Explosive devices
Abstract
An explosive device is provided, containing an explosive formulation or explosive ink, which is capable of being disposed of onto a substrate for the device by well known printing and depositing techniques, such as screen printing, ink jet printing or gravure methods. The formulation contains an ink resin binder, a metal and a non-metal in particulate form where the diameter of the particles is less than 10 μm, such that when the formulation is heated, a reactive output results. The substrate can be chosen from any inert material or alternatively an energetic material for which the formulation provides a means of initiation. Preferred metals are aluminum iron or titanium and non-metals are carbon, silicon, boron or metal oxides such as copper oxide, nickel oxide or molybedenum oxide. Devices according to the invention may take the form of a; pyrotechnic train, initiators, fuseheads, initiators for gas generators, microthrusters, and may form part of a larger system containing energetic materials.
Claims
exact text as granted — not AI-modified1 . An explosive device comprising a substrate on which one or more explosive formulations is deposited, wherein at least one of the explosive formulations comprises a binder, at least one metal and at least one non-metal, wherein the non-metal is selected from a metal oxide, or any non-metal from Group III or Group IV, wherein the metal and non-metal particles are 10 μm or less in diameter.
2 . An explosive device according to claim 1 wherein the metal and/or non metal particles are 1 μm or less in diameter
3 . An explosive device according to claim 2 wherein the metal and/or non-metal particles are 0.1 μm or less in diameter.
4 . An explosive device according to claim 1 wherein the deposited formulation comprises an insensitive explosive composition having a figure of insensitiveness greater than 60.
5 . An explosive device according to claim 4 wherein the figure of insensitiveness is greater than 150.
6 . An explosive device according to claim 1 wherein the metal is selected from aluminium, titanium or iron.
7 . An explosive device according to claim 1 wherein the non metal is selected from silicon, boron or carbon
8 . An explosive device according to claim 1 , wherein the metal oxide is selected from copper oxide, molybdenum oxide or nickel oxide.
9 . An explosive device according to claim 1 , wherein the metal is silicon and the non-metal is boron or carbon.
10 . An explosive device according to claim 1 , wherein the binder is selected from an ink resin Polyscreen®, Nylobag®, an epoxy resin or urethane.
11 . An explosive device according to claim 1 , wherein the binder is an energetic binder.
12 . An explosive device according to claim 11 , wherein the energetic binder is selected from Polyglyn (Glycidyl nitrate polymer), GAP (Glycidyl azide polymer) or Polynimmo (3-nitratomethyl-3-methyloxetane polymer).
13 . An explosive device according to claim 1 , wherein the binder is present in the range of from 10% to 50% by volume.
14 . An explosive device according to claim 13 , wherein the binder is present in the range of from 30% to 40% by volume.
15 . An explosive device according to claim 1 , wherein the substrate is an inert substrate such as polyester, polyimide, paper, PET, polystyrene or ceramic.
16 . An explosive device according to claim 1 , wherein the substrate comprises a surface of a consolidated explosive material.
17 . An explosive device according to claim 1 and being in the form of an initiator, wherein the deposited explosive formulation is connected to a heating element, such that, in use, the heating element ignites the explosive formulation.
18 . An explosive device according to claim 1 wherein the deposited explosive formulation is connected to a heating element and to an explosive material such as, in use, to form an explosive train connecting said heating element with said explosive material.
19 . An explosive device according to claim 18 wherein the explosive formulation is disposed on the substrate in an elongate pattern having a length which is chosen to provide in use a desired delay time prior to ignition of the explosive material.
20 . An explosive device according to claim 19 wherein the explosive formulation is disposed on the substrate in a spiral or zig-zag pattern.
21 . An explosive device according to claim 17 wherein the deposited explosive formulation is disposed on the substrate in a shape such that when it is ignited by a heating element, the explosive formulation burns with an increasing output of energy until the explosive formulation is exhausted.
22 . An explosive device according to claim 21 wherein the deposited explosive formulation is formed substantially in the shape of a circle, with the heating element located at the centre thereof.
23 . An explosive device according to claim 21 wherein the deposited explosive formulation is disposed on the substrate in a shape that is substantially a segment of a circle with the heating element located at the apex thereof.
24 . An explosive device according to claim 1 wherein the substrate has one or more voids and the explosive formulation fills said voids.
25 . A microthruster device comprising an explosive device according to claim 1 , wherein the substrate has a plurality of voids into which the explosive formulation is deposited, further comprising means for selectively igniting said deposits of the explosive formulation to provide thrust.
26 . A microthruster device, according to claim 25 wherein the voids have diameters in the range 0.25 mm to 11.0 mm.
27 . An initiator for a gas generator, comprising an explosive device according to claim 17 , wherein the deposited explosive formulation is connected to a heating element and to a gas generating explosive material, such that, in use, the device forms an explosive train connecting said element with said gas generating explosive material.
28 . An initiator for a gas generator according to claim 27 , wherein in use the gas generated inflates an air bag located in a vehicle, vessel or flying craft.
29 . An initiator for a gas generator according to claim 28 , wherein the generated gas actuates a seat belt pre-tensioner to restrain a passenger in a vehicle, vessel or flying craft.
30 . A pyrotechnic device comprising an explosive device according to claim 1 , wherein the deposited explosive formulation further includes one or more Group 1 or Group 2 metal salts to produce, in use, a coloured light or sound emission.
31 . A method of producing an explosive device comprising the steps of:
a) mixing a potion of a binder with at least one metal in the form of particles having a diameter of less than 10 μm; b) mixing a further portion of the binder with at least one non-metal, wherein the non-metal is selected from a metal oxide, or any non-metal from Group III or Group IV in the form of particles having a diameter of less than 10 μm; c) mixing together the products of a) and b) to provide an explosive formulation; d) depositing the formulation so produced onto a substrate; and e) causing the formulation to dry on said substrate.
32 . A method of producing an explosive device according to claim 31 wherein the process of deposition in step (d) is by spraying, brushing, dipping or printing.
33 . A method according to claim 32 wherein printing is achieved by a wet printing method.
34 . A method according to claim 33 wherein the wet printing method is selected from ink jet, bubble jet, screen printing or gravure.
35 . A method according to claim 33 comprising loading the explosive formulation into a printing apparatus having a nozzle for spraying a jet of explosive ink.
36 . A method of making an explosive device according to claim 31 , wherein the device is a microthruster device for use in space apparatus or airborne craft and wherein the substrate has a plurality of voids which are filled with deposits of the explosive formulation.
37 . A method of making an explosive device according to claim 31 , wherein the device is a gas generator device for use in a vehicle, vessel or flying craft, wherein the substrate in step (d) of claim 31 is a heating element and wherein the method further comprises the steps of:
f) placing a gas generating explosive material in intimate contact with the product of step (d); and g) placing the product of step (f) within a suitable containment means.
38 . A method of depositing an explosive formulation, including the steps of:
a) loading a printing apparatus with a mixture of a binder with at least one metal in the form of particles having a diameter of less than 10 μm and with a mixture of a binder with at least one non-metal, wherein the non-metal is selected from a metal oxide, or any non-metal from Group III or Group IV in the form of particles having a diameter of less than 10 μm such that the at least one metal and/or at least one non-metal mixtures are held separate in the apparatus; b) drawing up selected aliquots of the at least one metal and the at least one non-metal mixtures and mixing the same in-situ immediately prior to operation of the apparatus to deposit an explosive formulation onto a substrate.
39 . A method of depositing an explosive formulation according to claim 38 wherein the metal and non-metal particles are 1 μm or less in diameter.
40 . A method of depositing an explosive formulation according to claim 39 wherein the metal and non-metal particles are 0.1 μm or less in diameter.
41 . An explosive ink comprising an explosive formulation as described in claim 1 , together with a volatile organic solvent.
42 . An explosive ink according to claim 41 wherein the volatile organic solvent is selected from a lower alkyl alcohol, ketone or ether or from petroleum ethers ranging from C5 to C10.
43 . An explosive ink according to claim 41 , wherein the metal and/or non-metal particles are 1 μm or less in diameter.
44 . An explosive ink, according to claim 43 , wherein the metal and/or non-metal particles are 0.1 μm or less in diameter.Join the waitlist — get patent alerts
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