Disrupter driven highly efficient energy transfer fluid jets
US-11187487-B1 · Nov 30, 2021 · US
US11796279B1 · US · B1
| Field | Value |
|---|---|
| Publication number | US-11796279-B1 |
| Application number | US-202117300686-A |
| Country | US |
| Kind code | B1 |
| Filing date | Sep 29, 2021 |
| Priority date | Aug 18, 2017 |
| Publication date | Oct 24, 2023 |
| Grant date | Oct 24, 2023 |
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Provided herein are projectiles for use in a propellant driven disrupter device, and associated methods, to neutralize an explosive target. The projectile may comprise a friction reducing container at least partially filled with one or more fluids, fluid mixtures, particles, and other components to provide one or more desired fluid properties to achieve a desired one or more jet parameters upon target impact. The fluid(s) in the container are referred to as highly efficient energy transfer (HEET) fluids do to the improved fluid jet action on target compared to conventional water projectiles. The projectiles and disruptor can be more precisely individually tailored to the target, thereby increasing the likelihood of successful disablement and decreasing the likelihood of inadvertent and uncontrolled explosion.
Opening claim text (preview).
We claim: 1. A projectile system for use in a propellant driven disrupter, comprising: the propellant driven disrupter comprising: a barrel having a barrel lumen; a propellant-filled cartridge; a projectile in the barrel lumen comprising a highly efficient energy transfer (HEET) fluid having a HEET fluid distal end and a HEET fluid proximal end; a cap positioned in the barrel to fluidically seal the HEET fluid within the barrel lumen at the HEET fluid distal end; wherein: the barrel has a longitudinal length (L B ) and the projectile has a longitudinal length L p , and 0.1≤Lp/L B ≤1; the HEET fluid is configured during use to form a fluid jet having a jet length after exiting the barrel and before a target impact, the HEET fluid is selected from the group consisting of at least one of water, oil, syrup, ionic solutions, alcohol, a liquid polymer, a pre-polymer, an elastomer-containing liquid, a mechanophore, and a clay, having an effective density of between 0.5 g/mL to 15 g/mL at 20° C.; the projectile is a physically separate component from the propellant-filled cartridge; and wherein the projectile includes a plurality of HEET fluid zones, and wherein the HEET fluid comprises a plurality of unique HEET fluid compositions with a unique HEET fluid composition contained in each fluid zone. 2. The projectile system of claim 1 , wherein the HEET fluid has an effective viscosity selected from a range of 1 cP to 100,000 cP at 20° C. 3. The projectile system of claim 1 , wherein the HEET fluid has a surface tension selected from a range of 70 mN/m to 510 mN/m at 20° C. 4. The projectile system of claim 1 , wherein the projectile further comprises a friction reducing liner having a lumen extending between a proximal end and a distal end, the lumen at least partially filled by the HEET fluid, and wherein the friction reducing liner comprises a material selected from at least one of polymer, plastic, paper, wax, and polytetrafluoroethylene, and physically separates the HEET fluid from an inner surface of the barrel. 5. The projectile system of claim 1 , wherein the HEET fluid comprises a plurality of solid particles, and wherein the plurality of solid particles are positioned at the HEET fluid proximal end to form a HEET density gradient, with a highest effective density at the HEET fluid proximal end. 6. The projectile system of claim 1 , wherein the HEET fluid comprises solid particles immersed in a fluid. 7. A projectile system for use in a propellant driven disrupter, comprising: the propellant driven disrupter comprising: a barrel; a propellant-filled cartridge; and a projectile comprising a highly efficient energy transfer (HEET) fluid; wherein: the barrel has a longitudinal length (L B ) and the projectile has a longitudinal length L P , and 0.1≤L P /L B ≤1: the HEET fluid is configured during use to form a fluid jet having a let length after exiting the barrel and before a target impact, and the HEET fluid is selected from the group consisting of at least one of water, oil, syrup, ionic solutions, alcohol, a liquid polymer, a pre-polymer, an elastomer-containing liquid, a mechanophore, and a clay, having an effective density of between 0.5 g/mL to 15 g/mL at 20° C., wherein the projectile further comprises a friction reducing liner forming a container lumen filled by the HEET fluid, wherein the container lumen includes a plurality of HEET fluid zones, and wherein the HEET fluid comprises a plurality of unique HEET fluid compositions with a unique HEET fluid composition contained in each fluid zone. 8. The projectile system of claim 7 , further comprising a membrane separating adjacent fluid zones, wherein the membrane is configured to prevent migration of HEET fluid and any constituent thereof between adjacent fluid zones. 9. The projectile system of claim 6 , further comprising a proximal HEET fluid positioned in a proximal HEET fluid zone; and a distal HEET fluid positioned in a distal HEET fluid zone, wherein the proximal HEET fluid has a higher effective density and a higher effective viscosity than the distal HEET fluid, and wherein the proximal HEET fluid comprises the solid particles, which are one of suspended and dispersed in a fluid. 10. The projectile system of claim 6 , further comprising a proximal HEET fluid positioned in a proximal HEET fluid zone; and a distal HEET fluid positioned in a distal HEET fluid zone, wherein the proximal HEET fluid has a higher effective density and a higher effective viscosity than the distal HEET fluid, wherein the proximal HEET fluid comprises solid particles, which are one of suspended and dispersed in a fluid, wherein the distal HEET fluid comprises at least one of water, syrup, liquid polymer, pre-polymer, elastomer-containing liquid, alcohol, oil, ionic solution, mechanophore, and clay, and wherein the solid particles of the proximal HEET fluid are selected from the group consisting of at least one of clay, steel shot, lead shot, plastic beads, sand, metallic microparticles, garnet microparticles, ceramic powder, wood dust, and plastic dust. 11. The projectile system of claim 7 , wherein the HEET fluid is configured, so that when propelled in the barrel the HEET fluid has a Reynolds number in the barrel of between 75 and 4000. 12. The projectile system of claim 6 , wherein the solid particles have a distribution in the fluid that is substantially uniform. 13. The projectile system of claim 6 , wherein the solid particles have a distribution in the fluid that is not uniform. 14. The projectile system of claim 6 , wherein the HEET fluid is contained within a friction-reducing container. 15. A method of making a projectile for use in a propellant driven disrupter, comprising: providing a friction-reducing container being shaped for fitting within a barrel of the propellant driven disrupter; filling the container with a HEET fluid; sealing the friction reducing container containing the HEET fluid; filling a proximal end of the friction-reducing container with a proximal HEET fluid; filling a distal end of the friction-reducing container with a distal HEET fluid, wherein the proximal HEET fluid and distal HEET fluid have at least one fluid property that is different from each other, and wherein said at least one fluid property is selected from at least one of effective density, effective viscosity, a fluid composition type, and presence of particulates in the fluid, thereby reducing a reverse velocity gradient of a fluid let exiting the barrel after expulsion to increase fluid jet integrity. 16. The method of claim 15 , further comprising selecting a HEET fluid based on at least one fluid parameter for achieving at least one target disruption parameter, wherein said at least one fluid parameter selected is from at least one of effective viscosity; effective density; surface tension; presence of solid particles in the HEET fluid; absence of solid particles in the HEET fluid; average size of the solid particles in the HEET fluid; Reynolds number of propelled HEET fluid in a barrel of the propellant driven disrupter; density gradient; viscosity gradient; and a number of unique HEET fluids positioned in the container lumen, and wherein said at least one target disruption parameter is selected from at least one of fluid jet duration; fluid jet velocity; fluid jet length at impact; momentum and energy transfer to target; volumetric disruption; and penetration depth. 17. The method of claim 16 , wherein said at least one fluid parameter further comprises average s
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