Inflatable tool for plasma generation and shaped charge stand-off

Abstract

An explosive ordnance disposal (EOD) tool has an inflated state and a deflated, collapsed state. In the inflated state, the EOD tool includes a central longitudinal axis and a radially outer portion. The radially outer portion contains an inflation composition. The radially outer portion includes an opening for admitting the inflation composition into the radially outer portion, an exterior wall and an interior wall that defines a through opening centered on the central longitudinal axis.

Claims

1. An apparatus, comprising: an explosive ordnance disposal (EOD) tool including an inflated state and a deflated, collapsed state, wherein, in the inflated state, the EOD tool include a central longitudinal axis, a radially outer portion that contains an inflation composition and includes a plug to admit the inflation composition into the radially outer portion, an exterior wall and an interior wall that defines a through opening centered on the central longitudinal axis, wherein the through opening includes an upper portion configured to hold one of a hand-loaded energetic charge and a shaped charge, and a lower portion configured to act as an energetic guide for the one of the energetic charge and the shaped charge, wherein the upper portion of the through opening includes a cylindrical shape, and wherein the lower portion of the through opening includes one of a constant cross-section and a decreasing cross-section; and an energetic charge being disposed in the upper portion of the through opening, wherein the lower portion has a shape of a frustum, wherein an angle between a wall of the lower portion, and a horizontal is in a range of from less than 90 degrees to about 50 degrees, and wherein an inflation composition is one of air and water.

2. The apparatus of claim 1, wherein the through opening is a cylindrical shaped through opening.

3. The apparatus of claim 1, wherein the exterior wall of the radially outer portion includes a triangular cross-section.

4. The apparatus of claim 1, wherein the exterior wall of the radially outer portion includes a rectangular cross-section.

5. The apparatus of claim 1, wherein the exterior wall of the radially outer portion includes a hexagonal cross-section.

6. The apparatus of claim 1, wherein the lower portion has a shape of a frustum.

7. The apparatus of claim 1, further comprising a shaped charge being disposed in the upper portion of the through opening.

8. A method, comprising: providing the apparatus of claim 1; hand-loading an energetic charge in the upper portion of the through opening; and imparting a shockwave at an effective velocity and temperature on a gas in the through opening to ionize the gas for creating plasma and to drive the plasma.

9. The method of claim 8, further comprising, after the imparting step, impacting the plasma on a casing of an explosive ordnance containing an explosive to penetrate through the casing and, at least before causing an explosive event of the explosive within the casing, substantially consuming the explosive.

10. The method of claim 8, wherein the gas in the through opening is air.

11. The method of claim 9, wherein the energetic charge includes a detonation velocity of at least 7 mm/microsecond.

12. The method of claim 11, wherein the energetic charge has an effective velocity of at least 6 mm/microsecond.

13. A method, comprising: providing the apparatus of claim 1; loading a shaped charge in the upper portion of the through opening; and detonating the shaped charge for producing a jet that moves away from the shaped charge and through the lower portion of the through opening.

14. The method of claim 13, further comprising directing the jet from the lower opening to impact an explosive ordnance.

15. The method of claim 14, wherein the explosive ordnance is an improvised explosive device.

16. The method of claim 14, wherein the explosive ordnance is an unexploded ordnance.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) In the drawings, which are not necessarily to scale, like or corresponding parts are denoted by like or corresponding reference numerals.

(2) FIG. 1 is a top view of one embodiment of an explosive ordnance disposal (EOD) tool in an inflated state.

(3) FIG. 2 is a perspective view of the tool of FIG. 1.

(4) FIG. 3 is a sectional view taken along the line 3-3 of FIG. 1.

(5) FIG. 4 is a bottom view of the tool of FIG. 1.

(6) FIG. 5 is a top view of the tool of FIG. 1 in a deflated state.

(7) FIG. 6 is a schematic view of energetic material.

(8) FIG. 7 is a cut away side view of a shaped charge.

(9) FIG. 8 is a cut away view of one embodiment of an EOD tool placed on the surface of an explosive ordnance.

(10) FIG. 9 is a schematic view of another embodiment of the interior walls defining a through opening in an EOD tool.

(11) FIG. 10 is a schematic view of an additional embodiment of the interior walls defining a through opening in an EOD tool.

(12) FIG. 11 is a schematic view of a further embodiment of the interior walls defining a through opening in an EOD tool.

(13) FIGS. 12-13 show different geometries for the exterior walls of an EOD tool.

DETAILED DESCRIPTION OF THE INVENTION

(14) An explosive ordnance disposal (EOD) tool 10 has an inflated state and a deflated, collapsed state. FIGS. 1-4 are views of tool 10 in the inflated state. FIG. 5 is a top view of tool 10 in a deflated state. In the deflated state, tool 10 may be folded into a small flat shape. In the inflated state shown in FIGS. 1-4, the EOD tool 10 includes a central longitudinal axis A and a radially outer portion 12. The radially outer portion 12 contains an inflation composition 14. The inflation composition 14 may be, for example, air or water. A plug 16 that may be opened and closed is used to fill the radially outer portion 12 with the inflation composition 14 and seal the composition 14 therein. Radially outer portion 12 includes an exterior wall 18 and an interior wall 20. Tool 10 may be made of an inflatable material, such as, for example, vinyl.

(15) Interior wall 20 defines a through opening 22 centered on the central longitudinal axis A. The through opening 22 has an upper portion 24 configured to hold one of a hand-loaded energetic charge 26 (FIG. 6) and a shaped charge 28 (FIG. 7). Energetic charge 26 may be, for example, C-4 explosive. Shaped charge 28 may include, for example, a liner 30 fixed in a casing 32 filled with high explosive 34. A detonator 36 may be inserted in high explosive 34. Through opening 22 has a lower portion 38 configured to act as an energetic guide for the energetic charge 26 or shaped charge 28.

(16) In the embodiment of FIGS. 1-4, the upper portion 24 of through opening 22 has a cylindrical shape and the lower portion 38 of through opening 22 has the shape of a frustum of a cone. In other embodiments, the upper and lower portions may both have cylindrical shapes. For example, FIG. 9 shows a through opening 22a with a cylindrical upper portion 24a and a cylindrical lower portion 38a wherein the lower portion 38a has a smaller diameter than the upper portion 24a. In FIG. 10, through opening 22b has an upper portion 24b and lower portion 38b that are cylindrical shapes having the same diameter. In another variant shown in FIG. 11, the entire through opening 22c has the shape of a frustum having upper portion 24c and lower portion 38c. To function as an effective plasma generator, the diameter of the lower portion of the through opening 22 will be constant or decreasing.

(17) In the embodiment shown in FIGS. 1-4, the exterior wall 18 has the shape of a hexagon to allow for placing multiple tools 10 adjacent each other with a minimum amount of space between them. Exterior wall 18 may have other shapes, such as a triangle (FIG. 12) or a rectangle (FIG. 13).

(18) As seen in FIG. 3, the angle B between wall 20 of the lower portion 38 and the horizontal may be in a range of from less than 90 degrees to about 50 degrees. In an exemplary embodiment, the angle B is in the range of about 85 degrees to about 70 degrees. In one embodiment, the diameter d of the upper portion 24 is about 2 inches, a height c of the upper portion 24 is about 2 inches, a height e of the lower portion 38 is about 3 and inches and a width w (FIG. 1) of one hexagonal face of exterior wall 18 is about 3 inches.

(19) One manner of using tool 10 includes hand-loading an energetic charge 26 in the upper portion 24 of the through opening 22. Tool 10 is mounted on a surface 46 of an explosive ordnance 44 containing an explosive 48. An EOD technician detonates energetic charge 26 thereby imparting a shockwave at an effective velocity and temperature on the air in the through opening 22 to ionize the air to create plasma and to drive the plasma downward through the lower portion 38. The plasma impacts on the casing 46 of an explosive ordnance 44 containing an explosive 48 to penetrate through the casing 46. At least before causing an explosive event of the explosive 48 within the casing 46, the plasma substantially consumes the explosive 48. The energetic charge 26, in an exemplary embodiment, has a detonation velocity of at least 7 mm/microsecond. The energetic charge 26, in an exemplary embodiment, has an effective velocity of at least 6 mm/microsecond.

(20) Another manner of using tool 10 includes loading a shaped charge 28 in the upper portion 24 of the through opening 22. The open end 40 of liner 30 may rest on the bottom 42 of upper portion 24. In this way, the lower portion 38 provides a stand-off between shaped charge 28 and a surface 46 (FIG. 8) of an explosive ordnance, such as, for example, an IED or UXO. The stand-off distance is the height e of lower portion 38 of tool 10. Detonation of the shaped charge 28 produces a jet that moves away from the shaped charge 28 and through the lower portion 38 of the through opening 22. The jet is directed from the lower opening 38 to impact an explosive ordnance 44.

(21) Any numerical parameters set forth in the specification and attached claims are approximations that may vary depending upon the desired properties sought to be obtained by the present invention. At the very least, and not as an attempt to limit the application of the doctrine of equivalents to the scope of the claims, each numerical parameter should at least be construed in light of the number of significant digits and by applying ordinary rounding.