4'-epoxycyclohexane carboxylate,
2-(3,4-epoxycyclohexyl-5,5-spiro-3,4-epoxy)-cyclohexne-1,4-dioxane,
bis(3,4-epoxycyclohexylmethyl)adipate, vinylcyclohexene oxide,
4-vinylepoxycyclohexane, viniylcyclohexene dioxide, limonene oxide,
limonene dioxide, bis(3,4-epoxy-6-methycycoohexylmethyl)adipate,
3,4-epoxy-6-methylcyclohexyl-3',4'-epoxy-6'-methylcyclohexane
carboxylate, .epsilon.-caprolactone-modified
3,4-epoxycyclohexylmethyl-3', 4'-epoxycyclohedxane carboxylates,
trimethylcaprolactone-modified
3,4-epoxycyclohexylmethyl-3',4'-epoxycylohexane carboxylates,
.beta.-methyl-.delta.-valerolactone-modified
3,4-epoxycyclohexylmethyl-3',4'-epoxycyclohexane carboxylates,
methylene bis(3,4-epoxycyclohexane), bicyclohexyl-3,3'-epoxide,
bis(3,4-epoxycyclohexyl) with a linkage of --O--, --S--, --SO--,
--SO.sub.2--, --C(CH.sub.3)--, --CBr.sub.2--,
--C(CBr.sub.3).sub.2--, --C(CF.sub.3).sub.2--,
--C(CCl.sub.3).sub.2--, or --CH(C.sub.6H.sub.5)--,
dicyclopentadiene diepoxide, di(3,4-epoxycyclohexylmethyl)ether of
ethylene glycol, ethylene bis(3,4-epoxycyclohexanecarboxylate),
epoxyhexahydrodioctylphthalate, epoxyhexahydro-di-2-ethylhexyl
phthalate, 1,4-butanediol diglycidyl ether, 1,6-hexanediol
diglycidyl ether, neopentylglycol diglycidyl ether, glycerol
triglycidyl ether, trimethylolpropane triglycidyl ether,
polyethylene glycol diglycidyl ether, polypropylene glycol
diglycidyl ether, diglycidyl esters of aliphatic long-chain dibasic
acids, monoglycidyl ethers of aliphatic higher alcohols,
monoglycidyl ethers of phenol, cresol, butyl phenol, or polyether
alcohols obtained by the addition of alkylene oxide to these
compounds, glycidyl esters of higher fatty acids, epoxidated
soybean oil, epoxidated polybutadiene,
1,4-bis(3-ethylo-3-oxetanylmethoxy)methyl]benzene,
3-ethyl-3-hydroxymethyloxetane,
3-ethyl-3-(3-hydroxypropyl)oxymethyloxetane,
3-ethyl-3-(4-hydroxybutyl)oxymethyloxetane,
3-ethyl-3-(5-hydroxypentyl)oxymethyloxetane,
3-ethyl-3-phenoxymethyloxetane,
bis(1-ethyl(3-oxetanyl)methyl)ether,
3-ethyl-3-((2-ethylhexyloxy)methyl)oxetane,
3-ethyl-((triethoxysilylpropoxymethyl)oxetane,
3-(meth)-allyloxymethyl-3-ethyloxetane,
3-hydroxymethyl-3-ethyloxetane,
(3-ethyl-3-oxetanylmethoxy)methylbenzene,
4-fluoro-1-(3-ethyl-3-oxetanylmethoxy)methyl]benzene,
4-methoxy-[1-(3-ethyl-3-oxetanylmethoxy)methyl]-benzene,
[1-(3-ethyl-3-oxetanylmethoxy)ethyl]phenyl ether,
isobutoxymethyl(3-ethyl-3-oxetanylmethyl)ether,
2-ethylhexyl(3-ethyl-3-oxetanylmethyl)ether, ethyldiethylene
glycol(3-ethyl-3-oxetanylmethyl)ether, dicylcopentadiene
(3-ethyl-3-oxetanylmethyl)ether,
dicyclopentenyloxyethyl(3-ethyl-3-oxetanylmethyl)ether,
dicyclopentenyl(3-ethyl-3-oxetanylmethyl)ether,
tetrahydrofurfuryl(3-ethyl-3-oxetanylmethyl)ether,
2-hydroxyethyl(3-ethyl-3-oxetanylmethyl)ether,
2-hydroxypropyl(3-ethyl-oxetanylmethyl)ether, and combinations
thereof.
[0044] The cationically polymerisable component may be present in
the composition in an amount of 5-45% by total weight of the
composition, preferably 10-40%, more preferably 15-35%. If the
cationically polymerisable component comprises an oxetane, then the
oxetane is usually present in an amount of 5-20% by total weight of
the composition, such as 7-15%.
[0045] A cationically polymerisable component is used together with
a polymerisation photoinitiator for cationic polymerisation.
Suitable photoinitiators for cationic polymerisation include onium
salts, halonium salts, iodosyl salts, selenium salts, sulphonium
salts, sulphoxonium salts, diazonium salts, metallocene salts,
isoquinolinium salts, phosphonium salts, arsonium salts, tropylium
salts, dialkylphenacylsulphonium salts, thiopyrilium salts, diaryl
iodonium salts, triaryl sulphonium salts, ferrocenes,
di(cyclopentadienyliron)arene salt compounds, pyridinium salts, and
combinations thereof. Typically, the photoinitiator for cationic
polymerisation can be selected from triarylsulphonium salts,
diaryliodonium salts, metallocene based compounds, and combinations
thereof.
[0046] The photoinitiator for cationic polymerisation can suitably
have an anion selected from the group consisting of BF.sub.4.sup.-,
AsF.sub.6.sup.-, SbF.sub.6.sup.-, PF.sub.6.sup.-,
[B(CF.sub.3).sub.4].sup.-, B(C.sub.6F.sub.5).sub.4.sup.-,
B[C.sub.6H.sub.3-3,5(CF.sub.3).sub.2].sub.4.sup.-,
B(C.sub.6H.sub.4CF.sub.3).sub.4.sup.-,
B(C.sub.6H.sub.3F2).sub.4.sup.-,
B[C.sub.6F.sub.4-4(CF.sub.3)].sub.4.sup.-,
Ga(C.sub.6F.sub.5).sub.4.sup.-,
[(C.sub.6F.sub.5).sub.3B--C.sub.3H.sub.3N.sub.2--B(C.sub.6F.sub.5).sub.3]-
.sup.-,
[(C.sub.6F.sub.5).sub.3--NH.sub.2--B(C.sub.6F.sub.5).sub.3].sup.-,
tetrakis(3,5-difluoro-4-alkyloxyphenyl)borate,
tetrakis(2,3,5,6-tetrafluoro-4-alkyloxyphenyl)borate,
perfluoroalkylsulphonates, tris[(perfluoroalkyl)sulphonyl]methides,
bis[(perfluoroalkyl)sulphonyl]imides, perfluoroalkylphosphates,
tris(perfluoroalkyl)trifluorophosphates,
bis(perfluoroalkyl)tetrafluorophosphates,
tris(pentafluoroethyl)trifluorophosphates, and
(CH.sub.6B.sub.11Br.sub.6)--, (CH.sub.6B.sub.11Cl.sub.6).sup.- and
other halogenated carborane anions.
[0047] Some further examples of photoinitiators for cationic
polymerisation include 4-[4-(3-chlorobenzoyl)phenylthio]phenyl
bis(4-fluorophenyl)sulphonium hexafluoroantimonate,
4-[4-(3-chlorobenzoyl)phenylthio]phenyl
bis(4-fluorophenyl)sulphonium tetrakis(pentafluorophenyl)borate,
4-[4-(3-chlorobenzoyl)phenylthio]phenyl
bis(4-fluorophenyl)sulphonium
tetrakis(3,5-difluoro-4-methyloxyphenyl)borate,
4-[4-(3-chlorobenzoyl)phenylthio]phenyl
bis(4-fluorophenyl)sulphonium
tetrakis(2,3,5,6-tetrafluoro-4-methyloxyphenyl)borate,
tris(4-(4-acetylphenyl)thiophenyl)sulphonium
tetrakis(pentafluorophenyl)borate,
tris(4-(4-acetylphenyl)thiophenyl)sulphonium tris
[(trifluoromethyl)sulphonyl]methide,
tris(4-(4-acetylphenyl)thiophenyl)sulphonium hexafluorophosphate,
bis[4-diphenylsulphoniumphenyl]sulphide bis(hexafluoroantimonate),
thiophenoxyphenylsulphonium hexafluoroantimonate,
[4-(1-methylethyl)phenyl] (4-methylphenyl) iodonium
tetrakis(pentafluorophenyl)borate,
4-[4-(2-chlorobenzoyl)phenylthio]phenyl
bis(4-fluorophenyl)sulphonium hexafluoroantimonate, and aromatic
sulphonium salts with anions of
(PF.sub.6-m(C.sub.nF.sub.bn+2).sub.m).sup.- where m is an integer
from 1 to 5, and n is an integer from 1 to 4.
[0048] The use of aromatic triaryl sulphonium salts as
photoinitiator for cationic polymerisation is desirable in additive
manufacturing because the resulting composition attains a fast
photospeed, good thermal stability, and good photo stability.
[0049] The polymerisation photoinitiator for cationic
polymerisation may be present in the composition in an amount of
0.05-3% by total weight of the composition, such as 0.1-2%, or
0.2-1.5%.
[0050] The energetic component that is comprised in the radiation
curable energetic composition of the invention may be polymerisable
or non-polymerisable. In an embodiment, at least part of the
energetic components in the energetic composition are polymerisable
components. Hence, in such as case components (a) and (c) may
overlap. In an embodiment, at least part (such as all) of the
energetic components are radiation curable components, i.e. can be
cured by exposing the components to actinic radiation.
[0051] Some examples of suitable energetic materials include
2,4,6-trinitrotoluene (TNT),
cyclo-1,3,5-trimethylene-2,4,6-trinitramine (RDX),
cyclotetramethylenetetranitramine (HMX), pentaerythrol tetranitrate
(PETN), 3-nitro-1,2,4-triazol-5-one (NTO), nitroglycerine (NG),
nitrocellulose (13% N) (NC), ammonium nitrate (AN), potassium
nitrate, hydrazine nitrate, lithium nitrate, ammonium perchlorate
(AP), potassium perchlorate,
2,4,6,8,10,12-(hexanitro-hexaaza)tetracyclododecane (CL20 or HNIW),
1,3,3-trinitroazetidine (TNAZ), octanitrocubane (ONC),
1,1-diamino-2,2-dinitroethene (FOX-7), ammonium dinitramide (ADN),
2,2,2-trinitroethylacrylate, 2,2,2-trinitroethylmethacrylate
(TNEM), 2,2-dinitropropylacrylate (DNPA), 2-nitroethylacrylate, and
pentaerythritoltrinitrate acrylate.
[0052] The energetic component can be liquid or solid. Preferably,
at least part of the energetic component is solid. In an embodiment
the energetic component is solid. The solid energetic component can
be in the form of particulates, which may have an average particle
size as determined by laser diffraction of 0.5-100 .mu.m,
preferably 1-60 .mu.m, more preferably 2-40 .mu.m. Such particles
have excellent burn behaviour and mechanical strength, Smaller
particles are not preferred due to the increase in viscosity. The
solid energetic component can also be in the form of
nanoparticles.
[0053] The energetic component may be present in the composition in
an amount of 30% or more by total weight of the composition, such
as 40-95%, or 45-90%. These amounts include the possibility that
polymerisable components and optional plasticiser in the
composition are also energetic components.
[0054] The radiation curable energetic composition of the invention
may further comprise a hydroxy functional component. The hydroxy
functional component may have a hydroxyl functionality of at least
one. Suitable hydroxy functional components preferably contain one
or more primary or secondary aliphatic hydroxyl. The hydroxyl group
may be internal in the molecule or terminal.
[0055] Examples of suitable hydroxy functional components include
alkanols, monoalkyl ethers of polyoxyalkylene glycols, monoalkyl
ethers of alkylene glycols, alkylene and arylalkylene glycols and
polyols. Particular examples of suitable hydroxy functional
components include 1,2,4-butanetriol, 1,2,6-hexanetriol,
1,2,3-heptanetriol, 2,6-dimethyl-1,2,6-hexanetriol,
(2R,3R)-(-)-2-benzyloxy-1,3,4-butanetriol, 1,2,3-hexanetriol,
1,2,3-butanetriol, 3-methyl-1,3,5-pentanetriol,
1,2,3-cyclohexanetriol, 1,3,5-cyclohexanetriol,
3,7,11,15-tetramethyl-1,2,3-hexadecanetriol,
2-hydroxymethyltetrahydropyran-3,4,5-triol,
2,2,4,4-tetramethyl-1,3-cyclobutanetriol, 1,3-cyclopentanediol,
trans-1,2-cyclooctanediol, 1,16-hexadecanediol,
3,6-dithia-1,8-octanediol, 2-butyne-1,4-diol, 1,3-propanediol,
1,4-butanediol, 1,5-pentanediol, 1,6-hexanediol, 1,7-heptanediol,
1,8-octanediol, 1,9-nonanediol, 1-phenyl-1,2-ethanediol,
1,2-cyclohexanediol, 1,5-decalindiol,
2,5-dimethyl-3-hexyne-2,5-diol,
2,7-dimethyl-3,5-octadiyne-2,7-diol, 2,3-butanediol,
1,4-cyclohexanedimethanol, and combinations thereof.
[0056] Also oligomeric and polymeric hydroxy functional components
can be used. Examples thereof include polyoxyethylene and
polyoxypropylene glycols and triols with number average molecular
weights of 200-10 000 g/mol, polytetramethylene glycols of varying
molecular weights, poly(oxyethylene-oxybutylene) random or block
copolymers, copolymers containing pendant hydroxy groups formed by
hydrolysis or partial hydrolysis of vinyl acetate copolymers,
polyvinylacetal resins containing pendant hydroxyl groups,
hydroxy-terminated polyesters and hydroxy-terminated polylactones,
hydroxy-functionalised polyalkadienes, such as polybutadiene,
aliphatic polycarbonate polyols, such as an aliphatic polycarbonate
diol, and hydroxy-terminated polyethers, and combinations thereof.
Preferred polyether polyols are polypropylene glycols of various
molecular weight. Especially preferred are linear and branched
polytetrahydrofuran polyether polyols available in various
molecular weights, such as in the range of 150-4000 g/mol, in the
range of 150-1500 g/mol, or in the range of 150-750 g/mol.
[0057] The hydroxy functional component may be present in the
composition in an amount of 0-10% by total weight of the
composition, such as 0-5%, or 0.1-3%, or 0.2-2%.
[0058] A representative radiation curable energetic composition
according to the invention comprises
[0059] 5-45% by total weight of the composition of polymerisable
components, preferably 10-40%, even more preferably 15-35%;
[0060] 0.05-3% by total weight of the composition of polymerisation
photoinitiators (preferably photoinitiators), preferably 0.1-2%,
even more preferably 0.2-1.5%;
[0061] 30% or more by total weight of the composition of energetic
components, such as 40-95%, or 45-90%; and
[0062] 0-10% by total weight of the hydroxy functional component,
preferably 0.5-8%, even more preferably 1-5%.
[0063] Preferably, the radiation curable energetic composition of
the invention comprises one or more plasticisers. The use of a
plasticiser in the radiation curable energetic composition of the
invention is to tune the mechanical properties of the cured object
and/or to tune the total energetic value of the composition. The
plasticiser may also be added in order to tune the viscosity of the
radiation curable energetic composition during additive
manufacturing. These plasticisers may or may not be energetic. In a
preferred embodiment, the one or more plasticisers comprise one or
more energetic plasticisers.
[0064] Some examples of suitable non-energetic plasticisers include
acid esters such as dialkyl esters of phthalic acids, triorgano
esters of phosphoric acid, dialkyl esters of adipic acid,
trimellitic esters, fatty acid esters, acetic esters, maleic
esters, fumaric esters, citric esters. Explicit examples include
di-n-octyl phthalate, dimethyl phthalate, diethyl phthalate,
dibutyl phthalate, diheptyl phthalate and di-2-ethylhexyl
phthalate, tributyl phosphate, tri-2-ethylhexyl phosphate,
triphenyl phosphate and tricresyl phosphate, dibutyl adipate and
di-n-octyl adipate, tri-2-ethylhexyltrimellitate, dimethyl adipate,
dibutyl adipate, diisobutyl adipate, diisonorbornyl adipate,
di-2-ethylhexyl adipate, diisodecyl adipate, diethylene glycol
adipate, dibutyl diglycol adipate, di-2-ethylhexyl azelate,
dimethyl sebacate, dibutyl sebacate, di-2-ethylhexyl sebacate,
methyl acetyltricinolate, epoxidised soybean oil, glyceryl
triacetate, 2-ethylhexyl acetate, dimethyl maleate, dibutyl
maleate, di-2-ethylhexyl maleate, dibutyl fumarate, di-2-ethylhexyl
fumarate, trimethyl citrate, triethyl citrate, tripropyl citrate,
triisobutyl citrate, acetylated monoglycerides, acetyl triethyl
citrate, acetyl tributyl citrate, triacetin, benzyl benzoate,
glycerol, polyethylene glycols, oleic acid, castor oil, corn oil,
camphor, sorbitol, and combinations thereof.
[0065] Some examples of suitable energetic plasticisers include
alkyl ethyl nitramines, in particular the homologous series based
on N-(2-nitroxyethyl) nitramine,
NO.sub.2--N--CH.sub.2CH.sub.2ONO.sub.2. Explicit examples include
N-(2-nitroxyethyl) methylnitramine, N-(2-nitroxyethyl)
ethylnitramine, N-(2-nitroxyethyl) n-propylnitramine,
N-(2-nitroxyethyl) n-butylnitramine, N-(2-nitroxypropyl)
methylnitramine and N-(2-nitroxyethyl) cyclohexylnitramine. Further
examples include dinitroxydiethyl nitramine, nitroglycerin,
1,2,4-butane triol trinitrate, 1,5-diazido-3-nitrazapentane,
bis(2-fluoro-2,2-dinitroethyl)formal, triethyleneglycol dinitrate,
bis(2,2-dinitropropyl)formal, bis(2,2-dinitropropyl)acetal,
diglycol dinitrate, and combinations thereof.
[0066] The plasticiser may be present in the composition in an
amount of 0-40% by total weight of the composition, such as 10-35%,
or 15-30%.
[0067] In a preferred embodiment, the radiation curable energetic
composition of the invention comprises a dye and/or a pigment. This
can be advantageous in an additive manufacturing method. The dye
and/or pigment can, for instance, ensure that the irradiation light
is absorbed in the layer that is intended to cure (typically the
layer closest to the irradiation source) and that the light does
not penetrate deeper to other layers. The amount of dyes and/or
pigments in the radiation curable energetic composition can, for
instance, be 0-0.1% by total weight of the composition, such as
0.005-0.02% by total weight of the composition.
[0068] The radiation curable energetic composition of the invention
may further comprise one or more additives, such as fuels,
oxidisers, dispersants, photosensitisers, fillers, stabilising
agents, dyes, pigments, antioxidants, wetting agents, explosive
desensitisers, defoamers, and surfactants. In a further aspect, the
invention is directed to a method of forming a three-dimensional
energetic object comprising the steps of forming and selectively
curing a layer of the radiation curable energetic composition
according to the invention with actinic radiation and repeating the
steps of forming and selectively curing a layer of the radiation
curable energetic composition according to the invention a
plurality of times to obtain a three dimensional energetic
object.
[0069] Optionally, the obtained three-dimensional energetic object,
may be subjected to post-curing by heat and/or actinic irradiation.
Post-curing can aid in curing possible unreacted components in the
radiation curable composition, can control stickiness of the
surface of the object, and can improve the initial strength of the
object.
[0070] The actinic radiation used in the method of the invention
and in the optional post-curing is preferably ultraviolet
radiation. The term "ultraviolet radiation" as used in this
application includes typical wavelengths for ultraviolet curing in
the range of 200-500 nm (near ultraviolet").
[0071] In yet a further aspect, the invention is directed to a
three-dimensional energetic object formed from the radiation
curable energetic composition or by the method according to the
invention.
[0072] In yet a further aspect, the invention is directed to the
use of a radiation curable energetic composition according to the
invention in ballistics, pyromechnical devices (including
actuators), fireworks or solid or hybrid propellant rockets.
[0073] The invention has been described by reference to various
embodiments, compositions and methods. The skilled person
understands that features of various embodiments, compositions and
methods can be combined with each other.
[0074] All references cited herein are hereby completely
incorporated by reference to the same extent as if each reference
were individually and specifically indicated to be incorporated by
reference and were set forth in its entirety herein.
[0075] The use of the terms "a" and "an" and "the" and similar
referents in the context of describing the invention (especially in
the context of the claims) are to be construed to cover both the
singular and the plural, unless otherwise indicated herein or
clearly contradicted by context. The terms "comprising", "having",
"including" and "containing" are to be construed as open-ended
terms (i.e., meaning "including, but not limited to") unless
otherwise noted. Recitation of ranges of values herein are merely
intended to serve as a shorthand method of referring individually
to each separate value falling within the range, unless otherwise
indicated herein, and each separate value is incorporated into the
specification as if it were individually recited herein. The use of
any and all examples, or exemplary language (e.g., "such as")
provided herein, is intended merely to better illuminate the
invention and does not pose a limitation on the scope of the
invention unless otherwise claimed. No language in the
specification should be construed as indicating any non-claimed
element as essential to the practice of the invention. For the
purpose of the description and of the appended claims, except where
otherwise indicated, all numbers expressing amounts, quantities,
percentages, and so forth, are to be understood as being modified
in all instances by the term "about". Also, all ranges include any
combination of the maximum and minimum points disclosed and include
and intermediate ranges therein, which may or may not be
specifically enumerated herein.
[0076] Preferred embodiments of this invention are described
herein. Variation of those preferred embodiments may become
apparent to those of ordinary skill in the art upon reading the
foregoing description. The inventors expect skilled artisans to
employ such variations as appropriate, and the inventors intend for
the invention to be practiced otherwise than as specifically
described herein. Accordingly, this invention includes all
modifications and equivalents of the subject-matter recited in the
claims appended hereto as permitted by applicable law. Moreover,
any combination of the above-described elements in all possible
variations thereof is encompassed by the invention unless otherwise
indicated herein or otherwise clearly contradicted by context. The
claims are to be construed to include alternative embodiments to
the extent permitted by the prior art.
[0077] For the purpose of clarity and a concise description
features are described herein as part of the same or separate
embodiments, however, it will be appreciated that the scope of the
invention may include embodiments having combinations of all or
some of the features described.
[0078] The invention will now be further illustrated by the
following non-limiting example.
EXAMPLE
[0079] A radiation curable energetic composition was prepared by
blending the ingredients as mentioned in table 1 in the indicated
amounts.
TABLE-US-00001 TABLE 1 Radiation curable energetic composition
Ingredient wt. % Non-energetic binder 24 Energetic plasticiser
.sup.1) 24 Dispersant .sup.2) 2 Solid energetic material .sup.3) 50
.sup.1) N-(2-nitroxyethyl) ethylnitramine .sup.2) Disperbyk 116
dispersant obtained from Byk .sup.3) RDX
(cyclo-1,3,5-trimethylene-2,4,6-trinitramine)
[0080] The non-energetic binder was composed as indicated in Table
2.
TABLE-US-00002 TABLE 2 Composition of non-energetic binder
Ingredient wt. % Triethylene glycol diacrylate 49
Trimethylolpropane triacrylate 49 Photoinitiator .sup.4) 2 Colorant
.sup.5) <<1 .sup.4) Irgacure 819 obtained from BASF .sup.5)
Solvent Yellow 33, CAS No. 8003-22-3
* * * * *